| Abate, G. | MORPHING LEADING-EDGE TUBERCLES ON CESSNA 172 WING | ICAS2024_0047 |
| Abdul-Kaiyoom, M.A.S. | SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION | ICAS2024_0465 |
| Abdul-Kaiyoom, M.A.S. | ROBUST SCHUR-COMPLEMENT SOLVERS AND LARGE-SCALE MULTIDISCIPLINARY DESIGN OPTIMIZATION | ICAS2024_0687 |
| Abouhamzeh, M. | INVESTIGATING AN OPTIMAL AEROELASTIC DESIGN FOR AIRCRAFT WINGS WITH DISTRIBUTED PROPELLERS MADE OF COMPOSITES | ICAS2024_1017 |
| Abramovich, H. | LASER SHEAROGRAPGY-PREDICTION AND OPTIMIZING ITS FLAW DETECTION CAPABILITIES USING AN ADVANCED HYBRID APPROACH | ICAS2024_0923 |
| Abu Salem, K. | FROM THEORY TO FLIGHT: THE BOX-WING CONFIGURATION IMPLICATIONS FOR THE NEXT-GENERATION AIRCRAFT | ICAS2024_0217 |
| Abu Salem, K. | ENVIRONMENTAL IMPLICATIONS OF HYBRID-ELECTRIC REGIONAL AIRCRAFT: EMISSIONS AND CLIMATE CHANGE | ICAS2024_0222 |
| Abu Salem, K. | POWER MANAGEMENT SUPPLY OPTIMIZATION FOR HYBRID-ELECTRIC REGIONAL AIRCRAFT | ICAS2024_0303 |
| Accardo, D. | CLASSIFICATION OF EXTENDED REALITY BASED HUMAN MACHINE INTERFACES SCENARIOS FOR URBAN AIR MOBILITY | ICAS2024_0326 |
| Accardo, G. | HYDROGEN STORAGE SYSTEM DESIGN: CASE STUDIES FOR AIRBORNE APPLICATION | ICAS2024_0590 |
| Acerra, F. | POTENTIAL APPLICATION OF PHASE CHANGE MATERIALS FOR THERMAL MANAGEMENT SYSTEM OF NEXT GENERATION AIRCRAFT | ICAS2024_0295 |
| Acerra, F. | PRELIMINARY RESULTS FOR AN INSTRUCTION DESIGN PROCEDURE IN AERONAUTICAL MANUFACTURING | ICAS2024_0306 |
| Acerra, F. | REDESIGN OF AN AERONAUTICAL COMPOSITE STIFFENED PANEL WITH THE DOUBLE-DOUBLE DESIGN APPROACH | ICAS2024_0360 |
| Acerra, F. | COMPARATIVE ANALYSIS OF MACHINE LEARNING ALGORITHMS FOR HEAT EXCHANGERS DIAGNOSIS IN ELECTRIFIED AIRCRAFT | ICAS2024_0701 |
| Adamidis, S. | DESIGN SPACE EXPLORATION OF NEXT-GENERATION SUPERSONIC BUSINESS JET ENGINE WITH A FOCUS ON LANDING AND TAKE-OFF (LTO) NOISE | ICAS2024_1147 |
| Adams, C. | ACTIVE CONTROL DAMPING WITH THE USE OF VOICE COIL ACTUATORS | ICAS2024_1106 |
| Addo-Akoto, R. | ASPECT RATIO AND ADVANCE RATIO EFFECTS ON AERODYNAMIC CHARACTERISTICS OF FLEXIBLE FLAPPING WINGS | ICAS2024_0333 |
| Adhikari, S. | RANDOM MATRIX MODELLING FOR UNCERTAINTY QUANTIFICATION IN PRESTRESSED STRUCTURES | ICAS2024_0875 |
| Adler, E.J. | DUCTED HEAT EXCHANGER THERMAL AND AERODYNAMIC SHAPE OPTIMIZATION | ICAS2024_0080 |
| Adler, E.J. | SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION | ICAS2024_0465 |
| Ahn, H.J. | MEDIAL AXIS TRANSFORMATION-BASED CONVEX MODEL PREDICTIVE CONTROL FOR MULTIROTOR INDOOR AUTONOMOUS FLIGHT WITH FIXED ALTITUDE | ICAS2024_0294 |
| Ahn, S.M. | WHAT-IF SCENARIO ANALYSIS OF REGIONAL AIR MOBILITY OPERATIONS IN SOUTH KOREA | ICAS2024_0850 |
| Ahuja, J. | PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS | ICAS2024_1296 |
| Ai, X. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AEROELASTICITY OF HIGH-ASPECT-RATIO WINGS | ICAS2024_0423 |
| Ai, X. | AEROELASTIC DIVERGENCE AND FLUTTER ANALYSIS OF A WING WITH ALL MOVING WING TIP | ICAS2024_0642 |
| Ai, X.-Y. | COMPUTATIONAL/EXPERIMENTAL AEROELASTIC STUDY FOR AN ALL-MOVABLE HORIZONTAL TAIL WITH TORSION FREE-PLAY | ICAS2024_0728 |
| Ai, X.-Y. | STUDY OF AEROELASTIC PROBLEM OF RUDDER SYSTEM WITH ELECTRIC ACTUATOR AND STRUCTURAL NONLINEARITIES | ICAS2024_0784 |
| Aigner, J. | CINNABAR PROJECT – COST-BENEFIT ANALYSIS OF DIGITAL PROCESSES FOR NON-DESTRUCTIVE INSPECTIONS OF AIRCRAFT STRUCTURES | ICAS2024_0125 |
| Aimasso, A. | PRELIMINARY ANALYSIS OF TEMPERATURE EFFECTS AND MANEUVER-INDUCED DEFORMATIONS ON FBG OPTIC FIBER INTEGRATED SYSTEMS | ICAS2024_0483 |
| Airoldi, A. | IMPACT TOLERANCE OF CERAMIC MATRIX COMPOSITES FOR AEROSPACE APPLICATIONS | ICAS2024_1111 |
| Airoldi, A. | NUMERICAL TOOLS FOR SLOW-GROWTH APPROACHES TO DAMAGE TOLERANT COMPOSITE AERONAUTICAL STRUCTURES | ICAS2024_1146 |
| Akbari, J. | COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH | ICAS2024_1138 |
| Alaimo, A. | ADAPTIVE WING FLUTTER SUPPRESSION BY MEANS OF MULTIPLE TRAILING EDGE CONTROL SURFACES - A COMPARATIVE STUDY | ICAS2024_0513 |
| Alaimo, A. | METAMODELLING OF THE WORKLOAD ASSESSMENT IN SIMULATED FLIGHTS USING THE KRIGING METHOD | ICAS2024_0743 |
| Alaimo, A. | DESIGN AND DEVELOPMENT OF THE VISUAL AND AUDITORY LAYER FOR DIFFERENT CABIN/COCKPIT LAYOUT | ICAS2024_0799 |
| Alam, M. | STRUCTURAL AND AEROELASTIC OPTIMISATION OF A LARGE AIRCRAFT WING WITH A PASSIVE TWIST WINGTIP | ICAS2024_0111 |
| Albano, M. | PROPULSIVE CFD ANALYSIS OF THE SCRAMJET HYPERSONIC EXPERIMENTAL VEHICLE | ICAS2024_0255 |
| Albano, M. | LAUNCH SYSTEM ASSESSMENT OF AN EXPERIMENTAL HYPERSONIC SCRAMJET VEHICLE | ICAS2024_0363 |
| Alberti, M. | AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) | ICAS2024_0575 |
| Albisser, M. | SONIC BOOM COMPARATIVE STUDY BETWEEN MACH 4.7 OUTDOOR EXPERIMENTAL TESTS AND NUMERICAL SIMULATIONS | ICAS2024_0882 |
| Albuquerque, P.F. | IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN | ICAS2024_0057 |
| Albuquerque, P.F. | AIRCRAFT WING STRUCTURAL SIZING COMPUTATIONAL TOOL TAILORED FOR A COLLABORATIVE MULTIDISCIPLINARY DESIGN FRAMEWORK | ICAS2024_0079 |
| Alder, M. | GLOBAL SENSITIVITY ANALYSIS OF LIQUID HYDROGEN STORAGE DESIGN PARAMETERS FOR OVERALL AIRCRAFT DESIGN | ICAS2024_0092 |
| Alder, M. | EU IMPACT MONITOR PROJECT - OVERVIEW AND APPROACH | ICAS2024_1114 |
| Aleisa, H. | LOW-SUBSONIC AERODYNAMIC ANALYSES OF A NONPLANAR BWB MODEL: AN EXPERIMENTAL AND CFD STUDY | ICAS2024_0232 |
| Alexiev, M.M. | MODELING CARGO DEMAND FOR REGIONAL AIR TRANSPORT NETWORKS IN CANADA AND THE UNITED STATES | ICAS2024_0729 |
| Alfero, A. | NUMERICAL-THEORETICAL EVALUATION OF THE DITCHING OF A HULL WITH DIHEDRAL ANGLES BETWEEN -5 AND 20 DEGREES | ICAS2024_0665 |
| Alfredsson, H. | AIRPORT CHARGING SYSTEM DESIGNS AND POWER MANAGEMENT FOR MEGAWATT-LEVEL CHARGING OF BATTERY-ELECTRIC AIRCRAFT | ICAS2024_0442 |
| Alian, H. | DIGITAL TWIN OF AN AIRCRAFT LANDING GEAR TO ENHANCE FAILURE ANALYSIS AND MANAGE PREDICTIVE MAINTENANCE | ICAS2024_0065 |
| Allegaert, E. | HARDWARE-IN-THE-LOOP SIMULATION FRAMEWORK FOR THE EVALUATION OF AUTONOMOUS FLIGHT FUNCTIONS | ICAS2024_0897 |
| Almeida, H. | AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS | ICAS2024_1139 |
| Alves, M.P. | A-BASIS AND B-BASIS BUCKLING ALLOWABLES FOR AN AIRCRAFT COMPOSITE WING | ICAS2024_0322 |
| Amadori, K. | CONCEPT OF OPERATIONS IN AN AGENT-BASED SIMULATION: A SYSTEM-OF-SYSTEMS APPROACH | ICAS2024_0357 |
| Amadori, K. | SUSTAINABLE AVIATION IN NORDIC COUNTRIES | ICAS2024_0585 |
| Amadori, K. | COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH | ICAS2024_1138 |
| Ameduri, S. | CONCEPTUAL DESIGN AND TOPOLOGY OPTIMIZATION OF A COMPLIANT MORPHING FLAP FOR NEXT GENERATION HYBRID-ELECTRIC REGIONAL AIRCRAFT | ICAS2024_1206 |
| Ament, J. | ASSISTED AND AUTOMATED AERIAL REFUELLING – OVERVIEW OF THE CONDUCTED RESEARCH AT THE GERMAN AEROSPACE CENTER (DLR) | ICAS2024_0819 |
| Amore, V. | EXPERIMENTAL VALIDATION OF THE DYNAMIC FINITE ELEMENT MODEL OF A 1:8 SCALE SEAPLANE USING A LASER DOPPLER VIBROMETER (LDV) | ICAS2024_0730 |
| Ananthapuvirajah, A. | THE EFFECTS OF ENGINE MASS AND LOCATION ON THE FLUTTER CHARACTERISTICS OF AIRCRAFT WINGS | ICAS2024_0170 |
| Ananthkrishnan, N. | MODEL-BASED CONCEPTUAL DESIGN AND EVALUATION OF A SOLID-FUEL SCRAMJET VEHICLE | ICAS2024_0195 |
| Andreeva-Mori, A. | LOW-ALTITUDE INTEGRATED AIRSPACE OPERATIONS OF AIRCRAFT FLYING UNDER VISUAL FLIGHT RULES: THE VERTICAL DIMENSION | ICAS2024_0835 |
| Andreeva-Mori, A. | ENHANCING PUBLIC GOOD MISSIONS AND DISASTER RESPONSE WITH ADVANCED AERIAL TECHNOLOGY: OPPORTUNITIES AND CHALLENGES | ICAS2024_1259 |
| Angelini, D. | COMPARATIVE ANALYSIS OF EVTOL, DRONE AND GROUND TRANSPORTATION SYSTEMS FOR EMERGENCY DELIVERY OF BLOOD-DERIVED MEDICATION | ICAS2024_0700 |
| Anilir, B. | ON THE AERODYNAMIC CHARACTERISTICS OF CRESCENT WING | ICAS2024_0579 |
| Anilkumar Girija, A. | APPLYING MODEL-BASED SYSTEM ENGINEERING AND DEVOPS ON THE IMPLEMENTATION OF AN AI-BASED COLLISION AVOIDANCE SYSTEM | ICAS2024_0869 |
| Ansar, S.A. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Antoniazzi, F.C. | FAULT DETECTION FOR AN AIRCRAFT ELEVATOR | ICAS2024_0647 |
| Antonio Solazzo, M. | EU IMPACT MONITOR PROJECT - OVERVIEW AND APPROACH | ICAS2024_1114 |
| Apostolidis, A. | TOWARDS TRUSTWORTHY DATA-DRIVEN GAS TURBINE PROGNOSTICS | ICAS2024_0793 |
| Aprovitola, A. | WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS | ICAS2024_0348 |
| Aprovitola, A. | OPTIMIZATION PROCEDURE FOR THE WING OF A MARS EXPLORATION DRONE | ICAS2024_0862 |
| Apuleo, G. | AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) | ICAS2024_0575 |
| Araujo, A.-C. | FRICTION RIVETING OF THERMOPLASTIC COMPOSITE WITH A CNC MACHINE: EXPERIMENTAL WORK | ICAS2024_1127 |
| Aresi, T. | SIMPLIFIED MODELS OF PILOT BIOMECHANICS FOR ROTORCRAFT VERTICAL BOUNCE ANALYSIS | ICAS2024_0520 |
| Arnaldi, A. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Arnone , A. | HIGH FIDELITY MODELING OF ACOUSTIC LINERS FOR AERONAUTICAL APPLICATIONS | ICAS2024_1048 |
| Arroyo-Mora, J.P. | ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD | ICAS2024_1280 |
| Arteiro, A. | ON AN EFFICIENT GLOBAL/LOCAL STOCHASTIC METHODOLOGY FOR FAILURE PREDICTION OF AIRCRAFT COMPOSITE STRUCTURES | ICAS2024_0250 |
| Ascione, G. | UNCERTAINTY PROPAGATION IN VALUE-DRIVEN DECISION-MAKING FOR THE AIRCRAFT, MANUFACTURING AND SUPPLY CHAIN DESIGN | ICAS2024_0804 |
| Assonitis, A. | NUMERICAL STUDY ON THE FIRST-STAGE RE-ENTRY TRAJECTORY USING AN INFLATABLE BALLUTE | ICAS2024_0401 |
| Assonitis, A. | AERO-THERMAL ANALYSIS OF A REUSABLE LAUNCH VEHICLE DURING RE-ENTRY MANOEUVRER | ICAS2024_0877 |
| Astarita, T. | NUMERICAL STUDY ON ACTIVE FLOW CONTROL SOLUTIONS FOR HIGH LIFT | ICAS2024_1053 |
| Atherton, K. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Atinault, O. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Augello, R. | MACRO, MESO AND MICRO SCALE ENERGY EVALUATION IN LAMINATED AND COMPOSITE STRUCTURES USING THE COMPONENT-WISE APPROACH | ICAS2024_0252 |
| Avanesian, D. | X-57 TRACTION POWER AND COMMAND SYSTEMS DEVELOPMENT | ICAS2024_1288 |
| Avi, A. | AI-ASSISTED DESIGN OF UAV DOCKING STATION NETWORK FOR DUAL USE PURPOSES | ICAS2024_1133 |
| Avirovic, M. | PASSIVE FLOW CONTROL DEVICES ON LOW-REYNOLDS DU89-134 AIRFOIL | ICAS2024_0228 |
| Avirovic, M. | DESIGN OF MEASUREMENT SETUP FOR HIGH-ALTITUDE IN-FLIGHT EXPERIMENTS ON DU89-134/14 AIRFOIL AT LOW REYNOLDS NUMBER | ICAS2024_0757 |
| Avni, O. | NONLINEAR DROPLET DYNAMICS IN IDEALIZED TRAILING VORTICES | ICAS2024_0995 |
| Aydin, E. | REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS | ICAS2024_1172 |
| Azevedo, J.L.F. | ADJOINT-BASED TRANSONIC WING AERODYNAMIC SHAPE OPTIMIZATION INVESTIGATIONS | ICAS2024_0078 |
| Azevedo, J.L.F. | INVESTIGATING THE INFLUENCE OF AN INBOARD PROPELLER’S VERTICAL OFFSET ON A TRAILING WING’S LIFT AND DRAG DISTRIBUTIONS | ICAS2024_0124 |
| Azevedo, J.L.F. | DATA-DRIVEN UNSTEADY AERODYNAMIC MODELS FOR AEROELASTIC STABILITY ANALYSES | ICAS2024_0181 |
| Azevedo, J.L.F. | LINEAR SYSTEM TECHNIQUES APPLIED TO NONLINEAR AEROSERVOELASTIC ANALYSES | ICAS2024_1004 |
| Azevedo, J.L.F. | ANALYSIS OF THE R FAMILY OF LIMITERS APPLIED TO HIGH-ORDER FR/CPR SCHEMES FOR THE SIMULATION OF SUPERSONIC FLOWS | ICAS2024_1181 |
| Azevedo, J.L.F. | ASSESSMENT OF EXPLICIT ALGEBRAIC REYNOLDS STRESS MODELS APPLIED TO AERONAUTICAL FLOWS | ICAS2024_1190 |
| Azoti, W. | A DIGITAL METHOD FOR THE COMPENSATED MOLD DESIGN OF COMPOSITE PARTS | ICAS2024_0487 |
| Azzara, R. | COUPLED THERMOELASTIC ANALYSIS OF BEAM STRUCTURES USING A REFINED 1D FINITE ELEMENT MODEL | ICAS2024_0854 |
| Babel, R. | EFFECT OF INFILL STYLE AND DENSITY ON SELECTED MECHANICAL PROPERTIES OF THE CARBON FIBRE REINFORCED ABS MFD FILAMENT | ICAS2024_0806 |
| Bacci, D. | HIGH FIDELITY MODELING OF ACOUSTIC LINERS FOR AERONAUTICAL APPLICATIONS | ICAS2024_1048 |
| Bagassi, S. | DESIGN AND DEVELOPMENT OF THE VISUAL AND AUDITORY LAYER FOR DIFFERENT CABIN/COCKPIT LAYOUT | ICAS2024_0799 |
| Bagassi, S. | EXTENDED REALITY IN AIRPORT CONTROL TOWERS: FROM CONCEPT DESIGN TO PRELIMINARY ASSESSMENT OF AN INNOVATIVE HUMAN-MACHINE INTERFACE FOR AIR TRAFFIC CONTROL OPERATORS | ICAS2024_1016 |
| Bagassi, S. | ADVANCED HUMAN MACHINE INTERFACES FOR DRONE MONITORING: ASSESSMENT OF THE TECHNOLOGICAL FRAMEWORK FOR THE DESIGN OF AN AUGMENTED REALITY INTERFACE | ICAS2024_1059 |
| Bagherzadeh, A. | AN OPTICAL FLOW BASED GUIDANCE ALGORITHM FOR A QUADROTOR UAV MOVING INSIDE CIRCULAR CORRIDORS | ICAS2024_1209 |
| Bai, C.-Y. | IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM | ICAS2024_1186 |
| Bai, J. | AERODYNAMIC PERFORMANCE OF BLADELESS DUCTED FAN BASED ON EJECTION EFFECT WITH DIFFERENT DESIGN VARIABLES | ICAS2024_0419 |
| Bai, J.-B. | CONFIGURATION ANALYSIS OF INTEGRATED THERMAL MANAGEMENT BASED ON THE TURBINE-FAN REFRIGERATION SYSTEM | ICAS2024_0194 |
| Bai, X. | RESEARCH ON UNSTEADY AERODYNAMIC MODELING METHOD OF PREPOSITIVE WING - MAIN WING COMPOSITE SYSTEM AT HIGH ATTACK ANGLE | ICAS2024_0239 |
| Bai, X.-S. | EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR | ICAS2024_0518 |
| Bai, Y. | THE RESISTANCE TO THE HIGH-VELOCITY IMPACT OF THE INTRA-LAYER HYBRID PLAIN WEAVE COMPOSITES | ICAS2024_0212 |
| Bai, Y. | A MESO-SCALED SIMULATION ON THE THICKNESS EFFECT OF TWO-DIMENSIONAL TRIAXIALLY BRAIDED COMPOSITES UNDER TENSILE LOADS | ICAS2024_0259 |
| Bai, Y. | SIMULATION STUDY ON AERODYNAMIC CHARACTERISTICS OF COMBINED LOW ASPECT RATIO UAV | ICAS2024_0449 |
| Bai, Y. | A DYNAMIC TEST METHODOLOGY FOR DETERMINING THE LONGITUDINAL COMPRESSIVE RESPONSE OF CARBON FIBER COMPOSITE TOWS | ICAS2024_0584 |
| Baier, J. | CLOSED-LOOP GUST LOADS ANALYSIS OF A SUPERSONIC FIGHTER AIRCRAFT | ICAS2024_0011 |
| Bake, S. | THERMODYNAMIC DESIGN AND EMISSIONS MODEL OF A MACH 1.8 SUPERSONIC AIRLINER ENGINE | ICAS2024_0129 |
| Bake, S. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Balajewicz, M. | PARAMETERISATION OF NONLINEAR AEROELASTIC REDUCED ORDER MODELS WITH AERODYNAMIC AND STRUCTURAL NONLINEARITY | ICAS2024_0954 |
| Baldo, L. | THE JOURNEY TOWARDS CONDITION-BASED MAINTENANCE: A FRAMEWORK FOR THE HORIZONTAL TAIL ACTUATOR OF AN ADVANCED JET TRAINER AIRCRAFT | ICAS2024_0198 |
| Ballarin, P. | NUMERICAL TOOLS FOR SLOW-GROWTH APPROACHES TO DAMAGE TOLERANT COMPOSITE AERONAUTICAL STRUCTURES | ICAS2024_1146 |
| Bando, M. | STUDY ON CONTROL PERFORMANCE OF A NEW TYPE OF TILT-ROTOR AIRCRAFT | ICAS2024_0548 |
| Banerjee, J.R. | THE EFFECTS OF ENGINE MASS AND LOCATION ON THE FLUTTER CHARACTERISTICS OF AIRCRAFT WINGS | ICAS2024_0170 |
| Bang, H.-C. | DATA-DRIVEN MODEL DISCOVERY AND CONTROL OF HIGH-PERFORMANCE TRAINER AIRCRAFT VIA SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS | ICAS2024_0627 |
| Bang, H.-C. | AERODYNAMIC MODEL IDENTIFICATION OF A VTOL TAILSITTER UAV USING SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS | ICAS2024_0653 |
| Bang, H.C. | MEDIAL AXIS TRANSFORMATION-BASED CONVEX MODEL PREDICTIVE CONTROL FOR MULTIROTOR INDOOR AUTONOMOUS FLIGHT WITH FIXED ALTITUDE | ICAS2024_0294 |
| Bantscheff, K. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF A STRUCTURAL-DYNAMICALLY SCALED DELTA WING WITH TRAINING EDGE FLAPS | ICAS2024_0853 |
| Bao, S. | SUSTAINABLE FUELS SAFETY BOUNDARIES DEMARCATION METHOD | ICAS2024_0712 |
| Barbarino, M. | DUAL-STREAM JET NOISE TEST WITH INTERNAL MIXER DESIGN VARIATIONS FOR LTO NOISE OF SUPERSONIC AIRCRAFT | ICAS2024_0064 |
| Barbarino, M. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Barbarino, M. | SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT | ICAS2024_0361 |
| Barbato, G. | PRELIMINARY DESIGN OF A FIXED-WING DRONE FOR MARS EXPLORATION ACTIVITIES | ICAS2024_0863 |
| Bardenhagen, A. | A MORPHOLOGICAL ANALYSIS OF METHODS FOR CONCEPTUAL AIRCRAFT DESIGN UNDER UNCERTAINTIES | ICAS2024_1169 |
| Bardera, R. | EXPLORING WINGTIP COLUMNAR VORTEX GENERATORS FOR UAV PERFORMANCE ENHANCEMENT | ICAS2024_0219 |
| Bardera, R. | PIV AND AERODYNAMIC FORCES ANALYSIS OF A HELICOPTER OPERATING AROUND A BUILDING BY WIND-TUNNEL EXPERIMENTS | ICAS2024_0257 |
| Barqueira, A. | INSIGHTS INTO HUMAN FATIGUE: STATISTICAL ANALYSIS IN AIRCRAFT MAINTENANCE | ICAS2024_0131 |
| Barravecchia, F. | PRELIMINARY RESULTS FOR AN INSTRUCTION DESIGN PROCEDURE IN AERONAUTICAL MANUFACTURING | ICAS2024_0306 |
| Barrier, R. | GRADIENT-BASED OPTIMIZATION OF AN AXIAL COMPRESSOR UNDER INLET DISTORTION USING BODY-FORCE MODELING | ICAS2024_0726 |
| Barrière, L. | ON AN EFFICIENT GLOBAL/LOCAL STOCHASTIC METHODOLOGY FOR FAILURE PREDICTION OF AIRCRAFT COMPOSITE STRUCTURES | ICAS2024_0250 |
| Barroso, E. | EXPLORING WINGTIP COLUMNAR VORTEX GENERATORS FOR UAV PERFORMANCE ENHANCEMENT | ICAS2024_0219 |
| Barroso, E. | PIV AND AERODYNAMIC FORCES ANALYSIS OF A HELICOPTER OPERATING AROUND A BUILDING BY WIND-TUNNEL EXPERIMENTS | ICAS2024_0257 |
| Barry, N. | CHARACTERISING THE ROLE OF FLEET RENEWAL ON THE PATHWAY TO 2050: A EUROPEAN AIRLINE CASE STUDY | ICAS2024_0126 |
| Bartolomei, M. | PRELIMINARY RESULTS FOR AN INSTRUCTION DESIGN PROCEDURE IN AERONAUTICAL MANUFACTURING | ICAS2024_0306 |
| Bassolillo, S.R. | ENHANCING QUADCOPTER CONTROL: A MODEL REFERENCE ADAPTIVE CONTROL APPROACH WITH NEURAL NETWORKS | ICAS2024_0459 |
| Bassolillo, S.R. | A MODEL PREDICTIVE CONTROL ALGORITHM FOR THE FORMATION CONTROL OF NANOSATELLITES IN LEO ORBIT | ICAS2024_0494 |
| Batra, A. | A SENSITIVITY ANALYSIS ON THE ENDURANCE EQUATION FOR HYBRID-ELECTRIC AIRCRAFT | ICAS2024_1109 |
| Battiston, A. | DESIGN OPTIMISATION OF A BOUNDARY LAYER INGESTION PROPULSOR FOR A MULTI-FUEL HYDROGEN AIRCRAFT | ICAS2024_1060 |
| Bayandor, J. | BIRD AND DRONE IMPACT DAMAGE PROGNOSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT ENGINE | ICAS2024_1162 |
| Bayandor, J. | FLUID-SOLID INTERACTIVE MODELLING OF FABRIC-BASED ATMOSPHERIC ENTRY SIZED AERODYNAMIC DECELARATORS | ICAS2024_1178 |
| Baylon, P.B.A. | A NOVEL APPROACH TO AUTOMATED TRACKING CONTROL OF HYBRID TILTING ROTOR UAVS USING LQG CONTROLLER AND STATE MACHINE | ICAS2024_0535 |
| Beamer, C. | THE PRODUCTION OF HIGH-PERFORMANCE HEAT EXCHANGERS FOR AEROSPACE APPLICATIONS | ICAS2024_0022 |
| Beck, B. | FROM ONTOLOGY TO SYSTEM ARCHITECTURE: AN MBSE APPROACH TOWARD THE REALIZATION OF URBAN AIR MOBILITY | ICAS2024_0554 |
| Beezhold, T. | THE CHALLENGE OF SUSTAINABILITY IN COMMERCIAL AVIATION | ICAS2024_1227 |
| Beghetto, G. | DESIGN AND AERODYNAMIC OPTIMIZATION OF A THIN-HAUL AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION: ZETHA | ICAS2024_0394 |
| Bekdache, D. | FROM ONTOLOGY TO SYSTEM ARCHITECTURE: AN MBSE APPROACH TOWARD THE REALIZATION OF URBAN AIR MOBILITY | ICAS2024_0554 |
| Belan, M. | PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION PLASMA THRUSTERS | ICAS2024_0649 |
| Belderrain, M.C. | SLEEPINESS IN BRAZILIAN AVIATION: A PROBLEM-SOLVING APPROACH | ICAS2024_0027 |
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| Bertone, M. | PRELIMINARY ANALYSIS OF TEMPERATURE EFFECTS AND MANEUVER-INDUCED DEFORMATIONS ON FBG OPTIC FIBER INTEGRATED SYSTEMS | ICAS2024_0483 |
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| Bertram, O. | ADVANCING URBAN AIR MOBILITY: COLLABORATIVE EXCELLENCE AND INFRASTRUCTURE INITIATIVES BY DLR | ICAS2024_1223 |
| Berube, M.R. | FUTURE LANDSCAPE OF AVIATION ENERGY – US PERSPECTIVE | ICAS2024_1315 |
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| Bianchi, S. | FASTVIBE SW TOOL FOR RIDE-ALONG VIBRATION SURVEY ANALYSIS | ICAS2024_0455 |
| Bianchini, C. | CFD-BASED SCOUTING FOR THE DESIGN OF A MULTI-FUEL KEROSENE/HYDROGEN ATMOSPHERIC BURNER | ICAS2024_0432 |
| Bianchini, E. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Biancolini, M.-E. | EFFICIENT SHAPE OPTIMIZATION IN AERONAUTICS: INTEGRATING PARAMETRIC CAD AND MESH MORPHING FOR ENHANCED AERODYNAMIC PERFORMANCE | ICAS2024_0824 |
| Bidinotto, J.H. | HANDLING QUALITIES RATING SCALE: THE IMPACT OF THE PILOT SUBJECTIVITY IN WORKLOAD EVALUATION | ICAS2024_0848 |
| Bidinotto, J.H. | NONLINEAR BEHAVIOR IN AIRCRAFT FUEL GAUGE READINGS: AN EXPLORING ANALYSIS | ICAS2024_1187 |
| Biedermann, J. | INVESTIGATING THE FLEXIBLE HYDROGEN AIRCRAFT SYSTEM INTERFACE DESIGN USING THE XR CO-DESIGN APPROACH | ICAS2024_0358 |
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| Bierig, A. | GENERAL DESIGN CONSIDERATIONS FOR SOLAR-ELECTRIC HIGH-ALTITUDE LONG-ENDURANCE AIRCRAFT | ICAS2024_0910 |
| Biga, R. | HYDROGEN STORAGE SYSTEM DESIGN: CASE STUDIES FOR AIRBORNE APPLICATION | ICAS2024_0590 |
| Biggi, G. | EXPERIMENTAL VALIDATION OF THE DYNAMIC FINITE ELEMENT MODEL OF A 1:8 SCALE SEAPLANE USING A LASER DOPPLER VIBROMETER (LDV) | ICAS2024_0730 |
| Bil, C. | LIFE CYCLE ASSESSMENT OF ALTERNATIVE LAUNCH METHODS | ICAS2024_0545 |
| Binnebesel, J.H. | AUTOMATED OPERATION OF HIGH-PERFORMANCE FIXED-WING DRONES: A POTENTIAL GAME-CHANGER FOR GREEN AERIAL SERVICES | ICAS2024_0946 |
| Bisagni, C. | GUST LOAD PASSIVE ALLEVIATION BY MEANS ON NONLINEAR, BUCKLING DRIVEN, STRUCTURAL RESPONSE | ICAS2024_0147 |
| Bisagni, C. | NUMERICAL METHOD TO DETERMINE STRUCTURAL ELEMENT REDUCED STIFFNESS FOR DESIRED COMPOSITE WING STRUCTURES CONFIGURATIONS | ICAS2024_0727 |
| Bisagni, C. | NABUCCO TAKE-OFF: MULTI-STABLE PANELS FOR AN ADAPTIVE WING | ICAS2024_1230 |
| Bismark, A.H. | PERFORMANCE AND ECONOMIC ASSESSMENT OF A WING-INTEGRATED HYBRID LAMINAR FLOW CONTROL SYSTEM | ICAS2024_0097 |
| Bisschop, K.-J. | NOVEL TEST RIG TO DEMONSTRATE A MULTI FUNCTIONAL FLAP MECHANISM OFFERING A 2ND DEGREE OF FREEDOM | ICAS2024_0299 |
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| Blanco Garde, D. | HOT-WET CONDITIONING AND THE SENSITIVITY OF MECHANICAL TESTING WITHIN SURFACE TREATMENT QUALIFICATION FOR AIRCRAFT | ICAS2024_0407 |
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| Boccaccio, M. | REDESIGN OF AN AERONAUTICAL COMPOSITE STIFFENED PANEL WITH THE DOUBLE-DOUBLE DESIGN APPROACH | ICAS2024_0360 |
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| Bonnema, M. | BATTERY PERFORMANCE METRICS FOR LARGE ELECTRIC PASSENGER AIRCRAFT | ICAS2024_0636 |
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| Borgoltz, A. | THE BEVERLI HILL EXPERIMENTS FOR SMOOTH-BODY TURBULENT FLOW SEPARATION - RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS | ICAS2024_1219 |
| Borio, V. | INTEGRATING ECO-EFFICIENT FLIGHT PLANNING IN AIRCRAFT CONCEPTUAL DESIGN: MINIMAL NOX ROUTES FOR HIGH-SPEED AIRCRAFT USING HYDROGEN | ICAS2024_0950 |
| Boscagli, L. | UNSTEADY AERODYNAMICS OF A COUPLED COMPACT INTAKE-FAN IN CROSSWIND | ICAS2024_0263 |
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| Bouvet, C. | MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE SCALE | ICAS2024_0290 |
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| Breitsamter, C. | AERODYNAMIC INTERACTION EFFECTS OF TILTROTOR EVTOL AIRCRAFT | ICAS2024_0978 |
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| Budinger, M. | STUDY OF HYBRIDISATION SCENARIOS FOR TURBOPROP AIRCRAFT IN THE GENERAL AVIATION SEGMENT | ICAS2024_0153 |
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| Burschyk, T. | GLOBAL SENSITIVITY ANALYSIS OF LIQUID HYDROGEN STORAGE DESIGN PARAMETERS FOR OVERALL AIRCRAFT DESIGN | ICAS2024_0092 |
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| Bussemaker, J. | PROCESSES, METHODS AND TOOLS SUPPORTING THE DEVELOPMENT OF AERONAUTICAL SYSTEMS | ICAS2024_0285 |
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| Bustamante, J. | GUST LOAD ALLEVIATION IN A SCALED UAV DEMONSTRATOR | ICAS2024_0580 |
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| Cabaleiro de la Hoz, C. | AUTOMATING THE VERIFICATION OF GEOMETRIC REQUIREMENTS FOR AIRCRAFT FUEL SYSTEMS USING KNOWLEDGE-BASED ENGINEERING | ICAS2024_0148 |
| Cabral, P.H. | INFLUENCE OF SKIN CURVATURE ON WINGBOX OPTIMIZATION WITH NONLINEAR STRUCTURAL STABILITY CONSTRAINTS | ICAS2024_0114 |
| Cabral, P.H. | FAST TRANSONIC CORRECTIONS FOR PANEL METHODS USING VISCOUS-INVISCID INTERACTION | ICAS2024_0162 |
| Cabral, P.H. | AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING DESIGN | ICAS2024_0167 |
| Cabral, P.H. | THE EFFECTS OF ENGINE MASS AND LOCATION ON THE FLUTTER CHARACTERISTICS OF AIRCRAFT WINGS | ICAS2024_0170 |
| Cabral, P.H. | SANDWICH COMPOSITES SKIN PANEL OPTIMIZATION FOR THE COMMON RESEARCH MODEL WING | ICAS2024_0479 |
| Cabral, P.H. | RANDOM MATRIX MODELLING FOR UNCERTAINTY QUANTIFICATION IN PRESTRESSED STRUCTURES | ICAS2024_0875 |
| Cacciola, S. | STEADY ANALYSIS OF THREE-SURFACE AIRPLANES: IMPROVING THE AERODYNAMIC PERFORMANCE THROUGH REDUNDANT LONGITUDINAL CONTROL | ICAS2024_0273 |
| Cacciola, S. | PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION PLASMA THRUSTERS | ICAS2024_0649 |
| Cacciola, S. | IDENTIFICATION OF THE IMPACT OF BLOWING ON THE AERODYNAMIC MODEL OF AN AIRPLANE WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2024_1134 |
| Cafiero, G. | PRELIMINARY DESIGN OF A FULL ELECTRIC GENERAL AVIATION AIRCRAFT POWERED WITH FUEL CELL: A CASE STUDY. | ICAS2024_1207 |
| Caggese, S. | COMPARATIVE ANALYSIS OF MACHINE LEARNING ALGORITHMS FOR HEAT EXCHANGERS DIAGNOSIS IN ELECTRIFIED AIRCRAFT | ICAS2024_0701 |
| Cai, J. | LONG-WAVE INSTABILITY OF AIRCRAFT WAKE VORTEX UNDER SHEAR CROSSWIND | ICAS2024_0551 |
| Cai, J. | PASSIVE FAULT TOLERANT CONTROL OF A DUAL-SYSTEM UAV IN TRANSITION FLIGHT | ICAS2024_0570 |
| Cakir, B. | AERODYNAMIC NUMERICAL/EXPERIMENTAL COMPARISON OF A HYPERSONIC TEST VEHICLE IN MORE&LESS PROGRAM | ICAS2024_1026 |
| Cakir, B.O. | EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR | ICAS2024_0518 |
| Calia, A. | AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) | ICAS2024_0575 |
| Camacho, E.A.R. | MITIGATING DYNAMIC STALL WITH A MOVABLE LEADING-EDGE: THE NACA0012-IK30 WING | ICAS2024_0595 |
| Camanho, P.P. | ON AN EFFICIENT GLOBAL/LOCAL STOCHASTIC METHODOLOGY FOR FAILURE PREDICTION OF AIRCRAFT COMPOSITE STRUCTURES | ICAS2024_0250 |
| Camilleri, R. | A SENSITIVITY ANALYSIS ON THE ENDURANCE EQUATION FOR HYBRID-ELECTRIC AIRCRAFT | ICAS2024_1109 |
| Camporeale, S.M. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF NOISE GENERATION IN HYDROGEN AND METHANE-HYDROGEN LAMINAR FLAMES | ICAS2024_1129 |
| Candon, M. | PARAMETERISATION OF NONLINEAR AEROELASTIC REDUCED ORDER MODELS WITH AERODYNAMIC AND STRUCTURAL NONLINEARITY | ICAS2024_0954 |
| Cannizzaro, D. | PRELIMINARY RESULTS FOR AN INSTRUCTION DESIGN PROCEDURE IN AERONAUTICAL MANUFACTURING | ICAS2024_0306 |
| Cantrell, M. | WING OF TOMORROW - LONGER, LEANER, LIGHTER | ICAS2024_1283 |
| Cao, H. | TECHNICAL RISK MANAGEMENT OF SYSTEM OF SYSTEMS BASED ON TECHNOLOGY READINESS ASSESSMENT | ICAS2024_0041 |
| Cao, H. | REVIEW ON NONLINEAR AEROELASTIC ANALYSIS WITH FREEPLAY | ICAS2024_0922 |
| Cao, L. | RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS | ICAS2024_0550 |
| Cao, Z. | RESEARCH ON EFFICIENT ACTIVE T-S WAVE GENERATION METHOD IN BOUNDARY LAYER | ICAS2024_0543 |
| Cao, Z. | MEASUREMENTS OF T-S WAVES DUE TO ACOUSTIC DISTURBANCES IN EXPERIMENTS | ICAS2024_0682 |
| Cao Van, N. | ELECTRIC FIELD MEASUREMENT IN GLOW DISCHARGE PLASMA INTERACTING WITH SHOCK WAVE IN HYPERSONIC FLOW | ICAS2024_0390 |
| Capitan, A. | DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS | ICAS2024_0229 |
| Capitao Patrao, A. | LESSONS LEARNED FROM PROJECT BASED TEACHING IN AEROSPACE AT CHALMERS | ICAS2024_0867 |
| Capoluongo, F. | FLUIDODYNAMIC ANALYSIS OF LOW REYNOLDS NUMBER FLOWS | ICAS2024_0354 |
| Caporale, A.M. | IMPACT TOLERANCE OF CERAMIC MATRIX COMPOSITES FOR AEROSPACE APPLICATIONS | ICAS2024_1111 |
| Cardellino, G. | ACTIVE CONTROL DAMPING WITH THE USE OF VOICE COIL ACTUATORS | ICAS2024_1106 |
| Cardone, G. | NUMERICAL STUDY ON ACTIVE FLOW CONTROL SOLUTIONS FOR HIGH LIFT | ICAS2024_1053 |
| Cardone, L.M. | DESIGN OF HYDROGEN STORAGE SYSTEMS IN NEW-GENERATION REGIONAL AIRCRAFT | ICAS2024_0858 |
| Cardoso, R.A.S. | A-BASIS AND B-BASIS BUCKLING ALLOWABLES FOR AN AIRCRAFT COMPOSITE WING | ICAS2024_0322 |
| Cardoso Junior, M.M. | VALIDATING ASSUMPTIONS ABOUT PILOT RECOGNITION: A PCM-BASED APPROACH FOR AIRCRAFT CERTIFICATION SAFETY ASSESSMENT PROCESS | ICAS2024_0089 |
| Cardoso Júnior, M.M. | DECODING AN IN-FLIGHT REFUELING INCIDENT: AVIATION COMPLEXITY THROUGH STAMP/CAST AND ACCIMAP METHODS | ICAS2024_0106 |
| Cardoso Junior, M.M. | FROM THA TO REAL-TIME MONITORING: INTEGRATING NEW VIEW OF SAFETY INTO FLIGHT TEST PROGRAMS | ICAS2024_0127 |
| Cardoso Júnior, M.M. | A SYSTEMATIC REVIEW OF HUMAN FACTORS AND AI INFLUENCING OPERATOR PERFORMANCE IN MUM-T ENVIRONMENTS | ICAS2024_0132 |
| Cardoso Junior, M.M. | HELICOPTER ACCIDENTS IN BRAZIL: AN ANALYSIS OF MAINTENANCE FROM THE PERSPECTIVE OF HUMAN FACTORS | ICAS2024_0416 |
| Cardoso-Junior, M.M. | SLEEPINESS IN BRAZILIAN AVIATION: A PROBLEM-SOLVING APPROACH | ICAS2024_0027 |
| Cardoso-Junior, M.M. | ASSESSING MENTAL WORKLOAD AND INTERFACE USABILITY IN MILITARY PILOTS: AN ADVANCED EYE-TRACKING METHODOLOGY | ICAS2024_0202 |
| Carini, A. | CYBER-PHYSICAL SYSTEM IMPLEMENTATION FOR THE AR-ASSISTED AIT OF AEROSPACE COMPONENTS | ICAS2024_0672 |
| Carini, M. | GRADIENT-BASED OPTIMIZATION OF AN AXIAL COMPRESSOR UNDER INLET DISTORTION USING BODY-FORCE MODELING | ICAS2024_0726 |
| Carloni, A.C.N. | DATA-DRIVEN UNSTEADY AERODYNAMIC MODELS FOR AEROELASTIC STABILITY ANALYSES | ICAS2024_0181 |
| Carlsson, M. | ENHANCING EFFICIENCY FOR UNSTEADY CFD COMPUTATIONS IN AERONAUTICS | ICAS2024_0247 |
| Carnielo, B.T.V. | THE INFLUENCE OF DIFFERENT WING MOTIONS ON THE LIFT IN BIO-INSPIRED AERIAL VEHICLES | ICAS2024_0744 |
| Carrera, E. | AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING DESIGN | ICAS2024_0167 |
| Carrera, E. | MACRO, MESO AND MICRO SCALE ENERGY EVALUATION IN LAMINATED AND COMPOSITE STRUCTURES USING THE COMPONENT-WISE APPROACH | ICAS2024_0252 |
| Carrera, E. | DESIGN AND DEVELOPMENT OF THE VISUAL AND AUDITORY LAYER FOR DIFFERENT CABIN/COCKPIT LAYOUT | ICAS2024_0799 |
| Carrera, E. | NUMERICAL ANALYSIS OF PROCESS-INDUCED DEFORMATIONS AND STRESSES IN AERONAUTICAL COMPOSITE COMPONENTS | ICAS2024_0818 |
| Carrera, E. | COUPLED THERMOELASTIC ANALYSIS OF BEAM STRUCTURES USING A REFINED 1D FINITE ELEMENT MODEL | ICAS2024_0854 |
| Carrera, E. | HIGHER-ORDER 1D STICK MODELS FOR THE FLUTTER ANALYSIS OF AIRCRAFT STRUCTURES | ICAS2024_1001 |
| Carrera, E. | INVESTIGATING THE EFFECT OF DELAMINATION-INDUCED FRICTIONAL CONTACT ON THE DYNAMIC BEHAVIOR OF LAMINATE STRUCTURES | ICAS2024_1108 |
| Carrera, E. | A PRELIMINARY METHODOLOGY TO ASSESS GUST SPECTRA VIA SATELLITE DATA | ICAS2024_1142 |
| Carrera , E. | VIBRATION OF COMPOSITE SHELLS OF REVOLUTION USING EQUIVALENT SINGLE LAYER APPROACH | ICAS2024_1203 |
| Caruso, P. | HYDROGEN SAFETY: A COMPARATIVE ANALYSIS OF LEAK DETECTION SENSORS | ICAS2024_0149 |
| Carvalho, A. | STRUCTURED ANALYSIS ESTIMATION FOR ELECTRICAL ENERGY DEMAND ON AIRPORT OPERATIONS FOR HYBRID REGIONAL AND ELECTRIC TOWING PARAMETERIZED BY MOVEMENT METRICS CONSIDERING UPCOMING ELECTRIC INTENSIVE TECHNOLOGIES AND EMISSION REDUCTIONS IN THE UPCOMING DECADE | ICAS2024_1007 |
| Casciaro, E. | FULLY-EMBEDDED PRESSURE SENSOR FOR AERODYNAMICS SURFACES BASED ON FBG TECHNOLOGY | ICAS2024_0739 |
| Cascinelli, G. | ON THE FUTURE OF TRANSONIC FLIGHTS: CURVED PLANFORM WINGS FOR BUFFET-ONSET CONTROL | ICAS2024_0495 |
| Cascone, F. | LAUNCH SYSTEM ASSESSMENT OF AN EXPERIMENTAL HYPERSONIC SCRAMJET VEHICLE | ICAS2024_0363 |
| Cassese, A. | THE PRODUCTION OF HIGH-PERFORMANCE HEAT EXCHANGERS FOR AEROSPACE APPLICATIONS | ICAS2024_0022 |
| Cassineli Palharini, R. | AERODYNAMIC ANALYSIS OF A FLAP-BASED DEPLOYABLE RE-ENTRY SYSTEM UNDER RAREFIED CONDITIONS | ICAS2024_1201 |
| Cassoni, G. | SIMPLIFIED MODELS OF PILOT BIOMECHANICS FOR ROTORCRAFT VERTICAL BOUNCE ANALYSIS | ICAS2024_0520 |
| Castaneda, F. | AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS | ICAS2024_1139 |
| Castanié, B. | MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE SCALE | ICAS2024_0290 |
| Castanie, B. | A DIGITAL METHOD FOR THE COMPENSATED MOLD DESIGN OF COMPOSITE PARTS | ICAS2024_0487 |
| Castro, S.G.P. | EXPLORING MULTI-FIDELITY AEROELASTIC TAILORING: PROSPECT AND MODEL ASSESSMENT | ICAS2024_0150 |
| Castro, S.G.P. | TOWARDS EFFICIENT ANALYSIS OF POSTBUCKLING IN AIRCRAFT STIFFENED STRUCTURES | ICAS2024_0760 |
| Castro, Y. | MULTIPLATFORM SIMULATION USING ROS | ICAS2024_0755 |
| Catalano, P. | FLUIDODYNAMIC ANALYSIS OF LOW REYNOLDS NUMBER FLOWS | ICAS2024_0354 |
| Cattel, F. | COMPARATIVE ANALYSIS OF EVTOL, DRONE AND GROUND TRANSPORTATION SYSTEMS FOR EMERGENCY DELIVERY OF BLOOD-DERIVED MEDICATION | ICAS2024_0700 |
| Causa, F. | RESEARCH RESULTS AND PERSPECTIVES ON NON-COOPERATIVE SENSING FOR SAFE UAM OPERATIONS | ICAS2024_1267 |
| Cavalieri, V. | MULTI-OBJECTIVE DESIGN OPTIMIZATION OF A MORPHING AILERON FOR A HYBRID ELECTRIC REGIONAL AIRCRAFT | ICAS2024_0385 |
| Cavallaro, R. | LOCAL AIR QUALITY AND NOISE OPTIMIZATION OF A LARGE ASPECT RATIO WINGS WITH DISTRIBUTED HYBRID ELECTRIC PROPULSION | ICAS2024_1067 |
| Cavalli, L. | IMPACT TOLERANCE OF CERAMIC MATRIX COMPOSITES FOR AEROSPACE APPLICATIONS | ICAS2024_1111 |
| Cecrdle, J. | W-WING AEROELASTIC DEMONSTRATOR DESIGN MODIFICATION AND UPGRADE | ICAS2024_0054 |
| Cella, U. | EFFICIENT SHAPE OPTIMIZATION IN AERONAUTICS: INTEGRATING PARAMETRIC CAD AND MESH MORPHING FOR ENHANCED AERODYNAMIC PERFORMANCE | ICAS2024_0824 |
| Celli, S. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Centomo, S. | AUTOMATIC SYSTEM REQUIREMENTS VERIFICATION FOR THE MBSE-ORIENTED AIRCRAFT DESIGN PROCESS | ICAS2024_0860 |
| Cerino, G. | STRUCTURAL DESIGN OF NEXT-GENERATION REGIONAL GREEN AIRCRAFT | ICAS2024_1035 |
| Cesnik, C.E.S. | FINITE ELEMENT MODEL UPDATE OF VERY FLEXIBLE AIRCRAFT BASED ON GROUND VIBRATION TESTS | ICAS2024_0403 |
| Cesnik, C.E.S. | EXPLORING ROLL MANEUVERABILITY OF FUTURE AIRCRAFT WITH HIGH AR WINGS | ICAS2024_1286 |
| Cestino, D. | COMPARATIVE ANALYSIS OF EVTOL, DRONE AND GROUND TRANSPORTATION SYSTEMS FOR EMERGENCY DELIVERY OF BLOOD-DERIVED MEDICATION | ICAS2024_0700 |
| Cestino, E. | EXPERIMENTAL RESULTS OF ANTENNA PLACEMENT TEST ON A CARBON-FIBER SCALE REPLICA OF THE S55X SEAPLANE | ICAS2024_0504 |
| Cestino, E. | NUMERICAL-THEORETICAL EVALUATION OF THE DITCHING OF A HULL WITH DIHEDRAL ANGLES BETWEEN -5 AND 20 DEGREES | ICAS2024_0665 |
| Cestino, E. | COMPARATIVE ANALYSIS OF EVTOL, DRONE AND GROUND TRANSPORTATION SYSTEMS FOR EMERGENCY DELIVERY OF BLOOD-DERIVED MEDICATION | ICAS2024_0700 |
| Cestino, E. | EXPERIMENTAL VALIDATION OF THE DYNAMIC FINITE ELEMENT MODEL OF A 1:8 SCALE SEAPLANE USING A LASER DOPPLER VIBROMETER (LDV) | ICAS2024_0730 |
| Cha, J.-H. | INFLATABLE SPACE SHIELD STRUCTURE FOR SPACE HABITATION MODULE | ICAS2024_0878 |
| Chagas Silva, T. | ASSESSMENT OF EXPLICIT ALGEBRAIC REYNOLDS STRESS MODELS APPLIED TO AERONAUTICAL FLOWS | ICAS2024_1190 |
| Chai, J. | ANGLE AND DISTANCE EFFECT ON PHOSPHOR THERMOMETRY | ICAS2024_0529 |
| Chai, Y.J. | FLUID-STRUCTURE INTERACTION OF TWO-PHASE SCATTERER METAMATERIALS FOR VIBRATION SELF-SUPPRESSION | ICAS2024_0435 |
| Chakraborty, I. | EXPLICIT MODEL FOLLOWING TRAJECTORY CONTROL SYSTEM FOR MULTIPLE VERTICAL TAKEOFF AND LANDING CONFIGURATIONS | ICAS2024_1166 |
| Chakraborty, I. | INTEGRATED SIZING OF AN ELECTRIFIED TILT-WING AIRCRAFT FOR VERTICAL AND CONVENTIONAL TAKEOFF AND LANDING | ICAS2024_1170 |
| Chan, B. | OPTIMIZING FLEET ASSIGNMENT DECISIONS FOR REGIONAL AIRLINES WITH HYBRID ELECTRIC AIRCRAFT UPTAKE | ICAS2024_0781 |
| Chan, J.L.C. | PERFORMANCE ENHANCEMENTS BETWEEN DIFFERENT APPLICATIONS OF ALTERNATIVE FUELS AND NOVEL AIRCRAFT CONFIGURATIONS | ICAS2024_1046 |
| Chandran, S. | A PERFORMANCE COMPARISON OF HYDROGEN AIRCRAFT CONCEPTS | ICAS2024_0251 |
| Chang, J.W. | ENHANCED AIRCRAFT TAKEOFF/LANDING SAFETY USING DEEP LEARNING MODEL IN RUNWAY ASSISTANCE SYSTEM | ICAS2024_0786 |
| Chang, S. | STUDY OF DROPLET MOTION AND WATER FILM FLOW CHARACTERISTICS ON SUPERHYDROPHOBIC SURFACES UNDER AIRFLOW SHEARING | ICAS2024_0934 |
| Chao, T. | LINEAR QUADRATIC PURSUIT AND EVASION DIFFERENTIAL GAME GUIDANCE STRATEGY WITH OBSTACLE AVOIDANCE | ICAS2024_0008 |
| Charruaz, G. | FLIGHT PERFORMANCE AND DYNAMICS OF AN UNCONVENTIONAL SOLAR POWERED UAS | ICAS2024_0947 |
| Chauhan, S.S. | INVESTIGATING THE INFLUENCE OF AN INBOARD PROPELLER’S VERTICAL OFFSET ON A TRAILING WING’S LIFT AND DRAG DISTRIBUTIONS | ICAS2024_0124 |
| Che, A.-L. | FAST PARAMETRIC STRUCTURE MODELING FOR VARIETY OF AIRCRAFT CONFIGURATIONS | ICAS2024_0614 |
| Che, J. | SYSTEM ARCHITECTURE AND EVALUATION METHOD OF HUMAN-MACHINE COLLABORATION IN FLIGHT CONTROL SYSTEM | ICAS2024_0185 |
| Che, S. | SYSTEM ARCHITECTURE AND EVALUATION METHOD OF HUMAN-MACHINE COLLABORATION IN FLIGHT CONTROL SYSTEM | ICAS2024_0185 |
| Chen, B. | ATTITUDE ESTIMATION USING KALMAN FILTERING FOR SPACEBORNE SAR SYSTEMS | ICAS2024_0866 |
| Chen, D.-Y. | LARGE-SCALE STRUCTURAL DYNAMIC TOPOLOGY OPTIMIZATION DESIGN FOR AIRCRAFT VIBRATION REDUCTION UNDER RANDOM EXCITING RESPONSE | ICAS2024_0365 |
| Chen, F.-Z. | NUMERICAL INVESTIGATION ON THE EFFECT OF REYNOLDS NUMBER ON TANDEM DROPLET | ICAS2024_0426 |
| Chen, G. | INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF WINGS UNDER ICING CONDITIONS AT VARIOUS SWEEP ANGLES | ICAS2024_0287 |
| Chen, H. | DESIGN OF ATTITUDE CONTROL SYSTEM FOR DRAGONFLY-INSPIRED FLAPPING WING AERIAL VEHICLE | ICAS2024_0578 |
| Chen, J. | SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT | ICAS2024_0925 |
| Chen, J.-C. | NUMERICAL SIMULATION OF THE RESPONSE CHARACTERISTICS OF THE WING STRUCTURE OF A SEAPLANE PLANING IN WAVE | ICAS2024_0901 |
| Chen, J.-C. | ANALYSIS OF SUCTION FORCE EFFECT ON DIFFERENT FUSELAGE SHAPE DURING THE WATER DITCHING | ICAS2024_0929 |
| Chen, Q. | AERODYNAMIC DESIGN OF A SUPERSONIC TRANSPORT CONFIGURATION CONSIDERING AVERAGE LOUDNESS IN THE WHOLE BOOM CARPET | ICAS2024_0597 |
| Chen, S. | AERODYNAMIC CHARACTERISTICS RESEARCH OF A DISTRIBUTED PROPULSION AIRCRAFT | ICAS2024_0537 |
| Chen, S.-S. | DATA MINING ANALYSIS ON AERODYNAMIC STEALTH DESIGN PRINCIPLES OF AIRFOIL PROFILES | ICAS2024_0448 |
| Chen, T. | STUDY ON THE BALLISTIC-RESISTANT AIRWORTHINESS STANDARDS FOR COMMERCIAL AIRCRAFT COCKPIT DOOR | ICAS2024_0074 |
| Chen, T. | ATTITUDE ESTIMATION USING KALMAN FILTERING FOR SPACEBORNE SAR SYSTEMS | ICAS2024_0866 |
| Chen, W. | INTEGRITY MONITORING OF TIGHTLY INTEGRATED BDS/SINS USING MULTI-HYPOTHESIS SOLUTION SEPARATION (MHSS) ALGORITHM | ICAS2024_0244 |
| Chen, X. | SYSTEM ARCHITECTURE AND EVALUATION METHOD OF HUMAN-MACHINE COLLABORATION IN FLIGHT CONTROL SYSTEM | ICAS2024_0185 |
| Chen, X. | SET-BASED DESIGN TECHNIQUES FOR EVOLVABILITY EXPLORATION DURING CONCEPTUAL AIRCRAFT DESIGN | ICAS2024_0233 |
| Chen, X. | FAST PREDICTION OF PRESSURE DISTRIBUTION FOR 3D CONFIGURATION BASED ON LARGE LANGRAGE MODEL | ICAS2024_0679 |
| Chen, X.-Y. | COMPUTATIONAL/EXPERIMENTAL AEROELASTIC STUDY FOR AN ALL-MOVABLE HORIZONTAL TAIL WITH TORSION FREE-PLAY | ICAS2024_0728 |
| Chen, Z. | EXPERIMENTAL AND NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF A MARS ROTOR SYSTEM | ICAS2024_0790 |
| Chen, Z. | ANALYSIS OF BATTERY WEIGHT REQUIREMENTS IN THE DESIGN OF HYBRID ELECTRIC POWERED AIRCRAFT | ICAS2024_0813 |
| Chen, Z.L. | NUMERICAL STUDY ON ACOUSTIC RECEPTIVITY OF COMPRESSIBLE LAMINAR FLOW OVER A FLAT PLATE WITH MODIFIED SUPER-ELLIPSE LEADING EDGE | ICAS2024_0553 |
| Chen, Z.L. | NUMERICAL STUDIES ON NOISE-SHIELDING EFFECTS OF A BLENDED-WING-BODY AIRCRAFT USING BOUNDARY ELEMENT METHOD | ICAS2024_0556 |
| Cheng, C.W. | ABSOLUTE NODAL COORDINATE FORMULATION FOR NONLINEAR MULTIBODY MODELING OF FLARED HINGED WINGS | ICAS2024_0071 |
| Cheng, C.W. | NUMERICAL INVESTIGATION OF PASSIVE AND ACTIVE ALLEVIATION OF DYNAMIC LOADS ON HIGH-ASPECT-RATIO-WING VEHICLES | ICAS2024_0740 |
| Cheng, L. | AN EXPERIMENTAL SIMULATION ON THE INFLUENCE OF DIFFERENT FILM COOLING HOLE SHAPES ON PARTICLE DEPOSITION ON TURBINE VANE | ICAS2024_0341 |
| Cheng, P. | INVESTIGATION ON THE MECHANISM OF THERMAL CYCLING FAILURE IN C/SIC COATING COMPOSITE MATERIALS | ICAS2024_0796 |
| Cheng, R. | A MOMENTUM-INTEGRAL METHOD TO CALCULATE WINDAGE LOSSES ON A ROTATING DRUM WITH SUPERPOSED FLOW | ICAS2024_0281 |
| Cheng, W. | TECHNICAL RISK MANAGEMENT OF SYSTEM OF SYSTEMS BASED ON TECHNOLOGY READINESS ASSESSMENT | ICAS2024_0041 |
| Cheng, W. | RESEARCH ON TECHNOLOGICAL INNOVATION CAPABILITY EVALUATION INDEX FOR AVIATION INDUSTRIES | ICAS2024_0211 |
| Cheng, W. | REVIEW ON NONLINEAR AEROELASTIC ANALYSIS WITH FREEPLAY | ICAS2024_0922 |
| Cheng, W.-Y. | ANALYSIS ON COMPLEX HYPERSONIC FLOW DURING THE REENTRY OF EXPIRED SPACECRAFT | ICAS2024_0644 |
| Cheng, X. | CONJUGATED HEAT TRANSFER SIMULATION OF BUOYANCY-INDUCED FLOW AND HEAT TRANSFER MECHANISMS IN A COMPRESSOR CAVITY | ICAS2024_0531 |
| Cheng, Z.-H. | MODELING AND FLIGHT CONTROL LAW DESIGN FOR A SEAPLANE DURING WATER SURFACE TAKEOFF | ICAS2024_0977 |
| Chernoray, V. | LESSONS LEARNED FROM PROJECT BASED TEACHING IN AEROSPACE AT CHALMERS | ICAS2024_0867 |
| Chiarelli, M.R. | ON THE FUTURE OF TRANSONIC FLIGHTS: CURVED PLANFORM WINGS FOR BUFFET-ONSET CONTROL | ICAS2024_0495 |
| Chiarelli, M.R. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Cho, J.Y. | DEVELOPMENT OF A MACHINE LEARNING-BASED STRESS SPECTRUM ESTIMATION TECHNIQUE FOR FATIGUE MONITORING | ICAS2024_0525 |
| Chojnacki, M. | THERMAL HISTORY PAINT UNDER HIGH SUBSONIC FLOW | ICAS2024_0316 |
| Choudhari, M. | TRANSITION MODELING IN SUPPORT OF CFD VISION 2030 - HIGHLIGHTS OF RECENT EFFORTS AT THE NASA LANGLEY RESEARCH CENTER | ICAS2024_0081 |
| Choudhary, A. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Christensen, J.M. | APPLYING MODEL-BASED SYSTEM ENGINEERING AND DEVOPS ON THE IMPLEMENTATION OF AN AI-BASED COLLISION AVOIDANCE SYSTEM | ICAS2024_0869 |
| Christie, R. | UNSTEADY AERODYNAMICS OF A COUPLED COMPACT INTAKE-FAN IN CROSSWIND | ICAS2024_0263 |
| Chu, S.-Y. | ANALYSIS ON COMPLEX HYPERSONIC FLOW DURING THE REENTRY OF EXPIRED SPACECRAFT | ICAS2024_0644 |
| Chudy, K. | STUDY ON CONFIGURATIONS OF AIRBORNE LAUNCH SYSTEM FOR DELIVERY OF SMALL PAYLOAD TO LOW EARTH ORBIT | ICAS2024_0355 |
| Chudý, P. | HYBRID MODELING APPROACH FOR OPTIMIZATION BASED CONTROL OF MULTIROTOR UNMANNED AERIAL VEHICLES | ICAS2024_0029 |
| Chudý, P. | MODEL PREDICTIVE CONTROL DRIVEN AERIAL GRASPING WITH SOFT OPERATIONAL CONSTRAINTS | ICAS2024_0879 |
| Chudý, P. | PREDICTIVE CONTROL DRIVEN TACTICAL MANEUVERING | ICAS2024_1044 |
| Chung, J. | ENHANCED AIRCRAFT TAKEOFF/LANDING SAFETY USING DEEP LEARNING MODEL IN RUNWAY ASSISTANCE SYSTEM | ICAS2024_0786 |
| Cimini, M. | NUMERICAL INVESTIGATION ON THE LIQUID SLOSHING DAMPING INSIDE A TANK WITH A FLEXIBLE ANTI-SLOSHING DEVICE | ICAS2024_0930 |
| Cimini Jr., C.A. | A-BASIS AND B-BASIS BUCKLING ALLOWABLES FOR AN AIRCRAFT COMPOSITE WING | ICAS2024_0322 |
| Cinar, G. | OPTIMIZING FLEET ASSIGNMENT DECISIONS FOR REGIONAL AIRLINES WITH HYBRID ELECTRIC AIRCRAFT UPTAKE | ICAS2024_0781 |
| Cinefra, M. | DETECTION OF DELAMINATIONS IN DAMAGED COMPOSITE PLATES VIA LOCAL DAMAGE RESONANCE APPROACH | ICAS2024_0814 |
| Cini, A. | LOCAL AIR QUALITY AND NOISE OPTIMIZATION OF A LARGE ASPECT RATIO WINGS WITH DISTRIBUTED HYBRID ELECTRIC PROPULSION | ICAS2024_1067 |
| Ciottoli, P.P. | IMPACT OF WELL-TO-TANK EFFICIENCY AND EMISSIONS ON HYBRID AIRCRAFT DESIGN OPTIMIZATION | ICAS2024_0366 |
| Cirio, D. | AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) | ICAS2024_0575 |
| Clark, A.M. | CHALLENGES IN GEOMETRY DEVELOPMENT FOR THE CRM-HL ECOSYSTEM | ICAS2024_1212 |
| Clark, I.A. | REFINED PREDICTIONS COMPARED WITH THE PROPULSION AIRFRAME AEROACOUSTICS AND AIRCRAFT SYSTEM NOISE FLIGHT RESEARCH TEST DATA | ICAS2024_0069 |
| Clarke, S. | X-57 TRACTION POWER AND COMMAND SYSTEMS DEVELOPMENT | ICAS2024_1288 |
| Clay, M. | AERODYNAMIC NUMERICAL/EXPERIMENTAL COMPARISON OF A HYPERSONIC TEST VEHICLE IN MORE&LESS PROGRAM | ICAS2024_1026 |
| Cobleigh, B. | X-66: ACCELERATED LEARNING THROUGH FULL SCALE PROTOTYPING | ICAS2024_1240 |
| Coder, J.G. | EVALUATION OF CFD TRANSITION MODELING FOR TRANSONIC, NATURAL-LAMINAR-FLOW DESIGN | ICAS2024_1179 |
| Coelho, L. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Coen, P. | BREAKING THE SOUND BARRIER: ACHIEVING QUIET SUPERSONIC FLIGHT OVER LAND | ICAS2024_1251 |
| Cohen, G. | FRICTION RIVETING OF THERMOPLASTIC COMPOSITE WITH A CNC MACHINE: EXPERIMENTAL WORK | ICAS2024_1127 |
| Collier, F. | OBJECTIVES OF THE UNITED STATES FULL SCALE BLENDED WING BODY FLIGHT DEMONSTRATION | ICAS2024_1292 |
| Colonna, G. | ASSESSMENT OF A MACROSCOPIC MODEL FOR THE AEROTHERMODYNAMICS CHARACTERIZATION OF ICE GIANTS ATMOSPHERIC ENTRY | ICAS2024_0872 |
| Comer, A. | EXPLICIT MODEL FOLLOWING TRAJECTORY CONTROL SYSTEM FOR MULTIPLE VERTICAL TAKEOFF AND LANDING CONFIGURATIONS | ICAS2024_1166 |
| Comunian, P.J. | PRELIMINARY DESIGN OF A FULL ELECTRIC GENERAL AVIATION AIRCRAFT POWERED WITH FUEL CELL: A CASE STUDY. | ICAS2024_1207 |
| Concilio, A. | CONCEPTUAL DESIGN AND TOPOLOGY OPTIMIZATION OF A COMPLIANT MORPHING FLAP FOR NEXT GENERATION HYBRID-ELECTRIC REGIONAL AIRCRAFT | ICAS2024_1206 |
| Conen, P. | TRAIN ON SYNTHETIC - TEST ON REAL: DOMAIN ADAPTATION FOR STRAIN-BASED DAMAGE DETECTION ON AN AIRCRAFT WING | ICAS2024_0169 |
| Conte, C. | CLASSIFICATION OF EXTENDED REALITY BASED HUMAN MACHINE INTERFACES SCENARIOS FOR URBAN AIR MOBILITY | ICAS2024_0326 |
| Cooper, J. | CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT: HIGH ASPECT RATIO WINGS AND FLOATING WINGTIPS | ICAS2024_0386 |
| Cooper, J.E. | INFLUENCE OF SKIN CURVATURE ON WINGBOX OPTIMIZATION WITH NONLINEAR STRUCTURAL STABILITY CONSTRAINTS | ICAS2024_0114 |
| Cooper, J.E. | CONTINUING DEVELOPMENT OF A NOVEL CERTIFIABLE AIRLINER “GONDOLA” USING LIQUID HYDROGEN | ICAS2024_0939 |
| Corcione, S. | A COST-EFFICIENT PREDICTIVE METHOD FOR AERODYNAMIC PERFORMANCE DEGRADATION OF HORIZONTAL TAIL UNDER ICING CONDITIONS | ICAS2024_0415 |
| Cordoni, C. | A CFD STUDY OF THE ACTIVE FLOW CONTROL SYSTEM BEHAVIOUR ON A VERTICAL TAIL SECTION OF AN AIRPLANE, WITH THE AID OF AI | ICAS2024_0741 |
| Cornelje, S. | INVESTIGATING THE FLEXIBLE HYDROGEN AIRCRAFT SYSTEM INTERFACE DESIGN USING THE XR CO-DESIGN APPROACH | ICAS2024_0358 |
| Corsi, M. | EXTENDED REALITY IN AIRPORT CONTROL TOWERS: FROM CONCEPT DESIGN TO PRELIMINARY ASSESSMENT OF AN INNOVATIVE HUMAN-MACHINE INTERFACE FOR AIR TRAFFIC CONTROL OPERATORS | ICAS2024_1016 |
| Corsi, M. | ADVANCED HUMAN MACHINE INTERFACES FOR DRONE MONITORING: ASSESSMENT OF THE TECHNOLOGICAL FRAMEWORK FOR THE DESIGN OF AN AUGMENTED REALITY INTERFACE | ICAS2024_1059 |
| Cortez, J. | AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS | ICAS2024_1139 |
| Corti, M. | MULTI-OBJECTIVE DESIGN OPTIMIZATION OF A MORPHING AILERON FOR A HYBRID ELECTRIC REGIONAL AIRCRAFT | ICAS2024_0385 |
| Costa, M.A.C. | EXPERIMENTAL VALIDATION OF THE DYNAMIC FINITE ELEMENT MODEL OF A 1:8 SCALE SEAPLANE USING A LASER DOPPLER VIBROMETER (LDV) | ICAS2024_0730 |
| Costa Marques, H. | HOLISTIC AND SCALABLE SMART OPTIMIZATION FRAMEWORK FOR PRESCRIPTIVE MAINTENANCE | ICAS2024_0657 |
| Coupe, W.J. | TOWARDS SUSTAINABLE AVIATION WITH EFFICIENT AIRSPACE OPERATIONS | ICAS2024_1247 |
| Cox, D.E. | DISTRIBUTED THRUST TAKEOFF FOR THE NASA X-57 MOD IV FLIGHT DEMONSTRATOR | ICAS2024_1290 |
| Cozzolino, A. | AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) | ICAS2024_0575 |
| Crawley, B. | WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES | ICAS2024_1137 |
| Cremades, A. | EFFECT OF POPULAR ADDITIVE MANUFACTURING TECHNOLOGIES ON THE PERFORMANCE AND ACOUSTICS OF UAV PROPELLERS | ICAS2024_0896 |
| Cremaschi, M. | ESATTO: THE HOLISTIC FRAMEWORK TO SUPPORT THE DESIGN OF SUSTAINABLE SUPERSONIC AVIATION | ICAS2024_1032 |
| Crona, M. | LOW-SPEED PROPELLER FOR UAV APPLICATIONS, FROM DESIGN TO EXPERIMENTAL EVALUATION | ICAS2024_1157 |
| Crossley, W.A. | EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS | ICAS2024_0464 |
| Crothers, P.C. | SUSTAINABLE HIGH RATE COMPOSITE MANUFACTURE | ICAS2024_1302 |
| Crouch, J. | APPLICATION OF LAMINAR FLOW CONTROL FOR ENHANCED PERFORMANCE AND REDUCED EMISSIONS | ICAS2024_1231 |
| Crovato, A. | FAST TRANSONIC CORRECTIONS FOR PANEL METHODS USING VISCOUS-INVISCID INTERACTION | ICAS2024_0162 |
| Cruz Palacios, D. | PERFORMANCE AND ECONOMIC ASSESSMENT OF A WING-INTEGRATED HYBRID LAMINAR FLOW CONTROL SYSTEM | ICAS2024_0097 |
| Cuchet, D. | ATR COMMERCIAL AVIATION SUSTAINABILITY STRATEGY | ICAS2024_1244 |
| Cui, R. | AERODYNAMIC OPTIMIZATION OF HIGH-ALTITUDE PROPELLER COMBINED WITH MACHINE LEARNING METHOD | ICAS2024_0342 |
| Cui, Z. | TRANSFORMATIVE PEDAGOGY: CO-TEACHING COURSE CLUSTERS THROUGH COMPETITIVE TEAM DESIGNS FOR INNOVATIVE TALENT DEVELOPMENT IN AEROSPACE EDUCATION | ICAS2024_0324 |
| Cui, Z. | RESEARCH ON MULTI-ATTRIBUTE DECISION MAKING AND VERIFICATION METHODS FOR SYSTEMS CONFRONTATION | ICAS2024_0561 |
| Cui, Z. | A SEMANTIC MODEL-BASED SYSTEMS ENGINEERING APPROACH FOR SUPERSONIC BUSINESS JET CONCEPTUAL DESIGN | ICAS2024_0843 |
| Cumpsty, C. | HYDROGEN AIRLINER TANK OPTIMISATION | ICAS2024_0515 |
| Cuomo, F. | SMART ELECTRIC POWER MANAGEMENT ONBOARD FUTURE AIRCRAFT | ICAS2024_0085 |
| Cusati, V. | A COST-EFFICIENT PREDICTIVE METHOD FOR AERODYNAMIC PERFORMANCE DEGRADATION OF HORIZONTAL TAIL UNDER ICING CONDITIONS | ICAS2024_0415 |
| D'Accardi, E. | STIMULATED THERMOGRAPHY AS NON-DESTRUCTIVE TESTING TO ASSESS THE STRUCTURAL INTEGRITY OF AERONAUTICAL COMPONENT IN CFRP | ICAS2024_1076 |
| D'Alessio, G. | COMPARATIVE ANALYSIS OF MACHINE LEARNING ALGORITHMS FOR HEAT EXCHANGERS DIAGNOSIS IN ELECTRIFIED AIRCRAFT | ICAS2024_0701 |
| D'Alterio, G. | A SIMULINK APPROACH TO MODELING HETEROGENEOUS DRONE FORMATIONS FOR AGENT-BASED SIMULATION | ICAS2024_0608 |
| D'Amato, E. | ENHANCING QUADCOPTER CONTROL: A MODEL REFERENCE ADAPTIVE CONTROL APPROACH WITH NEURAL NETWORKS | ICAS2024_0459 |
| D'Amato, E. | A SIMULINK APPROACH TO MODELING HETEROGENEOUS DRONE FORMATIONS FOR AGENT-BASED SIMULATION | ICAS2024_0608 |
| D'Amato, E. | ADVANCED SOLUTIONS AND CHALLENGES IN MULTI-DRONE SYSTEMS FOR SEARCH AND RESCUE MISSIONS: TECHNICAL APPROACHES AND UNRESOLVED MATTER | ICAS2024_0795 |
| D'Onofrio, M. | CORUS-XUAM: TACKLING URBAN AIR MOBILITY AIRSPACE INTEGRATION CHALLENGES | ICAS2024_0347 |
| da Rocha, G.V. | DECODING AN IN-FLIGHT REFUELING INCIDENT: AVIATION COMPLEXITY THROUGH STAMP/CAST AND ACCIMAP METHODS | ICAS2024_0106 |
| da Silva, I.N.M. | HELICOPTER ACCIDENTS IN BRAZIL: AN ANALYSIS OF MAINTENANCE FROM THE PERSPECTIVE OF HUMAN FACTORS | ICAS2024_0416 |
| da Silva, R.G.A. | DYNAMIC FREE FLIGHT TESTS WITH A SUB-SCALE AIRPLANE DESIGNED ACCORDING TO THE FROUDE NUMBER | ICAS2024_1100 |
| da Silva, R.G.A. | INSTRUMENTATION OF A SUBESCALE GROUND EFFECT VEHICLE, VOLITAN, TO MEASURE FLIGHT PROPULSION EFFICIENCY | ICAS2024_1125 |
| Daelemans, L. | A CALL TO ACTION TO ENGAGE THE COMMUNITY TO MEET THE CHALLENGES THAT MUST BE TACKLED TO MAKE ELECTRIFIED AIRCRAFT PROPULSION REAL | ICAS2024_0834 |
| Dagan, Y. | NONLINEAR DROPLET DYNAMICS IN IDEALIZED TRAILING VORTICES | ICAS2024_0995 |
| Dagli, C.N. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Dagli, J. | AN AUTONOMOUS SYSTEM FOR DOCKING AND BATTERY SWAPPING IN UAVS | ICAS2024_1116 |
| Dagna, A. | AUTOMATIC SYSTEM REQUIREMENTS VERIFICATION FOR THE MBSE-ORIENTED AIRCRAFT DESIGN PROCESS | ICAS2024_0860 |
| Dahik, C. | AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS | ICAS2024_1139 |
| Dahlmann, K. | CLIMATE IMPACT AND ECONOMIC ASSESSMENT OF LIQUID HYDROGEN AND SYNTHETIC KEROSENE LONG-RANGE AIRCRAFT CONCEPTS | ICAS2024_0399 |
| Dai, H. | A HIGH-PRECESION PSEUDO ARC-LENGTH METHOD WITH POSITIVE VALUE PRESERVATION PROPERTIES BASED ON TV SPLITTING | ICAS2024_0694 |
| Dai, H. | FUZZING ON TARGET DETECTION SYSTEM OF UNMANNED AERIAL VEHICLE | ICAS2024_0794 |
| Daidié, A. | FRICTION RIVETING OF THERMOPLASTIC COMPOSITE WITH A CNC MACHINE: EXPERIMENTAL WORK | ICAS2024_1127 |
| Dalbera, A. | PASSIVE FLOW CONTROL DEVICES ON LOW-REYNOLDS DU89-134 AIRFOIL | ICAS2024_0228 |
| Dalla Vedova, M.D.L. | PRELIMINARY ANALYSIS OF TEMPERATURE EFFECTS AND MANEUVER-INDUCED DEFORMATIONS ON FBG OPTIC FIBER INTEGRATED SYSTEMS | ICAS2024_0483 |
| Damiani Ferretti, A.N. | PRELIMINARY DESIGN OF A FULL ELECTRIC GENERAL AVIATION AIRCRAFT POWERED WITH FUEL CELL: A CASE STUDY. | ICAS2024_1207 |
| Damljanovic, D. | REVITALIZATION OF A FLOW-CELL DEVICE FOR AIR INTAKE TESTING AND ITS INTEGRATION WITH WIND TUNNEL SYSTEMS | ICAS2024_0218 |
| Dance, H. | HYDROGEN AIRLINER TANK OPTIMISATION | ICAS2024_0515 |
| Danquah, F. | ANALYSIS OF AN ELECTRICAL-POWERED-DUCTED-THRUST VECTORING-FLAP | ICAS2024_0412 |
| Dantsker, O.D. | INTEGRATING UNMANNED AERIAL SYSTEMS INTO THE INTELLIGENT SYSTEMS ENGINEERING CURRICULUM | ICAS2024_1185 |
| Dave, K. | CFD-BASED SCOUTING FOR THE DESIGN OF A MULTI-FUEL KEROSENE/HYDROGEN ATMOSPHERIC BURNER | ICAS2024_0432 |
| Davi, A.S. | DYNAMIC FREE FLIGHT TESTS WITH A SUB-SCALE AIRPLANE DESIGNED ACCORDING TO THE FROUDE NUMBER | ICAS2024_1100 |
| David, C. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Davids, M. | FATIGUE PROPERTIES OF ADDITIVELY MANUFACTURED TOOL STEEL | ICAS2024_0633 |
| Dawson, C. | PROBING AND MODELING LARGE-SCALE AIRLINE NETWORK DISRUPTIONS: 2022 SOUTHWEST AIRLINES SCHEDULING CRISIS | ICAS2024_0782 |
| de Assis da Silva Junior, F. | HELICOPTER ACCIDENTS IN BRAZIL: AN ANALYSIS OF MAINTENANCE FROM THE PERSPECTIVE OF HUMAN FACTORS | ICAS2024_0416 |
| de Boer, S. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| De Bono, E. | ON THE OPTIMIZATION OF (GENERALIZED) IMPEDANCE FOR ACOUSTIC LINERS | ICAS2024_1123 |
| De Breuker, R. | EXPLORING MULTI-FIDELITY AEROELASTIC TAILORING: PROSPECT AND MODEL ASSESSMENT | ICAS2024_0150 |
| De Breuker, R. | SANDWICH COMPOSITES SKIN PANEL OPTIMIZATION FOR THE COMMON RESEARCH MODEL WING | ICAS2024_0479 |
| de Breuker, R. | TOWARDS EFFICIENT ANALYSIS OF POSTBUCKLING IN AIRCRAFT STIFFENED STRUCTURES | ICAS2024_0760 |
| De Crescenzio, F. | CLASSIFICATION OF EXTENDED REALITY BASED HUMAN MACHINE INTERFACES SCENARIOS FOR URBAN AIR MOBILITY | ICAS2024_0326 |
| de Domenico, F. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| De Domenico, F. | CFD-BASED SCOUTING FOR THE DESIGN OF A MULTI-FUEL KEROSENE/HYDROGEN ATMOSPHERIC BURNER | ICAS2024_0432 |
| De Felipe, P. | HYDROGEN AIRLINER TANK OPTIMISATION | ICAS2024_0515 |
| De Finis, R. | STRUCTURAL HEALTH MONITORING OF CFRP DURING FATIGUE LOAD VIA THE ASSESSMENT OF CRACK DENSITY BY MEANS OF THERMOGRAPHY | ICAS2024_1135 |
| De Gaspari, A. | MULTI-OBJECTIVE DESIGN OPTIMIZATION OF A MORPHING AILERON FOR A HYBRID ELECTRIC REGIONAL AIRCRAFT | ICAS2024_0385 |
| de Graaf, S. | PROJECTION OF KEY POWERTRAIN COMPONENT FIGURES OF MERIT FOR OVERALL ASSESSMENT OF ELECTRIC FLIGHT SCENARIOS | ICAS2024_1054 |
| de Lima, D.M.C. | VALIDATING ASSUMPTIONS ABOUT PILOT RECOGNITION: A PCM-BASED APPROACH FOR AIRCRAFT CERTIFICATION SAFETY ASSESSMENT PROCESS | ICAS2024_0089 |
| de Lima, D.M.C. | DECODING AN IN-FLIGHT REFUELING INCIDENT: AVIATION COMPLEXITY THROUGH STAMP/CAST AND ACCIMAP METHODS | ICAS2024_0106 |
| De Luca, S. | A SUPPORTING FRAMEWORK FOR AIRCRAFT MRO OPERATIONS. CAPACITY PLANNING, TASKS TRACEABILITY AND DISEMBARKED ITEMS TRACKING | ICAS2024_0100 |
| De Marco, A. | A COST-EFFICIENT PREDICTIVE METHOD FOR AERODYNAMIC PERFORMANCE DEGRADATION OF HORIZONTAL TAIL UNDER ICING CONDITIONS | ICAS2024_0415 |
| De Marco, A. | STRUT-BRACED WING INDUCED DRAG MODELING FOR REGIONAL TURBOPROP AIRCRAFT DESIGN | ICAS2024_0462 |
| De Martin, A. | THE JOURNEY TOWARDS CONDITION-BASED MAINTENANCE: A FRAMEWORK FOR THE HORIZONTAL TAIL ACTUATOR OF AN ADVANCED JET TRAINER AIRCRAFT | ICAS2024_0198 |
| De Martin, A. | COMPARATIVE ANALYSIS OF MACHINE LEARNING ALGORITHMS FOR HEAT EXCHANGERS DIAGNOSIS IN ELECTRIFIED AIRCRAFT | ICAS2024_0701 |
| De Paola, E. | ENSURING THE NEXT GENERATION GREEN AIRCRAFT’ SUSTAINABILITY FROM THE DESIGN PHASE VIA A LIFE-CYCLE COST ANALYSIS | ICAS2024_0350 |
| De Rosa, M. | AERODYNAMICS AND AEROACOUSTIC ANALYSIS OF A SUPERSONIC SLENDER-BODY GEOMETRY | ICAS2024_0309 |
| De Rosa, S. | DESIGN OF HYDROGEN STORAGE SYSTEMS IN NEW-GENERATION REGIONAL AIRCRAFT | ICAS2024_0858 |
| De Rosa, S. | ACTIVE CONTROL DAMPING WITH THE USE OF VOICE COIL ACTUATORS | ICAS2024_1106 |
| De Rosa, S. | ON THE OPTIMIZATION OF (GENERALIZED) IMPEDANCE FOR ACOUSTIC LINERS | ICAS2024_1123 |
| de Rosa Jacinto, M. | AEROACOUSTICS INVESTIGATION OF PROPELLER LEADING EDGE TUBERCLES APPLIED TO ADVANCED AIR MOBILITY | ICAS2024_0411 |
| de Saqui-Sannes, P. | MODEL-BASED APPROACH FOR HYDROGEN PRELIMINARY AIRCRAFT DESIGN CONSIDERING SAFETY AND OPERABILITY | ICAS2024_0095 |
| de Souza Rehder, I. | A SYSTEMATIC REVIEW OF HUMAN FACTORS AND AI INFLUENCING OPERATOR PERFORMANCE IN MUM-T ENVIRONMENTS | ICAS2024_0132 |
| De Stefano Fumo, M. | IMPACT TOLERANCE OF CERAMIC MATRIX COMPOSITES FOR AEROSPACE APPLICATIONS | ICAS2024_1111 |
| de Vries, R. | AERODYNAMIC PERFORMANCE AND INTERACTION EFFECTS OF AN OVER-THE-WING DISTRIBUTED-PROPELLER SYSTEM IN CRUISE CONDITIONS | ICAS2024_0632 |
| de Vries, R. | BATTERY PERFORMANCE METRICS FOR LARGE ELECTRIC PASSENGER AIRCRAFT | ICAS2024_0636 |
| de Wit, A.J. | ELECTROMAGNETIC INDUCTION HEATING OF TP-CFRP LAMINATES: FEM MODELLING AND VALIDATION | ICAS2024_0032 |
| de Wit, D. | NOVEL TEST RIG TO DEMONSTRATE A MULTI FUNCTIONAL FLAP MECHANISM OFFERING A 2ND DEGREE OF FREEDOM | ICAS2024_0299 |
| Dechamps, P. | FAST TRANSONIC CORRECTIONS FOR PANEL METHODS USING VISCOUS-INVISCID INTERACTION | ICAS2024_0162 |
| Decroix, J. | REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS | ICAS2024_1172 |
| Defoort, S. | INTEGRATING CRYOGENIC TANKS MODEL IN HYDROGEN AIRCRAFT DESIGN FOR PARAMETRIC PERFORMANCE ANALYSIS | ICAS2024_0439 |
| Defoort, S. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Degroote, J. | DESIGN OF MEASUREMENT SETUP FOR HIGH-ALTITUDE IN-FLIGHT EXPERIMENTS ON DU89-134/14 AIRFOIL AT LOW REYNOLDS NUMBER | ICAS2024_0757 |
| Deiler, C. | FLIGHT TEST RESULTS FOR PERFORMANCE-BASED ICE DETECTION | ICAS2024_0046 |
| Deiler, C. | SENS4ICE EU PROJECT HYBRID ICE DETECTION ARCHITECTURES DEMONSTRATION RESULTS | ICAS2024_0178 |
| Del Gatto, D. | DESIGN SPACE EXPLORATION OF NEXT-GENERATION SUPERSONIC BUSINESS JET ENGINE WITH A FOCUS ON LANDING AND TAKE-OFF (LTO) NOISE | ICAS2024_1147 |
| Del Priore, E. | IMPROVING SHAPE SENSING OF AERONAUTICAL STRUCTURES WITH STRAIN PRE-EXTRAPOLATION AND SENSOR PLACEMENT OPTIMIZATION | ICAS2024_0654 |
| DeLaurentis, D. | FROM ONTOLOGY TO SYSTEM ARCHITECTURE: AN MBSE APPROACH TOWARD THE REALIZATION OF URBAN AIR MOBILITY | ICAS2024_0554 |
| DeLaurentis, D.A. | EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS | ICAS2024_0464 |
| DeLaurentis, D.A. | TRAJECTORY OPTIMIZATION OF EVTOL VEHICLES FOR URBAN AIR MOBILITY USING INDIRECT METHODS | ICAS2024_0778 |
| Delbecq, S. | EVALUATION OF ASWING FOR OVERALL AIRCRAFT DESIGN OF UNCONVENTIONAL CONFIGURATIONS. APPLICATION TO JOINED WINGS WITH FOLDING WINGTIPS | ICAS2024_0254 |
| Delbecq, S. | INCREMENTAL TRADE-OFF STUDY OF A HYDROGEN FUEL CELL-BASED PROPULSION SYSTEM USING MDAO TECHNIQUES | ICAS2024_0301 |
| Delbecq, S. | AN EMPIRICAL AND CUSTOMISABLE FLEET RENEWAL MODEL FOR PROSPECTIVE SCENARIOS USING OPEN-ACCESS DATA | ICAS2024_0367 |
| Delbecq, S. | A COMPREHENSIVE METHODOLOGY FOR PERFORMING PROSPECTIVE LIFE CYCLE ASSESSMENTS OF FUTURE AIR TRANSPORT SCENARIOS | ICAS2024_0377 |
| Delgado Guevara, H.S. | DEVELOPMENT OF UAVS/DRONES EQUIPPED WITH THERMAL SENSORS FOR THE SEARCH OF INDIVIDUALS LOST UNDER RUBBLE DUE TO EARTHQUAKE COLLAPSES OR ANY EVENTUALITY REQUIRING SUCH CAPABILITIES | ICAS2024_1093 |
| Delgado-Gutierrez, A. | PARAMETERISATION OF NONLINEAR AEROELASTIC REDUCED ORDER MODELS WITH AERODYNAMIC AND STRUCTURAL NONLINEARITY | ICAS2024_0954 |
| Della Barba, F. | EFFICIENT SHAPE OPTIMIZATION IN AERONAUTICS: INTEGRATING PARAMETRIC CAD AND MESH MORPHING FOR ENHANCED AERODYNAMIC PERFORMANCE | ICAS2024_0824 |
| Della Vecchia, P. | WIND-TUNNEL TESTS OF INNOVATIVE TAILPLANE CONFIGURATIONS | ICAS2024_0370 |
| Della Vecchia, P. | MULTIDISCIPLINARY PRELIMINARY DESIGN PROCESS OF HYBRID-ELECTRIC SEAPLANE | ICAS2024_0470 |
| Della Vecchia, P. | A MODEL BASED SYSTEM ENGINEERING APPROACH TOWARDS AIRCRAFT DIGITAL CERTIFICATION | ICAS2024_0603 |
| Della Vecchia, P. | STRUCTURAL DESIGN OF NEXT-GENERATION REGIONAL GREEN AIRCRAFT | ICAS2024_1035 |
| Dell’Amico, A. | DESIGNING A HARDWARE-IN-THE-LOOP SIMULATION TEST BED FOR AIRCRAFT ENERGY MANAGEMENT APPLICATIONS | ICAS2024_0270 |
| Delprete, C. | HYDROGEN STORAGE SYSTEM DESIGN: CASE STUDIES FOR AIRBORNE APPLICATION | ICAS2024_0590 |
| Delprete, C. | AUTOMATIC SYSTEM REQUIREMENTS VERIFICATION FOR THE MBSE-ORIENTED AIRCRAFT DESIGN PROCESS | ICAS2024_0860 |
| Delprete, C. | FUEL-BASED THERMAL MANAGEMENT SYSTEM ARCHITECTURES AND TANK TEMPERATURE EVOLUTION MODELS FOR AVIATION | ICAS2024_0943 |
| Delsol, E. | A DIGITAL METHOD FOR THE COMPENSATED MOLD DESIGN OF COMPOSITE PARTS | ICAS2024_0487 |
| Deng, L. | RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS | ICAS2024_0550 |
| Deng, L.D. | INVESTIGATION ON AERODYNAMIC DESIGN OF VTOL AIRCRAFT PROPELLER | ICAS2024_0643 |
| Deng, S. | A NUMERICAL VIRTUAL FLIGHT PLATFORM DEVELOPMENT AND ITS APPLICATION ON HIGH MANEUVERABILITY FLIGHT VEHICLES | ICAS2024_0035 |
| Deng, S. | NUMERICAL AND THEORETICAL INVESTIGATION OF HELICOPTER DITCHING WITH VARIOUS INITIAL VELOCITY AND PITCHING ANGLE | ICAS2024_0216 |
| Deng, W.-J. | EXPERIMENTAL AND NUMERICAL INVESTIGATION ON SEPARATION CHARACTERISTICS OF SERPENTINE CONVERGENT-DIVERGENT NOZZLE | ICAS2024_0920 |
| Deng, Y. | OPTIMIZING FLEET ASSIGNMENT DECISIONS FOR REGIONAL AIRLINES WITH HYBRID ELECTRIC AIRCRAFT UPTAKE | ICAS2024_0781 |
| Deng, Y.-T. | EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN | ICAS2024_0962 |
| Dessemond, L. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Devenport, W.J. | THE BEVERLI HILL EXPERIMENTS FOR SMOOTH-BODY TURBULENT FLOW SEPARATION - RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS | ICAS2024_1219 |
| Dhouib, H. | AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS | ICAS2024_1139 |
| Di Benedetto, S. | PROPULSIVE CFD ANALYSIS OF THE SCRAMJET HYPERSONIC EXPERIMENTAL VEHICLE | ICAS2024_0255 |
| Di Benedetto, S. | LAUNCH SYSTEM ASSESSMENT OF AN EXPERIMENTAL HYPERSONIC SCRAMJET VEHICLE | ICAS2024_0363 |
| Di Bitonto, S. | HYBRID AIR DATA SYSTEM ARCHITECTURE: FROM DESIGN TO FLIGHT TEST VERIFICATION | ICAS2024_0056 |
| Di Cicca, G.M. | NUMERICAL STUDY OF THE FLOWFIELD IN A DIFFERENTIALLY-THROTTLED LINEAR AEROSPIKE | ICAS2024_0944 |
| Di Cicca, G.M. | GENETIC ALGORITHM OPTIMIZATION OF AN OPPOSITION CONTROL STRATEGY IN A FULLY TURBULENT CHANNEL FLOW | ICAS2024_1208 |
| Di Donfrancesco, F. | HYBRID AIR DATA SYSTEM ARCHITECTURE: FROM DESIGN TO FLIGHT TEST VERIFICATION | ICAS2024_0056 |
| Di Fede, F. | FUEL-BASED THERMAL MANAGEMENT SYSTEM ARCHITECTURES AND TANK TEMPERATURE EVOLUTION MODELS FOR AVIATION | ICAS2024_0943 |
| di Giuseppe, R. | INCREMENTAL TRADE-OFF STUDY OF A HYDROGEN FUEL CELL-BASED PROPULSION SYSTEM USING MDAO TECHNIQUES | ICAS2024_0301 |
| di Mare, F. | DESIGN APPROACH FOR HYBRID ELECTRIC PROPULSION CONCEPTS OF MID-RANGE AIRCRAFT INCLUDING SUSTAINABLE AVIATION FUELS | ICAS2024_1069 |
| Di Marzo, M.A.D. | NONLINEAR BEHAVIOR IN AIRCRAFT FUEL GAUGE READINGS: AN EXPLORING ANALYSIS | ICAS2024_1187 |
| Di Mauro, G. | MULTIPHYSICS MODELING FOR SAFE BATTERIES USING LS-DYNA | ICAS2024_0837 |
| di Mauro, G. | PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS | ICAS2024_1205 |
| Di Nuzzo, P.E. | ENGINEERING-BASED TOOL FOR THREE-DIMENSIONAL ESTIMATIONS OF RE-ENTRY VEHICLES AEROTHERMODYNAMICS | ICAS2024_0859 |
| Di Pasquale, D. | COMPUTATIONAL ANALYSIS ON THE EFFECTS OF LEADING EDGE TUBERCLES ON THE PERFORMANCE OF ROTATING PROPELLER | ICAS2024_0581 |
| Di Rito, G. | PRELIMINARY DESIGN OF POWER CONTROL STRATEGIES FOR THE HYBRID-ELECTRIC PROPULSION SYSTEM OF A LIGHTWEIGHT FIXED-WING UAV | ICAS2024_1050 |
| Dias, P.M. | APPLICATION OF CLUSTERING TECHNIQUES IN OPTIMISATION-BASED FLIGHT CONTROL SYSTEM CLEARANCE | ICAS2024_0044 |
| Dias, T. | SLEEPINESS IN BRAZILIAN AVIATION: A PROBLEM-SOLVING APPROACH | ICAS2024_0027 |
| Diaz, M.A.R. | INSTRUMENTATION OF A SUBESCALE GROUND EFFECT VEHICLE, VOLITAN, TO MEASURE FLIGHT PROPULSION EFFICIENCY | ICAS2024_1125 |
| Diehl, B. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Diepolder, J. | INTEGRATING POST-OPTIMAL SENSITIVITIES INTO SUPERVISED TRAINING OF NEURAL NETWORKS | ICAS2024_0601 |
| Dijoud, D. | SAFRAN PROPULSION STRATEGY AND ROADMAP FOR FUTURE SUSTAINABLE AVIATION | ICAS2024_1308 |
| Dikmen, C.-S. | NUMERICAL INVESTIGATION OF HYPERSONIC FLOWS | ICAS2024_0907 |
| Dillinger, J.K.S. | SANDWICH COMPOSITES SKIN PANEL OPTIMIZATION FOR THE COMMON RESEARCH MODEL WING | ICAS2024_0479 |
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| Diskin, A. | SURFACE QUALITY CHALLENGE FOR TI-6AL-4V ADDITIVE MANUFACTURED TOPOLOGIC OPTIMIZED LIGHTWEIGHT STRUCTURE | ICAS2024_0025 |
| do Nascimento Monteiro, F. | EXPERIMENTAL MEASUREMENTS OF SLIPSTREAM DEFORMATION FOR AN INSTALLED DISTRIBUTED PROPELLER CONFIGURATION. | ICAS2024_0264 |
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| do Prado, A.P. | SANDWICH COMPOSITES SKIN PANEL OPTIMIZATION FOR THE COMMON RESEARCH MODEL WING | ICAS2024_0479 |
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| Du, C. | HYDRODYNAMIC ANALYSIS OF STATIC WATER IMPACT ON WEDGE-SHAPED HULL WATERTIGHT TEST SPECIMEN THROUGH NUMERICAL ANALYSIS | ICAS2024_0904 |
| Du, S. | AN UNCERTAINTY MULTIDISCIPLINARY PROPAGATION ANALYSIS METHOD FOR CORRELATED HIGH-DIMENSIONAL DATA IN AIRCRAFT DESIGN | ICAS2024_0696 |
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| Du, Y.-Q. | EXPLORATION OF EFFICIENT HYPERPARAMETERS ADAPTION OF SUPPORT VECTOR REGRESSION FOR AERODYNAMIC DESIGN | ICAS2024_0625 |
| Duan, F. | RESEARCH ON AERODYNAMIC PERFORMANCE OF OVERSIZE MODULAR PARAFOIL IN RANDOM WIND FIELD | ICAS2024_0952 |
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| Dufour, J.-E. | MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE SCALE | ICAS2024_0290 |
| Duivenvoorden, R.R. | EXPERIMENTAL MEASUREMENTS OF SLIPSTREAM DEFORMATION FOR AN INSTALLED DISTRIBUTED PROPELLER CONFIGURATION. | ICAS2024_0264 |
| Dumont, A. | GRADIENT-BASED OPTIMIZATION OF AN AXIAL COMPRESSOR UNDER INLET DISTORTION USING BODY-FORCE MODELING | ICAS2024_0726 |
| Durand, M. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF NOISE GENERATION IN HYDROGEN AND METHANE-HYDROGEN LAMINAR FLAMES | ICAS2024_1129 |
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| Dziugiel, B. | ENHANCING PUBLIC GOOD MISSIONS AND DISASTER RESPONSE WITH ADVANCED AERIAL TECHNOLOGY: OPPORTUNITIES AND CHALLENGES | ICAS2024_1259 |
| Döll, C. | SCALED FLIGHT TESTING FOR EVALUATING DISTRIBUTED ELECTRIC PROPULSION | ICAS2024_0267 |
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| D’Alessandro, D.M. | COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A DIRECT AIR CAPTURE FILTER SYSTEM | ICAS2024_0463 |
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| Emmerson, B. | ON THE CHOICE OF TURBULENCE MODEL FOR THE SIMULATION OF AIRFOILS AT REYNOLDS NUMBER BELOW 200,000 | ICAS2024_0327 |
| Enea, G. | COMPARING CONVECTIVE WEATHER IMPACTS ON AIR TRAFFIC MANAGEMENT OPERATIONS IN UNITED STATES, CANADA & EUROPE | ICAS2024_0137 |
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| Eriksson, C. | DESIGN AND VISUALIZATION OF A KNOWLEDGE-BASED AIRCRAFT CABIN IN VIRTUAL REALITY | ICAS2024_0505 |
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| Fadda, T. | DESIGN AND DEVELOPMENT OF THE VISUAL AND AUDITORY LAYER FOR DIFFERENT CABIN/COCKPIT LAYOUT | ICAS2024_0799 |
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| Falissard, F. | SIMULATION OF AN INSTALLED PROPELLER BY MEANS OF STEADY AND UNSTEADY BODY-FORCE MODELING | ICAS2024_0134 |
| Fallucca, R. | EXPERIMENTAL RESULTS OF ANTENNA PLACEMENT TEST ON A CARBON-FIBER SCALE REPLICA OF THE S55X SEAPLANE | ICAS2024_0504 |
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| Farcy, D. | IDENTIFICATION METHOD OF LONGITUDINAL COEFFICIENTS BASED ON THE NUMERICAL STUDY OF THE FLOW TOPOLOGY AROUND THE SACCON GEOMETRY | ICAS2024_0506 |
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| Feldmann, R. | ACTIVE CONTROL DAMPING WITH THE USE OF VOICE COIL ACTUATORS | ICAS2024_1106 |
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| Feng, W.-Z. | STUDY OF AEROELASTIC PROBLEM OF RUDDER SYSTEM WITH ELECTRIC ACTUATOR AND STRUCTURAL NONLINEARITIES | ICAS2024_0784 |
| Ferlauto, M. | NUMERICAL STUDY OF THE FLOWFIELD IN A DIFFERENTIALLY-THROTTLED LINEAR AEROSPIKE | ICAS2024_0944 |
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| Fernández, J. | EXPLORING WINGTIP COLUMNAR VORTEX GENERATORS FOR UAV PERFORMANCE ENHANCEMENT | ICAS2024_0219 |
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| Ferrarini, L. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Ferraro, A. | A MODEL PREDICTIVE CONTROL ALGORITHM FOR THE FORMATION CONTROL OF NANOSATELLITES IN LEO ORBIT | ICAS2024_0494 |
| Ferrazzani, M. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
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| Ferreira, L.P.S. | A-BASIS AND B-BASIS BUCKLING ALLOWABLES FOR AN AIRCRAFT COMPOSITE WING | ICAS2024_0322 |
| Ferreira Marques, L.F. | MODELLING ASTEROID TRAJECTORY IN EARTH’S ATMOSPHERE | ICAS2024_0158 |
| Ferretto, D. | COMPARISON OF LIFE CYCLE COST FOR MACH 8 AND MACH 5 HYPERSONIC PASSENGERS AIRCRAFT | ICAS2024_0924 |
| Ferretto, D. | CONCEPTUAL DESIGN METHODOLOGY FOR LOW-SUPERSONIC LH2-POWERED PASSENGERS AIRCRAFT | ICAS2024_0927 |
| Ferretto, D. | ESATTO: THE HOLISTIC FRAMEWORK TO SUPPORT THE DESIGN OF SUSTAINABLE SUPERSONIC AVIATION | ICAS2024_1032 |
| Ferro, C. | PRELIMINARY ANALYSIS OF TEMPERATURE EFFECTS AND MANEUVER-INDUCED DEFORMATIONS ON FBG OPTIC FIBER INTEGRATED SYSTEMS | ICAS2024_0483 |
| Ferstl, S. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Fezans, N. | MEASURING THE ANGLE OF ATTACK – PRACTICAL CONSIDERATIONS FOR THE DEVELOPMENT OF FAULT DETECTION RESIDUALS | ICAS2024_0156 |
| Fezans, N. | FLIGHT MECHANICAL ANALYSIS OF A VERY FLEXIBLE HIGH-ALTITUDE PLATFORM UNDER UNCERTAINTY CONSIDERATIONS | ICAS2024_0310 |
| Fezans, N. | ASSISTED AND AUTOMATED AERIAL REFUELLING – OVERVIEW OF THE CONDUCTED RESEARCH AT THE GERMAN AEROSPACE CENTER (DLR) | ICAS2024_0819 |
| Figat, M. | STUDY ON CONFIGURATIONS OF AIRBORNE LAUNCH SYSTEM FOR DELIVERY OF SMALL PAYLOAD TO LOW EARTH ORBIT | ICAS2024_0355 |
| Filippatos, A. | A PROPOSAL TOWARDS A STEP CHANGE FROM ECO-DRIVEN TO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT COMPONENTS | ICAS2024_0088 |
| Filippi, M. | COUPLED THERMOELASTIC ANALYSIS OF BEAM STRUCTURES USING A REFINED 1D FINITE ELEMENT MODEL | ICAS2024_0854 |
| Filippi, M. | INVESTIGATING THE EFFECT OF DELAMINATION-INDUCED FRICTIONAL CONTACT ON THE DYNAMIC BEHAVIOR OF LAMINATE STRUCTURES | ICAS2024_1108 |
| Finck, T. | A ROADMAP FOR TRANSFORMING TRADITIONAL ATCO TEAMS INTO COLLABORATIVE HUMAN-MACHINE TEAMS | ICAS2024_0985 |
| Fioriti, M. | AUTOMATING THE VERIFICATION OF GEOMETRIC REQUIREMENTS FOR AIRCRAFT FUEL SYSTEMS USING KNOWLEDGE-BASED ENGINEERING | ICAS2024_0148 |
| Fioriti, M. | ENVIRONMENTAL AND ECONOMIC ASSESSMENT OF AN EVTOL AIRCRAFT FLEET FOR URBAN AIR MOBILITY | ICAS2024_0500 |
| Fioriti, M. | COMPARATIVE ANALYSIS OF MACHINE LEARNING ALGORITHMS FOR HEAT EXCHANGERS DIAGNOSIS IN ELECTRIFIED AIRCRAFT | ICAS2024_0701 |
| Fischer, C. | DYNAMIC FREE FLIGHT TESTS WITH A SUB-SCALE AIRPLANE DESIGNED ACCORDING TO THE FROUDE NUMBER | ICAS2024_1100 |
| Fischer, C. | INSTRUMENTATION OF A SUBESCALE GROUND EFFECT VEHICLE, VOLITAN, TO MEASURE FLIGHT PROPULSION EFFICIENCY | ICAS2024_1125 |
| Fischer, F. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Fitzgerald, S. | CHARACTERISING THE ROLE OF FLEET RENEWAL ON THE PATHWAY TO 2050: A EUROPEAN AIRLINE CASE STUDY | ICAS2024_0126 |
| Fitzgerald, S. | EVALUATION AND SIMULATION OF PARALLEL HYBRID ELECTRIC PROPULSION WITH REAL FLIGHT DATA | ICAS2024_0738 |
| Foley, R. | CLEAN AVIATION HIGH VOLTAGE NETWORK AND DEMONSTRATION | ICAS2024_1266 |
| Fong, K. | SAFETY-DRIVEN BASELINING OF HYBRID ELECTRIC AIRCRAFT ELECTRICAL POWER SYSTEM ARCHITECTURES | ICAS2024_1027 |
| Fontanella, A.P. | DETECTION OF DELAMINATIONS IN DAMAGED COMPOSITE PLATES VIA LOCAL DAMAGE RESONANCE APPROACH | ICAS2024_0814 |
| Fornaciari, E. | CORUS-XUAM: TACKLING URBAN AIR MOBILITY AIRSPACE INTEGRATION CHALLENGES | ICAS2024_0347 |
| Forte, M. | ON THE INFLUENCE OF SURFACE ROUGHNESS ON BOUNDARY-LAYER TRANSITION FOR SWEPT WINGS | ICAS2024_0987 |
| Foucault, J.-M. | IDENTIFICATION METHOD OF LONGITUDINAL COEFFICIENTS BASED ON THE NUMERICAL STUDY OF THE FLOW TOPOLOGY AROUND THE SACCON GEOMETRY | ICAS2024_0506 |
| Fouda, M. | AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS | ICAS2024_1139 |
| Fowler, J.G. | DECODING AN IN-FLIGHT REFUELING INCIDENT: AVIATION COMPLEXITY THROUGH STAMP/CAST AND ACCIMAP METHODS | ICAS2024_0106 |
| Franceschini, F. | PRELIMINARY RESULTS FOR AN INSTRUCTION DESIGN PROCEDURE IN AERONAUTICAL MANUFACTURING | ICAS2024_0306 |
| Franco, F. | ACTIVE CONTROL DAMPING WITH THE USE OF VOICE COIL ACTUATORS | ICAS2024_1106 |
| Frediani, A. | FROM THEORY TO FLIGHT: THE BOX-WING CONFIGURATION IMPLICATIONS FOR THE NEXT-GENERATION AIRCRAFT | ICAS2024_0217 |
| Friedrichs, J. | DESIGN APPROACH FOR HYBRID ELECTRIC PROPULSION CONCEPTS OF MID-RANGE AIRCRAFT INCLUDING SUSTAINABLE AVIATION FUELS | ICAS2024_1069 |
| Fronc, K. | THERMAL HISTORY PAINT UNDER HIGH SUBSONIC FLOW | ICAS2024_0316 |
| Fröhler, B. | GLOBAL SENSITIVITY ANALYSIS OF LIQUID HYDROGEN STORAGE DESIGN PARAMETERS FOR OVERALL AIRCRAFT DESIGN | ICAS2024_0092 |
| Fröhler, B.M.H.J. | PERFORMANCE AND ECONOMIC ASSESSMENT OF A WING-INTEGRATED HYBRID LAMINAR FLOW CONTROL SYSTEM | ICAS2024_0097 |
| Fu, B. | SURROGATE-ASSISTED HIERARCHICAL OPTIMIZATION METHOD FOR VARIABLE SWEEP FLIGHT VEHICLE TRAJECTORY | ICAS2024_0825 |
| Fu, G. | RESEARCH ON UNMANNED CLUSTER RECONNECTION DECISION-MAKING METHOD CONSIDERING RESOURCE SUPPLEMENTATION | ICAS2024_0343 |
| Fu, G.C. | A PHASE FIELD BASED DEEP LEARNING APPROACH FOR MECHANICAL PROPERTY PREDICTION OF SINTERED SILVER IN POWER ELECTRONICS | ICAS2024_0351 |
| Fu, J. | VALIDATION OF ENERGY CHARACTERISTICS IN FLIGHT CONTROL SYSTEM BASED ON A MULTIDISCIPLINARY VIRTUAL PLATFORM | ICAS2024_0646 |
| Fu, J. | RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS | ICAS2024_0674 |
| Fu, J. | MODEL-BASED DESIGN OF ACTIVE/ACTIVE ELECTRO-HYDROSTATIC ACTUATION FOR HELICOPTER FLIGHT CONTROLS | ICAS2024_0735 |
| Fu, P. | SURFACE MORPHOLOGY AND MICROSTRUCTURAL FEATURES OF ELECTRON BEAM SURFI-SCULPTED TI-6AL-4V ALLOY | ICAS2024_0262 |
| Fu, Q. | DYNAMICS ANALYSIS AND CONTROL OF A LARGE WINGSPAN FLAPPING-WING VEHICLE | ICAS2024_0621 |
| Fu, S. | CROSSFLOW AND GÖRTLER INSTABILITIES IN HYPERSONIC BOUNDARY LAYERS | ICAS2024_0574 |
| Fu, S. | STABILITY CHARACTERISTICS OF CROSSFLOW MODES IN HYPERSONIC BOUNDARY LAYER WITH EXPANSION CORNER | ICAS2024_0576 |
| Fu, S. | CLASSIFICATION OF COGNITIVE LOAD BASED ON THE PILOT’ VISUAL SCAN PATTERNS | ICAS2024_0955 |
| Fu, Y. | RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS | ICAS2024_0674 |
| Fuchs, M. | INVESTIGATING THE FLEXIBLE HYDROGEN AIRCRAFT SYSTEM INTERFACE DESIGN USING THE XR CO-DESIGN APPROACH | ICAS2024_0358 |
| Fuest, H. | INCREMENTAL NONLINEAR DYNAMIC INVERSION CONTROLLER FOR A FLYING WING OPERATED IN AN AIRBORNE WIND ENERGY SYSTEM | ICAS2024_0713 |
| Fuger, K. | MUTUAL POSITION PLAUSIBILITY CHECKING IN FLYING AD-HOC NETWORKS USING DISTANCE MEASUREMENTS | ICAS2024_0617 |
| Fujii, K. | VALIDATING FLOW-BASED EN ROUTE AMAN COUPLING ESCAPE LIGHT WITH AIRTOP SOFTWARE | ICAS2024_0968 |
| Fung, T.-Y. | FROM ONTOLOGY TO SYSTEM ARCHITECTURE: AN MBSE APPROACH TOWARD THE REALIZATION OF URBAN AIR MOBILITY | ICAS2024_0554 |
| Fureby, C. | EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR | ICAS2024_0518 |
| Furuya, R. | NUMERICAL EVALUATION FOR FAN-NOISE SHIELDING EFFECTS ON AFT-FUSELAGE MOUNTED AND EMBEDDED ENGINES | ICAS2024_0471 |
| Fusaro, R. | COMPARISON OF LIFE CYCLE COST FOR MACH 8 AND MACH 5 HYPERSONIC PASSENGERS AIRCRAFT | ICAS2024_0924 |
| Fusaro, R. | INTEGRATING ECO-EFFICIENT FLIGHT PLANNING IN AIRCRAFT CONCEPTUAL DESIGN: MINIMAL NOX ROUTES FOR HIGH-SPEED AIRCRAFT USING HYDROGEN | ICAS2024_0950 |
| Fusaro, R. | AERODYNAMIC NUMERICAL/EXPERIMENTAL COMPARISON OF A HYPERSONIC TEST VEHICLE IN MORE&LESS PROGRAM | ICAS2024_1026 |
| Fusaro, R. | ESATTO: THE HOLISTIC FRAMEWORK TO SUPPORT THE DESIGN OF SUSTAINABLE SUPERSONIC AVIATION | ICAS2024_1032 |
| Fürst, J. | ABOUT MODELLING OF EMPIRICAL CORRELATIONS WITHIN AERODYNAMIC PROFILES USING HIGHER ORDER ARTIFICIAL NEURAL NETWORKS | ICAS2024_1150 |
| Gadre, R. | EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS | ICAS2024_0464 |
| Gadre, R. | TRAJECTORY OPTIMIZATION OF EVTOL VEHICLES FOR URBAN AIR MOBILITY USING INDIRECT METHODS | ICAS2024_0778 |
| Gagliardi, G.M. | SEMI-ANALYTICAL SENSITIVITY METHODS FOR AEROELASTIC SHAPE OPTIMIZATION | ICAS2024_0666 |
| Gaglio, E. | AERODYNAMIC ANALYSIS OF A FLAP-BASED DEPLOYABLE RE-ENTRY SYSTEM UNDER RAREFIED CONDITIONS | ICAS2024_1201 |
| Galassi, R.M. | ADVANCED MULTIDISCIPLINARY DESIGN OF NEXT-GENERATION GREEN AIRCRAFT | ICAS2024_0486 |
| Galbraith, M. | SYSTEMATIC CFD VERIFICATION - RESULTS FROM THE 2024 HIGH FIDELITY CFD VERIFICATION WORKSHOP | ICAS2024_1220 |
| Galea, M. | A GENETIC ALGORITHM FOR TRAJECTORY GENERATION IN ENGINE-OUT EMERGENCY LANDING SCENARIOS OF COMMERCIAL AIRCRAFT | ICAS2024_0364 |
| Galietti, U. | STIMULATED THERMOGRAPHY AS NON-DESTRUCTIVE TESTING TO ASSESS THE STRUCTURAL INTEGRITY OF AERONAUTICAL COMPONENT IN CFRP | ICAS2024_1076 |
| Galietti, U. | STRUCTURAL HEALTH MONITORING OF CFRP DURING FATIGUE LOAD VIA THE ASSESSMENT OF CRACK DENSITY BY MEANS OF THERMOGRAPHY | ICAS2024_1135 |
| Gallagher, C. | CHARACTERISING THE ROLE OF FLEET RENEWAL ON THE PATHWAY TO 2050: A EUROPEAN AIRLINE CASE STUDY | ICAS2024_0126 |
| Gallagher, C. | EVALUATION AND SIMULATION OF PARALLEL HYBRID ELECTRIC PROPULSION WITH REAL FLIGHT DATA | ICAS2024_0738 |
| Gallina, S. | EXPERIMENTAL RESULTS OF ANTENNA PLACEMENT TEST ON A CARBON-FIBER SCALE REPLICA OF THE S55X SEAPLANE | ICAS2024_0504 |
| Gan, C. | SUSTAINABLE FUELS SAFETY BOUNDARIES DEMARCATION METHOD | ICAS2024_0712 |
| Gan, K. | SPARSE POLYNOMIAL CHAOS-BASED SONIC BOOM UNCERTAINTY QUANTIFICATION AND AERODYNAMIC/SONIC BOOM ROBUST DESIGN OPTIMIZATION UNDER MULTI-PARAMETER UNCERTAINTIES | ICAS2024_0373 |
| Gan, K.Y. | NOVEL GRADIENT-ENHANCED MULTI-FIDELITY SURROGATE MODEL ASSISTED ROBUST MULTIDISCIPLINARY DESIGN OPTIMIZATION OF TAILLESS FLYING WING | ICAS2024_0298 |
| Gan, Y. | SPARSE POLYNOMIAL CHAOS-BASED SONIC BOOM UNCERTAINTY QUANTIFICATION AND AERODYNAMIC/SONIC BOOM ROBUST DESIGN OPTIMIZATION UNDER MULTI-PARAMETER UNCERTAINTIES | ICAS2024_0373 |
| Gangoli Rao, A. | RESULTS FROM THE APPU PROJECT: THE POTENTIAL OF LOW-THRESHOLD HYDROGEN-POWERED BLI PROPULSION | ICAS2024_0179 |
| Gao, C.Q. | ACTIVE-PASSIVE HYBRID CONTROL OF SHOCK BUFFET | ICAS2024_0792 |
| Gao, T. | MULTI-DIMENTIONAL DESIGN AND THERMAL PROTECTION CAPABILITY OF A REGENERATIVE COOLED RBCC VARIABLE-GEOMETRY COMBUSTOR | ICAS2024_1012 |
| Gao, W.C. | EXPERIMENTAL INVESTIGATION AND NUMERICAL ANALYSIS OF THE EFFECT OF TEMPERATURE ON THE MECHANICAL PROPERTIES OF AEROSPACE COMPOSITE-METAL HYBRID JOINTS | ICAS2024_0530 |
| Gao, Z. | DEEP LEARNING BASED FAST PREDICTION OF AERODYNAMIC PARAMETERS FOR DUCTED PROPELLERS | ICAS2024_1011 |
| Gao, Z.-H. | DATA MINING ANALYSIS ON AERODYNAMIC STEALTH DESIGN PRINCIPLES OF AIRFOIL PROFILES | ICAS2024_0448 |
| Gao, Z.H. | FAST PREDICTION OF PRESSURE DISTRIBUTION FOR 3D CONFIGURATION BASED ON LARGE LANGRAGE MODEL | ICAS2024_0679 |
| Garcia, P.J. | STRUCTURED H-INFINITY DESIGN OF PREDICTORS FOR THE MONITORING OF AN AIRCRAFT IN ITS FLIGHT ENVELOPE | ICAS2024_0223 |
| García-Cuevas, L.M. | PERFORMANCE AND ACOUSTIC ANALYSIS OF A DISTRIBUTED ELECTRIC PROPULSION UNMANNED AIRCRAFT | ICAS2024_1009 |
| García-Tíscar, J. | EFFECT OF POPULAR ADDITIVE MANUFACTURING TECHNOLOGIES ON THE PERFORMANCE AND ACOUSTICS OF UAV PROPELLERS | ICAS2024_0896 |
| García-Tíscar, J. | PERFORMANCE AND ACOUSTIC ANALYSIS OF A DISTRIBUTED ELECTRIC PROPULSION UNMANNED AIRCRAFT | ICAS2024_1009 |
| Garg, S. | IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN | ICAS2024_0057 |
| Garg, S. | MDAX : ENHANCEMENTS IN A COLLABORATIVE MDAO WORKFLOW FORMULATION TOOL | ICAS2024_0059 |
| Gargiulo, A. | THE BEVERLI HILL EXPERIMENTS FOR SMOOTH-BODY TURBULENT FLOW SEPARATION - RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS | ICAS2024_1219 |
| Garijo, D. | DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS | ICAS2024_0229 |
| Garkun, A. | SURFACE QUALITY CHALLENGE FOR TI-6AL-4V ADDITIVE MANUFACTURED TOPOLOGIC OPTIMIZED LIGHTWEIGHT STRUCTURE | ICAS2024_0025 |
| Garnier, E. | IDENTIFICATION METHOD OF LONGITUDINAL COEFFICIENTS BASED ON THE NUMERICAL STUDY OF THE FLOW TOPOLOGY AROUND THE SACCON GEOMETRY | ICAS2024_0506 |
| Garofano, A. | REDESIGN OF AN AERONAUTICAL COMPOSITE STIFFENED PANEL WITH THE DOUBLE-DOUBLE DESIGN APPROACH | ICAS2024_0360 |
| Gaspar, A.V. | HELICOPTER ACCIDENTS IN BRAZIL: AN ANALYSIS OF MAINTENANCE FROM THE PERSPECTIVE OF HUMAN FACTORS | ICAS2024_0416 |
| Gaspari, E. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Gatlin, G.M. | NASA TRANSONIC TRUSS-BRACED WING STUDIES | ICAS2024_0108 |
| Gatta, D.M. | PRELIMINARY RESULTS FOR AN INSTRUCTION DESIGN PROCEDURE IN AERONAUTICAL MANUFACTURING | ICAS2024_0306 |
| Gauci, J. | A GENETIC ALGORITHM FOR TRAJECTORY GENERATION IN ENGINE-OUT EMERGENCY LANDING SCENARIOS OF COMMERCIAL AIRCRAFT | ICAS2024_0364 |
| Gaudenzi, P. | CYBER-PHYSICAL SYSTEM IMPLEMENTATION FOR THE AR-ASSISTED AIT OF AEROSPACE COMPONENTS | ICAS2024_0672 |
| Gautier, R. | REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS | ICAS2024_1172 |
| Gauvrit-Ledogar, J. | IMPACT OF HYDROGEN FUEL ON OVERALL DESIGN OF TRANSPORT AIRCRAFT | ICAS2024_0826 |
| Ge, Y. | RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS | ICAS2024_0550 |
| Ge, Z. | AERODYNAMIC OPTIMIZATION OF HIGH-ALTITUDE PROPELLER COMBINED WITH MACHINE LEARNING METHOD | ICAS2024_0342 |
| Gennaretti, M. | A BOUNDARY INTEGRAL EQUATION FORMULATION FOR POTENTIAL COMPRESSIBLE FLOWS AROUND DEFORMABLE BODIES | ICAS2024_0676 |
| Gennaretti, M. | FINITE-STATE AEROELASTIC MODELLING OF MORPHING WING THROUGH UNSTEADY LIFTING-LINE THEORY | ICAS2024_0677 |
| Genster, C. | A CALL TO ACTION TO ENGAGE THE COMMUNITY TO MEET THE CHALLENGES THAT MUST BE TACKLED TO MAKE ELECTRIFIED AIRCRAFT PROPULSION REAL | ICAS2024_0834 |
| Gentile, R. | AUTOMATIC SYSTEM REQUIREMENTS VERIFICATION FOR THE MBSE-ORIENTED AIRCRAFT DESIGN PROCESS | ICAS2024_0860 |
| Geraci, D. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Gerardus, J. | TRAJECTORY OPTIMIZATION OF EVTOL VEHICLES FOR URBAN AIR MOBILITY USING INDIRECT METHODS | ICAS2024_0778 |
| Ghanjaoui, Y. | AN ONTOLOGY-BASED APPROACH FOR THE CO-DEVELOPMENT AND OPTIMIZATION OF AIRCRAFT CABIN DESIGN AND ASSEMBLY ARCHITECTURES | ICAS2024_1152 |
| Ghiasvand, S. | NUMERICAL TOOLS FOR SLOW-GROWTH APPROACHES TO DAMAGE TOLERANT COMPOSITE AERONAUTICAL STRUCTURES | ICAS2024_1146 |
| Giacotto, A. | HOLISTIC AND SCALABLE SMART OPTIMIZATION FRAMEWORK FOR PRESCRIPTIVE MAINTENANCE | ICAS2024_0657 |
| Giannetti, M. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Giannino, S.M. | LOW SPEED AERODYNAMICS OF SIX OPTIMISED UNCONVENTIONAL RE-ENTRY VEHICLE AEROSHAPES | ICAS2024_0864 |
| Giansante, R. | FINITE-STATE AEROELASTIC MODELLING OF MORPHING WING THROUGH UNSTEADY LIFTING-LINE THEORY | ICAS2024_0677 |
| Giargia, F. | CFD STUDY OF AIR SUPPLY SYSTEM FOR COOLING OF A HYDROGEN POWERED UNMANNED SEAPLANE AND REDUCTION OF THE RESULTING DRAG | ICAS2024_0736 |
| Gierszewski, D.M. | ONBOARD TRAJECTORY OPTIMIZATION FOR RADIUS TO FIX TURNS | ICAS2024_0271 |
| Giglio, M. | ON THE DEVELOPMENT OF THE STRUCTURAL DIGITAL TWIN OF AN UNMANNED AERIAL VEHICLE | ICAS2024_0724 |
| Giorgi, A. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Giusti Degaspare, T. | APPLICATION OF A MORE INTEGRATED TOTAL ENERGY CONTROL SYSTEM FOR IMPROVING AIRCRAFT AND ENGINE CONTROL EFFICIENCY | ICAS2024_0891 |
| Gladin, J. | REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS | ICAS2024_1172 |
| Glenis, D. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Glorioso, A. | AERODYNAMICS AND AEROACOUSTIC ANALYSIS OF A SUPERSONIC SLENDER-BODY GEOMETRY | ICAS2024_0309 |
| Glorioso, A. | SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT | ICAS2024_0361 |
| Gluchshenko, O. | ATM CONTROLLER SUPPORT IN CASE OF SPACIOUS SEVERE WEATHER CONSTELLATIONS ILLUSTRATED USING TWO AIRSPACE EXAMPLES | ICAS2024_0061 |
| God, R. | ENABLING AIRWORTHINESS SECURITY BY A HOLISTIC SECURITY ENGINEERING PROCESS AT VARIOUS AIRCRAFT DESIGN LEVELS | ICAS2024_0707 |
| Goes, L.C.S. | DYNAMIC FREE FLIGHT TESTS WITH A SUB-SCALE AIRPLANE DESIGNED ACCORDING TO THE FROUDE NUMBER | ICAS2024_1100 |
| Goes, L.C.S. | INSTRUMENTATION OF A SUBESCALE GROUND EFFECT VEHICLE, VOLITAN, TO MEASURE FLIGHT PROPULSION EFFICIENCY | ICAS2024_1125 |
| Góes, L.C.S. | FLIGHT PATH RECONSTRUCTION OF A FLEXIBLE WING UAV WITH WING MOUNTED VANES | ICAS2024_1176 |
| Goetzendorf-Grabowski, T. | STUDY ON CONFIGURATIONS OF AIRBORNE LAUNCH SYSTEM FOR DELIVERY OF SMALL PAYLOAD TO LOW EARTH ORBIT | ICAS2024_0355 |
| Goetzendorf-Grabowski, T. | RAPID DESIGN OF UNCONVENTIONAL AIRCRAFT USING SOFTWARE TOOLS COUPLED IN OPTIMIZATION LOOP – LESSONS LEARNED | ICAS2024_0496 |
| Golan, O. | SURFACE QUALITY CHALLENGE FOR TI-6AL-4V ADDITIVE MANUFACTURED TOPOLOGIC OPTIMIZED LIGHTWEIGHT STRUCTURE | ICAS2024_0025 |
| Gollnick, V. | MITIGATING THE CLIMATE IMPACT OF AVIATION BY OPERATIONAL MEANS - A COMPARATIVE STUDY FOR DIFFERENT WEATHER SITUATIONS | ICAS2024_0096 |
| Gollnick, V. | A DESIGN APPROACH FOR A MODEL-SCALE VTOL POWERED BY TWO PIVOTING KEROSENE TURBINES | ICAS2024_0151 |
| Gollnick, V. | BUILDING METHODS FOR A COMPOSITE CONSTRUCTED VTOL USING 3D PRINTING TECHNIQUES | ICAS2024_0313 |
| Gollnick, V. | ANALYSIS OF AN ELECTRICAL-POWERED-DUCTED-THRUST VECTORING-FLAP | ICAS2024_0412 |
| Gollnick, V. | MRO FOR VTOLS IN A FUNCTIONAL SEQUENCES SOLUTION SPACE | ICAS2024_0705 |
| Gollnick, V. | DESIGN OF A UAM GROUND INFRASTRUCTURE NETWORK WITH RESPECT TO MAINTENANCE CAPACITY REQUIREMENTS | ICAS2024_0745 |
| Gomes, V. | SLEEPINESS IN BRAZILIAN AVIATION: A PROBLEM-SOLVING APPROACH | ICAS2024_0027 |
| Gomes Araujo, M. | CLASSIFICATION OF EXTENDED REALITY BASED HUMAN MACHINE INTERFACES SCENARIOS FOR URBAN AIR MOBILITY | ICAS2024_0326 |
| Gomez, L.M. | MULTIPHYSICS MODELING FOR SAFE BATTERIES USING LS-DYNA | ICAS2024_0837 |
| Gomez, L.M. | PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS | ICAS2024_1205 |
| Gomez-Escalonilla, J. | DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS | ICAS2024_0229 |
| Gong, C. | SPARSE RECONSTRUCTION OF SURFACE LOADS ON AIRCRAFT USING POD AND RBFNN | ICAS2024_0634 |
| Gong, C. | MULTI-FIDELITY SURROGATE MODELING BASED ON DATA EXTENSION USING POD AND ANN | ICAS2024_0957 |
| Gong, C.L. | A DISTRIBUTED UMDO ARCHITECTURE BASED ON SURROGATE MODELS FOR LAUNCH VEHICLE DESIGN | ICAS2024_0626 |
| Gong, Z. | SPARSE POLYNOMIAL CHAOS-BASED SONIC BOOM UNCERTAINTY QUANTIFICATION AND AERODYNAMIC/SONIC BOOM ROBUST DESIGN OPTIMIZATION UNDER MULTI-PARAMETER UNCERTAINTIES | ICAS2024_0373 |
| Gong, Z.-Y. | NOVEL GRADIENT-ENHANCED MULTI-FIDELITY SURROGATE MODEL ASSISTED ROBUST MULTIDISCIPLINARY DESIGN OPTIMIZATION OF TAILLESS FLYING WING | ICAS2024_0298 |
| Gonzalez Sorribes, A. | STRUCTURED H-INFINITY DESIGN OF PREDICTORS FOR THE MONITORING OF AN AIRCRAFT IN ITS FLIGHT ENVELOPE | ICAS2024_0223 |
| Gonzatto Junior, O.A. | NONLINEAR BEHAVIOR IN AIRCRAFT FUEL GAUGE READINGS: AN EXPLORING ANALYSIS | ICAS2024_1187 |
| Gori, G. | UNCERTAINTY ANALYSIS OF THE AERODYNAMIC PERFORMANCE OF EVTOL PROPELLERS VIA REYNOLDS STRESS TENSOR PERTURBATION | ICAS2024_1197 |
| Gorman, J. | ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD | ICAS2024_1280 |
| Goulos, I. | BASE FLOW CHARACTERISTICS FOR A SUB-SCALE HIGH-SPEED EXHAUST AT OVER-EXPANDED MODE | ICAS2024_0512 |
| Gourinat, Y. | INTEGRATING CRYOGENIC TANKS MODEL IN HYDROGEN AIRCRAFT DESIGN FOR PARAMETRIC PERFORMANCE ANALYSIS | ICAS2024_0439 |
| Gowree, E.R. | ON THE INFLUENCE OF SURFACE ROUGHNESS ON BOUNDARY-LAYER TRANSITION FOR SWEPT WINGS | ICAS2024_0987 |
| Gozzini, G. | ADAPTIVE CONTROL AND MISSION PLANNER DESIGN FOR UAV OPERATIONS WITH BATTERY MANAGEMENT | ICAS2024_1136 |
| Grabe, C. | CFD VALIDATION EXPERIMENTS AT DLR: OVERVIEW AND LESSONS-LEARNED | ICAS2024_1218 |
| Graebert, M. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Graham, C. | CHARACTERIZATION OF EXTERNAL LIQUID HYDROGEN TANK INTERFERENCE DRAG | ICAS2024_0414 |
| Grande, A.M. | MACHINE LEARNING AND NUMERICAL OPTIMIZATION OF BIO-INSPIRED 3D-PRINTABLE SANDWICH CORE CELL | ICAS2024_0307 |
| Grande, A.M. | OPTIMIZATION OF POST-PROCESSING HEAT TREATMENT FOR LPBF MODIFIED 2024 ALUMINIUM ALLOY | ICAS2024_0438 |
| Gravano, F. | AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) | ICAS2024_0575 |
| Gray, A.C. | SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION | ICAS2024_0465 |
| Graziani, S. | SONIC BOOM COMPARATIVE STUDY BETWEEN MACH 4.7 OUTDOOR EXPERIMENTAL TESTS AND NUMERICAL SIMULATIONS | ICAS2024_0882 |
| Grazioso, G. | STRUT-BRACED WING INDUCED DRAG MODELING FOR REGIONAL TURBOPROP AIRCRAFT DESIGN | ICAS2024_0462 |
| Greco, C.S. | NUMERICAL STUDY ON ACTIVE FLOW CONTROL SOLUTIONS FOR HIGH LIFT | ICAS2024_1053 |
| Groh, R.M.J. | ENHANCING THE PERFORMANCE OF SLENDER STRUCTURES WITH GEOMETRIC CONSTRAINTS: A CASE STUDY WITH THE ROORDA FRAME | ICAS2024_0192 |
| Groot Koerkamp, L.H. | FLYING WING CIRCULATION DISTRIBUTIONS, AERODYNAMIC PERFORMANCE AND WAKE ROLL-UP | ICAS2024_1153 |
| Grönstedt, T. | MODELLING HYDROGEN FUEL CELL AIRCRAFT IN SUAVE | ICAS2024_1078 |
| Gu, D. | EFFECT OF LASER PRINTING MODE ON SURFACE TOPOGRAPHY, MICROSTRUCTURE AND CORROSION PROPERTY OF ADDITIVE-MANUFACTURED NITI | ICAS2024_0339 |
| Gu, D.D. | LIGHT WEIGHT DESIGN AND LASER ADDITIVE MANUFACTURING OF METAL BIPOLAR PLATES FOR THE APPLICATION OF AIRCRAFT FUEL CELL | ICAS2024_0964 |
| Gu, H. | CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT: HIGH ASPECT RATIO WINGS AND FLOATING WINGTIPS | ICAS2024_0386 |
| Gu, J. | A DYNAMIC TEST METHODOLOGY FOR DETERMINING THE LONGITUDINAL COMPRESSIVE RESPONSE OF CARBON FIBER COMPOSITE TOWS | ICAS2024_0584 |
| Gu, Y. | RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS | ICAS2024_0550 |
| Gu, Y. | DESIGN OF A BODY FREEDOM FLUTTER FLIGHT MODEL WITH CONVENTIONAL CONFIGURATION | ICAS2024_0565 |
| Guagliardo, D. | NUMERICAL-THEORETICAL EVALUATION OF THE DITCHING OF A HULL WITH DIHEDRAL ANGLES BETWEEN -5 AND 20 DEGREES | ICAS2024_0665 |
| Guan, Z. | DYNAMIC BUCKLING ANALYSIS OF THIN-SHELL COMPOSITE STRUCTURES BASED ON ISOGEOMETRIC ANALYSIS | ICAS2024_0389 |
| Guariniello, C. | FROM ONTOLOGY TO SYSTEM ARCHITECTURE: AN MBSE APPROACH TOWARD THE REALIZATION OF URBAN AIR MOBILITY | ICAS2024_0554 |
| Guenov, M.D. | SET-BASED DESIGN TECHNIQUES FOR EVOLVABILITY EXPLORATION DURING CONCEPTUAL AIRCRAFT DESIGN | ICAS2024_0233 |
| Guerrero, R. | UNITED STATES' AIRCRAFT SUSTAINABILITY RESEARCH & DEVELOPMENT EFFORTS | ICAS2024_1229 |
| Gui, L. | REDESIGN AND MACHINING OF LEADING EDGE OF TRANSONIC COMPRESSOR BLADE IN ROBOTIC GRINDING OPERATION | ICAS2024_0260 |
| Guida, B. | SMART ELECTRIC POWER MANAGEMENT ONBOARD FUTURE AIRCRAFT | ICAS2024_0085 |
| Guida, D. | DESIGN OF A HIGH ENTHALPY HYPERSONIC NOZZLE FOR “GHIBLI” PLASMA WIND TUNNEL | ICAS2024_0894 |
| Guida, M. | COMPUTER VISION ALGORITHMS FOR THE IDENTIFICATION OF DAMAGES ON FULL-SCALE AIRCRAFT COMPONENTS | ICAS2024_0190 |
| Guida, M. | MULTIPHYSICS MODELING FOR SAFE BATTERIES USING LS-DYNA | ICAS2024_0837 |
| Guida, M. | PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS | ICAS2024_1205 |
| Guinard, S. | ON AN EFFICIENT GLOBAL/LOCAL STOCHASTIC METHODOLOGY FOR FAILURE PREDICTION OF AIRCRAFT COMPOSITE STRUCTURES | ICAS2024_0250 |
| Gulizzi, V. | A FORMULATION FOR WING AEROELASTIC ANALYSIS BASED ON THE UNSTEADY VLM AND STRUCTURAL DISCONTINUOUS GALERKIN TECHNIQUE | ICAS2024_1140 |
| Guo, B. | SEPARATION SAFETY ANALYSIS IN VARIABLE LAUNCH CONDITION OF SMALL AIR-LAUNCHED UAVS BASED ON NUMERICAL SIMULATION AND FLIGHT TEST | ICAS2024_0311 |
| Guo, H.-J. | EFFICIENT AEROSTRUCTURAL DESIGN OPTIMIZATION COMBINING GRADIENT-ENHANCED KRIGING WITH COUPLED ADJOINT METHOD | ICAS2024_0651 |
| Guo, T. | CONFIGURATION ANALYSIS OF INTEGRATED THERMAL MANAGEMENT BASED ON THE TURBINE-FAN REFRIGERATION SYSTEM | ICAS2024_0194 |
| Guo, X. | TRANSIENT SIMULATION CALCULATION FOR ELECTRIC THERMAL ANTI-ICING PERFORMANCE OF COMPOSITE WING IN ICING ENVIRONMENT | ICAS2024_0721 |
| Guo, Y. | REFINED PREDICTIONS COMPARED WITH THE PROPULSION AIRFRAME AEROACOUSTICS AND AIRCRAFT SYSTEM NOISE FLIGHT RESEARCH TEST DATA | ICAS2024_0069 |
| Guo, Y. | DYNAMIC BUCKLING ANALYSIS OF THIN-SHELL COMPOSITE STRUCTURES BASED ON ISOGEOMETRIC ANALYSIS | ICAS2024_0389 |
| Guo, Y.-Y. | THE EFFECTS OF INITIAL STRESS ON AERODYNAMIC PERFORMANCE OF FLEXIBLE MEMBRANE-SKELETON WINGS WITH FSI SIMULATION | ICAS2024_0752 |
| Guo, Z. | FLIGHT LOADS RESEARCH OF TWIN VERTICAL TAIL FOR BLENDED WING-BODY AIRCRAFT BASED ON STRAIN GAUGE CAILBRATION | ICAS2024_0072 |
| Guo, Z. | SEPARATION SAFETY ANALYSIS IN VARIABLE LAUNCH CONDITION OF SMALL AIR-LAUNCHED UAVS BASED ON NUMERICAL SIMULATION AND FLIGHT TEST | ICAS2024_0311 |
| Guo, Z. | AERODYNAMIC CHARACTERISTICS RESEARCH OF A DISTRIBUTED PROPULSION AIRCRAFT | ICAS2024_0537 |
| Guo, Z. | ANALYSIS OF STEALTH ENHANCEMENT DESIGN PROCESS AND METHODS FOR UNMANNED AERIAL VEHICLE | ICAS2024_0568 |
| Guo, Z. | ANALYSIS OF BATTERY WEIGHT REQUIREMENTS IN THE DESIGN OF HYBRID ELECTRIC POWERED AIRCRAFT | ICAS2024_0813 |
| Gupta, P. | AN AUTONOMOUS SYSTEM FOR DOCKING AND BATTERY SWAPPING IN UAVS | ICAS2024_1116 |
| Gupta, P. | CONCEPTUAL DESIGN AND SIZING OF A SOLAR POWERED QUAD-ROTOR FIXED WING HYBRID UAV FOR EXPLORATION OVER MARS | ICAS2024_1156 |
| Gupta, U. | EU IMPACT MONITOR PROJECT - OVERVIEW AND APPROACH | ICAS2024_1114 |
| Gårdstam, J. | THE PRODUCTION OF HIGH-PERFORMANCE HEAT EXCHANGERS FOR AEROSPACE APPLICATIONS | ICAS2024_0022 |
| Göing, J. | DESIGN APPROACH FOR HYBRID ELECTRIC PROPULSION CONCEPTS OF MID-RANGE AIRCRAFT INCLUDING SUSTAINABLE AVIATION FUELS | ICAS2024_1069 |
| Görtz, A. | ON THE WATER ENHANCED TURBOFAN CONCEPT: PART B – FLOW PATH AND MASS ASSESSMENT | ICAS2024_0135 |
| Görtz, A. | ON THE WATER ENHANCED TURBOFAN CONCEPT: PART A - THERMODYNAMICS AND OVERALL ENGINE DESIGN | ICAS2024_0199 |
| Görtz, A. | PERFORMANCE ASSESSMENT OF AN ENGINE-INTEGRATED CLOSED-AIR COOLING THERMAL MANAGEMENT SYSTEM IN A NEXT GENERATION FIGHTER CONFIGURATION | ICAS2024_0622 |
| Ha, M.D. | INTEGRATIVE ANALYSIS OF LOW-CYCLE FATIGUE AND CRACK PROPAGATION IN TURBINE BLADES | ICAS2024_0538 |
| Ha, S.K. | A-BASIS AND B-BASIS BUCKLING ALLOWABLES FOR AN AIRCRAFT COMPOSITE WING | ICAS2024_0322 |
| Habing, R. | DUAL-STREAM JET NOISE TEST WITH INTERNAL MIXER DESIGN VARIATIONS FOR LTO NOISE OF SUPERSONIC AIRCRAFT | ICAS2024_0064 |
| Habing, R. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Haglage, J.M. | NASA HYBRID THERMALLY EFFICIENT CORE (HYTEC) PROJECT OVERVIEW | ICAS2024_1245 |
| Haidl, R. | EXPERIMENTAL SETUP FOR THE INVESTIGATION OF WATER SEPARATION IN ANNULAR FLOW WITHIN A CIRCULAR CHANNEL | ICAS2024_0969 |
| Hajdik, H. | SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION | ICAS2024_0465 |
| Hajdik, H.M. | AERODYNAMIC SHAPE OPTIMIZATION OF FILLETED INTERSECTIONS WITH SURFACE MESH DEFORMATION | ICAS2024_0227 |
| Hale, E. | PARAMETERISATION OF NONLINEAR AEROELASTIC REDUCED ORDER MODELS WITH AERODYNAMIC AND STRUCTURAL NONLINEARITY | ICAS2024_0954 |
| Hales, M. | A PERFORMANCE COMPARISON OF HYDROGEN AIRCRAFT CONCEPTS | ICAS2024_0251 |
| Hallerbach, S. | APPLYING MODEL-BASED SYSTEM ENGINEERING AND DEVOPS ON THE IMPLEMENTATION OF AN AI-BASED COLLISION AVOIDANCE SYSTEM | ICAS2024_0869 |
| Hamilton Smith, C.O.L. | HOT-WIRE ANEMOMETRY OF THE BOUNDARY LAYER PRIOR TO A CAVITY IN RESPONSE TO VARIED UPSTREAM GEOMETRY | ICAS2024_0023 |
| Han, C.-X. | STUDY OF AEROELASTIC PROBLEM OF RUDDER SYSTEM WITH ELECTRIC ACTUATOR AND STRUCTURAL NONLINEARITIES | ICAS2024_0784 |
| Han, J. | LONG-WAVE INSTABILITY OF AIRCRAFT WAKE VORTEX UNDER SHEAR CROSSWIND | ICAS2024_0551 |
| Han, J.-H. | ASPECT RATIO AND ADVANCE RATIO EFFECTS ON AERODYNAMIC CHARACTERISTICS OF FLEXIBLE FLAPPING WINGS | ICAS2024_0333 |
| Han, J.-H. | DEVELOPMENT OF A SERVO-DRIVEN FLAPPING-WING AIR VEHICLE WITH FOLDING-WING MECHANISM | ICAS2024_0477 |
| Han, J.-S. | ASPECT RATIO AND ADVANCE RATIO EFFECTS ON AERODYNAMIC CHARACTERISTICS OF FLEXIBLE FLAPPING WINGS | ICAS2024_0333 |
| Han, J.W. | ENHANCED AIRCRAFT TAKEOFF/LANDING SAFETY USING DEEP LEARNING MODEL IN RUNWAY ASSISTANCE SYSTEM | ICAS2024_0786 |
| Han, K. | AERODYNAMIC PERFORMANCE OF BLADELESS DUCTED FAN BASED ON EJECTION EFFECT WITH DIFFERENT DESIGN VARIABLES | ICAS2024_0419 |
| Han, S.-Q. | EFFECTS OF GEOMETRY PARAMETERS ON AERODYNAMIC CHARACTERISTICS OF ROTOR AIRFOIL IN REVERSE FLOW | ICAS2024_0607 |
| Han, S.-Q. | NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF HOVERING ROTOR IN GROUND EFFECT | ICAS2024_0655 |
| Han, Y. | STABLE LOCALIZED CORROSION IN A 7075-T6 ALUMINUM ALLOY FSW JOINT: MECHANISM AND MITIGATION | ICAS2024_0300 |
| Han, Z. | ANALYSIS ON COMPLEX HYPERSONIC FLOW DURING THE REENTRY OF EXPIRED SPACECRAFT | ICAS2024_0644 |
| Han, Z. | BOUNDARY-LAYER SUCTION AND AERODYNAMIC SHAPE OPTIMIZATION FOR HYBRID LAMINAR FLOW CONTROL ON A FIN | ICAS2024_0681 |
| Han, Z. | REVIEW ON NONLINEAR AEROELASTIC ANALYSIS WITH FREEPLAY | ICAS2024_0922 |
| Han, Z.-H. | EFFICIENT MULTI-OBJECTIVE DESIGN OPTIMIZATION OF ROTOR AIRFOILS FOR IMPROVING DYNAMIC STALL CHARACTERISTICS | ICAS2024_0420 |
| Han, Z.-H. | AERODYNAMIC DESIGN OF A SUPERSONIC TRANSPORT CONFIGURATION CONSIDERING AVERAGE LOUDNESS IN THE WHOLE BOOM CARPET | ICAS2024_0597 |
| Han, Z.-H. | EFFECTS OF GEOMETRY PARAMETERS ON AERODYNAMIC CHARACTERISTICS OF ROTOR AIRFOIL IN REVERSE FLOW | ICAS2024_0607 |
| Han, Z.-H. | FAST PARAMETRIC STRUCTURE MODELING FOR VARIETY OF AIRCRAFT CONFIGURATIONS | ICAS2024_0614 |
| Han, Z.-H. | A SEQUENTIAL LOCAL ENUMERATION-BASED IMPROVED LATIN HYPERCUBE SAMPLING METHOD FOR BALLISTIC CONSTRAINT DESIGN SPACE | ICAS2024_0618 |
| Han, Z.-H. | EXPLORATION OF EFFICIENT HYPERPARAMETERS ADAPTION OF SUPPORT VECTOR REGRESSION FOR AERODYNAMIC DESIGN | ICAS2024_0625 |
| Han, Z.-H. | EFFICIENT AEROSTRUCTURAL DESIGN OPTIMIZATION COMBINING GRADIENT-ENHANCED KRIGING WITH COUPLED ADJOINT METHOD | ICAS2024_0651 |
| Han, Z.-H. | NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF HOVERING ROTOR IN GROUND EFFECT | ICAS2024_0655 |
| Han, Z.-H. | RESEARCH ON MULTI-OBJECTIVE AERODYNAMIC/STRUCTURAL DESIGN OPTIMIZATION METHOD FOR LARGE THICKNESS FLATBACK AIRFOILS | ICAS2024_0690 |
| Han, Z.-H. | ON THE INFLUENCE OF BASE FLOW CHARACTERISTICS ON CROSSFLOW INSTABILITY IN SWEPT BOUNDARY LAYERS | ICAS2024_0918 |
| Han, Z.H. | DESIGN OPTIMIZATION OF A WIG CRAFT’S HIGH LIFT DEVICE CONSIDERING GROUND EFFECT | ICAS2024_0572 |
| Hanák, J. | HYBRID MODELING APPROACH FOR OPTIMIZATION BASED CONTROL OF MULTIROTOR UNMANNED AERIAL VEHICLES | ICAS2024_0029 |
| Hanák, J. | MODEL PREDICTIVE CONTROL DRIVEN AERIAL GRASPING WITH SOFT OPERATIONAL CONSTRAINTS | ICAS2024_0879 |
| Hanák, J. | PREDICTIVE CONTROL DRIVEN TACTICAL MANEUVERING | ICAS2024_1044 |
| Handojo, V. | POTENTIAL LIMITS OF LOAD ALLEVIATION IN REDUCING THE STRUCTURAL MASS OF A LONG-RANGE TRANSPORT CONFIGURATION | ICAS2024_0012 |
| Hannappel, J.-P. | EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR | ICAS2024_0518 |
| Harada, A. | FEASIBILITY STUDY ON OPERATIONAL FLIGHT PLANS ADAPTED FOR TRAJECTORY BASED OPERATION | ICAS2024_1177 |
| Harris, K. | X-57 TRACTION POWER AND COMMAND SYSTEMS DEVELOPMENT | ICAS2024_1288 |
| Harrison, R.A. | MEASUREMENT OF WING BENDING IN-FLIGHT FROM A T67 SLINGSBY FIREFLY LIGHT AIRCRAFT | ICAS2024_0140 |
| Hartl, P. | EXPERIMENTAL INVESTIGATION OF THE DLR-F23 CONFIGURATION AT TRANSONIC SPEEDS USING FAST-RESPONSE PRESSURE-SENSITIVE PAINT | ICAS2024_0710 |
| Hasan, Y.J. | FLIGHT MECHANICAL ANALYSIS OF A VERY FLEXIBLE HIGH-ALTITUDE PLATFORM UNDER UNCERTAINTY CONSIDERATIONS | ICAS2024_0310 |
| Hashioka, T. | TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2024_1215 |
| Hassan , J. | NUMERICAL STUDY OF THE FLOWFIELD IN A DIFFERENTIALLY-THROTTLED LINEAR AEROSPIKE | ICAS2024_0944 |
| Haupt, M. | GUST LOAD ALLEVIATION IN A SCALED UAV DEMONSTRATOR | ICAS2024_0580 |
| Hayashi, Y. | IN-FLIGHT MEASUREMENT OF WING SURFACE PRESSURE DISTRIBUTION ON A FIXED-WING UAV AND ITS APPLICATION TO FLIGHT CONTROL | ICAS2024_0980 |
| Hayböck, S. | IMPLEMENTATION OF ACTIVE FLOW CONTROL ON A SHORT-INLET UHBR ENGINE NACELLE | ICAS2024_0870 |
| He, H.-L. | PRESERVING HUMAN EXPERTISE: EXPLORING MIXED REALITY TRAJECTORY PLANNING FOR ROBOTIC BELT GRINDING | ICAS2024_0378 |
| He, L. | A HIGH-PRECESION PSEUDO ARC-LENGTH METHOD WITH POSITIVE VALUE PRESERVATION PROPERTIES BASED ON TV SPLITTING | ICAS2024_0694 |
| He, L. | FUZZING ON TARGET DETECTION SYSTEM OF UNMANNED AERIAL VEHICLE | ICAS2024_0794 |
| He, S. | CONVEX PROGRAMMING APPROACH OF ROBUST POWERED DESCENT GUIDANCE THROUGH DYNAMIC TUBE MPC | ICAS2024_0839 |
| He, Y. | EFFECTS OF SHOCK IMPINGEMENT LOCATION ON PANEL AEROELASTIC STABILITY IN MACH REFLECTION | ICAS2024_0066 |
| He, Y. | A BRIEF REVIEW OF PANEL AEROELASTICITY WITH SHOCK INTERACTION | ICAS2024_0067 |
| He, Y. | A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION | ICAS2024_0314 |
| Healy, F. | CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT: HIGH ASPECT RATIO WINGS AND FLOATING WINGTIPS | ICAS2024_0386 |
| Hechelmann, A. | APPLICATION OF SYSML IN THE DEVELOPMENT OF AIRCRAFT CABIN HEALTH MANAGEMENT | ICAS2024_0318 |
| Heddrich, M.P. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Hegde, A. | HARDWARE-IN-THE-LOOP SIMULATION FRAMEWORK FOR THE EVALUATION OF AUTONOMOUS FLIGHT FUNCTIONS | ICAS2024_0897 |
| Heidebrecht, A. | RESULTS FROM THE APPU PROJECT: THE POTENTIAL OF LOW-THRESHOLD HYDROGEN-POWERED BLI PROPULSION | ICAS2024_0179 |
| Heidebrecht, A. | DESIGN OPTIMISATION OF A BOUNDARY LAYER INGESTION PROPULSOR FOR A MULTI-FUEL HYDROGEN AIRCRAFT | ICAS2024_1060 |
| Heimbs, S. | GUST LOAD ALLEVIATION IN A SCALED UAV DEMONSTRATOR | ICAS2024_0580 |
| Hellbrück, S. | CONCEPTUAL AIRCRAFT DESIGN OF A RESEARCH BASELINE WITH DIRECT LIQUID HYDROGEN COMBUSTION | ICAS2024_0503 |
| Hellgren, J. | AIRPORT CHARGING SYSTEM DESIGNS AND POWER MANAGEMENT FOR MEGAWATT-LEVEL CHARGING OF BATTERY-ELECTRIC AIRCRAFT | ICAS2024_0442 |
| Hengy, S. | SONIC BOOM COMPARATIVE STUDY BETWEEN MACH 4.7 OUTDOOR EXPERIMENTAL TESTS AND NUMERICAL SIMULATIONS | ICAS2024_0882 |
| Henneberg, A. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Hepperle, M. | CLIMATE IMPACT AND ECONOMIC ASSESSMENT OF LIQUID HYDROGEN AND SYNTHETIC KEROSENE LONG-RANGE AIRCRAFT CONCEPTS | ICAS2024_0399 |
| Herculano, A. | SLEEPINESS IN BRAZILIAN AVIATION: A PROBLEM-SOLVING APPROACH | ICAS2024_0027 |
| Herrera Velasco, J.A. | DEVELOPMENT OF UAVS/DRONES EQUIPPED WITH THERMAL SENSORS FOR THE SEARCH OF INDIVIDUALS LOST UNDER RUBBLE DUE TO EARTHQUAKE COLLAPSES OR ANY EVENTUALITY REQUIRING SUCH CAPABILITIES | ICAS2024_1093 |
| Herrgen, A. | VALIDATION OF MULTIPHASE FLOW SIMULATIONS BY EXPERIMENTAL MEASUREMENTS IN A CHANNEL FLOW | ICAS2024_0176 |
| Herrmann, P. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Herrmann, P. | MIXED FLIGHT CONTROL LAYOUT FOR ULTRALIGHT GENERAL AVIATION AIRCRAFT | ICAS2024_0517 |
| Herrmann, R. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Herwig, A. | GUST LOAD ALLEVIATION IN A SCALED UAV DEMONSTRATOR | ICAS2024_0580 |
| Herzig, J. | INVESTIGATING THE FLEXIBLE HYDROGEN AIRCRAFT SYSTEM INTERFACE DESIGN USING THE XR CO-DESIGN APPROACH | ICAS2024_0358 |
| Hesse, C. | EXPLORATION AND EVALUATION OF KNOWLEDGE-BASED ENGINEERING APPROACH FOR LIQUID HYDROGEN TANK INTEGRATION IN EXISTING FUSELAGE | ICAS2024_0488 |
| Hesse, C. | CONCEPTUAL AIRCRAFT DESIGN OF A RESEARCH BASELINE WITH DIRECT LIQUID HYDROGEN COMBUSTION | ICAS2024_0503 |
| Higuchi, R. | EFFICIENT THERMOMECHANICAL SIMULATION FOR METALLIC LATTICE STRUCTURES FABRICATED BY ADDITIVE MANUFACTURING | ICAS2024_0908 |
| Hildebrand, N. | TRANSITION MODELING IN SUPPORT OF CFD VISION 2030 - HIGHLIGHTS OF RECENT EFFORTS AT THE NASA LANGLEY RESEARCH CENTER | ICAS2024_0081 |
| Hillebrecht, A. | APPLICATIONS AND CHALLENGES FOR AIRBORNE AD-HOC COMMUNICATION NETWORKS IN ORP AIRSPACES USING THE L-BAND | ICAS2024_1038 |
| Hintze, H. | ENABLING AIRWORTHINESS SECURITY BY A HOLISTIC SECURITY ENGINEERING PROCESS AT VARIOUS AIRCRAFT DESIGN LEVELS | ICAS2024_0707 |
| Hoang, A.T. | DESIGN OF A WIND TUNNEL MODEL FOR A REUSABLE LAUNCH VEHICLE DURING ITS LANDING BURN | ICAS2024_0188 |
| Hoang, N.M. | INTEGRATIVE ANALYSIS OF LOW-CYCLE FATIGUE AND CRACK PROPAGATION IN TURBINE BLADES | ICAS2024_0538 |
| Hoeijmakers, H.W.M. | FLYING WING CIRCULATION DISTRIBUTIONS, AERODYNAMIC PERFORMANCE AND WAKE ROLL-UP | ICAS2024_1153 |
| Hoemann, E. | APPLYING MODEL-BASED SYSTEM ENGINEERING AND DEVOPS ON THE IMPLEMENTATION OF AN AI-BASED COLLISION AVOIDANCE SYSTEM | ICAS2024_0869 |
| Hoffmann, M. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Hofsäß, H. | DYNAMIC RESPONSE MONITORING OF FLIGHT CONTROL WITH INCREMENTAL NONLINEAR DYNAMIC INVERSION | ICAS2024_0719 |
| Hokamoto, S. | STUDY ON CONTROL PERFORMANCE OF A NEW TYPE OF TILT-ROTOR AIRCRAFT | ICAS2024_0548 |
| Hollmann, J. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Holtz, E. | A CALL TO ACTION TO ENGAGE THE COMMUNITY TO MEET THE CHALLENGES THAT MUST BE TACKLED TO MAKE ELECTRIFIED AIRCRAFT PROPULSION REAL | ICAS2024_0834 |
| Holzapfel, F. | ONBOARD TRAJECTORY OPTIMIZATION FOR RADIUS TO FIX TURNS | ICAS2024_0271 |
| Holzapfel, F. | DYNAMIC RESPONSE MONITORING OF FLIGHT CONTROL WITH INCREMENTAL NONLINEAR DYNAMIC INVERSION | ICAS2024_0719 |
| Homola, J. | ENHANCING PUBLIC GOOD MISSIONS AND DISASTER RESPONSE WITH ADVANCED AERIAL TECHNOLOGY: OPPORTUNITIES AND CHALLENGES | ICAS2024_1259 |
| Homola, J. | NASA RESEARCH TO EXPAND UAS OPERATIONS FOR DISASTER RESPONSE | ICAS2024_1281 |
| Hood, K. | BOEING CONTRIBUTIONS TO THE CRM-HL ECOSYSTEM | ICAS2024_1216 |
| Hoogreef, M. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Hoogreef, M. | RESULTS FROM THE APPU PROJECT: THE POTENTIAL OF LOW-THRESHOLD HYDROGEN-POWERED BLI PROPULSION | ICAS2024_0179 |
| Hoogreef, M. | SCALED FLIGHT TESTING FOR EVALUATING DISTRIBUTED ELECTRIC PROPULSION | ICAS2024_0267 |
| Hornung, M. | RETROFITTING A JET DRIVEN UAV TO FORM A MULTI-PURPOSE TEST PLATFORM | ICAS2024_0036 |
| Hornung, M. | GEOMETRIC OPTIMIZATION OF HYDROGEN AIRCRAFT FUSELAGES IN PRELIMINARY DESIGN | ICAS2024_0103 |
| Hornung, M. | MODELLING AND INITIAL ASSESSMENT OF A FUEL CELL AUXILIARY PROPULSION AND POWER UNIT | ICAS2024_0261 |
| Hornung, M. | NUMERICAL ANALYSIS OF GENERALIZED AERODYNAMIC FORCES CONSIDERING LAMINAR-TURBULENT TRANSITION ON A NLF WING | ICAS2024_0823 |
| Hosseini, S. | APPLICATION OF LAMBDA FRAMEWORK FOR AIRCRAFT MULTIDISCIPLINARY DESIGN, ANALYSIS AND OPTIMIZATION | ICAS2024_0068 |
| Hosseini, S.S. | SCOPING OF AN AIR SUPPLY CONFIGURATION FOR ACTIVE FLOW CONTROL ON A COMMERCIAL TRANSPORT AIRPLANE HIGH-LIFT SYSTEM | ICAS2024_0951 |
| Hou, P.-Y. | A METHOD FOR OPTIMISING THE ARRANGEMENT OF INTERNAL CHANNELS IN AIRCRAFT HYDRAULIC MANIFOLDS MANUFACTURED BY ADDITIVE MANUFACTURING | ICAS2024_0933 |
| Hou, R. | EXPERIMENTAL INVESTIGATION AND NUMERICAL ANALYSIS OF THE EFFECT OF TEMPERATURE ON THE MECHANICAL PROPERTIES OF AEROSPACE COMPOSITE-METAL HYBRID JOINTS | ICAS2024_0530 |
| Hu, D. | ANALYSIS OF STEALTH ENHANCEMENT DESIGN PROCESS AND METHODS FOR UNMANNED AERIAL VEHICLE | ICAS2024_0568 |
| Hu, J.-P. | STUDY OF THE SCAVENGE PUMP PERFORMANCE FOR TWO-PHASE FLOW IN AN AIRCRAFT ENGINE LUBRICATION SYSTEM | ICAS2024_0788 |
| Hu, J.-P. | EXPERIMENTAL STUDY ON MULTI-ATTITUDE OIL SUPPLY STRUCTURE | ICAS2024_0817 |
| Hu, J.-P. | VOID FRACTION CALCULATION MODEL BASED ON TWO-PHASE FLOW PATTERNS IN THE SCAVENGE PIPE | ICAS2024_1010 |
| Hu, M. | SURROGATE MODELING OF VORTEX SHEDDING TURBINE IN LOW REYNOLDS NUMBER | ICAS2024_0791 |
| Hu, R. | DYNAMIC AND STABILITY ANALYSES OF ROTATING THIN-WALLED FILAMENT WOUND GLASS FIBRE COMPOSITE CYLINDERS WITH METAL LINER | ICAS2024_0296 |
| Hu, T. | STUDY ON THE BALLISTIC-RESISTANT AIRWORTHINESS STANDARDS FOR COMMERCIAL AIRCRAFT COCKPIT DOOR | ICAS2024_0074 |
| Hu, X. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AEROELASTICITY OF HIGH-ASPECT-RATIO WINGS | ICAS2024_0423 |
| Hu, X. | RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS | ICAS2024_0674 |
| Hu, Z. | EXPLORING A CATEGORY OF LIMIT CYCLE OSCILLATIONS IN AIRCRAFT HYDRAULIC SYSTEMS | ICAS2024_0932 |
| Huang, C.-R. | PILOT FATIGUE DETECTION USING BP NEUTRAL NETWORKS | ICAS2024_0183 |
| Huang, G. | MECHANISM STUDY ON THE IMPACT OF PULSED JET AT THE BLADE TIP LEADING EDGE ON THE FLOW FIELD IN COMPRESSOR | ICAS2024_0849 |
| Huang, H. | HYDRODYNAMIC ANALYSIS OF STATIC WATER IMPACT ON WEDGE-SHAPED HULL WATERTIGHT TEST SPECIMEN THROUGH NUMERICAL ANALYSIS | ICAS2024_0904 |
| Huang, H.-X. | A METHOD FOR OPTIMISING THE ARRANGEMENT OF INTERNAL CHANNELS IN AIRCRAFT HYDRAULIC MANIFOLDS MANUFACTURED BY ADDITIVE MANUFACTURING | ICAS2024_0933 |
| Huang, H.-X. | ULTRA-LOW-ALTITUDE PENETRATION PATH PLANNING FOR FIXED-WING AIRCRAFT BASED ON NMP ALGORITHM | ICAS2024_0972 |
| Huang, J. | THE EFFECT OF TARGET THICKNESS ON THE BALLISTIC BEHAVIOR OF HYBRID CFRP/KFRP COMPOSITES | ICAS2024_0225 |
| Huang, J. | ROTOR DYNAMIC LOADS CHARACTERISTIC ANALYSIS WITH BLADE TIP TWIST DISTRIBUTION | ICAS2024_0418 |
| Huang, J. | AERODYNAMIC PERFORMANCE OF BLADELESS DUCTED FAN BASED ON EJECTION EFFECT WITH DIFFERENT DESIGN VARIABLES | ICAS2024_0419 |
| Huang, J.T. | FAST PREDICTION OF PRESSURE DISTRIBUTION FOR 3D CONFIGURATION BASED ON LARGE LANGRAGE MODEL | ICAS2024_0679 |
| Huang, L.-Y. | ANALYSIS OF AERODYNAMIC INTERFERENCE CHARACTERISTICS AND AEROACOUSTICS FOR HIGH-SPEED COMPOSITE HELICOPTER IN HOVER | ICAS2024_0704 |
| Huang, S. | NUMERICAL SIMULATION OF HEAT TRANSFER IN MINIATURE RADIALLY ROTATING SODIUM/POTASSIUM HEAT PIPES | ICAS2024_0323 |
| Huang, S. | ROTOR DYNAMIC LOADS CHARACTERISTIC ANALYSIS WITH BLADE TIP TWIST DISTRIBUTION | ICAS2024_0418 |
| Huang, S. | VIBRATION ANAYLYSIS AND INFLUENCING FACTOR STUTY OF HELICOPTER HYDRAULIC PIPELINNE | ICAS2024_0678 |
| Huang, S. | AERODYNAMIC DEFORMATION EXPERIMENT OF SERPENTINE NOZZLE FOR TURBOFAN AND ANALYSIS OF FLUID-STRUCTURE INTERACTION METHOD | ICAS2024_0919 |
| Huang, Y. | A NOVEL DEEP MULTIMODAO INFORMATION FUSION MODEL FOR AERO-ENGINE STATE PREDICTION | ICAS2024_0159 |
| Huang, Y. | THERMAL AND GRINDING PERFORMANCE OF 3D PRINTED COMPLIANCE GRINDING TOOLS WITH ROTARY-ENHANCED HEAT TRANSFER STRUCTURE | ICAS2024_0248 |
| Huang, Y. | FROM ONTOLOGY TO SYSTEM ARCHITECTURE: AN MBSE APPROACH TOWARD THE REALIZATION OF URBAN AIR MOBILITY | ICAS2024_0554 |
| Huang, Y.-P. | VIBRATION ANAYLYSIS AND INFLUENCING FACTOR STUTY OF HELICOPTER HYDRAULIC PIPELINNE | ICAS2024_0678 |
| Huang, Z. | MANNED AND UNMANNED AERIAL VEHICLES COOPERATIVE COMBAT FRAMEWORK BASED ON LARGE LANGUAGE MODELS | ICAS2024_0231 |
| Hubnerova, Z. | FUEL CONSUMPTION MONITORING OF TURBOPROP ENGINE | ICAS2024_0708 |
| Huet, M. | DUAL-STREAM JET NOISE TEST WITH INTERNAL MIXER DESIGN VARIATIONS FOR LTO NOISE OF SUPERSONIC AIRCRAFT | ICAS2024_0064 |
| Huet, M. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Humphrey, L.R. | PRELIMINARY APPLICATION OF FORMAL VERIFICATION TO AN AUTONOMY ARCHITECTURE FOR UNMANNED AIRCRAFT | ICAS2024_1278 |
| Huo, W.F. | A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION | ICAS2024_0314 |
| Hussein, O. | AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS | ICAS2024_1139 |
| Huyssen, R.J. | ON THE EXISTENCE OF A FAMILY OF IDEAL AIRCRAFT CONFIGURATIONS | ICAS2024_0723 |
| Hübner, A.-R. | APPLICATION OF DIFFERENT NUMERICAL TOOLS AND NUMERICAL METHODS FOR PREDICTION OF HEAT EXCHANGER RAMAIR-CONCEPTS FOR HYBRID ELECTRIC PROPULSION AIRCRAFT CONFIGURATIONS | ICAS2024_0062 |
| Hyde, L. | CONTINUING DEVELOPMENT OF A NOVEL CERTIFIABLE AIRLINER “GONDOLA” USING LIQUID HYDROGEN | ICAS2024_0939 |
| Hällqvist, R. | AUTOMATION OF ENGINEERING INTEROPERABILITY FOR AIRCRAFT SYSTEM DESIGN | ICAS2024_0510 |
| Häßy, J. | PERFORMANCE AND ECONOMIC ASSESSMENT OF A WING-INTEGRATED HYBRID LAMINAR FLOW CONTROL SYSTEM | ICAS2024_0097 |
| Häßy, J. | ON THE WATER ENHANCED TURBOFAN CONCEPT: PART B – FLOW PATH AND MASS ASSESSMENT | ICAS2024_0135 |
| Häßy, J. | ON THE WATER ENHANCED TURBOFAN CONCEPT: PART A - THERMODYNAMICS AND OVERALL ENGINE DESIGN | ICAS2024_0199 |
| Häßy, J. | KNOWLEDGE-BASED TURBINE DISK MODELING – A CONCEPTUAL DESIGN PROCESS CALIBRATED TO THE NASA ENERGY EFFICIENT ENGINE | ICAS2024_0272 |
| Häßy, J. | ESTABLISHING THE DLR-F25 AS A RESEARCH BASELINE AIRCRAFT FOR THE SHORT-MEDIUM RANGE MARKET IN 2035 | ICAS2024_0398 |
| Häßy, J. | CLIMATE IMPACT AND ECONOMIC ASSESSMENT OF LIQUID HYDROGEN AND SYNTHETIC KEROSENE LONG-RANGE AIRCRAFT CONCEPTS | ICAS2024_0399 |
| Häßy, J. | PERFORMANCE ASSESSMENT OF AN ENGINE-INTEGRATED CLOSED-AIR COOLING THERMAL MANAGEMENT SYSTEM IN A NEXT GENERATION FIGHTER CONFIGURATION | ICAS2024_0622 |
| Iacolino, G. | METAMODELLING OF THE WORKLOAD ASSESSMENT IN SIMULATED FLIGHTS USING THE KRIGING METHOD | ICAS2024_0743 |
| Iannelli, P. | SCALED FLIGHT TESTING FOR EVALUATING DISTRIBUTED ELECTRIC PROPULSION | ICAS2024_0267 |
| Iannelli, P. | RESULTS OF THE SCALED FLIGHT DEMONSTRATOR FLIGHT TESTS | ICAS2024_1151 |
| Iannuzzo, A. | EXPERIMENTAL RESULTS OF ANTENNA PLACEMENT TEST ON A CARBON-FIBER SCALE REPLICA OF THE S55X SEAPLANE | ICAS2024_0504 |
| Ifimov, G. | ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD | ICAS2024_1280 |
| Ignatyev, D. | PRELIMINARY DESIGN EXPLORATION OF PROSPECTIVE MULTIROTOR AEROBOTS FOR MARS | ICAS2024_0536 |
| Iijima, T. | DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY | ICAS2024_0325 |
| Ikeda, M. | OPTIMIZING FLEET ASSIGNMENT DECISIONS FOR REGIONAL AIRLINES WITH HYBRID ELECTRIC AIRCRAFT UPTAKE | ICAS2024_0781 |
| Ikeda, T. | NUMERICAL EVALUATION FOR FAN-NOISE SHIELDING EFFECTS ON AFT-FUSELAGE MOUNTED AND EMBEDDED ENGINES | ICAS2024_0471 |
| Ikeda, T. | EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) | ICAS2024_0549 |
| Ilic, B. | UPGRADE OF THE VTI T-38 BLOWDOWN TRISONIC TEST FACILITY: WIND TUNNEL CONTROL SYSTEM | ICAS2024_0456 |
| Iliopoulos, I.A. | IN-FLIGHT VIBRATION SIGNAL BASED DETECTION AND LOCALIZATION FOR UAV PROPELLER ANOMALIES UNDER UNCERTAINTY VIA MACHINE LEARNING TYPE METHODS | ICAS2024_0984 |
| Imamura, T. | EVALUATING INSTALLATION EFFECTS IN SEMI-SPAN WIND TUNNEL EXPERIMENTS USING CARTESIAN-GRID-BASED FLOW SOLVER UTCART | ICAS2024_0293 |
| Inaka, S. | REMOTE OBSERVATION EXPERIMENT OF VOLCANIC ASH USING POLARIZATION LIDAR | ICAS2024_0214 |
| Inohata, S. | FEASIBILITY STUDY ON OPERATIONAL FLIGHT PLANS ADAPTED FOR TRAJECTORY BASED OPERATION | ICAS2024_1177 |
| Inokuchi, H. | REMOTE OBSERVATION EXPERIMENT OF VOLCANIC ASH USING POLARIZATION LIDAR | ICAS2024_0214 |
| Inoue, N. | TIME-BASED CONTROL TO REDUCE TRAJECTORY COMPLEXITY IN THE FLOW-CENTRIC AIR TRAFFIC CONTROL PARADIGM | ICAS2024_0966 |
| Inoue, T. | DEVELOPMENT OF AIRCRAFT SYSTEM ELECTRIFICATION AND HYBRID ELECTRIC PROPULSION | ICAS2024_0971 |
| Invernizzi, D. | ADAPTIVE CONTROL AND MISSION PLANNER DESIGN FOR UAV OPERATIONS WITH BATTERY MANAGEMENT | ICAS2024_1136 |
| Inverno, M. | A SUPPORTING FRAMEWORK FOR AIRCRAFT MRO OPERATIONS. CAPACITY PLANNING, TASKS TRACEABILITY AND DISEMBARKED ITEMS TRACKING | ICAS2024_0100 |
| Ireland, W.A. | CLIMATE RESILIENCE – THE IMPACT OF EXTREME WEATHER EVENTS - A CASE STUDY: HEATHROW AIRPORT | ICAS2024_0292 |
| Isakovic, J. | UPGRADE OF THE VTI T-38 BLOWDOWN TRISONIC TEST FACILITY: WIND TUNNEL CONTROL SYSTEM | ICAS2024_0456 |
| Isikveren, A.T. | RESULTS FROM THE APPU PROJECT: THE POTENTIAL OF LOW-THRESHOLD HYDROGEN-POWERED BLI PROPULSION | ICAS2024_0179 |
| Iskenderian, H. | WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES | ICAS2024_1137 |
| Islam, T. | INCREMENTAL NONLINEAR DYNAMIC INVERSION CONTROLLER FOR A FLYING WING OPERATED IN AN AIRBORNE WIND ENERGY SYSTEM | ICAS2024_0713 |
| Isnard, B. | IDENTIFICATION METHOD OF LONGITUDINAL COEFFICIENTS BASED ON THE NUMERICAL STUDY OF THE FLOW TOPOLOGY AROUND THE SACCON GEOMETRY | ICAS2024_0506 |
| Issamu Kitadani Odaguil, F. | ADJOINT-BASED TRANSONIC WING AERODYNAMIC SHAPE OPTIMIZATION INVESTIGATIONS | ICAS2024_0078 |
| Itoh, E. | DEVELOPMENT OF A NEW OPERATIONAL FRAMEWORK TO ACCOMMODATE STOCHASTIC AIR TRAFFIC FLOW AT TOKYO INTERNATIONAL AIRPORT | ICAS2024_0963 |
| Itoh, E. | TIME-BASED CONTROL TO REDUCE TRAJECTORY COMPLEXITY IN THE FLOW-CENTRIC AIR TRAFFIC CONTROL PARADIGM | ICAS2024_0966 |
| Itoh, E. | VALIDATING FLOW-BASED EN ROUTE AMAN COUPLING ESCAPE LIGHT WITH AIRTOP SOFTWARE | ICAS2024_0968 |
| Itoh, H. | ELECTRIC FIELD MEASUREMENT IN GLOW DISCHARGE PLASMA INTERACTING WITH SHOCK WAVE IN HYPERSONIC FLOW | ICAS2024_0390 |
| Iturriaga, I. | HYDROGEN AIRLINER TANK OPTIMISATION | ICAS2024_0515 |
| Iuspa, L. | WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS | ICAS2024_0348 |
| Iuspa, L. | OPTIMIZATION PROCEDURE FOR THE WING OF A MARS EXPLORATION DRONE | ICAS2024_0862 |
| Iwami, Y. | EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) | ICAS2024_0549 |
| Iwanizki, M. | CLIMATE IMPACT AND ECONOMIC ASSESSMENT OF LIQUID HYDROGEN AND SYNTHETIC KEROSENE LONG-RANGE AIRCRAFT CONCEPTS | ICAS2024_0399 |
| Iwata, D. | DEVELOPMENT OF A NEW OPERATIONAL FRAMEWORK TO ACCOMMODATE STOCHASTIC AIR TRAFFIC FLOW AT TOKYO INTERNATIONAL AIRPORT | ICAS2024_0963 |
| Jacinto, M. | IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN | ICAS2024_0057 |
| Jahangirian, A. | MACHINE LEARNING INTEGRATION IN COMPUTATIONAL FLUID DYNAMICS FOR RAPID FLOW FIELD PREDICTION | ICAS2024_1033 |
| Jaisawal, P.K. | MRO FOR VTOLS IN A FUNCTIONAL SEQUENCES SOLUTION SPACE | ICAS2024_0705 |
| Jamakatel, P. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Jamakatel, P. | GENERATION AND COMMUNICATION OF STRATEGIC PLANS AT DIFFERENT LEVELS OF ABSTRACTION FOR INTELLIGENT ASSISTANCE SYSTEMS IN GENERAL AVIATION | ICAS2024_0268 |
| James, K.D. | VEHICLE ASSESSMENT AND SYSTEM-WIDE BENEFIT ANALYSES OF HYBRID-ELECTRIC COMMERCIAL AIRCRAFT – ELECTRIFIED POWERTRAIN FLIGHT DEMONSTRATION PROJECT (EPFD) | ICAS2024_1188 |
| Jamison, K. | DECOUPLING STORE AND PARENT AERODYNAMICS FOR FAST PREDICTION OF SUBSONIC STORE TRAJECTORIES | ICAS2024_0189 |
| Jan, R. | EVALUATION OF ASWING FOR OVERALL AIRCRAFT DESIGN OF UNCONVENTIONAL CONFIGURATIONS. APPLICATION TO JOINED WINGS WITH FOLDING WINGTIPS | ICAS2024_0254 |
| Jang, J.-I. | CONVEX PROGRAMMING APPROACH OF ROBUST POWERED DESCENT GUIDANCE THROUGH DYNAMIC TUBE MPC | ICAS2024_0839 |
| Jann, T. | ASSISTED AND AUTOMATED AERIAL REFUELLING – OVERVIEW OF THE CONDUCTED RESEARCH AT THE GERMAN AEROSPACE CENTER (DLR) | ICAS2024_0819 |
| Jansen, P.W. | SYSTEM OF SYSTEMS ANALYSIS OF AUTONOMOUS AIRCRAFT OPERATIONS IN AIR CARGO FEEDER NETWORKS | ICAS2024_0413 |
| Jansen, P.W. | MODELING CARGO DEMAND FOR REGIONAL AIR TRANSPORT NETWORKS IN CANADA AND THE UNITED STATES | ICAS2024_0729 |
| Jansen, R.H. | SIZING AND PERFORMANCE ANALYSIS OF A MW-CLASS ELECTRIFIED AIRCRAFT PROPULSION (EAP) SYSTEM FOR A PARALLEL HYBRID TURBOPROP CONCEPT | ICAS2024_0884 |
| Janssens, B. | PASSIVE FLOW CONTROL DEVICES ON LOW-REYNOLDS DU89-134 AIRFOIL | ICAS2024_0228 |
| Janszen, G. | IMPACT TOLERANCE OF CERAMIC MATRIX COMPOSITES FOR AEROSPACE APPLICATIONS | ICAS2024_1111 |
| Jaron, R. | DUAL-STREAM JET NOISE TEST WITH INTERNAL MIXER DESIGN VARIATIONS FOR LTO NOISE OF SUPERSONIC AIRCRAFT | ICAS2024_0064 |
| Jaron, R. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Jaron, R. | THE FUTURE OF CIVIL SUPERSONIC TRANSPORT IN EUROPE: THE SENECA AND MORE&LESS PROJECTS | ICAS2024_0820 |
| Jasak, H. | INITIAL DEVELOPMENT OF A CFD ICING TOOL | ICAS2024_1112 |
| Jebacek, I. | THE FATIGUE LIFE PREDICTION OF THIN-WALLED WELDED JOINTS | ICAS2024_1120 |
| Jentink, H. | SCALED FLIGHT TESTING FOR EVALUATING DISTRIBUTED ELECTRIC PROPULSION | ICAS2024_0267 |
| Jentink, H. | RESULTS OF THE SCALED FLIGHT DEMONSTRATOR FLIGHT TESTS | ICAS2024_1151 |
| Jeong, J.H. | PSYCHOACOUSTICAL ANALYSIS OF SYNTHESIZED MOTOR-PROPELLER ROTOR SYSTEM NOISE | ICAS2024_0973 |
| Jeong, S.H. | DEVELOPMENT OF A MACHINE LEARNING-BASED STRESS SPECTRUM ESTIMATION TECHNIQUE FOR FATIGUE MONITORING | ICAS2024_0525 |
| Jézégou, J. | MODEL-BASED APPROACH FOR HYDROGEN PRELIMINARY AIRCRAFT DESIGN CONSIDERING SAFETY AND OPERABILITY | ICAS2024_0095 |
| Jézégou, J. | STUDY OF HYBRIDISATION SCENARIOS FOR TURBOPROP AIRCRAFT IN THE GENERAL AVIATION SEGMENT | ICAS2024_0153 |
| Jha, P. | EMBEDDED SENSORS FOR AIRCRAFT PREDICTIVE MAINTENANCE: SHM SYSTEM INTEGRATION & TRADE-OFF ANALYSIS | ICAS2024_1081 |
| Jha, P. | USE OF GRAPHENE MATERIAL IN AIRCRAFT STRUCTURE FOR LIGHTNING STRIKE PROTECTION | ICAS2024_1141 |
| Ji, L. | STUDY ON FATIGUE PROPERTIES OF TITANIUM ALLOY BASE MATERIAL AND WELDED STRUCTURE IN THERMAL COMBINED ENVIRONMENT | ICAS2024_0422 |
| Ji, W.T. | EFFECTS OF SHAPE AND STREAMWISE SPACING OF PIN-FINS ARRAYS ON FLOW AND HEAT TRANSFER | ICAS2024_0720 |
| Ji, Z. | RESEARCH ON MULTI-ATTRIBUTE DECISION MAKING AND VERIFICATION METHODS FOR SYSTEMS CONFRONTATION | ICAS2024_0561 |
| Jia, G. | AERODYNAMIC CHARACTERISTICS RESEARCH OF A DISTRIBUTED PROPULSION AIRCRAFT | ICAS2024_0537 |
| Jia, G. | ANALYSIS OF STEALTH ENHANCEMENT DESIGN PROCESS AND METHODS FOR UNMANNED AERIAL VEHICLE | ICAS2024_0568 |
| Jia, G. | ANALYSIS OF BATTERY WEIGHT REQUIREMENTS IN THE DESIGN OF HYBRID ELECTRIC POWERED AIRCRAFT | ICAS2024_0813 |
| Jia, G.W. | SEPARATION SAFETY ANALYSIS IN VARIABLE LAUNCH CONDITION OF SMALL AIR-LAUNCHED UAVS BASED ON NUMERICAL SIMULATION AND FLIGHT TEST | ICAS2024_0311 |
| Jia, X. | SPARSE RECONSTRUCTION OF SURFACE LOADS ON AIRCRAFT USING POD AND RBFNN | ICAS2024_0634 |
| Jia, X. | MULTI-FIDELITY SURROGATE MODELING BASED ON DATA EXTENSION USING POD AND ANN | ICAS2024_0957 |
| Jian, M. | CONJUGATED HEAT TRANSFER SIMULATION OF BUOYANCY-INDUCED FLOW AND HEAT TRANSFER MECHANISMS IN A COMPRESSOR CAVITY | ICAS2024_0531 |
| Jiang, C. | MODELING AND ANALYSIS OF ELECTRO-HYDROSTATIC ACTUATORS EFFICIENCY | ICAS2024_1043 |
| Jiang, Q. | ROTOR DYNAMIC LOADS CHARACTERISTIC ANALYSIS WITH BLADE TIP TWIST DISTRIBUTION | ICAS2024_0418 |
| Jiang, T.-J. | IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM | ICAS2024_1186 |
| Jiao, J. | LOW ENERGY CONSUMPTION DESIGN METHOD AND STRATEGY FOR HIGH-ALTITUDE PROPELLERS BASED ON FLIGHT PROFILE | ICAS2024_0865 |
| Jiao, J. | ANALYSIS OF SUCTION FORCE EFFECT ON DIFFERENT FUSELAGE SHAPE DURING THE WATER DITCHING | ICAS2024_0929 |
| Jiménez-Varona, J. | GRID EFFECT ON M823 BOMB AT TRANSONIC REGIME | ICAS2024_0031 |
| Jimeno Altelarrea, S. | SET-BASED DESIGN TECHNIQUES FOR EVOLVABILITY EXPLORATION DURING CONCEPTUAL AIRCRAFT DESIGN | ICAS2024_0233 |
| Jin, L. | RESEARCH ON AIRSPEED CORRECTION TECHNOLOGY OF EJECTION SEAT BASED ON CFD | ICAS2024_0709 |
| Jin, S.-Y. | DATA MINING ANALYSIS ON AERODYNAMIC STEALTH DESIGN PRINCIPLES OF AIRFOIL PROFILES | ICAS2024_0448 |
| Jin, X. | FAST PREDICTION METHOD FOR RADIAL GROWTH OF LABYRINTH SEAL CLEARANCE BASED ON TRANSIENT THERMAL-FLUID COUPLING NETWORK | ICAS2024_0450 |
| Jing, Q. | FLIGHT LOADS RESEARCH OF TWIN VERTICAL TAIL FOR BLENDED WING-BODY AIRCRAFT BASED ON STRAIN GAUGE CAILBRATION | ICAS2024_0072 |
| Jing, T.-T. | MULTI-DIMENTIONAL DESIGN AND THERMAL PROTECTION CAPABILITY OF A REGENERATIVE COOLED RBCC VARIABLE-GEOMETRY COMBUSTOR | ICAS2024_1012 |
| Johansson, A. | MODELLING A HYDROGEN FUELLED COMPOSITE CYCLE AEROENGINE | ICAS2024_1103 |
| Johnson, D. | WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES | ICAS2024_1137 |
| Johnson, M. | NASA RESEARCH TO EXPAND UAS OPERATIONS FOR DISASTER RESPONSE | ICAS2024_1281 |
| Johnson, N. | FLYING V DIRECTIONAL FLIGHT CONTROL: AN EXPERIMENTAL INVESTIGATION | ICAS2024_1014 |
| Johnston, C.M. | FATIGUE PROPERTIES OF ADDITIVELY MANUFACTURED TOOL STEEL | ICAS2024_0633 |
| Jokinen, J. | HOT-WET CONDITIONING AND THE SENSITIVITY OF MECHANICAL TESTING WITHIN SURFACE TREATMENT QUALIFICATION FOR AIRCRAFT | ICAS2024_0407 |
| Jokinen, J. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Joly, L. | AN EMPIRICAL AND CUSTOMISABLE FLEET RENEWAL MODEL FOR PROSPECTIVE SCENARIOS USING OPEN-ACCESS DATA | ICAS2024_0367 |
| Jones, C.E. | SAFETY-DRIVEN BASELINING OF HYBRID ELECTRIC AIRCRAFT ELECTRICAL POWER SYSTEM ARCHITECTURES | ICAS2024_1027 |
| Jonsson, E. | SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION | ICAS2024_0465 |
| Jonsson, I. | LESSONS LEARNED FROM PROJECT BASED TEACHING IN AEROSPACE AT CHALMERS | ICAS2024_0867 |
| Jonsson, I. | LOW-SPEED PROPELLER FOR UAV APPLICATIONS, FROM DESIGN TO EXPERIMENTAL EVALUATION | ICAS2024_1157 |
| Jouanet, C. | SUSTAINABLE AVIATION IN NORDIC COUNTRIES | ICAS2024_0585 |
| Jouannet, C. | CONCEPT OF OPERATIONS IN AN AGENT-BASED SIMULATION: A SYSTEM-OF-SYSTEMS APPROACH | ICAS2024_0357 |
| Jouannet, C. | NAVIGATING COMPLEXITY: ADAPTING AEROSPACE DEVELOPMENT IN A DYNAMIC WORLD | ICAS2024_1258 |
| Jouannet, C. | MANAGING DIGITAL COMPLEXITY | ICAS2024_1328 |
| Joynt, M. | A PERFORMANCE COMPARISON OF HYDROGEN AIRCRAFT CONCEPTS | ICAS2024_0251 |
| Julien, C. | IMPACT OF HYDROGEN FUEL ON OVERALL DESIGN OF TRANSPORT AIRCRAFT | ICAS2024_0826 |
| Julien, C. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| June, J.C. | REFINED PREDICTIONS COMPARED WITH THE PROPULSION AIRFRAME AEROACOUSTICS AND AIRCRAFT SYSTEM NOISE FLIGHT RESEARCH TEST DATA | ICAS2024_0069 |
| June, J.C. | NASA TRANSONIC TRUSS-BRACED WING STUDIES | ICAS2024_0108 |
| Jung, C.-G. | TRAJECTORY OPTIMIZATION FOR LONG-RANGE AIR-LAUNCHED GLIDING VEHICLES USING CONVEX PROGRAMMING | ICAS2024_0468 |
| Jung, K.-W. | DOWNRANGE CONTROL GUIDANCE FOR REENTRY BURN OF REUSABLE LAUNCH VEHICLE | ICAS2024_0892 |
| Juracka, J. | FUEL CONSUMPTION MONITORING OF TURBOPROP ENGINE | ICAS2024_0708 |
| Jurkat-Witschas, T. | SENS4ICE EU PROJECT HYBRID ICE DETECTION ARCHITECTURES DEMONSTRATION RESULTS | ICAS2024_0178 |
| Jäschke, J. | ESATTO: THE HOLISTIC FRAMEWORK TO SUPPORT THE DESIGN OF SUSTAINABLE SUPERSONIC AVIATION | ICAS2024_1032 |
| Kabelac, S. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Kachel, S. | AERODYNAMIC ANALYSIS OF CAMBER MORPHING AIRFOILS USING PARTICLE IMAGE VELOCIMETRY AND COMPUTATIONAL FLUID DYNAMICS METHODS | ICAS2024_0691 |
| Kacik, D. | OVERVIEW OF FACTORS RELATED TO AIRCRAFT OPERATION ASSOCIATED WITH A NEGATIVE IMPACT ON THE ENVIRONMENT | ICAS2024_0410 |
| Kadlec, M. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Kaduce, E. | X-66: ACCELERATED LEARNING THROUGH FULL SCALE PROTOTYPING | ICAS2024_1240 |
| Kalacska, M. | ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD | ICAS2024_1280 |
| Kalampoukas, T. | A PROPOSAL TOWARDS A STEP CHANGE FROM ECO-DRIVEN TO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT COMPONENTS | ICAS2024_0088 |
| Kalgutkar, A. | CONCEPTUAL DESIGN AND SIZING OF A SOLAR POWERED QUAD-ROTOR FIXED WING HYBRID UAV FOR EXPLORATION OVER MARS | ICAS2024_1156 |
| Kamat, A. | PROBING AND MODELING LARGE-SCALE AIRLINE NETWORK DISRUPTIONS: 2022 SOUTHWEST AIRLINES SCHEDULING CRISIS | ICAS2024_0782 |
| Kaminska, I. | THERMAL HISTORY PAINT UNDER HIGH SUBSONIC FLOW | ICAS2024_0316 |
| Kan, Z. | IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM | ICAS2024_1186 |
| Kaneko, K. | MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM | ICAS2024_0573 |
| Kanerva, M. | HOT-WET CONDITIONING AND THE SENSITIVITY OF MECHANICAL TESTING WITHIN SURFACE TREATMENT QUALIFICATION FOR AIRCRAFT | ICAS2024_0407 |
| Kanerva, M. | MICKEY MOUSE AND A GIANT: COMPARISON OF AERONAUTICS EDUCATION IN FINLAND AND CHINA | ICAS2024_1263 |
| Kang, M.-W. | DATA-DRIVEN MODEL DISCOVERY AND CONTROL OF HIGH-PERFORMANCE TRAINER AIRCRAFT VIA SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS | ICAS2024_0627 |
| Karbowski, D. | ENERGY AND EMISSION ANALYSIS OF AN AIR-TAXI SERVICE USING DYNAMIC EVTOL SYSTEM MODELS | ICAS2024_0172 |
| Karbowski, D. | ANALYZING THE IMPACTS OF SUSTAINABLE POWERTRAINS FOR SHORT-HAUL COMMUTER AIRLINES | ICAS2024_0175 |
| Karger, J. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Karger, J. | MIXED FLIGHT CONTROL LAYOUT FOR ULTRALIGHT GENERAL AVIATION AIRCRAFT | ICAS2024_0517 |
| Kaschub, L. | CINNABAR PROJECT - AUGMENTED REALITY WORKFLOW FOR AIRCRAFT DENT & BUCKLE INSPECTION | ICAS2024_0152 |
| Kaschub, L. | CINNABAR PROJECT: EXAMINING REQUIREMENTS FOR USER ACCEPTANCE OF AIRCRAFT STRUCTURE INSPECTION IN AUGMENTED REALITY | ICAS2024_0164 |
| Katagiri, K. | EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) | ICAS2024_0549 |
| Katarzynski, J. | NOVEL TEST RIG TO DEMONSTRATE A MULTI FUNCTIONAL FLAP MECHANISM OFFERING A 2ND DEGREE OF FREEDOM | ICAS2024_0299 |
| Kawamura, T. | TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2024_1215 |
| Kazari, M. | DEVELOPMENT OF CORE TECHNOLOGIES FOR HYDROGEN AIRCRAFT | ICAS2024_0836 |
| Kazula, S. | SAFETY ANALYSIS (CCA) OF THE AIR SUPPLY SYSTEM OF A FUEL CELL-POWERED AERO ENGINE FOR ELECTRIC REGIONAL AIRCRAFT | ICAS2024_0191 |
| Kearns, E. | COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A DIRECT AIR CAPTURE FILTER SYSTEM | ICAS2024_0463 |
| Keimer, R. | DEVELOPMENT AND TESTING OF AN ACTUATION SYSTEM FOR A MORPHING CONTROL SURFACE | ICAS2024_0171 |
| Kekoc, V. | APPLICATION OF NATURAL LANGUAGE PROCESSING FOR AIRCRAFT DEFECT TRACKING IN MAINTENANCE OPERATIONS | ICAS2024_0083 |
| Keller, C. | SUSTAINABLE ENGINE MAINTENANCE: EVALUATING THE ECOLOGICAL IMPACT OF LIFE LIMITED PART REPLACEMENT | ICAS2024_0452 |
| Kenny, J. | REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS | ICAS2024_1172 |
| Keser, T. | MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION | ICAS2024_0020 |
| Keser, T. | CINNABAR PROJECT - AUGMENTED REALITY WORKFLOW FOR AIRCRAFT DENT & BUCKLE INSPECTION | ICAS2024_0152 |
| Keser, T. | CINNABAR PROJECT: EXAMINING REQUIREMENTS FOR USER ACCEPTANCE OF AIRCRAFT STRUCTURE INSPECTION IN AUGMENTED REALITY | ICAS2024_0164 |
| Keye, S. | SUMMARY OF DLR RESULTS FROM THE SEVENTH AIAA DRAG PREDICTION WORKSHOP | ICAS2024_0116 |
| Khaled, M. | VALIDATION OF MULTIPHASE FLOW SIMULATIONS BY EXPERIMENTAL MEASUREMENTS IN A CHANNEL FLOW | ICAS2024_0176 |
| Khan, Y.M. | CONCEPTUAL DESIGN OF A ZERO-EMISSION REGIONAL AIRCRAFT FOR ENHANCED SHORT-HAUL MOBILITY | ICAS2024_1085 |
| Khella, M. | NUMERICAL TOOLS FOR SLOW-GROWTH APPROACHES TO DAMAGE TOLERANT COMPOSITE AERONAUTICAL STRUCTURES | ICAS2024_1146 |
| Khot, E. | AN AUTONOMOUS SYSTEM FOR DOCKING AND BATTERY SWAPPING IN UAVS | ICAS2024_1116 |
| Ki, W.-D. | MODEL-BASED CONCEPTUAL DESIGN AND EVALUATION OF A SOLID-FUEL SCRAMJET VEHICLE | ICAS2024_0195 |
| Kiam, J.J. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Kiam , J.J. | GENERATION AND COMMUNICATION OF STRATEGIC PLANS AT DIFFERENT LEVELS OF ABSTRACTION FOR INTELLIGENT ASSISTANCE SYSTEMS IN GENERAL AVIATION | ICAS2024_0268 |
| Kiasat, S. | INVESTIGATING THE EFFECT OF DELAMINATION-INDUCED FRICTIONAL CONTACT ON THE DYNAMIC BEHAVIOR OF LAMINATE STRUCTURES | ICAS2024_1108 |
| Kienitz, K.H. | STRUCTURED H-INFINITY DESIGN OF PREDICTORS FOR THE MONITORING OF AN AIRCRAFT IN ITS FLIGHT ENVELOPE | ICAS2024_0223 |
| Kienitz, K.H. | SELF-DRIVING AND MODEL-BASED EXTREMUM SEEKING CONTROL IN TIGHT FORMATION FLIGHT FOR FUEL SAVING | ICAS2024_0861 |
| Kienitz, K.H. | APPLICATION OF A MORE INTEGRATED TOTAL ENERGY CONTROL SYSTEM FOR IMPROVING AIRCRAFT AND ENGINE CONTROL EFFICIENCY | ICAS2024_0891 |
| Kierbel, D. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Kierbel, D. | SCALED FLIGHT TESTING FOR EVALUATING DISTRIBUTED ELECTRIC PROPULSION | ICAS2024_0267 |
| Kierbel, D. | RESULTS OF THE SCALED FLIGHT DEMONSTRATOR FLIGHT TESTS | ICAS2024_1151 |
| Kikkawa, S. | DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY | ICAS2024_0325 |
| Kilbourne, M. | EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS | ICAS2024_0464 |
| Kilian, T. | PERFORMANCE AND ECONOMIC ASSESSMENT OF A WING-INTEGRATED HYBRID LAMINAR FLOW CONTROL SYSTEM | ICAS2024_0097 |
| Kim, B. | PURSUIT-BASED LONG-RANGE AIR-TO-AIR MISSILE MIDCOURSE GUIDANCE ROBUST TO CHANGES IN THE PREDICTED IMPACT POINT | ICAS2024_0828 |
| Kim, D. | MISSION-BASED OPTIMAL PROPELLER SELECTION FOR VTOL SUAV CONFIGURATION | ICAS2024_0564 |
| Kim, D. | DATA-DRIVEN MULTI-RANGE MISSION-BASED OVERALL AIRCRAFT CONCEPTUAL DESIGN OPTIMIZATION | ICAS2024_0611 |
| Kim, D. | AUTONOMOUS LANDING OF A QUADROTOR ON A MOVING TARGET WITH OCCLUSION AVOIDANCE MANEUVER | ICAS2024_0664 |
| Kim, H. | A STUDY ON BATTERY SEPARATION DRONES TO EXTEND ENDURANCE | ICAS2024_0785 |
| Kim, H.J. | AUTONOMOUS LANDING OF A QUADROTOR ON A MOVING TARGET WITH OCCLUSION AVOIDANCE MANEUVER | ICAS2024_0664 |
| Kim, J. | LEARNING-BASED FULL-ENVELOPE AUTOPILOT DESIGN BASED ON THE KOOPMAN OPERATOR THEORY | ICAS2024_0043 |
| Kim, J.-H. | IN-FLIGHT MEASUREMENT OF WING SURFACE PRESSURE DISTRIBUTION ON A FIXED-WING UAV AND ITS APPLICATION TO FLIGHT CONTROL | ICAS2024_0980 |
| Kim, J.H. | DEVELOPMENT OF A MACHINE LEARNING-BASED STRESS SPECTRUM ESTIMATION TECHNIQUE FOR FATIGUE MONITORING | ICAS2024_0525 |
| Kim, J.H. | WHAT-IF SCENARIO ANALYSIS OF REGIONAL AIR MOBILITY OPERATIONS IN SOUTH KOREA | ICAS2024_0850 |
| Kim, S. | A DESIGN OF VFR APPROACH AND DEPARTURE PROCEDURES OF UAM AT VERTIPORTS ADJACENT TO THE AIRPORT | ICAS2024_0110 |
| Kim, S.K. | WHAT-IF SCENARIO ANALYSIS OF REGIONAL AIR MOBILITY OPERATIONS IN SOUTH KOREA | ICAS2024_0850 |
| Kim, T. | A STUDY ON BATTERY SEPARATION DRONES TO EXTEND ENDURANCE | ICAS2024_0785 |
| Kim, Y. | LEARNING-BASED FULL-ENVELOPE AUTOPILOT DESIGN BASED ON THE KOOPMAN OPERATOR THEORY | ICAS2024_0043 |
| Kim, Y.H. | OPERATIONAL LIMITS ASSESSMENT FOR HIGH-ALTITUDE LONG-ENDURANCE UAVS CONSIDERING PROPELLER ICING EFFECT | ICAS2024_0507 |
| Kimura, K. | IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN | ICAS2024_0057 |
| Kipouros, T. | REQUIREMENTS UNCERTAINTY PROPAGATION IN CONCEPTUAL DESIGN USING BAYESIAN NETWORKS | ICAS2024_0076 |
| Kirkness-Duncombe, J.M. | AEROACOUSTIC CAVITY FLOW ENERGY HARVESTING | ICAS2024_0558 |
| Kirkpatrick, O. | APPLICATION OF NATURAL LANGUAGE PROCESSING FOR AIRCRAFT DEFECT TRACKING IN MAINTENANCE OPERATIONS | ICAS2024_0083 |
| Kirz, J. | APPLICATION OF DIFFERENT NUMERICAL TOOLS AND NUMERICAL METHODS FOR PREDICTION OF HEAT EXCHANGER RAMAIR-CONCEPTS FOR HYBRID ELECTRIC PROPULSION AIRCRAFT CONFIGURATIONS | ICAS2024_0062 |
| Kishimoto, N. | EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) | ICAS2024_0549 |
| Kiszkowiak, L. | STUDY ON CONFIGURATIONS OF AIRBORNE LAUNCH SYSTEM FOR DELIVERY OF SMALL PAYLOAD TO LOW EARTH ORBIT | ICAS2024_0355 |
| Kiszkowiak, L. | AERODYNAMIC ANALYSIS OF CAMBER MORPHING AIRFOILS USING PARTICLE IMAGE VELOCIMETRY AND COMPUTATIONAL FLUID DYNAMICS METHODS | ICAS2024_0691 |
| Kita, M. | EFFICIENT THERMOMECHANICAL SIMULATION FOR METALLIC LATTICE STRUCTURES FABRICATED BY ADDITIVE MANUFACTURING | ICAS2024_0908 |
| Klennert, J. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Klennert, J. | PILOT SAFETY – SUPPORT BY BIOMEDICAL MONITORING IN PILOTS WITH HEALTH RISKS | ICAS2024_0460 |
| Klennert, M. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Kloock-Schreiber, D. | MRO FOR VTOLS IN A FUNCTIONAL SEQUENCES SOLUTION SPACE | ICAS2024_0705 |
| Kloock-Schreiber, D. | DESIGN OF A UAM GROUND INFRASTRUCTURE NETWORK WITH RESPECT TO MAINTENANCE CAPACITY REQUIREMENTS | ICAS2024_0745 |
| Knöös Franzén, L. | CONCEPT OF OPERATIONS IN AN AGENT-BASED SIMULATION: A SYSTEM-OF-SYSTEMS APPROACH | ICAS2024_0357 |
| Knöös Franzen, L. | COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH | ICAS2024_1138 |
| Ko, J.W. | PSYCHOACOUSTICAL ANALYSIS OF SYNTHESIZED MOTOR-PROPELLER ROTOR SYSTEM NOISE | ICAS2024_0973 |
| Kobayashi, K. | LOW-ALTITUDE INTEGRATED AIRSPACE OPERATIONS OF AIRCRAFT FLYING UNDER VISUAL FLIGHT RULES: THE VERTICAL DIMENSION | ICAS2024_0835 |
| Koch, T. | SIMULATION AND VERIFICATION OF HYDRAULIC ROTOR GAP PARAMETERS OF A NOVEL HIGH EFFICIENT WET ELECTRO MOTOR PUMP FOR AEROSPACE APPLICATIONS | ICAS2024_0123 |
| Koenis, T.P.A. | ELECTROMAGNETIC INDUCTION HEATING OF TP-CFRP LAMINATES: FEM MODELLING AND VALIDATION | ICAS2024_0032 |
| Kohzai, M. | ACTIVITY PLANS USING CRM-HL AT JAXA | ICAS2024_1238 |
| Kolar, M. | W-WING AEROELASTIC DEMONSTRATOR DESIGN MODIFICATION AND UPGRADE | ICAS2024_0054 |
| Kolb, M.G. | MODELLING AND INITIAL ASSESSMENT OF A FUEL CELL AUXILIARY PROPULSION AND POWER UNIT | ICAS2024_0261 |
| Kolb, S. | PILOT INDUCED OSCILLATIONS AND FLIGHT PHASES IDENTIFICATION OF THE SPACE SHUTTLE AND TRANSPORT AIRPLANES | ICAS2024_0805 |
| Koloschin, A. | ASSISTED AND AUTOMATED AERIAL REFUELLING – OVERVIEW OF THE CONDUCTED RESEARCH AT THE GERMAN AEROSPACE CENTER (DLR) | ICAS2024_0819 |
| Komorek, A. | ANALYSIS OF THE POSSIBILITY OF INCREASING THE THERMAL RESISTANCE OF EPOXY RESIN WITH CWNT AND MMT | ICAS2024_0275 |
| Kong, L. | RESEARCH ON UNMANNED CLUSTER RECONNECTION DECISION-MAKING METHOD CONSIDERING RESOURCE SUPPLEMENTATION | ICAS2024_0343 |
| Kontis, K. | LOW-SUBSONIC AERODYNAMIC ANALYSES OF A NONPLANAR BWB MODEL: AN EXPERIMENTAL AND CFD STUDY | ICAS2024_0232 |
| Kontos, G. | DESIGNING A FRAMEWORK FOR FLIGHT SIMULATOR TRAINING SCENARIOS. AN EVIDENCE BASED TRAINING APPROACH. | ICAS2024_1098 |
| Koopman, C. | ENHANCED SAFETY THROUGH AI: AN ASSESSMENT OF ADVERSARIAL REINFORCEMENT LEARNING FOR CONTROL OF COMPLEX AIRCRAFT | ICAS2024_0440 |
| Koopman, J. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Kopacz, M. | VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA | ICAS2024_0104 |
| Kopardekar, P.H. | NASA’S ADVANCED AIR MOBILITY RESEARCH | ICAS2024_1322 |
| Kopec, I. | DESIGN OF REMOTE-CONTROLLED GROUND BASED AIRCRAFT TUG | ICAS2024_1021 |
| Korolis, J.S. | IN-FLIGHT VIBRATION SIGNAL BASED DETECTION AND LOCALIZATION FOR UAV PROPELLER ANOMALIES UNDER UNCERTAINTY VIA MACHINE LEARNING TYPE METHODS | ICAS2024_0984 |
| Kos, J. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Koschlik, A.-K. | MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION | ICAS2024_0020 |
| Koschlik, A.-K. | CINNABAR PROJECT – COST-BENEFIT ANALYSIS OF DIGITAL PROCESSES FOR NON-DESTRUCTIVE INSPECTIONS OF AIRCRAFT STRUCTURES | ICAS2024_0125 |
| Koschlik, A.-K. | CINNABAR PROJECT - AUGMENTED REALITY WORKFLOW FOR AIRCRAFT DENT & BUCKLE INSPECTION | ICAS2024_0152 |
| Koschlik, A.-K. | CINNABAR PROJECT: EXAMINING REQUIREMENTS FOR USER ACCEPTANCE OF AIRCRAFT STRUCTURE INSPECTION IN AUGMENTED REALITY | ICAS2024_0164 |
| Koschlik, K.K. | HARNESSING THE POWER OF METAVERSE TO REVOLUTIONIZE AIRCRAFT AND MRO RESEARCH | ICAS2024_1327 |
| Kotsonis, M. | METAMATERIALS FOR CONTROL OF FLUID FLOWS | ICAS2024_1234 |
| Kotzem, M. | CONCEPTUAL AIRCRAFT DESIGN OF A RESEARCH BASELINE WITH DIRECT LIQUID HYDROGEN COMBUSTION | ICAS2024_0503 |
| Kou, J. | EFFICIENT MULTI-FIDELITY REDUCED-ORDER MODELING FOR FLUTTER PREDICTIONS ACROSS MULTIPLE MACH NUMBERS | ICAS2024_0900 |
| Kou, J. | DYNAMIC STALL PREDICTION THROUGH COMBINING PHYSICAL MODELS AND MACHINE LEARNING | ICAS2024_1080 |
| Kou, J. | TRANSFER LEARNING FOR REDUCED-ORDER MODELING OF TRANSONIC FLOWS USING MULTIFIDELITY DATA | ICAS2024_1110 |
| Kovar, P. | PREDICTION OF TRANSIENT DEFORMATION BY COUPLING CFD AND FEM ANALYSIS USING MACHINE LEARNING BASED CORRELATION FUNCTION | ICAS2024_1084 |
| Kovar, P. | ABOUT MODELLING OF EMPIRICAL CORRELATIONS WITHIN AERODYNAMIC PROFILES USING HIGHER ORDER ARTIFICIAL NEURAL NETWORKS | ICAS2024_1150 |
| Kramar, V. | ENHANCING PUBLIC GOOD MISSIONS AND DISASTER RESPONSE WITH ADVANCED AERIAL TECHNOLOGY: OPPORTUNITIES AND CHALLENGES | ICAS2024_1259 |
| Krause, D. | DIGITALISATION AND SUSTAINABILITY IN CABIN DESIGN: SYNERGIES AND DEPENDENCIES | ICAS2024_0165 |
| Krause, D. | TOWARDS A HOLISTIC APPROACH TO INCREASE SUSTAINABILITY IN AIRCRAFT CABIN DESIGN | ICAS2024_0511 |
| Krause, S. | ASSISTED AND AUTOMATED AERIAL REFUELLING – OVERVIEW OF THE CONDUCTED RESEARCH AT THE GERMAN AEROSPACE CENTER (DLR) | ICAS2024_0819 |
| Krein, A. | SUSTAINABLE AVIATION TECHNOLOGY PROGRAMMES IN EUROPE | ICAS2024_1253 |
| Kriebel, L. | DLR DESIGN CHALLENGE 2024: DESIGN OF A COST AND ENERGY EFFICIENT REGIONAL AIRCRAFT | ICAS2024_1264 |
| Kriewall, V. | TECHMAPS – TECHNOLOGY MANAGEMENT FOR THE ARCHITECTING PROCESS OF AIRCRAFT ON-BOARD SYSTEMS | ICAS2024_0053 |
| Kriewall, V. | ESTABLISHING THE DLR-F25 AS A RESEARCH BASELINE AIRCRAFT FOR THE SHORT-MEDIUM RANGE MARKET IN 2035 | ICAS2024_0398 |
| Kroll, L. | SIMULATION AND VERIFICATION OF HYDRAULIC ROTOR GAP PARAMETERS OF A NOVEL HIGH EFFICIENT WET ELECTRO MOTOR PUMP FOR AEROSPACE APPLICATIONS | ICAS2024_0123 |
| Krupko, A. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Krus, P. | LARGE LANGUAGE MODEL-DRIVEN SIMULATIONS FOR SYSTEM OF SYSTEMS ANALYSIS IN FIREFIGHTING AIRCRAFT CONCEPTUAL DESIGN | ICAS2024_0346 |
| Krus, P. | A HUMAN-CENTERED SYSTEMS ENGINEERING APPROACH FOR INTEGRATING ARTIFICIAL INTELLIGENCE IN AVIATION: A REVIEW OF AI SYSTEMS | ICAS2024_0397 |
| Krus, P. | LARGE LANGUAGE MODEL IN AIRCRAFT SYSTEM DESIGN | ICAS2024_0514 |
| Krüger, T. | APPLYING MODEL-BASED SYSTEM ENGINEERING AND DEVOPS ON THE IMPLEMENTATION OF AN AI-BASED COLLISION AVOIDANCE SYSTEM | ICAS2024_0869 |
| Krüger, W.R. | SANDWICH COMPOSITES SKIN PANEL OPTIMIZATION FOR THE COMMON RESEARCH MODEL WING | ICAS2024_0479 |
| Krzyzak, A. | ANALYSIS OF THE POSSIBILITY OF INCREASING THE THERMAL RESISTANCE OF EPOXY RESIN WITH CWNT AND MMT | ICAS2024_0275 |
| Krzyzak, A. | EFFECT OF INFILL STYLE AND DENSITY ON SELECTED MECHANICAL PROPERTIES OF THE CARBON FIBRE REINFORCED ABS MFD FILAMENT | ICAS2024_0806 |
| Ksiazek, N. | CHALLENGES OF INTEGRATING PHOTOVOLTAIC CELLS ONTO THE WINGS OF AN UNMANNED SOLAR-POWERED AIRCRAFT | ICAS2024_1132 |
| Kuang, S. | INTEGRITY MONITORING OF TIGHTLY INTEGRATED BDS/SINS USING MULTI-HYPOTHESIS SOLUTION SEPARATION (MHSS) ALGORITHM | ICAS2024_0244 |
| Kuchar, R. | FAILURE HANDLING ON A SPLIT-FLAP ULTRALIGHT GENERAL AVIATION AIRCRAFT WITH HYBRID NONLINEAR DYNAMIC INVERSION | ICAS2024_0467 |
| Kuchar, R. | MIXED FLIGHT CONTROL LAYOUT FOR ULTRALIGHT GENERAL AVIATION AIRCRAFT | ICAS2024_0517 |
| Kuchar, R.O. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Kuelper, N. | TECHMAPS – TECHNOLOGY MANAGEMENT FOR THE ARCHITECTING PROCESS OF AIRCRAFT ON-BOARD SYSTEMS | ICAS2024_0053 |
| Kugler, L. | DLR DESIGN CHALLENGE 2024: DESIGN OF A COST AND ENERGY EFFICIENT REGIONAL AIRCRAFT | ICAS2024_1264 |
| Kulkarni, M.D. | SEMI-ANALYTICAL SENSITIVITY METHODS FOR AEROELASTIC SHAPE OPTIMIZATION | ICAS2024_0666 |
| Kunwar, B. | INTEGRATED SIZING OF AN ELECTRIFIED TILT-WING AIRCRAFT FOR VERTICAL AND CONVENTIONAL TAKEOFF AND LANDING | ICAS2024_1170 |
| Kurniawan, J.L. | A NOVEL APPROACH TO AUTOMATED TRACKING CONTROL OF HYBRID TILTING ROTOR UAVS USING LQG CONTROLLER AND STATE MACHINE | ICAS2024_0535 |
| Kurniawan, J.L. | SURROGATE MODELING OF VORTEX SHEDDING TURBINE IN LOW REYNOLDS NUMBER | ICAS2024_0791 |
| Kurtulus, D.F. | ON THE AERODYNAMIC CHARACTERISTICS OF CRESCENT WING | ICAS2024_0579 |
| Kute, I. | AN AUTONOMOUS SYSTEM FOR DOCKING AND BATTERY SWAPPING IN UAVS | ICAS2024_1116 |
| Kwiatkowski, T. | THERMAL HISTORY PAINT UNDER HIGH SUBSONIC FLOW | ICAS2024_0316 |
| Kwiek, A. | STUDY ON CONFIGURATIONS OF AIRBORNE LAUNCH SYSTEM FOR DELIVERY OF SMALL PAYLOAD TO LOW EARTH ORBIT | ICAS2024_0355 |
| Kwiek, A. | RAPID DESIGN OF UNCONVENTIONAL AIRCRAFT USING SOFTWARE TOOLS COUPLED IN OPTIMIZATION LOOP – LESSONS LEARNED | ICAS2024_0496 |
| Köhler, P. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| König, A. | ADVANCING URBAN AIR MOBILITY: COLLABORATIVE EXCELLENCE AND INFRASTRUCTURE INITIATIVES BY DLR | ICAS2024_1223 |
| Könözsy, L. | NUMERICAL SOLUTION OF LOX FLOW IN A LIQUID ROCKET ENGINE ADDITIVELY MANUFACTURED COOLING CHANNEL | ICAS2024_0105 |
| Köster, F. | APPLYING MODEL-BASED SYSTEM ENGINEERING AND DEVOPS ON THE IMPLEMENTATION OF AN AI-BASED COLLISION AVOIDANCE SYSTEM | ICAS2024_0869 |
| Lacy, D.S. | CHALLENGES IN GEOMETRY DEVELOPMENT FOR THE CRM-HL ECOSYSTEM | ICAS2024_1212 |
| Laera, D. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF NOISE GENERATION IN HYDROGEN AND METHANE-HYDROGEN LAMINAR FLAMES | ICAS2024_1129 |
| Lahmam, Z. | HYDROGEN TANKERING: TOOLS FOR ECONOMIC AND ENVIRONMENTAL IMPACT SCENARIO STUDIES | ICAS2024_0993 |
| Lamkin, A.H.R. | DUCTED HEAT EXCHANGER THERMAL AND AERODYNAMIC SHAPE OPTIMIZATION | ICAS2024_0080 |
| Lamkin, A.H.R. | SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION | ICAS2024_0465 |
| Lammering, T. | DEVELOPMENT OF AN ELECTRO-HYDROSTATIC NOSE LANDING GEAR ACTUATION AND STEERING SYSTEM | ICAS2024_0146 |
| Lampani, L. | IMPROVING SHAPE SENSING OF AERONAUTICAL STRUCTURES WITH STRAIN PRE-EXTRAPOLATION AND SENSOR PLACEMENT OPTIMIZATION | ICAS2024_0654 |
| Lang, X. | NUMERICAL SIMULATION STUDY ON THE INFLUENCE OF WING SPACING OF DRAGONFLY-INSPIRED FLAPPING WINGS | ICAS2024_0243 |
| Lang, X.-Y. | INFLUENCE OF REINFORCED TRAILING EDGE ON FLAPPING WING AERODYNAMIC FORCE AND DEFORMATION | ICAS2024_0526 |
| Langford, J.F. | INTEGRATING ACTIVE FLOW CONTROL ON AIRCRAFT | ICAS2024_1312 |
| Lannoo, A. | DEVELOPMENT OF A MASS EVALUATION TOOL FOR CLASSICAL AND DISRUPTIVE AIRCRAFT STRUCTURES | ICAS2024_0115 |
| Lannoo, A. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Lara, G. | DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS | ICAS2024_0229 |
| Laricchiuta, A. | ASSESSMENT OF A MACROSCOPIC MODEL FOR THE AEROTHERMODYNAMICS CHARACTERIZATION OF ICE GIANTS ATMOSPHERIC ENTRY | ICAS2024_0872 |
| Larsen, L. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Lau, A. | MITIGATING THE CLIMATE IMPACT OF AVIATION BY OPERATIONAL MEANS - A COMPARATIVE STUDY FOR DIFFERENT WEATHER SITUATIONS | ICAS2024_0096 |
| Lau, A. | COMPARING CONVECTIVE WEATHER IMPACTS ON AIR TRAFFIC MANAGEMENT OPERATIONS IN UNITED STATES, CANADA & EUROPE | ICAS2024_0137 |
| Lau, A. | ROUTE PLANNING FOR VOLCANIC ASH AND RADIOACTIVITY IN-SITU DRONE MEASUREMENTS USING A GENETIC ALGORITHM AND KRIGING | ICAS2024_0406 |
| Laukotka, F.N. | DIGITALISATION AND SUSTAINABILITY IN CABIN DESIGN: SYNERGIES AND DEPENDENCIES | ICAS2024_0165 |
| Lawson, C. | DESIGN OF THE SENECA MACH 1.8 SUPERSONIC AIRLINER WITH MULTI-FIDELITY AERODYNAMIC ANALYSIS FOR NOISE-OPTIMISED TAKE-OFF TRAJECTORIES | ICAS2024_0758 |
| Lawson, N.J. | HOT-WIRE ANEMOMETRY OF THE BOUNDARY LAYER PRIOR TO A CAVITY IN RESPONSE TO VARIED UPSTREAM GEOMETRY | ICAS2024_0023 |
| Lawson, N.J. | SURFACE VISUALISATION OF TIME AVERAGED FLOW BEHAVIOUR AROUND RIGID AND FLEXIBLE HEMISPHERES UTILISING UV SENSITIVE OIL | ICAS2024_0070 |
| Lawson, N.J. | MEASUREMENT OF WING BENDING IN-FLIGHT FROM A T67 SLINGSBY FIREFLY LIGHT AIRCRAFT | ICAS2024_0140 |
| Lawson, N.J. | DESIGN OF A WIND TUNNEL MODEL FOR A REUSABLE LAUNCH VEHICLE DURING ITS LANDING BURN | ICAS2024_0188 |
| Lawson, N.J. | COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A DIRECT AIR CAPTURE FILTER SYSTEM | ICAS2024_0463 |
| Lawson, N.J. | AEROACOUSTIC CAVITY FLOW ENERGY HARVESTING | ICAS2024_0558 |
| Le Dantec, S. | TOWARDS TRUSTWORTHY DATA-DRIVEN GAS TURBINE PROGNOSTICS | ICAS2024_0793 |
| Leanza, D. | CORUS-XUAM: TACKLING URBAN AIR MOBILITY AIRSPACE INTEGRATION CHALLENGES | ICAS2024_0347 |
| Leblanc, G. | ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD | ICAS2024_1280 |
| Lee, C. | MISSION-BASED OPTIMAL PROPELLER SELECTION FOR VTOL SUAV CONFIGURATION | ICAS2024_0564 |
| Lee, C.-H. | TRAJECTORY OPTIMIZATION FOR LONG-RANGE AIR-LAUNCHED GLIDING VEHICLES USING CONVEX PROGRAMMING | ICAS2024_0468 |
| Lee, C.-H. | PURSUIT-BASED LONG-RANGE AIR-TO-AIR MISSILE MIDCOURSE GUIDANCE ROBUST TO CHANGES IN THE PREDICTED IMPACT POINT | ICAS2024_0828 |
| Lee, C.-H. | CONVEX PROGRAMMING APPROACH OF ROBUST POWERED DESCENT GUIDANCE THROUGH DYNAMIC TUBE MPC | ICAS2024_0839 |
| Lee, C.-H. | DOWNRANGE CONTROL GUIDANCE FOR REENTRY BURN OF REUSABLE LAUNCH VEHICLE | ICAS2024_0892 |
| Lee, D. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Lee, D.-W. | DATA-DRIVEN MODEL DISCOVERY AND CONTROL OF HIGH-PERFORMANCE TRAINER AIRCRAFT VIA SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS | ICAS2024_0627 |
| Lee, D.-W. | AERODYNAMIC MODEL IDENTIFICATION OF A VTOL TAILSITTER UAV USING SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS | ICAS2024_0653 |
| Lee, E.-H. | DEVELOPMENT OF A SERVO-DRIVEN FLAPPING-WING AIR VEHICLE WITH FOLDING-WING MECHANISM | ICAS2024_0477 |
| Lee, H. | A COMPARSION OF TRAJECTORY GENERATION ALGORITHMS FOR A TERRAIN FOLLOWING FLIGHT | ICAS2024_0424 |
| Lee, H. | DEVELOPMENT OF THRUST CONTROL SYSTEM FOR SPACECRAFT’S DOCKING MANEUVER | ICAS2024_0425 |
| Lee, H. | DEVELOPMENT OF THRUST CONTROL SYSTEM FOR SPACECRAFT’S DOCKING MANEUVER | ICAS2024_0425 |
| Lee, H.-S. | AERODYNAMIC MODEL IDENTIFICATION OF A VTOL TAILSITTER UAV USING SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS | ICAS2024_0653 |
| Lee, J.-W. | ENHANCED AIRCRAFT TAKEOFF/LANDING SAFETY USING DEEP LEARNING MODEL IN RUNWAY ASSISTANCE SYSTEM | ICAS2024_0786 |
| Lee, J.C. | WHAT-IF SCENARIO ANALYSIS OF REGIONAL AIR MOBILITY OPERATIONS IN SOUTH KOREA | ICAS2024_0850 |
| Lee, S. | A COMPARSION OF TRAJECTORY GENERATION ALGORITHMS FOR A TERRAIN FOLLOWING FLIGHT | ICAS2024_0424 |
| Lee, S. | DEVELOPMENT OF THRUST CONTROL SYSTEM FOR SPACECRAFT’S DOCKING MANEUVER | ICAS2024_0425 |
| Lee, S.-G. | ASPECT RATIO AND ADVANCE RATIO EFFECTS ON AERODYNAMIC CHARACTERISTICS OF FLEXIBLE FLAPPING WINGS | ICAS2024_0333 |
| Lee, S.-G. | DEVELOPMENT OF A SERVO-DRIVEN FLAPPING-WING AIR VEHICLE WITH FOLDING-WING MECHANISM | ICAS2024_0477 |
| Lee, Y. | LEARNING-BASED FULL-ENVELOPE AUTOPILOT DESIGN BASED ON THE KOOPMAN OPERATOR THEORY | ICAS2024_0043 |
| Lefebvre, T. | EU IMPACT MONITOR PROJECT - OVERVIEW AND APPROACH | ICAS2024_1114 |
| Lefebvre, T. | COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH | ICAS2024_1138 |
| Lehmann, O. | DESIGNING A FRAMEWORK FOR FLIGHT SIMULATOR TRAINING SCENARIOS. AN EVIDENCE BASED TRAINING APPROACH. | ICAS2024_1098 |
| Lei, Z. | POTENTIAL OF THE RANGE EXTENSION OF SUPERSONIC TRANSPORT | ICAS2024_0566 |
| Lekzian, E. | APPLICATION OF LAMBDA FRAMEWORK FOR AIRCRAFT MULTIDISCIPLINARY DESIGN, ANALYSIS AND OPTIMIZATION | ICAS2024_0068 |
| Lemetti, A. | COMPARING CONVECTIVE WEATHER IMPACTS ON AIR TRAFFIC MANAGEMENT OPERATIONS IN UNITED STATES, CANADA & EUROPE | ICAS2024_0137 |
| Lemmens, Y. | HARDWARE-IN-THE-LOOP SIMULATION FRAMEWORK FOR THE EVALUATION OF AUTONOMOUS FLIGHT FUNCTIONS | ICAS2024_0897 |
| Lerro, A. | PRELIMINARY DESIGN OF A FULL ELECTRIC GENERAL AVIATION AIRCRAFT POWERED WITH FUEL CELL: A CASE STUDY. | ICAS2024_1207 |
| Lessis, A. | ON THE WATER ENHANCED TURBOFAN CONCEPT: PART A - THERMODYNAMICS AND OVERALL ENGINE DESIGN | ICAS2024_0199 |
| Levati, E. | A BOUNDARY INTEGRAL EQUATION FORMULATION FOR POTENTIAL COMPRESSIBLE FLOWS AROUND DEFORMABLE BODIES | ICAS2024_0676 |
| Leyland, P. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Li, A. | MANNED AND UNMANNED AERIAL VEHICLES COOPERATIVE COMBAT FRAMEWORK BASED ON LARGE LANGUAGE MODELS | ICAS2024_0231 |
| Li, A.J. | ROBUST SLIDING MODE CONTROL FOR UAV FORMATION WITH EXTERNAL DISTURBANCES UNDER EVENT-TRIGGERED STRATEGY | ICAS2024_0013 |
| Li, C. | SPARSE RECONSTRUCTION OF SURFACE LOADS ON AIRCRAFT USING POD AND RBFNN | ICAS2024_0634 |
| Li, C. | AN UNCERTAINTY MULTIDISCIPLINARY PROPAGATION ANALYSIS METHOD FOR CORRELATED HIGH-DIMENSIONAL DATA IN AIRCRAFT DESIGN | ICAS2024_0696 |
| Li, C. | MULTI-FIDELITY SURROGATE MODELING BASED ON DATA EXTENSION USING POD AND ANN | ICAS2024_0957 |
| Li, C.N. | A DISTRIBUTED UMDO ARCHITECTURE BASED ON SURROGATE MODELS FOR LAUNCH VEHICLE DESIGN | ICAS2024_0626 |
| Li, C.P. | DESIGN OF DUAL-FUSELAGE FLIGHT PLATFORM FOR JET CONTROL FUNCTION VERIFICATION | ICAS2024_0812 |
| Li, C.R. | A NOLINEAR MODEL PREDICTIVE CONTROL METHOD FOR AIRBREATHING HYPERSONIC VEHICLE BASED ON KOOPMAN OPERATOR | ICAS2024_1119 |
| Li, D. | AERODYNAMIC OPTIMIZATION OF HIGH-ALTITUDE PROPELLER COMBINED WITH MACHINE LEARNING METHOD | ICAS2024_0342 |
| Li, D. | RESEARCH ON EFFICIENT ACTIVE T-S WAVE GENERATION METHOD IN BOUNDARY LAYER | ICAS2024_0543 |
| Li, D. | LONG-WAVE INSTABILITY OF AIRCRAFT WAKE VORTEX UNDER SHEAR CROSSWIND | ICAS2024_0551 |
| Li, D. | MEASUREMENTS OF T-S WAVES DUE TO ACOUSTIC DISTURBANCES IN EXPERIMENTS | ICAS2024_0682 |
| Li, D.-B. | A METHOD FOR OPTIMISING THE ARRANGEMENT OF INTERNAL CHANNELS IN AIRCRAFT HYDRAULIC MANIFOLDS MANUFACTURED BY ADDITIVE MANUFACTURING | ICAS2024_0933 |
| Li, D.-B. | ULTRA-LOW-ALTITUDE PENETRATION PATH PLANNING FOR FIXED-WING AIRCRAFT BASED ON NMP ALGORITHM | ICAS2024_0972 |
| Li, F. | TRANSITION MODELING IN SUPPORT OF CFD VISION 2030 - HIGHLIGHTS OF RECENT EFFORTS AT THE NASA LANGLEY RESEARCH CENTER | ICAS2024_0081 |
| Li, G. | NUMERICAL SIMULATION OF HEAT TRANSFER IN MINIATURE RADIALLY ROTATING SODIUM/POTASSIUM HEAT PIPES | ICAS2024_0323 |
| Li, G. | A METHOD FOR AUTOMATIC GENERATING SAFETY ANALYSIS BASED ON AVIATION PISTON ENGINE MODEL | ICAS2024_0587 |
| Li, G. | SENSITIVITY ANALYSIS OF SAFETY FACTORS BASED ON MODEL OF AVIATION RECIPROCATING ENGINE TURBOCHARGING SYSTEM | ICAS2024_0599 |
| Li, G. | A HIGH-PRECESION PSEUDO ARC-LENGTH METHOD WITH POSITIVE VALUE PRESERVATION PROPERTIES BASED ON TV SPLITTING | ICAS2024_0694 |
| Li, G. | FUZZING ON TARGET DETECTION SYSTEM OF UNMANNED AERIAL VEHICLE | ICAS2024_0794 |
| Li, G.-D. | CONFIGURATION ANALYSIS OF INTEGRATED THERMAL MANAGEMENT BASED ON THE TURBINE-FAN REFRIGERATION SYSTEM | ICAS2024_0194 |
| Li, G.-M. | THE DESIGN FOR TESTABILITY OF CIVIL AIRCRAFT AVIONICS SYSTEMS | ICAS2024_0033 |
| Li, H. | REDESIGN AND MACHINING OF LEADING EDGE OF TRANSONIC COMPRESSOR BLADE IN ROBOTIC GRINDING OPERATION | ICAS2024_0260 |
| Li, J. | SYSTEM ARCHITECTURE AND EVALUATION METHOD OF HUMAN-MACHINE COLLABORATION IN FLIGHT CONTROL SYSTEM | ICAS2024_0185 |
| Li, J. | A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION | ICAS2024_0314 |
| Li, J. | DATA-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION AND MULTI-FIDELITY DESIGN EXPLORATION USING CONDITIONAL DIFFUSION-BASED GEOMETRY SAMPLING METHOD | ICAS2024_0431 |
| Li, J. | DESIGN OF ATTITUDE CONTROL SYSTEM FOR DRAGONFLY-INSPIRED FLAPPING WING AERIAL VEHICLE | ICAS2024_0578 |
| Li, J. | DYNAMICS ANALYSIS AND CONTROL OF A LARGE WINGSPAN FLAPPING-WING VEHICLE | ICAS2024_0621 |
| Li, J.-J. | EFFECTS OF PROCESSING STRATEGIES ON SURFACE QUALITY AND MECHANICAL PROPERTIES IN HYBRID ADDITIVE MANUFACTURING OF IN718 ALLOY | ICAS2024_0593 |
| Li, J.-Y. | ANALYSIS OF SUCTION FORCE EFFECT ON DIFFERENT FUSELAGE SHAPE DURING THE WATER DITCHING | ICAS2024_0929 |
| Li, J.-Y. | RESEARCH ON AERODYNAMIC PERFORMANCE OF OVERSIZE MODULAR PARAFOIL IN RANDOM WIND FIELD | ICAS2024_0952 |
| Li, J.Z. | AIRFOIL PRESSURE PREDICTION BASED ON PHYSICS-INFORMED DEEP LEARNING APPROACH | ICAS2024_1036 |
| Li, K. | SURFACE MORPHOLOGY AND MICROSTRUCTURAL FEATURES OF ELECTRON BEAM SURFI-SCULPTED TI-6AL-4V ALLOY | ICAS2024_0262 |
| Li, K. | STABLE LOCALIZED CORROSION IN A 7075-T6 ALUMINUM ALLOY FSW JOINT: MECHANISM AND MITIGATION | ICAS2024_0300 |
| Li, K. | AN UAV MANEUVERING DECISION-MAKING ALGORITHM BASED ON DEEP TRANSFER REINFORCEMENT LEARNING | ICAS2024_1020 |
| Li, L. | INVESTIGATION ON THE MECHANISM OF THERMAL CYCLING FAILURE IN C/SIC COATING COMPOSITE MATERIALS | ICAS2024_0796 |
| Li, L.W. | EFFECTS OF SHAPE AND STREAMWISE SPACING OF PIN-FINS ARRAYS ON FLOW AND HEAT TRANSFER | ICAS2024_0720 |
| Li, M. | MODELING AND ANALYSIS OF ELECTRO-HYDROSTATIC ACTUATORS EFFICIENCY | ICAS2024_1043 |
| Li, M.C. | THERMAL AND GRINDING PERFORMANCE OF 3D PRINTED COMPLIANCE GRINDING TOOLS WITH ROTARY-ENHANCED HEAT TRANSFER STRUCTURE | ICAS2024_0248 |
| Li, M.Z. | OPTIMIZING FLEET ASSIGNMENT DECISIONS FOR REGIONAL AIRLINES WITH HYBRID ELECTRIC AIRCRAFT UPTAKE | ICAS2024_0781 |
| Li, M.Z. | PROBING AND MODELING LARGE-SCALE AIRLINE NETWORK DISRUPTIONS: 2022 SOUTHWEST AIRLINES SCHEDULING CRISIS | ICAS2024_0782 |
| Li, N. | DYNAMIC DROP SIMULATION OF THE MAIN LANDING GEAR OF A GENERAL AVIATION AIRCRAFT | ICAS2024_0588 |
| Li, P. | RESEARCH ON EFFICIENT ACTIVE T-S WAVE GENERATION METHOD IN BOUNDARY LAYER | ICAS2024_0543 |
| Li, P. | A HIGH-PRECESION PSEUDO ARC-LENGTH METHOD WITH POSITIVE VALUE PRESERVATION PROPERTIES BASED ON TV SPLITTING | ICAS2024_0694 |
| Li, P.-F. | EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN | ICAS2024_0962 |
| Li, P.F. | MEASUREMENTS OF T-S WAVES DUE TO ACOUSTIC DISTURBANCES IN EXPERIMENTS | ICAS2024_0682 |
| Li, Q. | KINETIC MONTE CARLO BASED CATALYTIC VISCOUS WALL BOUNDARY MODELING IN CFD SIMULATION OF HIGH-ENTHALPY NON-EQUILIBRIUM FLOW | ICAS2024_0276 |
| Li, Q. | NUMERICAL STUDY OF FLOWS OVER LAUNCH VEHICLES WITH VARIOUS FAIRING BY SECOND-MOMENT CLOSURE DETACHED-EDDY SIMULATION | ICAS2024_0641 |
| Li, Q.-L. | AERODYNAMIC DEFORMATION EXPERIMENT OF SERPENTINE NOZZLE FOR TURBOFAN AND ANALYSIS OF FLUID-STRUCTURE INTERACTION METHOD | ICAS2024_0919 |
| Li, Q.Z. | NUMERICAL INVESTIGATION OF THE INTERACTION OF OPPOSING JETS AND SUPERSONIC FREE FLOWS | ICAS2024_0783 |
| Li, R. | AN IMPROVED END-TO-END STAR MAP RECOGNITION METHOD FOR AEROSPACE VEHICLE | ICAS2024_0697 |
| Li, S. | MANNED AND UNMANNED AERIAL VEHICLES COOPERATIVE COMBAT FRAMEWORK BASED ON LARGE LANGUAGE MODELS | ICAS2024_0231 |
| Li, S. | MANNED AND UNMANNED AERIAL VEHICLES COOPERATIVE COMBAT FRAMEWORK BASED ON LARGE LANGUAGE MODELS | ICAS2024_0231 |
| Li, S. | STUDY ON FATIGUE PROPERTIES OF TITANIUM ALLOY BASE MATERIAL AND WELDED STRUCTURE IN THERMAL COMBINED ENVIRONMENT | ICAS2024_0422 |
| Li, W.Q. | A NOLINEAR MODEL PREDICTIVE CONTROL METHOD FOR AIRBREATHING HYPERSONIC VEHICLE BASED ON KOOPMAN OPERATOR | ICAS2024_1119 |
| Li, X. | RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS | ICAS2024_0550 |
| Li, X.-C. | ANALYSIS OF AERODYNAMIC INTERFERENCE CHARACTERISTICS AND AEROACOUSTICS FOR HIGH-SPEED COMPOSITE HELICOPTER IN HOVER | ICAS2024_0704 |
| Li, X.-H. | RESEARCH ON AERODYNAMIC DESIGN OF ENGINE NACELLE UNDER THE INFLUENCE OF PROPELLER SLIPSTREAM FOR THE TURBOPROP AIRCRAFT | ICAS2024_0605 |
| Li, X.-L. | RESEARCH ON AERODYNAMIC DESIGN OF ENGINE NACELLE UNDER THE INFLUENCE OF PROPELLER SLIPSTREAM FOR THE TURBOPROP AIRCRAFT | ICAS2024_0605 |
| Li, X.-L. | NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF HOVERING ROTOR IN GROUND EFFECT | ICAS2024_0655 |
| Li, X.Y. | WALL TEMPERATURE EFFECTS ON AERODYNAMIC HEATING MECHANISMS IN SHOCK WAVE TURBULENT BOUNDARY LAYER INTERACTION | ICAS2024_0569 |
| Li, Y. | SIMULATION STUDY ON AERODYNAMIC CHARACTERISTICS OF COMBINED LOW ASPECT RATIO UAV | ICAS2024_0449 |
| Li, Y. | HIGH-VELOCITY DROPLET IMPACT STUDIES ON C/SIC AND C/C COMPOSITES | ICAS2024_0808 |
| Li, Y. | ATTITUDE ESTIMATION USING KALMAN FILTERING FOR SPACEBORNE SAR SYSTEMS | ICAS2024_0866 |
| Li, Y. | AN UAV MANEUVERING DECISION-MAKING ALGORITHM BASED ON DEEP TRANSFER REINFORCEMENT LEARNING | ICAS2024_1020 |
| Li, Y. | A NOLINEAR MODEL PREDICTIVE CONTROL METHOD FOR AIRBREATHING HYPERSONIC VEHICLE BASED ON KOOPMAN OPERATOR | ICAS2024_1119 |
| Li, Y.-H. | NUMERICAL SIMULATION OF THE RESPONSE CHARACTERISTICS OF THE WING STRUCTURE OF A SEAPLANE PLANING IN WAVE | ICAS2024_0901 |
| Li, Y.-L. | MODELING THE TEMPERATURE-RISE BEHAVIOR OF 2D TRIAXIAL BRAIDED COMPOSITES UNDER IMPACT LOADS | ICAS2024_0215 |
| Li, Y.M. | FLUID-STRUCTURE INTERACTION OF TWO-PHASE SCATTERER METAMATERIALS FOR VIBRATION SELF-SUPPRESSION | ICAS2024_0435 |
| Li, Z. | FAST PREDICTION METHOD FOR RADIAL GROWTH OF LABYRINTH SEAL CLEARANCE BASED ON TRANSIENT THERMAL-FLUID COUPLING NETWORK | ICAS2024_0450 |
| Li, Z.-D. | RESEARCH ON AERODYNAMIC PERFORMANCE OF OVERSIZE MODULAR PARAFOIL IN RANDOM WIND FIELD | ICAS2024_0952 |
| Li, Z.-H. | ANALYSIS ON COMPLEX HYPERSONIC FLOW DURING THE REENTRY OF EXPIRED SPACECRAFT | ICAS2024_0644 |
| Li, Z.Q. | DYNAMIC DROP SIMULATION OF THE MAIN LANDING GEAR OF A GENERAL AVIATION AIRCRAFT | ICAS2024_0588 |
| Lian, Y.-J. | TRAJECTORY DESIGN FOR ASTEROID SAMPLE RETURN COMBINING BALLISTIC CAPTURE AND AEROBRAKING | ICAS2024_1070 |
| Liang, M. | ASSESSMENT OF A HIGHLY PARAMETERIZED STEADY-STATE MICROSCALE WIND SIMULATOR FOR URBAN AIR MOBILITY APPLICATIONS | ICAS2024_0379 |
| Liang, Z.-H. | REDUCED ORDER MODELLING OF UNSTEADY AERODYNAMICS FOR GROUND FLUTTER TEST SYSTEM | ICAS2024_0430 |
| Liaño, G. | GRID EFFECT ON M823 BOMB AT TRANSONIC REGIME | ICAS2024_0031 |
| Liao, H.-H. | A METHOD FOR OPTIMISING THE ARRANGEMENT OF INTERNAL CHANNELS IN AIRCRAFT HYDRAULIC MANIFOLDS MANUFACTURED BY ADDITIVE MANUFACTURING | ICAS2024_0933 |
| Liberatori, J. | IMPACT OF WELL-TO-TANK EFFICIENCY AND EMISSIONS ON HYBRID AIRCRAFT DESIGN OPTIMIZATION | ICAS2024_0366 |
| Licheva, G. | CRYOGENIC TANK SIZING MODEL FOR THE CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT | ICAS2024_0193 |
| Lieder, D. | DESIGN APPROACH FOR HYBRID ELECTRIC PROPULSION CONCEPTS OF MID-RANGE AIRCRAFT INCLUDING SUSTAINABLE AVIATION FUELS | ICAS2024_1069 |
| Liem, R. | DATA-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION AND MULTI-FIDELITY DESIGN EXPLORATION USING CONDITIONAL DIFFUSION-BASED GEOMETRY SAMPLING METHOD | ICAS2024_0431 |
| Liem, R.P. | MISSION-BASED OPTIMAL PROPELLER SELECTION FOR VTOL SUAV CONFIGURATION | ICAS2024_0564 |
| Liem, R.P. | DATA-DRIVEN MULTI-RANGE MISSION-BASED OVERALL AIRCRAFT CONCEPTUAL DESIGN OPTIMIZATION | ICAS2024_0611 |
| Lim, L. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Lima da Silva, G.A. | INITIAL DEVELOPMENT OF A CFD ICING TOOL | ICAS2024_1112 |
| Lin, K. | A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION | ICAS2024_0314 |
| Lin, K.J. | LIGHT WEIGHT DESIGN AND LASER ADDITIVE MANUFACTURING OF METAL BIPOLAR PLATES FOR THE APPLICATION OF AIRCRAFT FUEL CELL | ICAS2024_0964 |
| Lin, R.-X. | EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN | ICAS2024_0962 |
| Lindlar, M. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Lindlar, M. | PILOT SAFETY – SUPPORT BY BIOMEDICAL MONITORING IN PILOTS WITH HEALTH RISKS | ICAS2024_0460 |
| Ling, M. | A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION | ICAS2024_0314 |
| Link, A. | PROJECTION OF KEY POWERTRAIN COMPONENT FIGURES OF MERIT FOR OVERALL ASSESSMENT OF ELECTRIC FLIGHT SCENARIOS | ICAS2024_1054 |
| Link, P. | ASSISTED AND AUTOMATED AERIAL REFUELLING – OVERVIEW OF THE CONDUCTED RESEARCH AT THE GERMAN AEROSPACE CENTER (DLR) | ICAS2024_0819 |
| Link, S. | CFD-BASED SCOUTING FOR THE DESIGN OF A MULTI-FUEL KEROSENE/HYDROGEN ATMOSPHERIC BURNER | ICAS2024_0432 |
| Liscouët-Hanke, S. | CRYOGENIC TANK SIZING MODEL FOR THE CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT | ICAS2024_0193 |
| Liu, B. | ELASTIC/PLASTIC SEMI-ANALYTICAL METHOD FOR ARBITRARY CURVED SURFACES OF SCARF REPAIRED COMPOSITES | ICAS2024_0544 |
| Liu, C. | A MOMENTUM-INTEGRAL METHOD TO CALCULATE WINDAGE LOSSES ON A ROTATING DRUM WITH SUPERPOSED FLOW | ICAS2024_0281 |
| Liu, C. | FAST PREDICTION METHOD FOR RADIAL GROWTH OF LABYRINTH SEAL CLEARANCE BASED ON TRANSIENT THERMAL-FLUID COUPLING NETWORK | ICAS2024_0450 |
| Liu, C.-P. | EFFECTS OF GEOMETRY PARAMETERS ON AERODYNAMIC CHARACTERISTICS OF ROTOR AIRFOIL IN REVERSE FLOW | ICAS2024_0607 |
| Liu, D. | AERODYNAMIC CHARACTERISTICS RESEARCH OF A DISTRIBUTED PROPULSION AIRCRAFT | ICAS2024_0537 |
| Liu, D. | ANALYSIS OF STEALTH ENHANCEMENT DESIGN PROCESS AND METHODS FOR UNMANNED AERIAL VEHICLE | ICAS2024_0568 |
| Liu, D. | ANALYSIS OF BATTERY WEIGHT REQUIREMENTS IN THE DESIGN OF HYBRID ELECTRIC POWERED AIRCRAFT | ICAS2024_0813 |
| Liu, D.N. | SEPARATION SAFETY ANALYSIS IN VARIABLE LAUNCH CONDITION OF SMALL AIR-LAUNCHED UAVS BASED ON NUMERICAL SIMULATION AND FLIGHT TEST | ICAS2024_0311 |
| Liu, H. | TRANSFORMATIVE PEDAGOGY: CO-TEACHING COURSE CLUSTERS THROUGH COMPETITIVE TEAM DESIGNS FOR INNOVATIVE TALENT DEVELOPMENT IN AEROSPACE EDUCATION | ICAS2024_0324 |
| Liu, H. | FUZZING ON TARGET DETECTION SYSTEM OF UNMANNED AERIAL VEHICLE | ICAS2024_0794 |
| Liu, H. | EFFICIENT MULTI-FIDELITY REDUCED-ORDER MODELING FOR FLUTTER PREDICTIONS ACROSS MULTIPLE MACH NUMBERS | ICAS2024_0900 |
| Liu, H. | AN UAV MANEUVERING DECISION-MAKING ALGORITHM BASED ON DEEP TRANSFER REINFORCEMENT LEARNING | ICAS2024_1020 |
| Liu, J. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AEROELASTICITY OF HIGH-ASPECT-RATIO WINGS | ICAS2024_0423 |
| Liu, J. | RESEARCH ON OPTIMAL TORSIONAL DEFORMATION OF FLAPPING WING | ICAS2024_0473 |
| Liu, J. | ANGLE AND DISTANCE EFFECT ON PHOSPHOR THERMOMETRY | ICAS2024_0529 |
| Liu, J. | ANGLE AND DISTANCE EFFECT ON PHOSPHOR THERMOMETRY | ICAS2024_0529 |
| Liu, J. | COMPUTATIONAL/EXPERIMENTAL AEROELASTIC STUDY FOR AN ALL-MOVABLE HORIZONTAL TAIL WITH TORSION FREE-PLAY | ICAS2024_0728 |
| Liu, J. | DEVELOPMENT AND ANALYSIS OF THE THEORY OF COMPOSITE EXPANSION RING UNDER ELECTROMAGNETIC LOADING | ICAS2024_0830 |
| Liu, J. | HIGH TEMPERATURE BALLISTIC IMPACT TEST TECHNOLOGY BASED ON ELECTROMAGNETIC LAUNCH | ICAS2024_0841 |
| Liu, L. | DEEP LEARNING BASED FAST PREDICTION OF AERODYNAMIC PARAMETERS FOR DUCTED PROPELLERS | ICAS2024_1011 |
| Liu, L.-Y. | LARGE-SCALE STRUCTURAL DYNAMIC TOPOLOGY OPTIMIZATION DESIGN FOR AIRCRAFT VIBRATION REDUCTION UNDER RANDOM EXCITING RESPONSE | ICAS2024_0365 |
| Liu, L.J. | DATA-DRIVEN MULTI-RANGE MISSION-BASED OVERALL AIRCRAFT CONCEPTUAL DESIGN OPTIMIZATION | ICAS2024_0611 |
| Liu, N. | DESIGN OF DUAL-FUSELAGE FLIGHT PLATFORM FOR JET CONTROL FUNCTION VERIFICATION | ICAS2024_0812 |
| Liu, P. | MODELING THE TEMPERATURE-RISE BEHAVIOR OF 2D TRIAXIAL BRAIDED COMPOSITES UNDER IMPACT LOADS | ICAS2024_0215 |
| Liu, P. | A MESO-SCALED SIMULATION ON THE THICKNESS EFFECT OF TWO-DIMENSIONAL TRIAXIALLY BRAIDED COMPOSITES UNDER TENSILE LOADS | ICAS2024_0259 |
| Liu, P. | A MOMENTUM-INTEGRAL METHOD TO CALCULATE WINDAGE LOSSES ON A ROTATING DRUM WITH SUPERPOSED FLOW | ICAS2024_0281 |
| Liu, P. | FAST PREDICTION METHOD FOR RADIAL GROWTH OF LABYRINTH SEAL CLEARANCE BASED ON TRANSIENT THERMAL-FLUID COUPLING NETWORK | ICAS2024_0450 |
| Liu, R. | INTEGRITY MONITORING OF TIGHTLY INTEGRATED BDS/SINS USING MULTI-HYPOTHESIS SOLUTION SEPARATION (MHSS) ALGORITHM | ICAS2024_0244 |
| Liu, W.-Z. | EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN | ICAS2024_0962 |
| Liu, X. | EFFECT OF LASER PRINTING MODE ON SURFACE TOPOGRAPHY, MICROSTRUCTURE AND CORROSION PROPERTY OF ADDITIVE-MANUFACTURED NITI | ICAS2024_0339 |
| Liu, X. | FLIGHT TEST AND CFD STUDY OF THE EFFECT OF WING BOUNDARY LAYER TRANSITION ON AILERON BALANCE | ICAS2024_0501 |
| Liu, X. | INVESTIGATION ON THE MECHANISM OF THERMAL CYCLING FAILURE IN C/SIC COATING COMPOSITE MATERIALS | ICAS2024_0796 |
| Liu, X. | MODELING AND FLIGHT CONTROL LAW DESIGN FOR A SEAPLANE DURING WATER SURFACE TAKEOFF | ICAS2024_0977 |
| Liu, X.-C. | A METHOD FOR OPTIMISING THE ARRANGEMENT OF INTERNAL CHANNELS IN AIRCRAFT HYDRAULIC MANIFOLDS MANUFACTURED BY ADDITIVE MANUFACTURING | ICAS2024_0933 |
| Liu, X.-C. | IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM | ICAS2024_1186 |
| Liu, Y. | WEAR EVOLUTION OF PYRAMID-STRUCTURED ABRASIVE BELTS AND ITS EFFECT ON GRINDING OPERATIONS | ICAS2024_0368 |
| Liu, Y. | ANALYSIS AND STUDY ON FLUTTER CHARACTERISTICS OF WINGS UNDER TYPICAL FRAGMENT DAMAGE | ICAS2024_0446 |
| Liu, Y. | ELASTIC/PLASTIC SEMI-ANALYTICAL METHOD FOR ARBITRARY CURVED SURFACES OF SCARF REPAIRED COMPOSITES | ICAS2024_0544 |
| Liu, Y. | A DISTRIBUTED UMDO ARCHITECTURE BASED ON SURROGATE MODELS FOR LAUNCH VEHICLE DESIGN | ICAS2024_0626 |
| Liu, Y. | AN UNCERTAINTY MULTIDISCIPLINARY PROPAGATION ANALYSIS METHOD FOR CORRELATED HIGH-DIMENSIONAL DATA IN AIRCRAFT DESIGN | ICAS2024_0696 |
| Liu, Y. | EXPERIMENTAL AND NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF A MARS ROTOR SYSTEM | ICAS2024_0790 |
| Liu, Y. | MODELING AND FLIGHT CONTROL LAW DESIGN FOR A SEAPLANE DURING WATER SURFACE TAKEOFF | ICAS2024_0977 |
| Liu, Y.-L. | TILT-DUCT AIRCRAFT WING AERODYNAMIC DESIGN AND OPTIMIZATION BASED ON ADJOINT METHOD | ICAS2024_0332 |
| Liu, Y.-L. | OPTIMIZATION OF COMPOSITE WING STRUCTURE FOR TILT-DUCT AIRCRAFT CONSIDERING DISCRETE AND CONTINUOUS DESIGN VARIABLES | ICAS2024_0405 |
| Liu, Y.L. | NUMERICAL INVESTIGATION OF THE INTERACTION OF OPPOSING JETS AND SUPERSONIC FREE FLOWS | ICAS2024_0783 |
| Liu, Z. | AN EXPERIMENTAL SIMULATION ON THE INFLUENCE OF DIFFERENT FILM COOLING HOLE SHAPES ON PARTICLE DEPOSITION ON TURBINE VANE | ICAS2024_0341 |
| Liu, Z. | AN EXPERIMENTAL SIMULATION ON THE INFLUENCE OF DIFFERENT FILM COOLING HOLE SHAPES ON PARTICLE DEPOSITION ON TURBINE VANE | ICAS2024_0341 |
| Liu, Z. | RESEARCH ON MULTI-ATTRIBUTE DECISION MAKING AND VERIFICATION METHODS FOR SYSTEMS CONFRONTATION | ICAS2024_0561 |
| Liu, Z. | EXPERIMENTAL STUDY ON MULTI-ATTITUDE OIL SUPPLY STRUCTURE | ICAS2024_0817 |
| Liu, Z. | MODELING AND ANALYSIS OF ELECTRO-HYDROSTATIC ACTUATORS EFFICIENCY | ICAS2024_1043 |
| Liu, Z. | DYNAMIC STALL PREDICTION THROUGH COMBINING PHYSICAL MODELS AND MACHINE LEARNING | ICAS2024_1080 |
| Liu, Z.-X. | STUDY OF THE SCAVENGE PUMP PERFORMANCE FOR TWO-PHASE FLOW IN AN AIRCRAFT ENGINE LUBRICATION SYSTEM | ICAS2024_0788 |
| Liu, Z.-X. | DEVELOPMENT AND ANALYSIS OF THE THEORY OF COMPOSITE EXPANSION RING UNDER ELECTROMAGNETIC LOADING | ICAS2024_0830 |
| Liu, Z.-X. | VOID FRACTION CALCULATION MODEL BASED ON TWO-PHASE FLOW PATTERNS IN THE SCAVENGE PIPE | ICAS2024_1010 |
| Liu, Z.-X. | A STUDY ON THE AIRLOCK MECHANISM OF THE OIL SUPPLY PUMP IN AERO-ENGINE LUBRICATING OIL SYSTEM | ICAS2024_1030 |
| Liu, Z.K. | NUMERICAL INVESTIGATION OF THE INTERACTION OF OPPOSING JETS AND SUPERSONIC FREE FLOWS | ICAS2024_0783 |
| Llewellyn, G. | TOWARDS ZERO CLIMATE IMPACT AVIATION | ICAS2024_1254 |
| lLyu, Y.-G. | EXPERIMENTAL STUDY ON MULTI-ATTITUDE OIL SUPPLY STRUCTURE | ICAS2024_0817 |
| Lo Cascio, M. | FREE VIBRATIONS OF CYLINDRICAL SHELLS WITH CUTOUTS BY A SINGLE-DOMAIN RITZ FORMULATION | ICAS2024_0832 |
| Lobuono, L. | UNSTEADY AERODYNAMICS OF A COUPLED COMPACT INTAKE-FAN IN CROSSWIND | ICAS2024_0263 |
| Logan, M.J. | APPLICATION OF UAS TECHNOLOGIES TO CREATE RESILIENT RURAL COMMUNITIES | ICAS2024_1300 |
| Lois, C. | CLIMATE IMPACT AND ECONOMIC ASSESSMENT OF LIQUID HYDROGEN AND SYNTHETIC KEROSENE LONG-RANGE AIRCRAFT CONCEPTS | ICAS2024_0399 |
| Lombardi, S. | EXPERIMENTAL VALIDATION OF THE DYNAMIC FINITE ELEMENT MODEL OF A 1:8 SCALE SEAPLANE USING A LASER DOPPLER VIBROMETER (LDV) | ICAS2024_0730 |
| Long, T. | SURROGATE-ASSISTED HIERARCHICAL OPTIMIZATION METHOD FOR VARIABLE SWEEP FLIGHT VEHICLE TRAJECTORY | ICAS2024_0825 |
| Long, Y. | EXPLORING A CATEGORY OF LIMIT CYCLE OSCILLATIONS IN AIRCRAFT HYDRAULIC SYSTEMS | ICAS2024_0932 |
| Looye, G. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Looye, G. | FAILURE HANDLING ON A SPLIT-FLAP ULTRALIGHT GENERAL AVIATION AIRCRAFT WITH HYBRID NONLINEAR DYNAMIC INVERSION | ICAS2024_0467 |
| Lopes, M.E.M.C. | INITIAL DEVELOPMENT OF A CFD ICING TOOL | ICAS2024_1112 |
| Lopez, A. | EFFICIENT SHAPE OPTIMIZATION IN AERONAUTICS: INTEGRATING PARAMETRIC CAD AND MESH MORPHING FOR ENHANCED AERODYNAMIC PERFORMANCE | ICAS2024_0824 |
| Lopusiewicz, R. | CHALLENGES OF INTEGRATING PHOTOVOLTAIC CELLS ONTO THE WINGS OF AN UNMANNED SOLAR-POWERED AIRCRAFT | ICAS2024_1132 |
| Losada Costoso, D. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Loukil, M.S. | THERMAL AND MECHANICAL CYCLING OF THIN-PLY COMPOSITES FOR CRYOGENIC APPLICATIONS | ICAS2024_1052 |
| Lovaco, J.L. | LARGE LANGUAGE MODEL-DRIVEN SIMULATIONS FOR SYSTEM OF SYSTEMS ANALYSIS IN FIREFIGHTING AIRCRAFT CONCEPTUAL DESIGN | ICAS2024_0346 |
| Lovera, M. | PASSIVE FAULT TOLERANT CONTROL OF A DUAL-SYSTEM UAV IN TRANSITION FLIGHT | ICAS2024_0570 |
| Lovero, F. | EXPERIMENTAL VALIDATION OF THE DYNAMIC FINITE ELEMENT MODEL OF A 1:8 SCALE SEAPLANE USING A LASER DOPPLER VIBROMETER (LDV) | ICAS2024_0730 |
| Lowe, K.T. | THE BEVERLI HILL EXPERIMENTS FOR SMOOTH-BODY TURBULENT FLOW SEPARATION - RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS | ICAS2024_1219 |
| Lozano, M. | DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS | ICAS2024_0229 |
| Lu, J. | A SEMANTIC MODEL-BASED SYSTEMS ENGINEERING APPROACH FOR SUPERSONIC BUSINESS JET CONCEPTUAL DESIGN | ICAS2024_0843 |
| Lu, P. | STABILITY CHARACTERISTICS OF CROSSFLOW MODES IN HYPERSONIC BOUNDARY LAYER WITH EXPANSION CORNER | ICAS2024_0576 |
| Lu, W. | MECHANISM STUDY ON THE IMPACT OF PULSED JET AT THE BLADE TIP LEADING EDGE ON THE FLOW FIELD IN COMPRESSOR | ICAS2024_0849 |
| Lu, Y. | NUMERICAL AND THEORETICAL INVESTIGATION OF HELICOPTER DITCHING WITH VARIOUS INITIAL VELOCITY AND PITCHING ANGLE | ICAS2024_0216 |
| Lu, Y. | ANALYSIS OF STEALTH ENHANCEMENT DESIGN PROCESS AND METHODS FOR UNMANNED AERIAL VEHICLE | ICAS2024_0568 |
| Lu, Y. | CLASSIFICATION OF COGNITIVE LOAD BASED ON THE PILOT’ VISUAL SCAN PATTERNS | ICAS2024_0955 |
| Lu, Y. | IMPACT RESPONSES AND FAILURE MECHANISMS OF ALMGB14 UNDER DYNAMIC LOADS | ICAS2024_1006 |
| Lu, Y.F. | SEPARATION SAFETY ANALYSIS IN VARIABLE LAUNCH CONDITION OF SMALL AIR-LAUNCHED UAVS BASED ON NUMERICAL SIMULATION AND FLIGHT TEST | ICAS2024_0311 |
| Lu, Z. | EFFICIENT MULTI-OBJECTIVE DESIGN OPTIMIZATION OF ROTOR AIRFOILS FOR IMPROVING DYNAMIC STALL CHARACTERISTICS | ICAS2024_0420 |
| Lu, Z.-W. | NUMERICAL SIMULATION OF THE RESPONSE CHARACTERISTICS OF THE WING STRUCTURE OF A SEAPLANE PLANING IN WAVE | ICAS2024_0901 |
| Lucanus, O. | ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD | ICAS2024_1280 |
| Lucke, J. | SENS4ICE EU PROJECT HYBRID ICE DETECTION ARCHITECTURES DEMONSTRATION RESULTS | ICAS2024_0178 |
| Ludvik, J. | FUEL CELL BASED POWERTRAINS | ICAS2024_1242 |
| Luehrmann, J. | ANALYSIS OF AN ELECTRICAL-POWERED-DUCTED-THRUST VECTORING-FLAP | ICAS2024_0412 |
| Lundbladh, A. | MODELLING A HYDROGEN FUELLED COMPOSITE CYCLE AEROENGINE | ICAS2024_1103 |
| Luo, J.-Q. | EFFICIENT AEROSTRUCTURAL DESIGN OPTIMIZATION COMBINING GRADIENT-ENHANCED KRIGING WITH COUPLED ADJOINT METHOD | ICAS2024_0651 |
| Luo, M. | TRANSFORMATIVE PEDAGOGY: CO-TEACHING COURSE CLUSTERS THROUGH COMPETITIVE TEAM DESIGNS FOR INNOVATIVE TALENT DEVELOPMENT IN AEROSPACE EDUCATION | ICAS2024_0324 |
| Luo, M. | RESEARCH ON MULTI-ATTRIBUTE DECISION MAKING AND VERIFICATION METHODS FOR SYSTEMS CONFRONTATION | ICAS2024_0561 |
| Luo, M. | A SEMANTIC MODEL-BASED SYSTEMS ENGINEERING APPROACH FOR SUPERSONIC BUSINESS JET CONCEPTUAL DESIGN | ICAS2024_0843 |
| Luo, Y. | NUMERICAL SIMULATION STUDY ON THE INFLUENCE OF WING SPACING OF DRAGONFLY-INSPIRED FLAPPING WINGS | ICAS2024_0243 |
| Luo, Y. | A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION | ICAS2024_0314 |
| Luo, Y. | INFLUENCE OF REINFORCED TRAILING EDGE ON FLAPPING WING AERODYNAMIC FORCE AND DEFORMATION | ICAS2024_0526 |
| Luo, Y. | DESIGN OF ATTITUDE CONTROL SYSTEM FOR DRAGONFLY-INSPIRED FLAPPING WING AERIAL VEHICLE | ICAS2024_0578 |
| Luo, Z.-F. | TRAJECTORY DESIGN FOR ASTEROID SAMPLE RETURN COMBINING BALLISTIC CAPTURE AND AEROBRAKING | ICAS2024_1070 |
| Luo, Z.-F. | REENTRY TRAJECTORY DESIGN FOR DEFORMABLE HYPERSONIC VEHICLES BASED ON NEURAL NETWORKS | ICAS2024_1087 |
| Luo, Z.-P. | IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM | ICAS2024_1186 |
| Lutz, F. | STUDY OF HYBRIDISATION SCENARIOS FOR TURBOPROP AIRCRAFT IN THE GENERAL AVIATION SEGMENT | ICAS2024_0153 |
| Lübbe, S.M. | MASS AND POWER ESTIMATIONS IN PRELIMINARY FLIGHT CONTROL SYSTEM DESIGN | ICAS2024_0166 |
| Lyrio, J.A.A. | LINEAR SYSTEM TECHNIQUES APPLIED TO NONLINEAR AEROSERVOELASTIC ANALYSES | ICAS2024_1004 |
| Lyu, D. | RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS | ICAS2024_0674 |
| Lyu, D.-C. | MODEL-BASED DESIGN OF ACTIVE/ACTIVE ELECTRO-HYDROSTATIC ACTUATION FOR HELICOPTER FLIGHT CONTROLS | ICAS2024_0735 |
| Lyu, Y.-G. | STUDY OF THE SCAVENGE PUMP PERFORMANCE FOR TWO-PHASE FLOW IN AN AIRCRAFT ENGINE LUBRICATION SYSTEM | ICAS2024_0788 |
| Lyv, Y.-G. | VOID FRACTION CALCULATION MODEL BASED ON TWO-PHASE FLOW PATTERNS IN THE SCAVENGE PIPE | ICAS2024_1010 |
| Ma, H.-C. | CONFIGURATION ANALYSIS OF INTEGRATED THERMAL MANAGEMENT BASED ON THE TURBINE-FAN REFRIGERATION SYSTEM | ICAS2024_0194 |
| Ma, L. | ANGLE AND DISTANCE EFFECT ON PHOSPHOR THERMOMETRY | ICAS2024_0529 |
| Ma, P. | LINEAR QUADRATIC PURSUIT AND EVASION DIFFERENTIAL GAME GUIDANCE STRATEGY WITH OBSTACLE AVOIDANCE | ICAS2024_0008 |
| Ma, Q. | SUSTAINABLE FUELS SAFETY BOUNDARIES DEMARCATION METHOD | ICAS2024_0712 |
| Ma, X. | INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF WINGS UNDER ICING CONDITIONS AT VARIOUS SWEEP ANGLES | ICAS2024_0287 |
| Ma, Y. | MODELLING AND INITIAL ASSESSMENT OF A FUEL CELL AUXILIARY PROPULSION AND POWER UNIT | ICAS2024_0261 |
| Ma, Y. | SURFACE MORPHOLOGY AND MICROSTRUCTURAL FEATURES OF ELECTRON BEAM SURFI-SCULPTED TI-6AL-4V ALLOY | ICAS2024_0262 |
| Ma, Y. | STABLE LOCALIZED CORROSION IN A 7075-T6 ALUMINUM ALLOY FSW JOINT: MECHANISM AND MITIGATION | ICAS2024_0300 |
| Ma, Y. | INVESTIGATION ON THE MECHANISM OF THERMAL CYCLING FAILURE IN C/SIC COATING COMPOSITE MATERIALS | ICAS2024_0796 |
| Ma, Y. | INVESTIGATING AN OPTIMAL AEROELASTIC DESIGN FOR AIRCRAFT WINGS WITH DISTRIBUTED PROPELLERS MADE OF COMPOSITES | ICAS2024_1017 |
| Maas, P. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Maathuis, H.F. | EXPLORING MULTI-FIDELITY AEROELASTIC TAILORING: PROSPECT AND MODEL ASSESSMENT | ICAS2024_0150 |
| Macchini, D.M. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Macedo , J.P.C.A | HANDLING QUALITIES RATING SCALE: THE IMPACT OF THE PILOT SUBJECTIVITY IN WORKLOAD EVALUATION | ICAS2024_0848 |
| Macedo, T.F. | FROM THA TO REAL-TIME MONITORING: INTEGRATING NEW VIEW OF SAFETY INTO FLIGHT TEST PROGRAMS | ICAS2024_0127 |
| Machac, M. | THE FATIGUE LIFE PREDICTION OF THIN-WALLED WELDED JOINTS | ICAS2024_1120 |
| MacManus, D. | UNSTEADY AERODYNAMICS OF A COUPLED COMPACT INTAKE-FAN IN CROSSWIND | ICAS2024_0263 |
| Macquart, T. | INFLUENCE OF SKIN CURVATURE ON WINGBOX OPTIMIZATION WITH NONLINEAR STRUCTURAL STABILITY CONSTRAINTS | ICAS2024_0114 |
| Madden, P. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Magalhães, L.B. | INSIGHTS INTO HUMAN FATIGUE: STATISTICAL ANALYSIS IN AIRCRAFT MAINTENANCE | ICAS2024_0131 |
| Magalhães, L.B. | E-KEROSENE POTENTIAL FOR COMMERCIAL AVIATION DECARBONIZATION | ICAS2024_0680 |
| Maggiore, P. | PRELIMINARY ANALYSIS OF TEMPERATURE EFFECTS AND MANEUVER-INDUCED DEFORMATIONS ON FBG OPTIC FIBER INTEGRATED SYSTEMS | ICAS2024_0483 |
| Magnusson, A. | THE PRODUCTION OF HIGH-PERFORMANCE HEAT EXCHANGERS FOR AEROSPACE APPLICATIONS | ICAS2024_0022 |
| Magrì, G. | EFFICIENT SHAPE OPTIMIZATION IN AERONAUTICS: INTEGRATING PARAMETRIC CAD AND MESH MORPHING FOR ENHANCED AERODYNAMIC PERFORMANCE | ICAS2024_0824 |
| Magrini, A. | DESIGN OPTIMISATION OF A BOUNDARY LAYER INGESTION PROPULSOR FOR A MULTI-FUEL HYDROGEN AIRCRAFT | ICAS2024_1060 |
| Maheshwari, S. | EMBEDDED SENSORS FOR AIRCRAFT PREDICTIVE MAINTENANCE: SHM SYSTEM INTEGRATION & TRADE-OFF ANALYSIS | ICAS2024_1081 |
| Maheshwari, S. | USE OF GRAPHENE MATERIAL IN AIRCRAFT STRUCTURE FOR LIGHTNING STRIKE PROTECTION | ICAS2024_1141 |
| Mai, H. | EXPERIMENTAL INVESTIGATION OF THE DLR-F23 CONFIGURATION AT TRANSONIC SPEEDS USING FAST-RESPONSE PRESSURE-SENSITIVE PAINT | ICAS2024_0710 |
| Maiaru, M. | PROCESS MODELLING OF COMPOSITES USING A MULTISCALE FRAMEWORK | ICAS2024_0058 |
| Mainieri, F. | A SUPPORTING FRAMEWORK FOR AIRCRAFT MRO OPERATIONS. CAPACITY PLANNING, TASKS TRACEABILITY AND DISEMBARKED ITEMS TRACKING | ICAS2024_0100 |
| Maione, M. | ENGINEERING-BASED TOOL FOR THREE-DIMENSIONAL ESTIMATIONS OF RE-ENTRY VEHICLES AEROTHERMODYNAMICS | ICAS2024_0859 |
| Malefaki, S. | A PROPOSAL TOWARDS A STEP CHANGE FROM ECO-DRIVEN TO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT COMPONENTS | ICAS2024_0088 |
| Malicki, L. | AERODYNAMIC ANALYSIS OF CAMBER MORPHING AIRFOILS USING PARTICLE IMAGE VELOCIMETRY AND COMPUTATIONAL FLUID DYNAMICS METHODS | ICAS2024_0691 |
| Maliska, H. | THE NASA X-57 “MAXWELL” DISTRIBUTED ELECTRIC PROPULSION FLIGHT DEMONSTRATOR PROJECT | ICAS2024_1287 |
| Mall, K. | EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS | ICAS2024_0464 |
| Mall, K. | TRAJECTORY OPTIMIZATION OF EVTOL VEHICLES FOR URBAN AIR MOBILITY USING INDIRECT METHODS | ICAS2024_0778 |
| Mallardo, S. | PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS | ICAS2024_1205 |
| Malof, E. | FLUID-SOLID INTERACTIVE MODELLING OF FABRIC-BASED ATMOSPHERIC ENTRY SIZED AERODYNAMIC DECELARATORS | ICAS2024_1178 |
| Malpica Galassi, R. | IMPACT OF WELL-TO-TANK EFFICIENCY AND EMISSIONS ON HYBRID AIRCRAFT DESIGN OPTIMIZATION | ICAS2024_0366 |
| Mamatha, G.S. | EMBEDDED SENSORS FOR AIRCRAFT PREDICTIVE MAINTENANCE: SHM SYSTEM INTEGRATION & TRADE-OFF ANALYSIS | ICAS2024_1081 |
| Manassis, K. | RAMJET/SCRAMJET TEST BENCH WITH CAVITY INJECTION OF HYDROGEN | ICAS2024_0235 |
| Mancini, M. | AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) | ICAS2024_0575 |
| Manfriani, L. | FLIGHT TEST AND CFD STUDY OF THE EFFECT OF WING BOUNDARY LAYER TRANSITION ON AILERON BALANCE | ICAS2024_0501 |
| Mannchen, T. | APPLICATION OF SYSML IN THE DEVELOPMENT OF AIRCRAFT CABIN HEALTH MANAGEMENT | ICAS2024_0318 |
| Mannoosseril, A. | RANDOM MATRIX MODELLING FOR UNCERTAINTY QUANTIFICATION IN PRESTRESSED STRUCTURES | ICAS2024_0875 |
| Manrique, C. | DUAL STAGE BATTERY SIZING AND PERFORMANCE ASSESSMENT ON-BOARD HYBRID ELECTRIC AIRCRAFT | ICAS2024_1072 |
| Manrique-Escobar, C.A. | HYDROGEN STORAGE SYSTEM DESIGN: CASE STUDIES FOR AIRBORNE APPLICATION | ICAS2024_0590 |
| Mantegna, G. | ADAPTIVE WING FLUTTER SUPPRESSION BY MEANS OF MULTIPLE TRAILING EDGE CONTROL SURFACES - A COMPARATIVE STUDY | ICAS2024_0513 |
| Marchetti, D. | HYBRID AIR DATA SYSTEM ARCHITECTURE: FROM DESIGN TO FLIGHT TEST VERIFICATION | ICAS2024_0056 |
| Marciniuk, M. | AERODYNAMIC ANALYSIS OF CAMBER MORPHING AIRFOILS USING PARTICLE IMAGE VELOCIMETRY AND COMPUTATIONAL FLUID DYNAMICS METHODS | ICAS2024_0691 |
| Marconcini, M. | HIGH FIDELITY MODELING OF ACOUSTIC LINERS FOR AERONAUTICAL APPLICATIONS | ICAS2024_1048 |
| Mare, J.-C. | MODEL-BASED DESIGN OF ACTIVE/ACTIVE ELECTRO-HYDROSTATIC ACTUATION FOR HELICOPTER FLIGHT CONTROLS | ICAS2024_0735 |
| Marien, T.V. | NASA TRANSONIC TRUSS-BRACED WING STUDIES | ICAS2024_0108 |
| Marinacci, M. | CYBER-PHYSICAL SYSTEM IMPLEMENTATION FOR THE AR-ASSISTED AIT OF AEROSPACE COMPONENTS | ICAS2024_0672 |
| Marini, M. | PROPULSIVE CFD ANALYSIS OF THE SCRAMJET HYPERSONIC EXPERIMENTAL VEHICLE | ICAS2024_0255 |
| Marini, M. | LAUNCH SYSTEM ASSESSMENT OF AN EXPERIMENTAL HYPERSONIC SCRAMJET VEHICLE | ICAS2024_0363 |
| Marini, M. | AERODYNAMIC NUMERICAL/EXPERIMENTAL COMPARISON OF A HYPERSONIC TEST VEHICLE IN MORE&LESS PROGRAM | ICAS2024_1026 |
| Marinus, B.G. | PASSIVE FLOW CONTROL DEVICES ON LOW-REYNOLDS DU89-134 AIRFOIL | ICAS2024_0228 |
| Marinus, B.G. | DESIGN OF MEASUREMENT SETUP FOR HIGH-ALTITUDE IN-FLIGHT EXPERIMENTS ON DU89-134/14 AIRFOIL AT LOW REYNOLDS NUMBER | ICAS2024_0757 |
| Markatos, D.N. | A PROPOSAL TOWARDS A STEP CHANGE FROM ECO-DRIVEN TO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT COMPONENTS | ICAS2024_0088 |
| Marklund, E. | THERMAL AND MECHANICAL CYCLING OF THIN-PLY COMPOSITES FOR CRYOGENIC APPLICATIONS | ICAS2024_1052 |
| Marks, T. | MUTUAL POSITION PLAUSIBILITY CHECKING IN FLYING AD-HOC NETWORKS USING DISTANCE MEASUREMENTS | ICAS2024_0617 |
| Marks, T. | APPLICATIONS AND CHALLENGES FOR AIRBORNE AD-HOC COMMUNICATION NETWORKS IN ORP AIRSPACES USING THE L-BAND | ICAS2024_1038 |
| Marocco, P. | ASSESSING THE TECHNICAL VIABILITY OF ALL-ELECTRIC HYDROGEN-POWERED AIRCRAFTS | ICAS2024_1003 |
| Marques, F.D. | MITIGATING DYNAMIC STALL WITH A MOVABLE LEADING-EDGE: THE NACA0012-IK30 WING | ICAS2024_0595 |
| Marsano, A. | CFD STUDY OF AIR SUPPLY SYSTEM FOR COOLING OF A HYDROGEN POWERED UNMANNED SEAPLANE AND REDUCTION OF THE RESULTING DRAG | ICAS2024_0736 |
| Marsh, D. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Marsilio, R. | NUMERICAL STUDY OF THE FLOWFIELD IN A DIFFERENTIALLY-THROTTLED LINEAR AEROSPIKE | ICAS2024_0944 |
| Martin Ferres, J. | NUMERICAL ANALYSIS OF GENERALIZED AERODYNAMIC FORCES CONSIDERING LAMINAR-TURBULENT TRANSITION ON A NLF WING | ICAS2024_0823 |
| Martinetti, A. | HOLISTIC AND SCALABLE SMART OPTIMIZATION FRAMEWORK FOR PRESCRIPTIVE MAINTENANCE | ICAS2024_0657 |
| Martinez, B. | SONIC BOOM COMPARATIVE STUDY BETWEEN MACH 4.7 OUTDOOR EXPERIMENTAL TESTS AND NUMERICAL SIMULATIONS | ICAS2024_0882 |
| Martins, J. | FAILURE HANDLING ON A SPLIT-FLAP ULTRALIGHT GENERAL AVIATION AIRCRAFT WITH HYBRID NONLINEAR DYNAMIC INVERSION | ICAS2024_0467 |
| Martins, J.R.R.A. | DUCTED HEAT EXCHANGER THERMAL AND AERODYNAMIC SHAPE OPTIMIZATION | ICAS2024_0080 |
| Martins, J.R.R.A. | INVESTIGATING THE INFLUENCE OF AN INBOARD PROPELLER’S VERTICAL OFFSET ON A TRAILING WING’S LIFT AND DRAG DISTRIBUTIONS | ICAS2024_0124 |
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| Martins, J.R.R.A. | SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION | ICAS2024_0465 |
| Martins, J.R.R.A. | ROBUST SCHUR-COMPLEMENT SOLVERS AND LARGE-SCALE MULTIDISCIPLINARY DESIGN OPTIMIZATION | ICAS2024_0687 |
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| Martucci, A. | HYDROGEN SAFETY: A COMPARATIVE ANALYSIS OF LEAK DETECTION SENSORS | ICAS2024_0149 |
| Martulli, L. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Maruccia, E. | HYBRID AIR DATA SYSTEM ARCHITECTURE: FROM DESIGN TO FLIGHT TEST VERIFICATION | ICAS2024_0056 |
| Marulo, F. | COMPUTER VISION ALGORITHMS FOR THE IDENTIFICATION OF DAMAGES ON FULL-SCALE AIRCRAFT COMPONENTS | ICAS2024_0190 |
| Marulo, F. | SEMI-ANALYTICAL SENSITIVITY METHODS FOR AEROELASTIC SHAPE OPTIMIZATION | ICAS2024_0666 |
| Marzioli, P. | CYBER-PHYSICAL SYSTEM IMPLEMENTATION FOR THE AR-ASSISTED AIT OF AEROSPACE COMPONENTS | ICAS2024_0672 |
| Marzocca, P. | MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION | ICAS2024_0020 |
| Marzocca, P. | APPLICATION OF NATURAL LANGUAGE PROCESSING FOR AIRCRAFT DEFECT TRACKING IN MAINTENANCE OPERATIONS | ICAS2024_0083 |
| Marzocca, P. | PARAMETERISATION OF NONLINEAR AEROELASTIC REDUCED ORDER MODELS WITH AERODYNAMIC AND STRUCTURAL NONLINEARITY | ICAS2024_0954 |
| Masarati, P. | SIMPLIFIED MODELS OF PILOT BIOMECHANICS FOR ROTORCRAFT VERTICAL BOUNCE ANALYSIS | ICAS2024_0520 |
| Masciopinto, G. | STIMULATED THERMOGRAPHY AS NON-DESTRUCTIVE TESTING TO ASSESS THE STRUCTURAL INTEGRITY OF AERONAUTICAL COMPONENT IN CFRP | ICAS2024_1076 |
| Masia, R. | NUMERICAL ANALYSIS OF PROCESS-INDUCED DEFORMATIONS AND STRESSES IN AERONAUTICAL COMPOSITE COMPONENTS | ICAS2024_0818 |
| Massaro, M.C. | ASSESSING THE TECHNICAL VIABILITY OF ALL-ELECTRIC HYDROGEN-POWERED AIRCRAFTS | ICAS2024_1003 |
| Mastroddi, F. | ENSURING THE NEXT GENERATION GREEN AIRCRAFT’ SUSTAINABILITY FROM THE DESIGN PHASE VIA A LIFE-CYCLE COST ANALYSIS | ICAS2024_0350 |
| Mastroddi, F. | ADVANCED MULTIDISCIPLINARY DESIGN OF NEXT-GENERATION GREEN AIRCRAFT | ICAS2024_0486 |
| Mastroddi, F. | STRUCTURAL DESIGN OF NEXT-GENERATION REGIONAL GREEN AIRCRAFT | ICAS2024_1035 |
| Mastrogiacomo, L. | PRELIMINARY RESULTS FOR AN INSTRUCTION DESIGN PROCEDURE IN AERONAUTICAL MANUFACTURING | ICAS2024_0306 |
| Masuki, T. | FEASIBILITY STUDY ON OPERATIONAL FLIGHT PLANS ADAPTED FOR TRAJECTORY BASED OPERATION | ICAS2024_1177 |
| Matayoshi, N. | DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY | ICAS2024_0325 |
| Matias, C. | SURFACE QUALITY CHALLENGE FOR TI-6AL-4V ADDITIVE MANUFACTURED TOPOLOGIC OPTIMIZED LIGHTWEIGHT STRUCTURE | ICAS2024_0025 |
| Matías, J.C. | EXPLORING WINGTIP COLUMNAR VORTEX GENERATORS FOR UAV PERFORMANCE ENHANCEMENT | ICAS2024_0219 |
| Matias, J.C. | PIV AND AERODYNAMIC FORCES ANALYSIS OF A HELICOPTER OPERATING AROUND A BUILDING BY WIND-TUNNEL EXPERIMENTS | ICAS2024_0257 |
| Matsubara, I. | EFFICIENT THERMOMECHANICAL SIMULATION FOR METALLIC LATTICE STRUCTURES FABRICATED BY ADDITIVE MANUFACTURING | ICAS2024_0908 |
| Matthes, S. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Matthews, M. | WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES | ICAS2024_1137 |
| Matuschek, T. | PERFORMANCE ASSESSMENT OF AN ENGINE-INTEGRATED CLOSED-AIR COOLING THERMAL MANAGEMENT SYSTEM IN A NEXT GENERATION FIGHTER CONFIGURATION | ICAS2024_0622 |
| Matyja, D. | DESIGN OF REMOTE-CONTROLLED GROUND BASED AIRCRAFT TUG | ICAS2024_1021 |
| Mavris, D. | REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS | ICAS2024_1172 |
| Mavris, D.N. | PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS | ICAS2024_1296 |
| Maw, A.A. | ENHANCED AIRCRAFT TAKEOFF/LANDING SAFETY USING DEEP LEARNING MODEL IN RUNWAY ASSISTANCE SYSTEM | ICAS2024_0786 |
| May, G. | PASSIVE FLOW CONTROL DEVICES ON LOW-REYNOLDS DU89-134 AIRFOIL | ICAS2024_0228 |
| May, M. | FAILURE HANDLING ON A SPLIT-FLAP ULTRALIGHT GENERAL AVIATION AIRCRAFT WITH HYBRID NONLINEAR DYNAMIC INVERSION | ICAS2024_0467 |
| May, M. | MIXED FLIGHT CONTROL LAYOUT FOR ULTRALIGHT GENERAL AVIATION AIRCRAFT | ICAS2024_0517 |
| May, M.S. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Mazzei, L. | CFD-BASED SCOUTING FOR THE DESIGN OF A MULTI-FUEL KEROSENE/HYDROGEN ATMOSPHERIC BURNER | ICAS2024_0432 |
| Mazzoni, F. | HYDROGEN STORAGE SYSTEM DESIGN: CASE STUDIES FOR AIRBORNE APPLICATION | ICAS2024_0590 |
| McCullough, S. | BOMBARDIER ECOJET RESEARCH PROJECT - THE QUEST FOR SUSTAINABLE AVIATION | ICAS2024_1261 |
| McFayden, C. | ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD | ICAS2024_1280 |
| Meade, A. | VEHICLE ASSESSMENT AND SYSTEM-WIDE BENEFIT ANALYSES OF HYBRID-ELECTRIC COMMERCIAL AIRCRAFT – ELECTRIFIED POWERTRAIN FLIGHT DEMONSTRATION PROJECT (EPFD) | ICAS2024_1188 |
| Mecella, M. | CYBER-PHYSICAL SYSTEM IMPLEMENTATION FOR THE AR-ASSISTED AIT OF AEROSPACE COMPONENTS | ICAS2024_0672 |
| Meddaikar, Y.M. | SANDWICH COMPOSITES SKIN PANEL OPTIMIZATION FOR THE COMMON RESEARCH MODEL WING | ICAS2024_0479 |
| Méheut, M. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Mehnen, J. | AUTOMATED OPERATION OF HIGH-PERFORMANCE FIXED-WING DRONES: A POTENTIAL GAME-CHANGER FOR GREEN AERIAL SERVICES | ICAS2024_0946 |
| Melber-Wilkending, S. | SUMMARY OF DLR RESULTS FROM THE SEVENTH AIAA DRAG PREDICTION WORKSHOP | ICAS2024_0116 |
| Melicio, R. | MODELLING ASTEROID TRAJECTORY IN EARTH’S ATMOSPHERE | ICAS2024_0158 |
| Mello, J.M.G.D. | VALUE-DRIVEN TRADESPACE EXPLORATION FOR AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN | ICAS2024_0589 |
| Melz, T. | ACTIVE CONTROL DAMPING WITH THE USE OF VOICE COIL ACTUATORS | ICAS2024_1106 |
| Memmolo, V. | DESIGN OF HYDROGEN STORAGE SYSTEMS IN NEW-GENERATION REGIONAL AIRCRAFT | ICAS2024_0858 |
| Menakath, N. | SURFACE VISUALISATION OF TIME AVERAGED FLOW BEHAVIOUR AROUND RIGID AND FLEXIBLE HEMISPHERES UTILISING UV SENSITIVE OIL | ICAS2024_0070 |
| Mendiguchia Meuser, M. | MITIGATING THE CLIMATE IMPACT OF AVIATION BY OPERATIONAL MEANS - A COMPARATIVE STUDY FOR DIFFERENT WEATHER SITUATIONS | ICAS2024_0096 |
| Mengdehl, C. | DESIGN OF MEASUREMENT SETUP FOR HIGH-ALTITUDE IN-FLIGHT EXPERIMENTS ON DU89-134/14 AIRFOIL AT LOW REYNOLDS NUMBER | ICAS2024_0757 |
| Merola , S. | COMPUTER VISION ALGORITHMS FOR THE IDENTIFICATION OF DAMAGES ON FULL-SCALE AIRCRAFT COMPONENTS | ICAS2024_0190 |
| Merzkirch, M. | THERMAL AND MECHANICAL CYCLING OF THIN-PLY COMPOSITES FOR CRYOGENIC APPLICATIONS | ICAS2024_1052 |
| Metten, M. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Metzler, D. | SIMULATION AND VERIFICATION OF HYDRAULIC ROTOR GAP PARAMETERS OF A NOVEL HIGH EFFICIENT WET ELECTRO MOTOR PUMP FOR AEROSPACE APPLICATIONS | ICAS2024_0123 |
| Mews, F. | HOT-WET CONDITIONING AND THE SENSITIVITY OF MECHANICAL TESTING WITHIN SURFACE TREATMENT QUALIFICATION FOR AIRCRAFT | ICAS2024_0407 |
| Meyer, H. | MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION | ICAS2024_0020 |
| Meyer, H. | CINNABAR PROJECT – COST-BENEFIT ANALYSIS OF DIGITAL PROCESSES FOR NON-DESTRUCTIVE INSPECTIONS OF AIRCRAFT STRUCTURES | ICAS2024_0125 |
| Mi, B. | FLOW CHARACTERISTICS OF THE INLET IN TURBOPROP ENGINE WITH THE INFLUENCE OF SANDS | ICAS2024_0143 |
| Mi, B. | RESEARCH ON UNSTEADY AERODYNAMIC MODELING METHOD OF PREPOSITIVE WING - MAIN WING COMPOSITE SYSTEM AT HIGH ATTACK ANGLE | ICAS2024_0239 |
| Mi, B. | INVESTIGATION ON INFLUENCE PARAMETER OF AIRCRAFT-MISSILE SEPARATION BY CONSIDERING AEROELASTICITY | ICAS2024_0445 |
| Mi, B. | ANALYSIS AND STUDY ON FLUTTER CHARACTERISTICS OF WINGS UNDER TYPICAL FRAGMENT DAMAGE | ICAS2024_0446 |
| Mi, B. | FLIGHT CONTROL SYSTEM KNOWLEDGE GRAPH CONSTRUCTION BASED ON AERONAUTICAL DOMAIN KNOWLEDGE AUGMENTED LARGE LANGUAGE MODEL | ICAS2024_0610 |
| Mi, B.-G. | FAULT DIAGNOSIS AND TOLERANCE SYSTEM OF FLIGHT STATE PERCEPTION MODEL BASED ON MACHINE LEARNING FOR CO-FLOW JET AIRFOIL | ICAS2024_0662 |
| Miao, B. | THE IMPACT OF PIEZOELECTRIC STACK HEATING ON AIRCRAFT DEICING | ICAS2024_0279 |
| Mieloszyk, J. | RAPID DESIGN OF UNCONVENTIONAL AIRCRAFT USING SOFTWARE TOOLS COUPLED IN OPTIMIZATION LOOP – LESSONS LEARNED | ICAS2024_0496 |
| Migliore, D.F. | COMPARATIVE ANALYSIS OF MACHINE LEARNING ALGORITHMS FOR HEAT EXCHANGERS DIAGNOSIS IN ELECTRIFIED AIRCRAFT | ICAS2024_0701 |
| Mignemi, U. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Milazzo, A. | FREE VIBRATIONS OF CYLINDRICAL SHELLS WITH CUTOUTS BY A SINGLE-DOMAIN RITZ FORMULATION | ICAS2024_0832 |
| Miltén, P. | MODELLING HYDROGEN FUEL CELL AIRCRAFT IN SUAVE | ICAS2024_1078 |
| Miltén, P. | MODELLING A HYDROGEN FUELLED COMPOSITE CYCLE AEROENGINE | ICAS2024_1103 |
| Milz, D. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Milz, D. | FAILURE HANDLING ON A SPLIT-FLAP ULTRALIGHT GENERAL AVIATION AIRCRAFT WITH HYBRID NONLINEAR DYNAMIC INVERSION | ICAS2024_0467 |
| Milz, D. | MIXED FLIGHT CONTROL LAYOUT FOR ULTRALIGHT GENERAL AVIATION AIRCRAFT | ICAS2024_0517 |
| Minigher, P. | ON AN EFFICIENT GLOBAL/LOCAL STOCHASTIC METHODOLOGY FOR FAILURE PREDICTION OF AIRCRAFT COMPOSITE STRUCTURES | ICAS2024_0250 |
| Mirabella, C. | A MODEL BASED SYSTEM ENGINEERING APPROACH TOWARDS AIRCRAFT DIGITAL CERTIFICATION | ICAS2024_0603 |
| Mishra, A.A. | INTEGRATED SIZING OF AN ELECTRIFIED TILT-WING AIRCRAFT FOR VERTICAL AND CONVENTIONAL TAKEOFF AND LANDING | ICAS2024_1170 |
| Mishra, A.N. | MRO FOR VTOLS IN A FUNCTIONAL SEQUENCES SOLUTION SPACE | ICAS2024_0705 |
| Mitrotta, F.M.A. | INFLUENCE OF SKIN CURVATURE ON WINGBOX OPTIMIZATION WITH NONLINEAR STRUCTURAL STABILITY CONSTRAINTS | ICAS2024_0114 |
| Miyabe, K. | STUDY ON CONTROL PERFORMANCE OF A NEW TYPE OF TILT-ROTOR AIRCRAFT | ICAS2024_0548 |
| Mizoguchi, M. | ELECTRIC FIELD MEASUREMENT IN GLOW DISCHARGE PLASMA INTERACTING WITH SHOCK WAVE IN HYPERSONIC FLOW | ICAS2024_0390 |
| Moens, F. | IMPACT OF HYDROGEN FUEL ON OVERALL DESIGN OF TRANSPORT AIRCRAFT | ICAS2024_0826 |
| Moens, F. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Moerland, E. | AUTOMATING THE VERIFICATION OF GEOMETRIC REQUIREMENTS FOR AIRCRAFT FUEL SYSTEMS USING KNOWLEDGE-BASED ENGINEERING | ICAS2024_0148 |
| Mohammadi, H. | PRELIMINARY SIZING OF HYDROGEN-BURNING JETLINER FOR DIRECT OPERATING COST OPTIMIZATION | ICAS2024_0109 |
| Mokaddem, K. | CLEAN AVIATION SHORT MEDIUM RANGE AIRCRAFT CONCEPT | ICAS2024_1324 |
| Molina-Cristóbal, A. | SET-BASED DESIGN TECHNIQUES FOR EVOLVABILITY EXPLORATION DURING CONCEPTUAL AIRCRAFT DESIGN | ICAS2024_0233 |
| Molinari, M.M. | IMPACT OF WELL-TO-TANK EFFICIENCY AND EMISSIONS ON HYBRID AIRCRAFT DESIGN OPTIMIZATION | ICAS2024_0366 |
| Molinario, M. | CORUS-XUAM: TACKLING URBAN AIR MOBILITY AIRSPACE INTEGRATION CHALLENGES | ICAS2024_0347 |
| Monaco, E. | CONVOLUTIONAL NEURAL NETWORKS ALGORITHMS FOR STRUCTURAL HEALTH MONITORING OF AIRCRAFTS COMPOSITES PANELS | ICAS2024_0120 |
| Monner, H.P. | MORPHING LEADING-EDGE TUBERCLES ON CESSNA 172 WING | ICAS2024_0047 |
| Monokrousos, N. | NUMERICAL SOLUTION OF LOX FLOW IN A LIQUID ROCKET ENGINE ADDITIVELY MANUFACTURED COOLING CHANNEL | ICAS2024_0105 |
| Monroe, S.E. | PARELLEL UNSTEADY REYNOLDS-AVERAGED NAVIER-STOKES (URANS) STUDEIS OF THE PERFORMANCE OF ONR WATERJET AXWJ-2 | ICAS2024_1198 |
| Montano, F. | A FORMULATION FOR WING AEROELASTIC ANALYSIS BASED ON THE UNSTEADY VLM AND STRUCTURAL DISCONTINUOUS GALERKIN TECHNIQUE | ICAS2024_1140 |
| Montella, N. | WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS | ICAS2024_0348 |
| Monteverde, A. | POTENTIAL APPLICATION OF PHASE CHANGE MATERIALS FOR THERMAL MANAGEMENT SYSTEM OF NEXT GENERATION AIRCRAFT | ICAS2024_0295 |
| Monteverde, A.H.A. | ASSESSING THE TECHNICAL VIABILITY OF ALL-ELECTRIC HYDROGEN-POWERED AIRCRAFTS | ICAS2024_1003 |
| Moore, R. | RECENT FLIGHT EXPERIMENTS SHOW THE CLIMATE BENEFITS OF SUSTAINABLE AVIATION FUELS (SAF) AND ADVANCED ENGINE TECHNOLOGIES | ICAS2024_1252 |
| Moormann, D. | INCREMENTAL NONLINEAR DYNAMIC INVERSION CONTROLLER FOR A FLYING WING OPERATED IN AN AIRBORNE WIND ENERGY SYSTEM | ICAS2024_0713 |
| Morais, L.D.O. | A HUMAN-CENTERED SYSTEMS ENGINEERING APPROACH FOR INTEGRATING ARTIFICIAL INTELLIGENCE IN AVIATION: A REVIEW OF AI SYSTEMS | ICAS2024_0397 |
| Morais, R.H. | MODELLING ASTEROID TRAJECTORY IN EARTH’S ATMOSPHERE | ICAS2024_0158 |
| Moreau, F. | THERMAL AND MECHANICAL CYCLING OF THIN-PLY COMPOSITES FOR CRYOGENIC APPLICATIONS | ICAS2024_1052 |
| Moreira, C. | AERODYNAMIC INTERACTION EFFECTS OF TILTROTOR EVTOL AIRCRAFT | ICAS2024_0978 |
| Morgans, A. | THERMOACOUSTIC INSTABILITY IN AERO-ENGINE COMBUSTORS | ICAS2024_1232 |
| Mori, R. | IDENTIFICATION OF FACTORS CONTRIBUTING TO UNFAVORABLE LANDINGS | ICAS2024_0049 |
| Morimoto, G. | REMOTE OBSERVATION EXPERIMENT OF VOLCANIC ASH USING POLARIZATION LIDAR | ICAS2024_0214 |
| Morioka, S. | A FAST INFORMATION THEORETICALLY SECURE RADIO COMMUNICATION PROTOCOL BASED ON GNSS POSITIONING | ICAS2024_0559 |
| Moruzzi, M.C. | DESIGN AND DEVELOPMENT OF THE VISUAL AND AUDITORY LAYER FOR DIFFERENT CABIN/COCKPIT LAYOUT | ICAS2024_0799 |
| Moss, S.D. | AEROACOUSTIC CAVITY FLOW ENERGY HARVESTING | ICAS2024_0558 |
| Most, C. | AI DRIVEN DECISION SUPPORT IN OPERATIONS STEERING | ICAS2024_1279 |
| Mourouzidis, C. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Mourouzidis, C. | DESIGN SPACE EXPLORATION OF NEXT-GENERATION SUPERSONIC BUSINESS JET ENGINE WITH A FOCUS ON LANDING AND TAKE-OFF (LTO) NOISE | ICAS2024_1147 |
| Mthembu, N. | DECOUPLING STORE AND PARENT AERODYNAMICS FOR FAST PREDICTION OF SUBSONIC STORE TRAJECTORIES | ICAS2024_0189 |
| Mu, Q.-X. | OPTIMIZATION DESIGN OF MULTI-SCALE ACTIVE COOLING STRUCTURE FOR AIRCRAFT | ICAS2024_0375 |
| Mucha, M. | EFFECT OF INFILL STYLE AND DENSITY ON SELECTED MECHANICAL PROPERTIES OF THE CARBON FIBRE REINFORCED ABS MFD FILAMENT | ICAS2024_0806 |
| Mueller, T. | ANALYSIS OF AN ELECTRICAL-POWERED-DUCTED-THRUST VECTORING-FLAP | ICAS2024_0412 |
| Mujika, Z. | DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS | ICAS2024_0229 |
| Muller, M. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Mumm, N. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Mumm, N. | MIXED FLIGHT CONTROL LAYOUT FOR ULTRALIGHT GENERAL AVIATION AIRCRAFT | ICAS2024_0517 |
| Munch, L. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Muniz, M.V.G. | LINEAR SYSTEM TECHNIQUES APPLIED TO NONLINEAR AEROSERVOELASTIC ANALYSES | ICAS2024_1004 |
| Munjuluru, R.C. | DESIGN AND VISUALIZATION OF A KNOWLEDGE-BASED AIRCRAFT CABIN IN VIRTUAL REALITY | ICAS2024_0505 |
| Munjulury, R.C. | LARGE LANGUAGE MODEL-DRIVEN SIMULATIONS FOR SYSTEM OF SYSTEMS ANALYSIS IN FIREFIGHTING AIRCRAFT CONCEPTUAL DESIGN | ICAS2024_0346 |
| Munjulury, R.C. | EXPLORATION AND EVALUATION OF KNOWLEDGE-BASED ENGINEERING APPROACH FOR LIQUID HYDROGEN TANK INTEGRATION IN EXISTING FUSELAGE | ICAS2024_0488 |
| Munjulury, R.C. | AUTOMATION OF ENGINEERING INTEROPERABILITY FOR AIRCRAFT SYSTEM DESIGN | ICAS2024_0510 |
| Munk, D.J. | AEROACOUSTIC CAVITY FLOW ENERGY HARVESTING | ICAS2024_0558 |
| Muñoz, C.A. | PRELIMINARY APPLICATION OF FORMAL VERIFICATION TO AN AUTONOMY ARCHITECTURE FOR UNMANNED AIRCRAFT | ICAS2024_1278 |
| Murahashi, Y. | TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2024_1215 |
| Murayama, M. | NUMERICAL EVALUATION FOR FAN-NOISE SHIELDING EFFECTS ON AFT-FUSELAGE MOUNTED AND EMBEDDED ENGINES | ICAS2024_0471 |
| Murça, M.C.R. | ENHANCING PUBLIC GOOD MISSIONS AND DISASTER RESPONSE WITH ADVANCED AERIAL TECHNOLOGY: OPPORTUNITIES AND CHALLENGES | ICAS2024_1259 |
| Murphy, A.J. | PRATT & WHITNEY SUSTAINABILITY STRATEGY & DEMONSTRATORS | ICAS2024_1307 |
| Murphy, H. | EVALUATION AND SIMULATION OF PARALLEL HYBRID ELECTRIC PROPULSION WITH REAL FLIGHT DATA | ICAS2024_0738 |
| Muscarello, V. | ASSESSMENT OF A HIGHLY PARAMETERIZED STEADY-STATE MICROSCALE WIND SIMULATOR FOR URBAN AIR MOBILITY APPLICATIONS | ICAS2024_0379 |
| Muscarello, V. | PARAMETERISATION OF NONLINEAR AEROELASTIC REDUCED ORDER MODELS WITH AERODYNAMIC AND STRUCTURAL NONLINEARITY | ICAS2024_0954 |
| Musto, C. | SMART ELECTRIC POWER MANAGEMENT ONBOARD FUTURE AIRCRAFT | ICAS2024_0085 |
| Mutasa, C.T. | NUMERICAL STUDIES ON NOISE-SHIELDING EFFECTS OF A BLENDED-WING-BODY AIRCRAFT USING BOUNDARY ELEMENT METHOD | ICAS2024_0556 |
| Muth, K. | ATM CONTROLLER SUPPORT IN CASE OF SPACIOUS SEVERE WEATHER CONSTELLATIONS ILLUSTRATED USING TWO AIRSPACE EXAMPLES | ICAS2024_0061 |
| Mühlmann, P. | THE CRM-HL ECOSYSTEM - DLR CONTRIBUTIONS | ICAS2024_1214 |
| Müller, J. | INCREMENTAL NONLINEAR DYNAMIC INVERSION CONTROLLER FOR A FLYING WING OPERATED IN AN AIRBORNE WIND ENERGY SYSTEM | ICAS2024_0713 |
| Müller, J.U. | RIBLETS IN AVIATION- FIRST EVER INDUSTRIALIZATION WITH AEROSHARK | ICAS2024_1246 |
| Müller, S. | DLR DESIGN CHALLENGE 2024: DESIGN OF A COST AND ENERGY EFFICIENT REGIONAL AIRCRAFT | ICAS2024_1264 |
| Müller, T. | A DESIGN APPROACH FOR A MODEL-SCALE VTOL POWERED BY TWO PIVOTING KEROSENE TURBINES | ICAS2024_0151 |
| Müller, T. | BUILDING METHODS FOR A COMPOSITE CONSTRUCTED VTOL USING 3D PRINTING TECHNIQUES | ICAS2024_0313 |
| Månsson, P. | INFLUENCE OF CONTROL POWER RATE ON HIGH-ALPHA ROLL MANOEUVRABILITY | ICAS2024_0317 |
| Naeem, N. | COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH | ICAS2024_1138 |
| Nagata, N. | FEASIBILITY STUDY ON OPERATIONAL FLIGHT PLANS ADAPTED FOR TRAJECTORY BASED OPERATION | ICAS2024_1177 |
| Nagel, B. | TRANSLATING THE CONCEPT OF SUSTAINABILITY FOR THE DETERMINATION OF REQUIREMENTS FOR THE DESIGN OF FUTURE AIRCRAFT | ICAS2024_0042 |
| Nagel, B. | IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN | ICAS2024_0057 |
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| Nagel, B. | VALUE-DRIVEN TRADESPACE EXPLORATION FOR AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN | ICAS2024_0589 |
| Nagel, B. | UNCERTAINTY PROPAGATION IN VALUE-DRIVEN DECISION-MAKING FOR THE AIRCRAFT, MANUFACTURING AND SUPPLY CHAIN DESIGN | ICAS2024_0804 |
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| Nagel, B. | COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH | ICAS2024_1138 |
| Nagel, B. | AN ONTOLOGY-BASED APPROACH FOR THE CO-DEVELOPMENT AND OPTIMIZATION OF AIRCRAFT CABIN DESIGN AND ASSEMBLY ARCHITECTURES | ICAS2024_1152 |
| Nagel, B. | PIONEERING THE EXCHANGE OF KNOWLEDGE | ICAS2024_1325 |
| Najafabadi, H.N. | NONLINEAR BEHAVIOR IN AIRCRAFT FUEL GAUGE READINGS: AN EXPLORING ANALYSIS | ICAS2024_1187 |
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| Nakahata, H. | FEASIBILITY STUDY ON OPERATIONAL FLIGHT PLANS ADAPTED FOR TRAJECTORY BASED OPERATION | ICAS2024_1177 |
| Nakamura, Y. | ESTIMATING THE IMPACT OF NUMERICAL WEATHER PREDICTION DATA MODELS ON SHORT-HAUL MINIMUM COST TRACKS | ICAS2024_0142 |
| Nakamura, Y. | RELATIONSHIPS BETWEEN AIRCRAFT ROUTES AND TURBULENCE-RELATED WEATHER DATA | ICAS2024_0380 |
| Nakley, L.M. | NASA HYBRID THERMALLY EFFICIENT CORE (HYTEC) PROJECT OVERVIEW | ICAS2024_1245 |
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| Nan, T. | MICROMECHANICAL MODELING OF THE VISCOELASTIC-VISCOPLASTIC RESPONSE OF FIBER-REINFORCED COMPOSITES | ICAS2024_0213 |
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| Nascimento, R.C. | FLIGHT PATH RECONSTRUCTION OF A FLEXIBLE WING UAV WITH WING MOUNTED VANES | ICAS2024_1176 |
| Navarro, R. | PERFORMANCE AND ACOUSTIC ANALYSIS OF A DISTRIBUTED ELECTRIC PROPULSION UNMANNED AIRCRAFT | ICAS2024_1009 |
| Nayman, M. | LOCALIZED AERODYNAMIC SHAPE OPTIMIZATION FOR AUTOMOTIVE APPLICATIONS | ICAS2024_0265 |
| Ndebele, B. | DECOUPLING STORE AND PARENT AERODYNAMICS FOR FAST PREDICTION OF SUBSONIC STORE TRAJECTORIES | ICAS2024_0189 |
| Ndlovu, H. | DECOUPLING STORE AND PARENT AERODYNAMICS FOR FAST PREDICTION OF SUBSONIC STORE TRAJECTORIES | ICAS2024_0189 |
| Negroni, F. | FASTVIBE SW TOOL FOR RIDE-ALONG VIBRATION SURVEY ANALYSIS | ICAS2024_0455 |
| Nehter, P. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Nemati, M. | MACHINE LEARNING INTEGRATION IN COMPUTATIONAL FLUID DYNAMICS FOR RAPID FLOW FIELD PREDICTION | ICAS2024_1033 |
| Nendel, W. | SIMULATION AND VERIFICATION OF HYDRAULIC ROTOR GAP PARAMETERS OF A NOVEL HIGH EFFICIENT WET ELECTRO MOTOR PUMP FOR AEROSPACE APPLICATIONS | ICAS2024_0123 |
| Neogi, N. | NASA RESEARCH TO EXPAND UAS OPERATIONS FOR DISASTER RESPONSE | ICAS2024_1281 |
| Neri, A. | AERO-THERMAL ANALYSIS OF A REUSABLE LAUNCH VEHICLE DURING RE-ENTRY MANOEUVRER | ICAS2024_0877 |
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| Nesbitt, E.H. | REFINED PREDICTIONS COMPARED WITH THE PROPULSION AIRFRAME AEROACOUSTICS AND AIRCRAFT SYSTEM NOISE FLIGHT RESEARCH TEST DATA | ICAS2024_0069 |
| Neuland, T. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Newby, T. | DELIVERING THE ROLLS-ROYCE NET ZERO ROADMAP | ICAS2024_1306 |
| Nghiem, Q.-H. | AERODYNAMIC DESIGN METHODOLOGY OF A NON-UNIFORM PERFORATED INVERSE CONICAL FLOW SPREADER IN INTERMITTENT BLOW DOWN WIND TUNNEL | ICAS2024_0731 |
| Nghiem, Q.-H. | NUMERICAL METHOD FOR DESIGNING AND MODELING AN EXHAUST CLUSTER FOR A SMALL TURBOJET ENGINE TEST CELL | ICAS2024_0737 |
| Nguyen, P.-M. | AERODYNAMIC DESIGN METHODOLOGY OF A NON-UNIFORM PERFORATED INVERSE CONICAL FLOW SPREADER IN INTERMITTENT BLOW DOWN WIND TUNNEL | ICAS2024_0731 |
| Nguyen, P.-M. | NUMERICAL METHOD FOR DESIGNING AND MODELING AN EXHAUST CLUSTER FOR A SMALL TURBOJET ENGINE TEST CELL | ICAS2024_0737 |
| Nguyen, P.M. | INTEGRATIVE ANALYSIS OF LOW-CYCLE FATIGUE AND CRACK PROPAGATION IN TURBINE BLADES | ICAS2024_0538 |
| Nguyen, T.-G. | AERODYNAMIC DESIGN METHODOLOGY OF A NON-UNIFORM PERFORATED INVERSE CONICAL FLOW SPREADER IN INTERMITTENT BLOW DOWN WIND TUNNEL | ICAS2024_0731 |
| Nguyen, T.-G. | NUMERICAL METHOD FOR DESIGNING AND MODELING AN EXHAUST CLUSTER FOR A SMALL TURBOJET ENGINE TEST CELL | ICAS2024_0737 |
| Nguyen, T.Q. | INTEGRATIVE ANALYSIS OF LOW-CYCLE FATIGUE AND CRACK PROPAGATION IN TURBINE BLADES | ICAS2024_0538 |
| Nguyen Dinh, Q. | APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) FOR PREDICTION OF DRAG COEFFICIENT OF AXISYMMETRIC BOATTAIL MODELS | ICAS2024_0205 |
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| Nguyen Van, E. | IMPACT OF HYDROGEN FUEL ON OVERALL DESIGN OF TRANSPORT AIRCRAFT | ICAS2024_0826 |
| NGuyen Van, E. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Nicassio, F. | DETECTION OF DELAMINATIONS IN DAMAGED COMPOSITE PLATES VIA LOCAL DAMAGE RESONANCE APPROACH | ICAS2024_0814 |
| Nickl, M. | ON THE WATER ENHANCED TURBOFAN CONCEPT: PART A - THERMODYNAMICS AND OVERALL ENGINE DESIGN | ICAS2024_0199 |
| Nicolosi, F. | WIND-TUNNEL TESTS OF INNOVATIVE TAILPLANE CONFIGURATIONS | ICAS2024_0370 |
| Nicolosi, F. | COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH | ICAS2024_1138 |
| Nie, H. | DESIGN OPTIMIZATION OF A WIG CRAFT’S HIGH LIFT DEVICE CONSIDERING GROUND EFFECT | ICAS2024_0572 |
| Nie, H. | BOUNDARY-LAYER SUCTION AND AERODYNAMIC SHAPE OPTIMIZATION FOR HYBRID LAMINAR FLOW CONTROL ON A FIN | ICAS2024_0681 |
| Nie, H. | ON THE INFLUENCE OF BASE FLOW CHARACTERISTICS ON CROSSFLOW INSTABILITY IN SWEPT BOUNDARY LAYERS | ICAS2024_0918 |
| Nijhuis, P. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Nikbay, M. | LOW-SUBSONIC AERODYNAMIC ANALYSES OF A NONPLANAR BWB MODEL: AN EXPERIMENTAL AND CFD STUDY | ICAS2024_0232 |
| Niklasson, F. | DESIGN OF A SUSTAINABLE FLEXFORMING PROCEDURE FOR AERO ENGINE COMPONENTS IS ALLOY 718 | ICAS2024_1194 |
| Nikodem, F. | GENERAL DESIGN CONSIDERATIONS FOR SOLAR-ELECTRIC HIGH-ALTITUDE LONG-ENDURANCE AIRCRAFT | ICAS2024_0910 |
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| Ning, C. | TRANSFER LEARNING FOR REDUCED-ORDER MODELING OF TRANSONIC FLOWS USING MULTIFIDELITY DATA | ICAS2024_1110 |
| Ning, Y. | FATIGUE CRACK LIFE PREDICTION BASED ON BAYESIAN DYNAMIC UPDATE | ICAS2024_0393 |
| Ninni, D. | ASSESSMENT OF A MACROSCOPIC MODEL FOR THE AEROTHERMODYNAMICS CHARACTERIZATION OF ICE GIANTS ATMOSPHERIC ENTRY | ICAS2024_0872 |
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| Niu, M. | HYDRODYNAMIC ANALYSIS OF STATIC WATER IMPACT ON WEDGE-SHAPED HULL WATERTIGHT TEST SPECIMEN THROUGH NUMERICAL ANALYSIS | ICAS2024_0904 |
| Nobari, A.S. | INVESTIGATING THE EFFECT OF DELAMINATION-INDUCED FRICTIONAL CONTACT ON THE DYNAMIC BEHAVIOR OF LAMINATE STRUCTURES | ICAS2024_1108 |
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| Nong, Y.-H. | MODELING AND FLIGHT CONTROL LAW DESIGN FOR A SEAPLANE DURING WATER SURFACE TAKEOFF | ICAS2024_0977 |
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| Norman, P. | SAFETY-DRIVEN BASELINING OF HYBRID ELECTRIC AIRCRAFT ELECTRICAL POWER SYSTEM ARCHITECTURES | ICAS2024_1027 |
| Norris, G. | A VIEW LOOKING IN - AVIATION WEEK'S ASSESSMENT OF SUSTAINABLE AVIATION R&D IN CHINA AND THE ASIA-PACIFIC REGION | ICAS2024_1255 |
| Nospes, D. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
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| Notaro, I. | A SIMULINK APPROACH TO MODELING HETEROGENEOUS DRONE FORMATIONS FOR AGENT-BASED SIMULATION | ICAS2024_0608 |
| Novák , J. | HYBRID MODELING APPROACH FOR OPTIMIZATION BASED CONTROL OF MULTIROTOR UNMANNED AERIAL VEHICLES | ICAS2024_0029 |
| Novák , J. | MODEL PREDICTIVE CONTROL DRIVEN AERIAL GRASPING WITH SOFT OPERATIONAL CONSTRAINTS | ICAS2024_0879 |
| Novák , J. | PREDICTIVE CONTROL DRIVEN TACTICAL MANEUVERING | ICAS2024_1044 |
| Noviello, M.C. | CONCEPTUAL DESIGN AND TOPOLOGY OPTIMIZATION OF A COMPLIANT MORPHING FLAP FOR NEXT GENERATION HYBRID-ELECTRIC REGIONAL AIRCRAFT | ICAS2024_1206 |
| Nugnes, V. | A SYSTEM OF SYSTEMS AIRCRAFT DESIGN FRAMEWORK: DEMONSTRATION USING A SEAPLANE TRANSPORT NETWORK IN THE GREEK ISLANDS | ICAS2024_0402 |
| Numata, D. | DEVELOPMENT OF UNSTEADY PRESSURE-SENSITIVE PAINT FOR LOW REYNOLDS NUMBER WIND TUNNEL TESTS IN LOW-PRESSURE ENVIRONMENTS | ICAS2024_0840 |
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| Nöhren, L. | ATM CONTROLLER SUPPORT IN CASE OF SPACIOUS SEVERE WEATHER CONSTELLATIONS ILLUSTRATED USING TWO AIRSPACE EXAMPLES | ICAS2024_0061 |
| Obana, S. | A FAST INFORMATION THEORETICALLY SECURE RADIO COMMUNICATION PROTOCOL BASED ON GNSS POSITIONING | ICAS2024_0559 |
| Ocokoljic, G. | UPGRADE OF THE VTI T-38 BLOWDOWN TRISONIC TEST FACILITY: WIND TUNNEL CONTROL SYSTEM | ICAS2024_0456 |
| Odaguil, F.I.K. | VALUE-DRIVEN TRADESPACE EXPLORATION FOR AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN | ICAS2024_0589 |
| Odegard, G.M. | PROCESS MODELLING OF COMPOSITES USING A MULTISCALE FRAMEWORK | ICAS2024_0058 |
| Oestreicher, A. | SUSTAINABLE ENGINE MAINTENANCE: EVALUATING THE ECOLOGICAL IMPACT OF LIFE LIMITED PART REPLACEMENT | ICAS2024_0452 |
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| Ohishi, M. | EFFICIENT THERMOMECHANICAL SIMULATION FOR METALLIC LATTICE STRUCTURES FABRICATED BY ADDITIVE MANUFACTURING | ICAS2024_0908 |
| Ohlsson, F. | THERMAL AND MECHANICAL CYCLING OF THIN-PLY COMPOSITES FOR CRYOGENIC APPLICATIONS | ICAS2024_1052 |
| Oikawa, H. | REMOTE OBSERVATION EXPERIMENT OF VOLCANIC ASH USING POLARIZATION LIDAR | ICAS2024_0214 |
| Ojeda, M. | EXPLORING WINGTIP COLUMNAR VORTEX GENERATORS FOR UAV PERFORMANCE ENHANCEMENT | ICAS2024_0219 |
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| Olichevis Halila, G.L. | ADJOINT-BASED TRANSONIC WING AERODYNAMIC SHAPE OPTIMIZATION INVESTIGATIONS | ICAS2024_0078 |
| Olichevis Halila, G.L. | INVESTIGATING THE INFLUENCE OF AN INBOARD PROPELLER’S VERTICAL OFFSET ON A TRAILING WING’S LIFT AND DRAG DISTRIBUTIONS | ICAS2024_0124 |
| Olivares, G. | MULTIPHYSICS MODELING FOR SAFE BATTERIES USING LS-DYNA | ICAS2024_0837 |
| Olivares, G. | PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS | ICAS2024_1205 |
| Oliveira, F.B. | ANALYSIS OF THE R FAMILY OF LIMITERS APPLIED TO HIGH-ORDER FR/CPR SCHEMES FOR THE SIMULATION OF SUPERSONIC FLOWS | ICAS2024_1181 |
| Oliveira, T. | STRUCTURED ANALYSIS ESTIMATION FOR ELECTRICAL ENERGY DEMAND ON AIRPORT OPERATIONS FOR HYBRID REGIONAL AND ELECTRIC TOWING PARAMETERIZED BY MOVEMENT METRICS CONSIDERING UPCOMING ELECTRIC INTENSIVE TECHNOLOGIES AND EMISSION REDUCTIONS IN THE UPCOMING DECADE | ICAS2024_1007 |
| Olivier, P. | A DIGITAL METHOD FOR THE COMPENSATED MOLD DESIGN OF COMPOSITE PARTS | ICAS2024_0487 |
| Omede', B. | MACHINE LEARNING AND NUMERICAL OPTIMIZATION OF BIO-INSPIRED 3D-PRINTABLE SANDWICH CORE CELL | ICAS2024_0307 |
| Onda, S. | TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2024_1215 |
| Oosedo, A. | DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY | ICAS2024_0325 |
| Opromolla, R. | RESEARCH RESULTS AND PERSPECTIVES ON NON-COOPERATIVE SENSING FOR SAFE UAM OPERATIONS | ICAS2024_1267 |
| Orazzo, A. | SENS4ICE EU PROJECT HYBRID ICE DETECTION ARCHITECTURES DEMONSTRATION RESULTS | ICAS2024_0178 |
| Orlandini, V. | NUMERICAL STUDY ON THE FIRST-STAGE RE-ENTRY TRAJECTORY USING AN INFLATABLE BALLUTE | ICAS2024_0401 |
| Orlandini, V. | AERO-THERMAL ANALYSIS OF A REUSABLE LAUNCH VEHICLE DURING RE-ENTRY MANOEUVRER | ICAS2024_0877 |
| Orlando, C. | ADAPTIVE WING FLUTTER SUPPRESSION BY MEANS OF MULTIPLE TRAILING EDGE CONTROL SURFACES - A COMPARATIVE STUDY | ICAS2024_0513 |
| Orlando, C. | METAMODELLING OF THE WORKLOAD ASSESSMENT IN SIMULATED FLIGHTS USING THE KRIGING METHOD | ICAS2024_0743 |
| Orton, A. | UNITED STATES' AIRCRAFT SUSTAINABILITY RESEARCH & DEVELOPMENT EFFORTS | ICAS2024_1229 |
| Osund-Ireland, M. | CLIMATE RESILIENCE – THE IMPACT OF EXTREME WEATHER EVENTS - A CASE STUDY: HEATHROW AIRPORT | ICAS2024_0292 |
| Otsuka, K. | ABSOLUTE NODAL COORDINATE FORMULATION FOR NONLINEAR MULTIBODY MODELING OF FLARED HINGED WINGS | ICAS2024_0071 |
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| Ouisse, M. | ON THE OPTIMIZATION OF (GENERALIZED) IMPEDANCE FOR ACOUSTIC LINERS | ICAS2024_1123 |
| Ovesy, H.R. | APPLICATION OF LAMBDA FRAMEWORK FOR AIRCRAFT MULTIDISCIPLINARY DESIGN, ANALYSIS AND OPTIMIZATION | ICAS2024_0068 |
| Owen, B. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Oyama, A. | MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM | ICAS2024_0573 |
| Pachidis, V. | NUMERICAL SOLUTION OF LOX FLOW IN A LIQUID ROCKET ENGINE ADDITIVELY MANUFACTURED COOLING CHANNEL | ICAS2024_0105 |
| Pachidis, V. | BASE FLOW CHARACTERISTICS FOR A SUB-SCALE HIGH-SPEED EXHAUST AT OVER-EXPANDED MODE | ICAS2024_0512 |
| Pachidis, V. | DESIGN SPACE EXPLORATION OF NEXT-GENERATION SUPERSONIC BUSINESS JET ENGINE WITH A FOCUS ON LANDING AND TAKE-OFF (LTO) NOISE | ICAS2024_1147 |
| Pacini, B. | SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION | ICAS2024_0465 |
| Paciorri, R. | NUMERICAL STUDY ON THE FIRST-STAGE RE-ENTRY TRAJECTORY USING AN INFLATABLE BALLUTE | ICAS2024_0401 |
| Paciorri , R. | AERO-THERMAL ANALYSIS OF A REUSABLE LAUNCH VEHICLE DURING RE-ENTRY MANOEUVRER | ICAS2024_0877 |
| Padilha, M. | AUTOMATING THE VERIFICATION OF GEOMETRIC REQUIREMENTS FOR AIRCRAFT FUEL SYSTEMS USING KNOWLEDGE-BASED ENGINEERING | ICAS2024_0148 |
| Padovany da Silva, G. | INVESTIGATING THE INFLUENCE OF AN INBOARD PROPELLER’S VERTICAL OFFSET ON A TRAILING WING’S LIFT AND DRAG DISTRIBUTIONS | ICAS2024_0124 |
| Pagani, A. | AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING DESIGN | ICAS2024_0167 |
| Pagani, A. | A PRELIMINARY METHODOLOGY TO ASSESS GUST SPECTRA VIA SATELLITE DATA | ICAS2024_1142 |
| Page, M. | TECHNICAL APPROACH FOR A BWB AIRLINER TO MEET MARKET DEMANDS | ICAS2024_1293 |
| Page, M. | TECHNICAL FINDINGS TO DATE TO SUPPORT MARKET DEMANDS OF A BWB AIRLINER | ICAS2024_1294 |
| Page, M. | GROUND AND SCALED FLIGHT TEST PLANS TO SUPPORT DEVELOPMENT OF A BWB AIRLINER | ICAS2024_1295 |
| Paiva, T. | SLEEPINESS IN BRAZILIAN AVIATION: A PROBLEM-SOLVING APPROACH | ICAS2024_0027 |
| Palacios, R. | ABSOLUTE NODAL COORDINATE FORMULATION FOR NONLINEAR MULTIBODY MODELING OF FLARED HINGED WINGS | ICAS2024_0071 |
| Palacios, R. | NUMERICAL INVESTIGATION OF PASSIVE AND ACTIVE ALLEVIATION OF DYNAMIC LOADS ON HIGH-ASPECT-RATIO-WING VEHICLES | ICAS2024_0740 |
| Palaia, G. | FROM THEORY TO FLIGHT: THE BOX-WING CONFIGURATION IMPLICATIONS FOR THE NEXT-GENERATION AIRCRAFT | ICAS2024_0217 |
| Palaia, G. | ENVIRONMENTAL IMPLICATIONS OF HYBRID-ELECTRIC REGIONAL AIRCRAFT: EMISSIONS AND CLIMATE CHANGE | ICAS2024_0222 |
| Palaia, G. | POWER MANAGEMENT SUPPLY OPTIMIZATION FOR HYBRID-ELECTRIC REGIONAL AIRCRAFT | ICAS2024_0303 |
| Palaia, G. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Palaia, G. | A PRELIMINARY METHODOLOGY TO ASSESS GUST SPECTRA VIA SATELLITE DATA | ICAS2024_1142 |
| Palanti, L. | CFD-BASED SCOUTING FOR THE DESIGN OF A MULTI-FUEL KEROSENE/HYDROGEN ATMOSPHERIC BURNER | ICAS2024_0432 |
| Paletti, L. | TRANSLATING THE CONCEPT OF SUSTAINABILITY FOR THE DETERMINATION OF REQUIREMENTS FOR THE DESIGN OF FUTURE AIRCRAFT | ICAS2024_0042 |
| Palomar, A. | DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS | ICAS2024_0229 |
| Paluch, B. | IMPACT OF HYDROGEN FUEL ON OVERALL DESIGN OF TRANSPORT AIRCRAFT | ICAS2024_0826 |
| Palumbo, D. | STIMULATED THERMOGRAPHY AS NON-DESTRUCTIVE TESTING TO ASSESS THE STRUCTURAL INTEGRITY OF AERONAUTICAL COMPONENT IN CFRP | ICAS2024_1076 |
| Palumbo, D. | STRUCTURAL HEALTH MONITORING OF CFRP DURING FATIGUE LOAD VIA THE ASSESSMENT OF CRACK DENSITY BY MEANS OF THERMOGRAPHY | ICAS2024_1135 |
| Pan, Y. | DYNAMIC BUCKLING ANALYSIS OF THIN-SHELL COMPOSITE STRUCTURES BASED ON ISOGEOMETRIC ANALYSIS | ICAS2024_0389 |
| Pan, Y.J. | STRUCTURAL AND AEROELASTIC OPTIMISATION OF A LARGE AIRCRAFT WING WITH A PASSIVE TWIST WINGTIP | ICAS2024_0111 |
| Panagopoulos, M. | COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A DIRECT AIR CAPTURE FILTER SYSTEM | ICAS2024_0463 |
| Pandya, S.A. | SCOPING OF AN AIR SUPPLY CONFIGURATION FOR ACTIVE FLOW CONTROL ON A COMMERCIAL TRANSPORT AIRPLANE HIGH-LIFT SYSTEM | ICAS2024_0951 |
| Pant, R. | AN AUTONOMOUS SYSTEM FOR DOCKING AND BATTERY SWAPPING IN UAVS | ICAS2024_1116 |
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| Paolillo, G. | NUMERICAL STUDY ON ACTIVE FLOW CONTROL SOLUTIONS FOR HIGH LIFT | ICAS2024_1053 |
| Papakonstantinou, S. | MRO FOR VTOLS IN A FUNCTIONAL SEQUENCES SOLUTION SPACE | ICAS2024_0705 |
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| Parez, J. | PREDICTION OF TRANSIENT DEFORMATION BY COUPLING CFD AND FEM ANALYSIS USING MACHINE LEARNING BASED CORRELATION FUNCTION | ICAS2024_1084 |
| Park, E.G. | DEVELOPMENT OF A MACHINE LEARNING-BASED STRESS SPECTRUM ESTIMATION TECHNIQUE FOR FATIGUE MONITORING | ICAS2024_0525 |
| Park, M. | MAXIMUM SPEED OF BATTERY-POWERED TILT-ROTOR AIRCRAFT | ICAS2024_0141 |
| Park, M. | DETERMINISTIC HYBRID POWER RATIOS CONSIDERING VARIOUS FAILURE CASES FOR QUAD TILTROTOR AIRCRAFT | ICAS2024_0352 |
| Park, O. | A DESIGN OF VFR APPROACH AND DEPARTURE PROCEDURES OF UAM AT VERTIPORTS ADJACENT TO THE AIRPORT | ICAS2024_0110 |
| Pascazio, G. | ASSESSMENT OF A MACROSCOPIC MODEL FOR THE AEROTHERMODYNAMICS CHARACTERIZATION OF ICE GIANTS ATMOSPHERIC ENTRY | ICAS2024_0872 |
| Pasquali, C. | A BOUNDARY INTEGRAL EQUATION FORMULATION FOR POTENTIAL COMPRESSIBLE FLOWS AROUND DEFORMABLE BODIES | ICAS2024_0676 |
| Pasquali, M. | CYBER-PHYSICAL SYSTEM IMPLEMENTATION FOR THE AR-ASSISTED AIT OF AEROSPACE COMPONENTS | ICAS2024_0672 |
| Passieux, J.-C. | MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE SCALE | ICAS2024_0290 |
| Patriarca, R. | ENSURING THE NEXT GENERATION GREEN AIRCRAFT’ SUSTAINABILITY FROM THE DESIGN PHASE VIA A LIFE-CYCLE COST ANALYSIS | ICAS2024_0350 |
| Patterson, M.D. | EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS | ICAS2024_0464 |
| Pauen, J. | TOWARDS REFINED CONTRAIL SIMULATIONS OF FORMATION FLIGHT SCENARIOS | ICAS2024_0502 |
| Paula, T.R. | FLIGHT PATH RECONSTRUCTION OF A FLEXIBLE WING UAV WITH WING MOUNTED VANES | ICAS2024_1176 |
| Pauvert, V. | INCREMENTAL TRADE-OFF STUDY OF A HYDROGEN FUEL CELL-BASED PROPULSION SYSTEM USING MDAO TECHNIQUES | ICAS2024_0301 |
| Pavan, G. | ENVIRONMENTAL AND ECONOMIC ASSESSMENT OF AN EVTOL AIRCRAFT FLEET FOR URBAN AIR MOBILITY | ICAS2024_0500 |
| Pecora, R. | TRADE OFF STUDIES ON WING MANEUVER LOAD ALLEVIATION STRATEGIES BASED ON AILERONS AND WINGLETS MOVABLE SURFACES | ICAS2024_0130 |
| Pei, Y. | RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS | ICAS2024_0550 |
| Pei, Z. | NUMERICAL INVESTIGATION OF THE FLOW FEATURES ON THE TURRET WITH DIFFERENT CYLINDER HEIGHT IN THE TRANSONIC FLOW | ICAS2024_0282 |
| Peng, H. | FATIGUE CRACK LIFE PREDICTION BASED ON BAYESIAN DYNAMIC UPDATE | ICAS2024_0393 |
| Peng, H. | STUDY ON FATIGUE PROPERTIES OF TITANIUM ALLOY BASE MATERIAL AND WELDED STRUCTURE IN THERMAL COMBINED ENVIRONMENT | ICAS2024_0422 |
| Peng, M. | PROBING AND MODELING LARGE-SCALE AIRLINE NETWORK DISRUPTIONS: 2022 SOUTHWEST AIRLINES SCHEDULING CRISIS | ICAS2024_0782 |
| Peng, S.-T. | NUMERICAL INVESTIGATION ON THE EFFECT OF REYNOLDS NUMBER ON TANDEM DROPLET | ICAS2024_0426 |
| Peng, X. | EFFICIENT MULTI-FIDELITY REDUCED-ORDER MODELING FOR FLUTTER PREDICTIONS ACROSS MULTIPLE MACH NUMBERS | ICAS2024_0900 |
| Pepelea, D. | AERODYNAMIC NUMERICAL/EXPERIMENTAL COMPARISON OF A HYPERSONIC TEST VEHICLE IN MORE&LESS PROGRAM | ICAS2024_1026 |
| Pereira, A. | AIRCRAFT WING STRUCTURAL SIZING COMPUTATIONAL TOOL TAILORED FOR A COLLABORATIVE MULTIDISCIPLINARY DESIGN FRAMEWORK | ICAS2024_0079 |
| Pereira, L. | A HUMAN-CENTERED SYSTEMS ENGINEERING APPROACH FOR INTEGRATING ARTIFICIAL INTELLIGENCE IN AVIATION: A REVIEW OF AI SYSTEMS | ICAS2024_0397 |
| Pereira do Prado, A. | INFLUENCE OF SKIN CURVATURE ON WINGBOX OPTIMIZATION WITH NONLINEAR STRUCTURAL STABILITY CONSTRAINTS | ICAS2024_0114 |
| Pereira Mesquita, A.C. | HOLISTIC AND SCALABLE SMART OPTIMIZATION FRAMEWORK FOR PRESCRIPTIVE MAINTENANCE | ICAS2024_0657 |
| Perez, R.E. | LOCALIZED AERODYNAMIC SHAPE OPTIMIZATION FOR AUTOMOTIVE APPLICATIONS | ICAS2024_0265 |
| Perez, R.E. | LONGITUDINAL STABILITY PARAMETERS FOR FLYING BOOM AERIAL REFUELING | ICAS2024_0371 |
| Perez, R.E. | SYSTEM OF SYSTEMS ANALYSIS OF AUTONOMOUS AIRCRAFT OPERATIONS IN AIR CARGO FEEDER NETWORKS | ICAS2024_0413 |
| Perez, R.E. | CHARACTERIZATION OF EXTERNAL LIQUID HYDROGEN TANK INTERFERENCE DRAG | ICAS2024_0414 |
| Perez, R.E. | MODELING CARGO DEMAND FOR REGIONAL AIR TRANSPORT NETWORKS IN CANADA AND THE UNITED STATES | ICAS2024_0729 |
| Périé, J.-N. | MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE SCALE | ICAS2024_0290 |
| Peristy, L.H. | LONGITUDINAL STABILITY PARAMETERS FOR FLYING BOOM AERIAL REFUELING | ICAS2024_0371 |
| Perron, C. | PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS | ICAS2024_1296 |
| Persson, M. | AIRPORT CHARGING SYSTEM DESIGNS AND POWER MANAGEMENT FOR MEGAWATT-LEVEL CHARGING OF BATTERY-ELECTRIC AIRCRAFT | ICAS2024_0442 |
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| Petrolo, M. | COUPLED THERMOELASTIC ANALYSIS OF BEAM STRUCTURES USING A REFINED 1D FINITE ELEMENT MODEL | ICAS2024_0854 |
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| Petrosino, F. | DUAL-STREAM JET NOISE TEST WITH INTERNAL MIXER DESIGN VARIATIONS FOR LTO NOISE OF SUPERSONIC AIRCRAFT | ICAS2024_0064 |
| Petrosino, F. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Petrosino, F. | SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT | ICAS2024_0361 |
| Petrosino, F. | SONIC BOOM COMPARATIVE STUDY BETWEEN MACH 4.7 OUTDOOR EXPERIMENTAL TESTS AND NUMERICAL SIMULATIONS | ICAS2024_0882 |
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| Pezzella, G. | FLUIDODYNAMIC ANALYSIS OF LOW REYNOLDS NUMBER FLOWS | ICAS2024_0354 |
| Pezzella, G. | SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT | ICAS2024_0361 |
| Pezzella, G. | ENGINEERING-BASED TOOL FOR THREE-DIMENSIONAL ESTIMATIONS OF RE-ENTRY VEHICLES AEROTHERMODYNAMICS | ICAS2024_0859 |
| Pezzella, G. | OPTIMIZATION PROCEDURE FOR THE WING OF A MARS EXPLORATION DRONE | ICAS2024_0862 |
| Pezzella, G. | PRELIMINARY DESIGN OF A FIXED-WING DRONE FOR MARS EXPLORATION ACTIVITIES | ICAS2024_0863 |
| Pezzella, G. | LOW SPEED AERODYNAMICS OF SIX OPTIMISED UNCONVENTIONAL RE-ENTRY VEHICLE AEROSHAPES | ICAS2024_0864 |
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| Piacquadio, S. | NUMERICAL TOOLS FOR SLOW-GROWTH APPROACHES TO DAMAGE TOLERANT COMPOSITE AERONAUTICAL STRUCTURES | ICAS2024_1146 |
| Piccirillo, G. | ESATTO: THE HOLISTIC FRAMEWORK TO SUPPORT THE DESIGN OF SUSTAINABLE SUPERSONIC AVIATION | ICAS2024_1032 |
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| Pinelli, L. | HIGH FIDELITY MODELING OF ACOUSTIC LINERS FOR AERONAUTICAL APPLICATIONS | ICAS2024_1048 |
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| Piprek, P. | ONBOARD TRAJECTORY OPTIMIZATION FOR RADIUS TO FIX TURNS | ICAS2024_0271 |
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| Pirrera, A. | INFLUENCE OF SKIN CURVATURE ON WINGBOX OPTIMIZATION WITH NONLINEAR STRUCTURAL STABILITY CONSTRAINTS | ICAS2024_0114 |
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| Pla Guerrero, D. | HARDWARE-IN-THE-LOOP SIMULATION FRAMEWORK FOR THE EVALUATION OF AUTONOMOUS FLIGHT FUNCTIONS | ICAS2024_0897 |
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| Qian, W. | REDUCED ORDER MODELLING OF UNSTEADY AERODYNAMICS FOR GROUND FLUTTER TEST SYSTEM | ICAS2024_0430 |
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| Qian, W. | MODELING AND VALIDATION OF MORPHING WING TRAILING EDGE BASED ON ZERO POISSON'S RATIO HONEYCOMB | ICAS2024_1015 |
| Qian, Z. | EFFECT OF FREESTREAM DISTURBANCES ON BOUNDARY LAYER TRANSITION IN HYPERSONIC WIND TUNNEL | ICAS2024_0540 |
| Qiao, H. | A NUMERICAL VIRTUAL FLIGHT PLATFORM DEVELOPMENT AND ITS APPLICATION ON HIGH MANEUVERABILITY FLIGHT VEHICLES | ICAS2024_0035 |
| Qiao, H. | NUMERICAL AND THEORETICAL INVESTIGATION OF HELICOPTER DITCHING WITH VARIOUS INITIAL VELOCITY AND PITCHING ANGLE | ICAS2024_0216 |
| Qiao, H.-L. | FAST PARAMETRIC STRUCTURE MODELING FOR VARIETY OF AIRCRAFT CONFIGURATIONS | ICAS2024_0614 |
| Qiao, H.-L. | EXPLORATION OF EFFICIENT HYPERPARAMETERS ADAPTION OF SUPPORT VECTOR REGRESSION FOR AERODYNAMIC DESIGN | ICAS2024_0625 |
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| Raab, C. | MEASURING THE ANGLE OF ATTACK – PRACTICAL CONSIDERATIONS FOR THE DEVELOPMENT OF FAULT DETECTION RESIDUALS | ICAS2024_0156 |
| Racionero Sánchez-Majano, A. | AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING DESIGN | ICAS2024_0167 |
| Raddatz, F. | MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION | ICAS2024_0020 |
| Raddatz, F. | CINNABAR PROJECT – COST-BENEFIT ANALYSIS OF DIGITAL PROCESSES FOR NON-DESTRUCTIVE INSPECTIONS OF AIRCRAFT STRUCTURES | ICAS2024_0125 |
| Raddatz, F. | TRAIN ON SYNTHETIC - TEST ON REAL: DOMAIN ADAPTATION FOR STRAIN-BASED DAMAGE DETECTION ON AN AIRCRAFT WING | ICAS2024_0169 |
| Rade, D.A. | STOCHASTIC BUCKLING ANALYSES OF LAMINATED COMPOSITE PLATES UNDER HYGROTHERMAL, GEOMETRIC AND MATERIAL UNCERTAINTIES MODELED AS NON-GAUSSIAN RANDOM FIELDS | ICAS2024_1097 |
| Radestock, M. | PERFORMANCE AND ECONOMIC ASSESSMENT OF A WING-INTEGRATED HYBRID LAMINAR FLOW CONTROL SYSTEM | ICAS2024_0097 |
| Rafael, C.F. | INITIAL DEVELOPMENT OF A CFD ICING TOOL | ICAS2024_1112 |
| Rahn, A. | SUSTAINABLE ENGINE MAINTENANCE: EVALUATING THE ECOLOGICAL IMPACT OF LIFE LIMITED PART REPLACEMENT | ICAS2024_0452 |
| Raj, P. | EFFECTIVENESS OF CFD FOR AIRCRAFT DESIGN: STATUS AND PROSPECTS | ICAS2024_0283 |
| Raj, P. | EFFECTIVENESS OF CFD FOR AIRCRAFT DESIGN: STATUS AND PROSPECTS PART 2 | ICAS2024_1313 |
| Rajashankar, S. | MODEL-BASED CONCEPTUAL DESIGN AND EVALUATION OF A SOLID-FUEL SCRAMJET VEHICLE | ICAS2024_0195 |
| Rakov, D. | A MORPHOLOGICAL ANALYSIS OF METHODS FOR CONCEPTUAL AIRCRAFT DESIGN UNDER UNCERTAINTIES | ICAS2024_1169 |
| Ramírez, F.N. | EFFECT OF POPULAR ADDITIVE MANUFACTURING TECHNOLOGIES ON THE PERFORMANCE AND ACOUSTICS OF UAV PROPELLERS | ICAS2024_0896 |
| Ramírez, F.N. | PERFORMANCE AND ACOUSTIC ANALYSIS OF A DISTRIBUTED ELECTRIC PROPULSION UNMANNED AIRCRAFT | ICAS2024_1009 |
| Ramirez Correra, E. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Ramm, J. | SUSTAINABLE ENGINE MAINTENANCE: EVALUATING THE ECOLOGICAL IMPACT OF LIFE LIMITED PART REPLACEMENT | ICAS2024_0452 |
| Ran, X. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AEROELASTICITY OF HIGH-ASPECT-RATIO WINGS | ICAS2024_0423 |
| Ran, X.-J. | COMPUTATIONAL/EXPERIMENTAL AEROELASTIC STUDY FOR AN ALL-MOVABLE HORIZONTAL TAIL WITH TORSION FREE-PLAY | ICAS2024_0728 |
| Ranuzzi, G. | PROPULSIVE CFD ANALYSIS OF THE SCRAMJET HYPERSONIC EXPERIMENTAL VEHICLE | ICAS2024_0255 |
| Ranuzzi, G. | LAUNCH SYSTEM ASSESSMENT OF AN EXPERIMENTAL HYPERSONIC SCRAMJET VEHICLE | ICAS2024_0363 |
| Rao, A.G. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Rao, A.G. | CFD-BASED SCOUTING FOR THE DESIGN OF A MULTI-FUEL KEROSENE/HYDROGEN ATMOSPHERIC BURNER | ICAS2024_0432 |
| Rao, C. | AERO-KINEMATIC OPTIMIZATION OF HIGH-LIFT DEVICES WITH DOWNWARD DEFLECTION OF SPOILER | ICAS2024_0639 |
| Rasines, J. | ON THE CHALLENGES OF SURROGATE-BASED AERODYNAMIC SHAPE OPTIMISATION | ICAS2024_0319 |
| Raspaolo, G. | ENHANCING QUADCOPTER CONTROL: A MODEL REFERENCE ADAPTIVE CONTROL APPROACH WITH NEURAL NETWORKS | ICAS2024_0459 |
| Raspaolo, G. | A SIMULINK APPROACH TO MODELING HETEROGENEOUS DRONE FORMATIONS FOR AGENT-BASED SIMULATION | ICAS2024_0608 |
| Ratei, P. | A SYSTEM OF SYSTEMS AIRCRAFT DESIGN FRAMEWORK: DEMONSTRATION USING A SEAPLANE TRANSPORT NETWORK IN THE GREEK ISLANDS | ICAS2024_0402 |
| Ratei, P. | EU IMPACT MONITOR PROJECT - OVERVIEW AND APPROACH | ICAS2024_1114 |
| Ratsifandrihana, L. | A DIGITAL METHOD FOR THE COMPENSATED MOLD DESIGN OF COMPOSITE PARTS | ICAS2024_0487 |
| Rauscher, F. | MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION | ICAS2024_0020 |
| Raute, R. | A SENSITIVITY ANALYSIS ON THE ENDURANCE EQUATION FOR HYBRID-ELECTRIC AIRCRAFT | ICAS2024_1109 |
| Raymer, D. | ON THE AERODYNAMIC CHARACTERISTICS OF CRESCENT WING | ICAS2024_0579 |
| Raza, H. | BIRD AND DRONE IMPACT DAMAGE PROGNOSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT ENGINE | ICAS2024_1162 |
| Rebollo, M. | DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS | ICAS2024_0229 |
| Recine, C. | SIZING AND PERFORMANCE ANALYSIS OF A MW-CLASS ELECTRIFIED AIRCRAFT PROPULSION (EAP) SYSTEM FOR A PARALLEL HYBRID TURBOPROP CONCEPT | ICAS2024_0884 |
| Reckzeh, D. | PERSPECTIVES ON FLOW CONTROL APPLICATIONS FOR LARGE TRANSPORT AIRCRAFT | ICAS2024_1297 |
| Rehder, I.S. | ASSESSING MENTAL WORKLOAD AND INTERFACE USABILITY IN MILITARY PILOTS: AN ADVANCED EYE-TRACKING METHODOLOGY | ICAS2024_0202 |
| Reimer, F. | INVESTIGATING THE FLEXIBLE HYDROGEN AIRCRAFT SYSTEM INTERFACE DESIGN USING THE XR CO-DESIGN APPROACH | ICAS2024_0358 |
| Reis, M.S. | A-BASIS AND B-BASIS BUCKLING ALLOWABLES FOR AN AIRCRAFT COMPOSITE WING | ICAS2024_0322 |
| Ren, J. | WALL TEMPERATURE EFFECTS ON AERODYNAMIC HEATING MECHANISMS IN SHOCK WAVE TURBULENT BOUNDARY LAYER INTERACTION | ICAS2024_0569 |
| Ren, K. | ACTIVE-PASSIVE HYBRID CONTROL OF SHOCK BUFFET | ICAS2024_0792 |
| Resende Rodrigues da Silva, A. | MODELLING ASTEROID TRAJECTORY IN EARTH’S ATMOSPHERE | ICAS2024_0158 |
| Revello, E. | POTENTIAL APPLICATION OF PHASE CHANGE MATERIALS FOR THERMAL MANAGEMENT SYSTEM OF NEXT GENERATION AIRCRAFT | ICAS2024_0295 |
| Reyner, C. | MISSION-BASED OPTIMAL PROPELLER SELECTION FOR VTOL SUAV CONFIGURATION | ICAS2024_0564 |
| Reyner, C. | DATA-DRIVEN MULTI-RANGE MISSION-BASED OVERALL AIRCRAFT CONCEPTUAL DESIGN OPTIMIZATION | ICAS2024_0611 |
| Reynolds, J.R. | DISTRIBUTED THRUST TAKEOFF FOR THE NASA X-57 MOD IV FLIGHT DEMONSTRATOR | ICAS2024_1290 |
| Reynolds, T. | COMPARING CONVECTIVE WEATHER IMPACTS ON AIR TRAFFIC MANAGEMENT OPERATIONS IN UNITED STATES, CANADA & EUROPE | ICAS2024_0137 |
| Reynolds, T. | WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES | ICAS2024_1137 |
| Reysset, A. | STUDY OF HYBRIDISATION SCENARIOS FOR TURBOPROP AIRCRAFT IN THE GENERAL AVIATION SEGMENT | ICAS2024_0153 |
| Rezende Sanches, L.V. | ADJOINT-BASED TRANSONIC WING AERODYNAMIC SHAPE OPTIMIZATION INVESTIGATIONS | ICAS2024_0078 |
| Rezgui, D. | CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT: HIGH ASPECT RATIO WINGS AND FLOATING WINGTIPS | ICAS2024_0386 |
| Riaz, A. | SET-BASED DESIGN TECHNIQUES FOR EVOLVABILITY EXPLORATION DURING CONCEPTUAL AIRCRAFT DESIGN | ICAS2024_0233 |
| Riaz, A. | DESIGN OF THE SENECA MACH 1.8 SUPERSONIC AIRLINER WITH MULTI-FIDELITY AERODYNAMIC ANALYSIS FOR NOISE-OPTIMISED TAKE-OFF TRAJECTORIES | ICAS2024_0758 |
| Riboldi, C.E.D. | STEADY ANALYSIS OF THREE-SURFACE AIRPLANES: IMPROVING THE AERODYNAMIC PERFORMANCE THROUGH REDUNDANT LONGITUDINAL CONTROL | ICAS2024_0273 |
| Riboldi, C.E.D. | PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION PLASMA THRUSTERS | ICAS2024_0649 |
| Riboldi, C.E.D. | METHODOLOGIES FOR THE PRELIMINARY SIZING OF HYDROGEN-POWERED AIRCRAFT AND SUPPORTING AIRPORT INFRASTRUCTURES | ICAS2024_1002 |
| Riboldi, C.E.D. | CONCEPTUAL DESIGN OF A ZERO-EMISSION REGIONAL AIRCRAFT FOR ENHANCED SHORT-HAUL MOBILITY | ICAS2024_1085 |
| Riboldi, C.E.D. | IDENTIFICATION OF THE IMPACT OF BLOWING ON THE AERODYNAMIC MODEL OF AN AIRPLANE WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2024_1134 |
| Riccardi, G. | CORUS-XUAM: TACKLING URBAN AIR MOBILITY AIRSPACE INTEGRATION CHALLENGES | ICAS2024_0347 |
| Ricci, F. | CONVOLUTIONAL NEURAL NETWORKS ALGORITHMS FOR STRUCTURAL HEALTH MONITORING OF AIRCRAFTS COMPOSITES PANELS | ICAS2024_0120 |
| Ricci, S. | MULTI-OBJECTIVE DESIGN OPTIMIZATION OF A MORPHING AILERON FOR A HYBRID ELECTRIC REGIONAL AIRCRAFT | ICAS2024_0385 |
| Ricci, S. | AEROELASTIC ISSUES IN THE DESIGN OF HIGH ASPECT RATIO STRUT-BRACED WING AIRCRAFT | ICAS2024_0874 |
| Riccio, A. | REDESIGN OF AN AERONAUTICAL COMPOSITE STIFFENED PANEL WITH THE DOUBLE-DOUBLE DESIGN APPROACH | ICAS2024_0360 |
| Richter, C. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Richter, M. | EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR | ICAS2024_0518 |
| Richters, J. | ROUTE PLANNING FOR VOLCANIC ASH AND RADIOACTIVITY IN-SITU DRONE MEASUREMENTS USING A GENETIC ALGORITHM AND KRIGING | ICAS2024_0406 |
| Rider, C. | VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA | ICAS2024_0104 |
| Rietdijk, B. | ARCHITECTURE DESIGN FOR A COMMERCIALLY VIABLE HYDROGEN-ELECTRIC POWERED RETROFITTED REGIONAL AIRCRAFT | ICAS2024_1090 |
| Riganti, M. | FASTVIBE SW TOOL FOR RIDE-ALONG VIBRATION SURVEY ANALYSIS | ICAS2024_0455 |
| Rigliaco, G. | REDESIGN OF AN AERONAUTICAL COMPOSITE STIFFENED PANEL WITH THE DOUBLE-DOUBLE DESIGN APPROACH | ICAS2024_0360 |
| Ringelberg, W.M. | DISTRIBUTED THRUST TAKEOFF FOR THE NASA X-57 MOD IV FLIGHT DEMONSTRATOR | ICAS2024_1290 |
| Ripamonti, F. | FLUID-STRUCTURE INTERACTION OF TWO-PHASE SCATTERER METAMATERIALS FOR VIBRATION SELF-SUPPRESSION | ICAS2024_0435 |
| Riso, C. | EXPLORING ROLL MANEUVERABILITY OF FUTURE AIRCRAFT WITH HIGH AR WINGS | ICAS2024_1286 |
| Ritschel, M. | EXPERIMENTAL INVESTIGATION OF THE DLR-F23 CONFIGURATION AT TRANSONIC SPEEDS USING FAST-RESPONSE PRESSURE-SENSITIVE PAINT | ICAS2024_0710 |
| Ritter, M.R. | PRELIMINARY STRUCTURAL DESIGN OF A HIGH ASPECT RATIO RANSPORT AIRCRAFT WITH LAMINAR WING | ICAS2024_0604 |
| Rivera, R.D.B. | PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS | ICAS2024_1296 |
| Rivero, I. | DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS | ICAS2024_0229 |
| Rivers, M. | NASA CONTRIBUTIONS TO THE HIGH LIFT COMMON RESEARCH MODEL ECOSYSTEM | ICAS2024_1213 |
| Riyadl, A. | DETACHED EDDY SIMULATION OF HYPERSONIC SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE-CYLINDER-FLARE | ICAS2024_1175 |
| Rodeck, R. | CINNABAR PROJECT - AUGMENTED REALITY WORKFLOW FOR AIRCRAFT DENT & BUCKLE INSPECTION | ICAS2024_0152 |
| Rodeck, R. | CINNABAR PROJECT: EXAMINING REQUIREMENTS FOR USER ACCEPTANCE OF AIRCRAFT STRUCTURE INSPECTION IN AUGMENTED REALITY | ICAS2024_0164 |
| Rodriguez DE Leon, R. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Rodríguez-Sevillano, A.A. | EXPLORING WINGTIP COLUMNAR VORTEX GENERATORS FOR UAV PERFORMANCE ENHANCEMENT | ICAS2024_0219 |
| Roesing, J. | FACTORS INFLUENCING THE CLIMATE-RELEVANT ENVIRONMENTAL IMPACT OF AIR TRANSPORT COMPARED TO RAIL AND ROAD TRANSPORT | ICAS2024_0671 |
| Roh, N. | MAXIMUM SPEED OF BATTERY-POWERED TILT-ROTOR AIRCRAFT | ICAS2024_0141 |
| Roh, N. | DETERMINISTIC HYBRID POWER RATIOS CONSIDERING VARIOUS FAILURE CASES FOR QUAD TILTROTOR AIRCRAFT | ICAS2024_0352 |
| Romano, F. | DAMAGE TOLERANCE OF A CURVED COMPOSITE STIFFENED PANEL FABRICATED BY AN OUT OF AUTOCLAVE – LIQUID RESIN INFUSION PROCESS | ICAS2024_1158 |
| Romano, G. | A SUPPORTING FRAMEWORK FOR AIRCRAFT MRO OPERATIONS. CAPACITY PLANNING, TASKS TRACEABILITY AND DISEMBARKED ITEMS TRACKING | ICAS2024_0100 |
| Roncioni, P. | PROPULSIVE CFD ANALYSIS OF THE SCRAMJET HYPERSONIC EXPERIMENTAL VEHICLE | ICAS2024_0255 |
| Roncioni, P. | LAUNCH SYSTEM ASSESSMENT OF AN EXPERIMENTAL HYPERSONIC SCRAMJET VEHICLE | ICAS2024_0363 |
| Roncioni, P. | AERODYNAMIC NUMERICAL/EXPERIMENTAL COMPARISON OF A HYPERSONIC TEST VEHICLE IN MORE&LESS PROGRAM | ICAS2024_1026 |
| Roncolini, E. | AEROELASTIC ISSUES IN THE DESIGN OF HIGH ASPECT RATIO STRUT-BRACED WING AIRCRAFT | ICAS2024_0874 |
| Rosen Jacobson, D. | BATTERY PERFORMANCE METRICS FOR LARGE ELECTRIC PASSENGER AIRCRAFT | ICAS2024_0636 |
| Rossato, D.B. | SELF-DRIVING AND MODEL-BASED EXTREMUM SEEKING CONTROL IN TIGHT FORMATION FLIGHT FOR FUEL SAVING | ICAS2024_0861 |
| Rossetti, F. | NUMERICAL INVESTIGATION ON THE LIQUID SLOSHING DAMPING INSIDE A TANK WITH A FLEXIBLE ANTI-SLOSHING DEVICE | ICAS2024_0930 |
| Rossi, F. | NUMERICAL SOLUTION OF LOX FLOW IN A LIQUID ROCKET ENGINE ADDITIVELY MANUFACTURED COOLING CHANNEL | ICAS2024_0105 |
| Rossignol, C. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Roth, Y.C. | FUSELAGE, CABIN & CARGO AND EMPENNAGE OF TOMORROW @ AIRBUS COMMERCIAL - NEW FUSELAGE DESIGN & MATERIALS | ICAS2024_1318 |
| Roth, Y.C. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Rothe, D. | GENERAL DESIGN CONSIDERATIONS FOR SOLAR-ELECTRIC HIGH-ALTITUDE LONG-ENDURANCE AIRCRAFT | ICAS2024_0910 |
| Roux, P.-E. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Rovelli, M. | HYBRID AIR DATA SYSTEM ARCHITECTURE: FROM DESIGN TO FLIGHT TEST VERIFICATION | ICAS2024_0056 |
| Roy, C.J. | THE BEVERLI HILL EXPERIMENTS FOR SMOOTH-BODY TURBULENT FLOW SEPARATION - RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS | ICAS2024_1219 |
| Ruan, J.L. | IMPACT OF HYDROGEN FUEL ON OVERALL DESIGN OF TRANSPORT AIRCRAFT | ICAS2024_0826 |
| Ruan, R. | AN EXPERIMENTAL SIMULATION ON THE INFLUENCE OF DIFFERENT FILM COOLING HOLE SHAPES ON PARTICLE DEPOSITION ON TURBINE VANE | ICAS2024_0341 |
| Ruberte Bailo, J. | DESIGN OF A HIGHLY EFFICIENT TRANSPORT NLF AIRCRAFT WITH A BACKWARD SWEPT WING AND A LONG SINGLE-AISLE FUSELAGE | ICAS2024_0102 |
| Rudnik, R. | THE CRM-HL ECOSYSTEM - DLR CONTRIBUTIONS | ICAS2024_1214 |
| Rumsey, C.L. | HIGH-LIFT PREDICTION WORKSHOPS: RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS | ICAS2024_1217 |
| Runacres, M. | PASSIVE FLOW CONTROL DEVICES ON LOW-REYNOLDS DU89-134 AIRFOIL | ICAS2024_0228 |
| Ruocco, M. | COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH | ICAS2024_1138 |
| Russo, A.C. | ASSESSING MENTAL WORKLOAD AND INTERFACE USABILITY IN MILITARY PILOTS: AN ADVANCED EYE-TRACKING METHODOLOGY | ICAS2024_0202 |
| Russo, O. | PROPULSIVE CFD ANALYSIS OF THE SCRAMJET HYPERSONIC EXPERIMENTAL VEHICLE | ICAS2024_0255 |
| Russo, O. | LAUNCH SYSTEM ASSESSMENT OF AN EXPERIMENTAL HYPERSONIC SCRAMJET VEHICLE | ICAS2024_0363 |
| Russo, P. | PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS | ICAS2024_1205 |
| Ruzek, R. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Sabag, D.Y. | DIGITAL TWIN OF AN AIRCRAFT LANDING GEAR TO ENHANCE FAILURE ANALYSIS AND MANAGE PREDICTIVE MAINTENANCE | ICAS2024_0065 |
| Saccaggi, E. | GENETIC ALGORITHM OPTIMIZATION OF AN OPPOSITION CONTROL STRATEGY IN A FULLY TURBULENT CHANNEL FLOW | ICAS2024_1208 |
| Saccone, G. | INTEGRATING ECO-EFFICIENT FLIGHT PLANNING IN AIRCRAFT CONCEPTUAL DESIGN: MINIMAL NOX ROUTES FOR HIGH-SPEED AIRCRAFT USING HYDROGEN | ICAS2024_0950 |
| Saccone, G. | ESATTO: THE HOLISTIC FRAMEWORK TO SUPPORT THE DESIGN OF SUSTAINABLE SUPERSONIC AVIATION | ICAS2024_1032 |
| Saghafi, F. | AN OPTICAL FLOW BASED GUIDANCE ALGORITHM FOR A QUADROTOR UAV MOVING INSIDE CIRCULAR CORRIDORS | ICAS2024_1209 |
| Sagvolden, G. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Sakellariou, J.S. | IN-FLIGHT VIBRATION SIGNAL BASED DETECTION AND LOCALIZATION FOR UAV PROPELLER ANOMALIES UNDER UNCERTAINTY VIA MACHINE LEARNING TYPE METHODS | ICAS2024_0984 |
| Salazar, M. | AIRPORT INFRASTRUCTURE SIZING FOR A REGIONAL ELECTRIC AVIATION NETWORK | ICAS2024_0686 |
| Sales, C. | DISTRIBUTED THRUST TAKEOFF FOR THE NASA X-57 MOD IV FLIGHT DEMONSTRATOR | ICAS2024_1290 |
| Salgas, A. | AN EMPIRICAL AND CUSTOMISABLE FLEET RENEWAL MODEL FOR PROSPECTIVE SCENARIOS USING OPEN-ACCESS DATA | ICAS2024_0367 |
| Salucci, F. | ENERGY AND EMISSION ANALYSIS OF AN AIR-TAXI SERVICE USING DYNAMIC EVTOL SYSTEM MODELS | ICAS2024_0172 |
| Salucci, F. | ANALYZING THE IMPACTS OF SUSTAINABLE POWERTRAINS FOR SHORT-HAUL COMMUTER AIRLINES | ICAS2024_0175 |
| Salucci, F. | CONCEPTUAL DESIGN OF A ZERO-EMISSION REGIONAL AIRCRAFT FOR ENHANCED SHORT-HAUL MOBILITY | ICAS2024_1085 |
| Samanyusree, V. | EMBEDDED SENSORS FOR AIRCRAFT PREDICTIVE MAINTENANCE: SHM SYSTEM INTEGRATION & TRADE-OFF ANALYSIS | ICAS2024_1081 |
| Samanyusree, V. | USE OF GRAPHENE MATERIAL IN AIRCRAFT STRUCTURE FOR LIGHTNING STRIKE PROTECTION | ICAS2024_1141 |
| Samardžic, M. | UPGRADE OF THE VTI T-38 BLOWDOWN TRISONIC TEST FACILITY: WIND TUNNEL CONTROL SYSTEM | ICAS2024_0456 |
| Samuelsson, P. | LOW-SPEED PROPELLER FOR UAV APPLICATIONS, FROM DESIGN TO EXPERIMENTAL EVALUATION | ICAS2024_1157 |
| Sanby, B. | VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA | ICAS2024_0104 |
| Sanchez Santos, C. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Sanders, M.P.J | FLYING WING CIRCULATION DISTRIBUTIONS, AERODYNAMIC PERFORMANCE AND WAKE ROLL-UP | ICAS2024_1153 |
| Sanghi, D. | EXPLORING ROLL MANEUVERABILITY OF FUTURE AIRCRAFT WITH HIGH AR WINGS | ICAS2024_1286 |
| Sanjeevekumar, D. | A PERFORMANCE COMPARISON OF HYDROGEN AIRCRAFT CONCEPTS | ICAS2024_0251 |
| Sanna, M. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Sanned, D. | EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR | ICAS2024_0518 |
| Santagata, G. | PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS | ICAS2024_1205 |
| Santarella, G. | CFD STUDY OF AIR SUPPLY SYSTEM FOR COOLING OF A HYDROGEN POWERED UNMANNED SEAPLANE AND REDUCTION OF THE RESULTING DRAG | ICAS2024_0736 |
| Santarelli, M. | ASSESSING THE TECHNICAL VIABILITY OF ALL-ELECTRIC HYDROGEN-POWERED AIRCRAFTS | ICAS2024_1003 |
| Santelli, F. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF A STRUCTURAL-DYNAMICALLY SCALED DELTA WING WITH TRAINING EDGE FLAPS | ICAS2024_0853 |
| Santori, M. | COUPLED THERMOELASTIC ANALYSIS OF BEAM STRUCTURES USING A REFINED 1D FINITE ELEMENT MODEL | ICAS2024_0854 |
| Santori, M. | HIGHER-ORDER 1D STICK MODELS FOR THE FLUTTER ANALYSIS OF AIRCRAFT STRUCTURES | ICAS2024_1001 |
| Santoro, C. | A MODEL PREDICTIVE CONTROL ALGORITHM FOR THE FORMATION CONTROL OF NANOSATELLITES IN LEO ORBIT | ICAS2024_0494 |
| Santos, H.E.A.A. | STOCHASTIC BUCKLING ANALYSES OF LAMINATED COMPOSITE PLATES UNDER HYGROTHERMAL, GEOMETRIC AND MATERIAL UNCERTAINTIES MODELED AS NON-GAUSSIAN RANDOM FIELDS | ICAS2024_1097 |
| Santos, L.F.F.M. | INSIGHTS INTO HUMAN FATIGUE: STATISTICAL ANALYSIS IN AIRCRAFT MAINTENANCE | ICAS2024_0131 |
| Sanz Diaz, R. | STRUCTURED H-INFINITY DESIGN OF PREDICTORS FOR THE MONITORING OF AN AIRCRAFT IN ITS FLIGHT ENVELOPE | ICAS2024_0223 |
| Sapienza, V. | EXPERIMENTAL RESULTS OF ANTENNA PLACEMENT TEST ON A CARBON-FIBER SCALE REPLICA OF THE S55X SEAPLANE | ICAS2024_0504 |
| Sapienza, V. | NUMERICAL-THEORETICAL EVALUATION OF THE DITCHING OF A HULL WITH DIHEDRAL ANGLES BETWEEN -5 AND 20 DEGREES | ICAS2024_0665 |
| Saporiti, A. | A CFD STUDY OF THE ACTIVE FLOW CONTROL SYSTEM BEHAVIOUR ON A VERTICAL TAIL SECTION OF AN AIRPLANE, WITH THE AID OF AI | ICAS2024_0741 |
| Saputo, S. | MACRO, MESO AND MICRO SCALE ENERGY EVALUATION IN LAMINATED AND COMPOSITE STRUCTURES USING THE COMPONENT-WISE APPROACH | ICAS2024_0252 |
| Sarmento, A. | ASSESSING MENTAL WORKLOAD AND INTERFACE USABILITY IN MILITARY PILOTS: AN ADVANCED EYE-TRACKING METHODOLOGY | ICAS2024_0202 |
| Sarmento, A. | MULTIPLATFORM SIMULATION USING ROS | ICAS2024_0755 |
| Sarmento, A.G.P. | FAULT DETECTION FOR AN AIRCRAFT ELEVATOR | ICAS2024_0647 |
| Sarr, A. | MODEL-BASED APPROACH FOR HYDROGEN PRELIMINARY AIRCRAFT DESIGN CONSIDERING SAFETY AND OPERABILITY | ICAS2024_0095 |
| Sasongko, R.A. | A NOVEL APPROACH TO AUTOMATED TRACKING CONTROL OF HYBRID TILTING ROTOR UAVS USING LQG CONTROLLER AND STATE MACHINE | ICAS2024_0535 |
| Sato, G. | DEMAND CAPACITY BALANCING FOR URBAN AIR MOBILITY USING MULTIAGENT SIMULATION | ICAS2024_0953 |
| Sato, M. | MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM | ICAS2024_0573 |
| Satwan, P. | EXPLORATION AND EVALUATION OF KNOWLEDGE-BASED ENGINEERING APPROACH FOR LIQUID HYDROGEN TANK INTEGRATION IN EXISTING FUSELAGE | ICAS2024_0488 |
| Savian, S.S. | JETZERO: RESHAPING AVIATION WITH THE BLENDED WING | ICAS2024_1305 |
| Savino, R. | AERODYNAMIC ANALYSIS OF A FLAP-BASED DEPLOYABLE RE-ENTRY SYSTEM UNDER RAREFIED CONDITIONS | ICAS2024_1201 |
| Sawaki, Y. | TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2024_1215 |
| Saxena, S. | TOWARDS SUSTAINABLE AVIATION WITH EFFICIENT AIRSPACE OPERATIONS | ICAS2024_1247 |
| Sbarufatti, C. | ON THE DEVELOPMENT OF THE STRUCTURAL DIGITAL TWIN OF AN UNMANNED AERIAL VEHICLE | ICAS2024_0724 |
| Sbarufatti, C. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Scarselli, G. | DETECTION OF DELAMINATIONS IN DAMAGED COMPOSITE PLATES VIA LOCAL DAMAGE RESONANCE APPROACH | ICAS2024_0814 |
| Scavella, P. | NUMERICAL STUDY ON ACTIVE FLOW CONTROL SOLUTIONS FOR HIGH LIFT | ICAS2024_1053 |
| Schenk, M. | ENHANCING THE PERFORMANCE OF SLENDER STRUCTURES WITH GEOMETRIC CONSTRAINTS: A CASE STUDY WITH THE ROORDA FRAME | ICAS2024_0192 |
| Schettino, A. | DESIGN OF A HIGH ENTHALPY HYPERSONIC NOZZLE FOR “GHIBLI” PLASMA WIND TUNNEL | ICAS2024_0894 |
| Schiavone, F.G. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF NOISE GENERATION IN HYDROGEN AND METHANE-HYDROGEN LAMINAR FLAMES | ICAS2024_1129 |
| Schlickenmaier, H. | A CALL TO ACTION TO ENGAGE THE COMMUNITY TO MEET THE CHALLENGES THAT MUST BE TACKLED TO MAKE ELECTRIFIED AIRCRAFT PROPULSION REAL | ICAS2024_0834 |
| Schmalz, M. | PRELIMINARY STRUCTURAL DESIGN OF A HIGH ASPECT RATIO RANSPORT AIRCRAFT WITH LAMINAR WING | ICAS2024_0604 |
| Schmeink, J. | ON THE WATER ENHANCED TURBOFAN CONCEPT: PART B – FLOW PATH AND MASS ASSESSMENT | ICAS2024_0135 |
| Schmeink, J. | KNOWLEDGE-BASED TURBINE DISK MODELING – A CONCEPTUAL DESIGN PROCESS CALIBRATED TO THE NASA ENERGY EFFICIENT ENGINE | ICAS2024_0272 |
| Schmelcher, M. | ON THE WATER ENHANCED TURBOFAN CONCEPT: PART B – FLOW PATH AND MASS ASSESSMENT | ICAS2024_0135 |
| Schmelcher, M. | ON THE WATER ENHANCED TURBOFAN CONCEPT: PART A - THERMODYNAMICS AND OVERALL ENGINE DESIGN | ICAS2024_0199 |
| Schmelcher, M. | PERFORMANCE ASSESSMENT OF AN ENGINE-INTEGRATED CLOSED-AIR COOLING THERMAL MANAGEMENT SYSTEM IN A NEXT GENERATION FIGHTER CONFIGURATION | ICAS2024_0622 |
| Schmidt, F. | THE CRM-HL ECOSYSTEM - DLR CONTRIBUTIONS | ICAS2024_1214 |
| Schmidt, S.-O. | ASSISTED AND AUTOMATED AERIAL REFUELLING – OVERVIEW OF THE CONDUCTED RESEARCH AT THE GERMAN AEROSPACE CENTER (DLR) | ICAS2024_0819 |
| Schmied-Kowarzik, R. | CINNABAR PROJECT - AUGMENTED REALITY WORKFLOW FOR AIRCRAFT DENT & BUCKLE INSPECTION | ICAS2024_0152 |
| Schmied-Kowarzik, R. | CINNABAR PROJECT: EXAMINING REQUIREMENTS FOR USER ACCEPTANCE OF AIRCRAFT STRUCTURE INSPECTION IN AUGMENTED REALITY | ICAS2024_0164 |
| Schmollgruber, P. | RESULTS OF THE SCALED FLIGHT DEMONSTRATOR FLIGHT TESTS | ICAS2024_1151 |
| Schmollgruber, P. | HIGH ASPECT RATION WING CONCEPTS | ICAS2024_1298 |
| Schneider, T.M. | TOWARDS A FIRST-PRINCIPLE BASED QUANTITATIVE DESCRIPTION OF TURBULENCE WITHOUT THE NEED FOR ADHOC MODELS | ICAS2024_1239 |
| Schneiders, K. | ROUTE PLANNING FOR VOLCANIC ASH AND RADIOACTIVITY IN-SITU DRONE MEASUREMENTS USING A GENETIC ALGORITHM AND KRIGING | ICAS2024_0406 |
| Scholz, W. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Scholz, W. | MIXED FLIGHT CONTROL LAYOUT FOR ULTRALIGHT GENERAL AVIATION AIRCRAFT | ICAS2024_0517 |
| Schröder, A. | THE CRM-HL ECOSYSTEM - DLR CONTRIBUTIONS | ICAS2024_1214 |
| Schuchardt, B. | ADVANCING URBAN AIR MOBILITY: COLLABORATIVE EXCELLENCE AND INFRASTRUCTURE INITIATIVES BY DLR | ICAS2024_1223 |
| Schuller, T. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF NOISE GENERATION IN HYDROGEN AND METHANE-HYDROGEN LAMINAR FLAMES | ICAS2024_1129 |
| Schulte, A. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Schultz, M. | TIME-BASED CONTROL TO REDUCE TRAJECTORY COMPLEXITY IN THE FLOW-CENTRIC AIR TRAFFIC CONTROL PARADIGM | ICAS2024_0966 |
| Schultz, V.P. | A CALL TO ACTION TO ENGAGE THE COMMUNITY TO MEET THE CHALLENGES THAT MUST BE TACKLED TO MAKE ELECTRIFIED AIRCRAFT PROPULSION REAL | ICAS2024_0834 |
| Schulz, T. | DLR DESIGN CHALLENGE 2024: DESIGN OF A COST AND ENERGY EFFICIENT REGIONAL AIRCRAFT | ICAS2024_1264 |
| Schwalb, D. | APPLICATION OF CLUSTERING TECHNIQUES IN OPTIMISATION-BASED FLIGHT CONTROL SYSTEM CLEARANCE | ICAS2024_0044 |
| Schwan, L. | TOWARDS A HOLISTIC APPROACH TO INCREASE SUSTAINABILITY IN AIRCRAFT CABIN DESIGN | ICAS2024_0511 |
| Schwarz, C.W. | SENS4ICE EU PROJECT HYBRID ICE DETECTION ARCHITECTURES DEMONSTRATION RESULTS | ICAS2024_0178 |
| Schwingel, J. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Schwoch, G. | ENHANCING PUBLIC GOOD MISSIONS AND DISASTER RESPONSE WITH ADVANCED AERIAL TECHNOLOGY: OPPORTUNITIES AND CHALLENGES | ICAS2024_1259 |
| Schäfer, M. | MASS AND POWER ESTIMATIONS IN PRELIMINARY FLIGHT CONTROL SYSTEM DESIGN | ICAS2024_0166 |
| Schäfer, M. | DEVELOPMENT AND TESTING OF AN ACTUATION SYSTEM FOR A MORPHING CONTROL SURFACE | ICAS2024_0171 |
| Scott, M.J. | MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION | ICAS2024_0020 |
| Scott, M.J. | APPLICATION OF NATURAL LANGUAGE PROCESSING FOR AIRCRAFT DEFECT TRACKING IN MAINTENANCE OPERATIONS | ICAS2024_0083 |
| Scott, M.J. | CINNABAR PROJECT - AUGMENTED REALITY WORKFLOW FOR AIRCRAFT DENT & BUCKLE INSPECTION | ICAS2024_0152 |
| Sebastia Saez, C. | NUMERICAL ANALYSIS OF GENERALIZED AERODYNAMIC FORCES CONSIDERING LAMINAR-TURBULENT TRANSITION ON A NLF WING | ICAS2024_0823 |
| Sedlacek, D. | ASSESSMENT OF AN ADAPTIVE ONE-EQUATION TURBULENCE MODEL FOR LEADING-EDGE VORTEX FLOWS ON MULTIPLE SWEPT DELTA WINGS | ICAS2024_0822 |
| Seele, R. | GE AEROSPACE: RISING TO THE CHALLENGE FOR MORE SUSTAINABLE FLIGHT | ICAS2024_1235 |
| Seitz, A. | DESIGN OF A HIGHLY EFFICIENT TRANSPORT NLF AIRCRAFT WITH A BACKWARD SWEPT WING AND A LONG SINGLE-AISLE FUSELAGE | ICAS2024_0102 |
| Seitz, A. | MODELLING AND INITIAL ASSESSMENT OF A FUEL CELL AUXILIARY PROPULSION AND POWER UNIT | ICAS2024_0261 |
| Seitz, A. | DESIGN OPTIMISATION OF A BOUNDARY LAYER INGESTION PROPULSOR FOR A MULTI-FUEL HYDROGEN AIRCRAFT | ICAS2024_1060 |
| Seki, N. | DEVELOPMENT OF AIRCRAFT SYSTEM ELECTRIFICATION AND HYBRID ELECTRIC PROPULSION | ICAS2024_0971 |
| Sekine, K. | VALIDATING FLOW-BASED EN ROUTE AMAN COUPLING ESCAPE LIGHT WITH AIRTOP SOFTWARE | ICAS2024_0968 |
| Selier, M. | ARCHITECTURE DESIGN FOR A COMMERCIALLY VIABLE HYDROGEN-ELECTRIC POWERED RETROFITTED REGIONAL AIRCRAFT | ICAS2024_1090 |
| Sells, B.E. | EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS | ICAS2024_0464 |
| Semke, A. | ANALYSIS OF AN ELECTRICAL-POWERED-DUCTED-THRUST VECTORING-FLAP | ICAS2024_0412 |
| Senoguchi, A. | ESTIMATING THE IMPACT OF NUMERICAL WEATHER PREDICTION DATA MODELS ON SHORT-HAUL MINIMUM COST TRACKS | ICAS2024_0142 |
| Senoguchi, A. | RELATIONSHIPS BETWEEN AIRCRAFT ROUTES AND TURBULENCE-RELATED WEATHER DATA | ICAS2024_0380 |
| Sequeira, C. | VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA | ICAS2024_0104 |
| Serra, J. | MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE SCALE | ICAS2024_0290 |
| Shahjahan, S. | ON THE CHOICE OF TURBULENCE MODEL FOR THE SIMULATION OF AIRFOILS AT REYNOLDS NUMBER BELOW 200,000 | ICAS2024_0327 |
| Shahjahan, S. | INFLUENCE OF MOTOR CHARACTERISTICS ON OPTIMAL PROPROTOR DESIGN | ICAS2024_0329 |
| Shan, J.H. | LIGHT WEIGHT DESIGN AND LASER ADDITIVE MANUFACTURING OF METAL BIPOLAR PLATES FOR THE APPLICATION OF AIRCRAFT FUEL CELL | ICAS2024_0964 |
| Shang, B.-L. | EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN | ICAS2024_0962 |
| Shang, Y. | MODELING AND ANALYSIS OF ELECTRO-HYDROSTATIC ACTUATORS EFFICIENCY | ICAS2024_1043 |
| Shang, Y.-X. | ULTRA-LOW-ALTITUDE PENETRATION PATH PLANNING FOR FIXED-WING AIRCRAFT BASED ON NMP ALGORITHM | ICAS2024_0972 |
| Shao, X. | DEEP LEARNING BASED FAST PREDICTION OF AERODYNAMIC PARAMETERS FOR DUCTED PROPELLERS | ICAS2024_1011 |
| Sharma, A. | REQUIREMENTS UNCERTAINTY PROPAGATION IN CONCEPTUAL DESIGN USING BAYESIAN NETWORKS | ICAS2024_0076 |
| Sharma, A. | MODEL-BASED CONCEPTUAL DESIGN AND EVALUATION OF A SOLID-FUEL SCRAMJET VEHICLE | ICAS2024_0195 |
| Sharma, A. | DESIGN OF THE SENECA MACH 1.8 SUPERSONIC AIRLINER WITH MULTI-FIDELITY AERODYNAMIC ANALYSIS FOR NOISE-OPTIMISED TAKE-OFF TRAJECTORIES | ICAS2024_0758 |
| Sharma, A. | EMBEDDED SENSORS FOR AIRCRAFT PREDICTIVE MAINTENANCE: SHM SYSTEM INTEGRATION & TRADE-OFF ANALYSIS | ICAS2024_1081 |
| Sharma, A. | USE OF GRAPHENE MATERIAL IN AIRCRAFT STRUCTURE FOR LIGHTNING STRIKE PROTECTION | ICAS2024_1141 |
| Sharma, G. | APPLICATION OF CONVOLUTIONAL NEURAL NETWORKS IN DETERMINING THE VELOCITY AND PRESSURE FIELDS AROUND AIRFOIL MODELS | ICAS2024_0197 |
| Sharma, G. | APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) FOR PREDICTION OF DRAG COEFFICIENT OF AXISYMMETRIC BOATTAIL MODELS | ICAS2024_0205 |
| Sharma, V.M. | EMBEDDED SENSORS FOR AIRCRAFT PREDICTIVE MAINTENANCE: SHM SYSTEM INTEGRATION & TRADE-OFF ANALYSIS | ICAS2024_1081 |
| Sharma, V.M. | USE OF GRAPHENE MATERIAL IN AIRCRAFT STRUCTURE FOR LIGHTNING STRIKE PROTECTION | ICAS2024_1141 |
| Sharpe, J. | VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA | ICAS2024_0104 |
| Sharqi, S. | FINITE ELEMENT MODEL UPDATE OF VERY FLEXIBLE AIRCRAFT BASED ON GROUND VIBRATION TESTS | ICAS2024_0403 |
| Shen, J. | ENHANCING THE PERFORMANCE OF SLENDER STRUCTURES WITH GEOMETRIC CONSTRAINTS: A CASE STUDY WITH THE ROORDA FRAME | ICAS2024_0192 |
| Shen, Z. | SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT | ICAS2024_0925 |
| Shi, A. | EFFECTS OF SHOCK IMPINGEMENT LOCATION ON PANEL AEROELASTIC STABILITY IN MACH REFLECTION | ICAS2024_0066 |
| Shi, A. | A BRIEF REVIEW OF PANEL AEROELASTICITY WITH SHOCK INTERACTION | ICAS2024_0067 |
| Shi, A. | RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS | ICAS2024_0550 |
| Shi, H. | MANNED AND UNMANNED AERIAL VEHICLES COOPERATIVE COMBAT FRAMEWORK BASED ON LARGE LANGUAGE MODELS | ICAS2024_0231 |
| Shi, H.-L. | PILOT FATIGUE DETECTION USING BP NEUTRAL NETWORKS | ICAS2024_0183 |
| Shi, J.-W. | EXPERIMENTAL AND NUMERICAL INVESTIGATION ON SEPARATION CHARACTERISTICS OF SERPENTINE CONVERGENT-DIVERGENT NOZZLE | ICAS2024_0920 |
| Shi, K.Y. | LIGHT WEIGHT DESIGN AND LASER ADDITIVE MANUFACTURING OF METAL BIPOLAR PLATES FOR THE APPLICATION OF AIRCRAFT FUEL CELL | ICAS2024_0964 |
| Shi, R.-H. | SURROGATE-ASSISTED HIERARCHICAL OPTIMIZATION METHOD FOR VARIABLE SWEEP FLIGHT VEHICLE TRAJECTORY | ICAS2024_0825 |
| Shibata, K. | DEVELOPMENT OF UNSTEADY PRESSURE-SENSITIVE PAINT FOR LOW REYNOLDS NUMBER WIND TUNNEL TESTS IN LOW-PRESSURE ENVIRONMENTS | ICAS2024_0840 |
| Shin, H.-S. | A DESIGN OF VFR APPROACH AND DEPARTURE PROCEDURES OF UAM AT VERTIPORTS ADJACENT TO THE AIRPORT | ICAS2024_0110 |
| Shin, J.-H. | OPERATIONAL LIMITS ASSESSMENT FOR HIGH-ALTITUDE LONG-ENDURANCE UAVS CONSIDERING PROPELLER ICING EFFECT | ICAS2024_0507 |
| Shin, M. | PURSUIT-BASED LONG-RANGE AIR-TO-AIR MISSILE MIDCOURSE GUIDANCE ROBUST TO CHANGES IN THE PREDICTED IMPACT POINT | ICAS2024_0828 |
| Shipley, J. | THE PRODUCTION OF HIGH-PERFORMANCE HEAT EXCHANGERS FOR AEROSPACE APPLICATIONS | ICAS2024_0022 |
| Shiratsuchi, Y. | MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM | ICAS2024_0573 |
| Shiva Prakasha, P. | IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN | ICAS2024_0057 |
| Shiva Prakasha, P. | A SYSTEM OF SYSTEMS AIRCRAFT DESIGN FRAMEWORK: DEMONSTRATION USING A SEAPLANE TRANSPORT NETWORK IN THE GREEK ISLANDS | ICAS2024_0402 |
| Shiva Prakasha, P. | EU IMPACT MONITOR PROJECT - OVERVIEW AND APPROACH | ICAS2024_1114 |
| Shiva Prakasha, P. | COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH | ICAS2024_1138 |
| Shiva Prakasha, P. | ADVANCING URBAN AIR MOBILITY: COLLABORATIVE EXCELLENCE AND INFRASTRUCTURE INITIATIVES BY DLR | ICAS2024_1223 |
| Shu, B.W. | FAST PREDICTION OF PRESSURE DISTRIBUTION FOR 3D CONFIGURATION BASED ON LARGE LANGRAGE MODEL | ICAS2024_0679 |
| Shubham, S. | COMPUTATIONAL ANALYSIS ON THE EFFECTS OF LEADING EDGE TUBERCLES ON THE PERFORMANCE OF ROTATING PROPELLER | ICAS2024_0581 |
| Shukla, D. | AN AUTONOMOUS SYSTEM FOR DOCKING AND BATTERY SWAPPING IN UAVS | ICAS2024_1116 |
| Sibilski, K. | AERODYNAMIC ANALYSIS OF CAMBER MORPHING AIRFOILS USING PARTICLE IMAGE VELOCIMETRY AND COMPUTATIONAL FLUID DYNAMICS METHODS | ICAS2024_0691 |
| Sikorski, D. | EFFECT OF INFILL STYLE AND DENSITY ON SELECTED MECHANICAL PROPERTIES OF THE CARBON FIBRE REINFORCED ABS MFD FILAMENT | ICAS2024_0806 |
| Silva, A. | E-KEROSENE POTENTIAL FOR COMMERCIAL AVIATION DECARBONIZATION | ICAS2024_0680 |
| Silva, A.M.P. | IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN | ICAS2024_0057 |
| Silva, A.M.P. | AIRCRAFT WING STRUCTURAL SIZING COMPUTATIONAL TOOL TAILORED FOR A COLLABORATIVE MULTIDISCIPLINARY DESIGN FRAMEWORK | ICAS2024_0079 |
| Silva, A.R.R. | MITIGATING DYNAMIC STALL WITH A MOVABLE LEADING-EDGE: THE NACA0012-IK30 WING | ICAS2024_0595 |
| Silva, C.C.D. | MULTIPLATFORM SIMULATION USING ROS | ICAS2024_0755 |
| Silva, C.S. | EMBRAER SUSTAINABILITY STRATEGY | ICAS2024_1301 |
| Silva, G.C. | AILERON-FLAP-INTEGRATED ROLL CONTROL LAW BY OPTIMIZED CONTROL ALLOCATION FOR FLEXIBLE TRANSPORT AIRCRAFT | ICAS2024_0613 |
| Silva, G.H. | SANDWICH COMPOSITES SKIN PANEL OPTIMIZATION FOR THE COMMON RESEARCH MODEL WING | ICAS2024_0479 |
| Silva, J.C. | INSIGHTS INTO HUMAN FATIGUE: STATISTICAL ANALYSIS IN AIRCRAFT MAINTENANCE | ICAS2024_0131 |
| Silva, R.C. | DYNAMICS OF THE MECHANISM FOR VENTILATION ACROSS FEATHERS IN FLAPPING WING UAV | ICAS2024_0516 |
| Silva, R.G.A. | FLIGHT PATH RECONSTRUCTION OF A FLEXIBLE WING UAV WITH WING MOUNTED VANES | ICAS2024_1176 |
| Silvestre, F.J. | AILERON-FLAP-INTEGRATED ROLL CONTROL LAW BY OPTIMIZED CONTROL ALLOCATION FOR FLEXIBLE TRANSPORT AIRCRAFT | ICAS2024_0613 |
| Sinechal, J.-B. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Sinha Roy, S. | FROM ONTOLOGY TO SYSTEM ARCHITECTURE: AN MBSE APPROACH TOWARD THE REALIZATION OF URBAN AIR MOBILITY | ICAS2024_0554 |
| Sinnige, T. | EXPERIMENTAL MEASUREMENTS OF SLIPSTREAM DEFORMATION FOR AN INSTALLED DISTRIBUTED PROPELLER CONFIGURATION. | ICAS2024_0264 |
| Sinnige, T. | AERODYNAMIC PERFORMANCE AND INTERACTION EFFECTS OF AN OVER-THE-WING DISTRIBUTED-PROPELLER SYSTEM IN CRUISE CONDITIONS | ICAS2024_0632 |
| Sirtori, G. | PRELIMINARY SIZING OF HYDROGEN-BURNING JETLINER FOR DIRECT OPERATING COST OPTIMIZATION | ICAS2024_0109 |
| Sirtori, G. | HYDROGEN TANKERING: TOOLS FOR ECONOMIC AND ENVIRONMENTAL IMPACT SCENARIO STUDIES | ICAS2024_0993 |
| Sirtori, G. | METHODOLOGIES FOR THE PRELIMINARY SIZING OF HYDROGEN-POWERED AIRCRAFT AND SUPPORTING AIRPORT INFRASTRUCTURES | ICAS2024_1002 |
| Sirtori, G. | CONCEPTUAL DESIGN OF A ZERO-EMISSION REGIONAL AIRCRAFT FOR ENHANCED SHORT-HAUL MOBILITY | ICAS2024_1085 |
| Sissing, T.B. | RETROFITTING A JET DRIVEN UAV TO FORM A MULTI-PURPOSE TEST PLATFORM | ICAS2024_0036 |
| Skowron, A. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Skrna, D. | AEROACOUSTICS INVESTIGATION OF PROPELLER LEADING EDGE TUBERCLES APPLIED TO ADVANCED AIR MOBILITY | ICAS2024_0411 |
| Sladky, M. | THE FATIGUE LIFE PREDICTION OF THIN-WALLED WELDED JOINTS | ICAS2024_1120 |
| Slotnick, J.P. | A CFD VALIDATION ECOSYSTEM TO ADVANCE THE PREDICTION OF LOW-SPEED AERODYNAMICS | ICAS2024_1210 |
| Smid, M. | W-WING AEROELASTIC DEMONSTRATOR DESIGN MODIFICATION AND UPGRADE | ICAS2024_0054 |
| Smith, H. | PERFORMANCE ENHANCEMENTS BETWEEN DIFFERENT APPLICATIONS OF ALTERNATIVE FUELS AND NOVEL AIRCRAFT CONFIGURATIONS | ICAS2024_1046 |
| Smoraldi, A. | DESIGN OF A HIGH ENTHALPY HYPERSONIC NOZZLE FOR “GHIBLI” PLASMA WIND TUNNEL | ICAS2024_0894 |
| Snellen, M. | OPTIMAL APPROACH AND DEPARTURE TRAJECTORIES WITH ACOUSTIC FOOTPRINT ASSESSMENT FOR AN AIR MOBILITY QUAD-ROTOR | ICAS2024_1115 |
| Sodja, J. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Solzer, J. | COMPARING CONVECTIVE WEATHER IMPACTS ON AIR TRAFFIC MANAGEMENT OPERATIONS IN UNITED STATES, CANADA & EUROPE | ICAS2024_0137 |
| Son, C. | A STUDY ON BATTERY SEPARATION DRONES TO EXTEND ENDURANCE | ICAS2024_0785 |
| Son, C.K. | OPERATIONAL LIMITS ASSESSMENT FOR HIGH-ALTITUDE LONG-ENDURANCE UAVS CONSIDERING PROPELLER ICING EFFECT | ICAS2024_0507 |
| Song, B. | DYNAMICS ANALYSIS AND CONTROL OF A LARGE WINGSPAN FLAPPING-WING VEHICLE | ICAS2024_0621 |
| Song, B.-F. | INFLUENCE OF REINFORCED TRAILING EDGE ON FLAPPING WING AERODYNAMIC FORCE AND DEFORMATION | ICAS2024_0526 |
| Song, G. | TECHNICAL RISK MANAGEMENT OF SYSTEM OF SYSTEMS BASED ON TECHNOLOGY READINESS ASSESSMENT | ICAS2024_0041 |
| Song, J. | STUDY ON THE BALLISTIC-RESISTANT AIRWORTHINESS STANDARDS FOR COMMERCIAL AIRCRAFT COCKPIT DOOR | ICAS2024_0074 |
| Song, W. | AERODYNAMIC OPTIMIZATION OF HIGH-ALTITUDE PROPELLER COMBINED WITH MACHINE LEARNING METHOD | ICAS2024_0342 |
| Song, W. | BOUNDARY-LAYER SUCTION AND AERODYNAMIC SHAPE OPTIMIZATION FOR HYBRID LAMINAR FLOW CONTROL ON A FIN | ICAS2024_0681 |
| Song, W.-P. | EFFICIENT MULTI-OBJECTIVE DESIGN OPTIMIZATION OF ROTOR AIRFOILS FOR IMPROVING DYNAMIC STALL CHARACTERISTICS | ICAS2024_0420 |
| Song, W.-P. | AERODYNAMIC DESIGN OF A SUPERSONIC TRANSPORT CONFIGURATION CONSIDERING AVERAGE LOUDNESS IN THE WHOLE BOOM CARPET | ICAS2024_0597 |
| Song, W.-P. | RESEARCH ON AERODYNAMIC DESIGN OF ENGINE NACELLE UNDER THE INFLUENCE OF PROPELLER SLIPSTREAM FOR THE TURBOPROP AIRCRAFT | ICAS2024_0605 |
| Song, W.-P. | EFFECTS OF GEOMETRY PARAMETERS ON AERODYNAMIC CHARACTERISTICS OF ROTOR AIRFOIL IN REVERSE FLOW | ICAS2024_0607 |
| Song, W.-P. | EFFICIENT AEROSTRUCTURAL DESIGN OPTIMIZATION COMBINING GRADIENT-ENHANCED KRIGING WITH COUPLED ADJOINT METHOD | ICAS2024_0651 |
| Song, W.-P. | NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF HOVERING ROTOR IN GROUND EFFECT | ICAS2024_0655 |
| Song, W.-P. | RESEARCH ON MULTI-OBJECTIVE AERODYNAMIC/STRUCTURAL DESIGN OPTIMIZATION METHOD FOR LARGE THICKNESS FLATBACK AIRFOILS | ICAS2024_0690 |
| Song, W.-P. | ON THE INFLUENCE OF BASE FLOW CHARACTERISTICS ON CROSSFLOW INSTABILITY IN SWEPT BOUNDARY LAYERS | ICAS2024_0918 |
| Song, W.P. | DESIGN OPTIMIZATION OF A WIG CRAFT’S HIGH LIFT DEVICE CONSIDERING GROUND EFFECT | ICAS2024_0572 |
| Song, W.P. | INVESTIGATION ON AERODYNAMIC DESIGN OF VTOL AIRCRAFT PROPELLER | ICAS2024_0643 |
| Song, Y. | WEAR EVOLUTION OF PYRAMID-STRUCTURED ABRASIVE BELTS AND ITS EFFECT ON GRINDING OPERATIONS | ICAS2024_0368 |
| Sorli, M. | THE JOURNEY TOWARDS CONDITION-BASED MAINTENANCE: A FRAMEWORK FOR THE HORIZONTAL TAIL ACTUATOR OF AN ADVANCED JET TRAINER AIRCRAFT | ICAS2024_0198 |
| Sorli, M. | COMPARATIVE ANALYSIS OF MACHINE LEARNING ALGORITHMS FOR HEAT EXCHANGERS DIAGNOSIS IN ELECTRIFIED AIRCRAFT | ICAS2024_0701 |
| Soundararajan, S.G. | CFD STUDY OF AIR SUPPLY SYSTEM FOR COOLING OF A HYDROGEN POWERED UNMANNED SEAPLANE AND REDUCTION OF THE RESULTING DRAG | ICAS2024_0736 |
| Souza, L. | INSTRUMENTATION OF A SUBESCALE GROUND EFFECT VEHICLE, VOLITAN, TO MEASURE FLIGHT PROPULSION EFFICIENCY | ICAS2024_1125 |
| Souza Villela, P.C. | INITIAL DEVELOPMENT OF A CFD ICING TOOL | ICAS2024_1112 |
| Sozio, E. | NUMERICAL SOLUTION OF LOX FLOW IN A LIQUID ROCKET ENGINE ADDITIVELY MANUFACTURED COOLING CHANNEL | ICAS2024_0105 |
| Spedding, G.R. | ON THE EXISTENCE OF A FAMILY OF IDEAL AIRCRAFT CONFIGURATIONS | ICAS2024_0723 |
| Spehr, C. | THE CRM-HL ECOSYSTEM - DLR CONTRIBUTIONS | ICAS2024_1214 |
| Spence, S. | EVALUATION AND SIMULATION OF PARALLEL HYBRID ELECTRIC PROPULSION WITH REAL FLIGHT DATA | ICAS2024_0738 |
| Spieck, M. | AUTOMATED OPERATION OF HIGH-PERFORMANCE FIXED-WING DRONES: A POTENTIAL GAME-CHANGER FOR GREEN AERIAL SERVICES | ICAS2024_0946 |
| Spieler, M. | SIMULATION AND VERIFICATION OF HYDRAULIC ROTOR GAP PARAMETERS OF A NOVEL HIGH EFFICIENT WET ELECTRO MOTOR PUMP FOR AEROSPACE APPLICATIONS | ICAS2024_0123 |
| Spinelli, A. | REQUIREMENTS UNCERTAINTY PROPAGATION IN CONCEPTUAL DESIGN USING BAYESIAN NETWORKS | ICAS2024_0076 |
| Spinelli, A. | STRUCTURAL AND AEROELASTIC OPTIMISATION OF A LARGE AIRCRAFT WING WITH A PASSIVE TWIST WINGTIP | ICAS2024_0111 |
| Spitale, C. | STEADY ANALYSIS OF THREE-SURFACE AIRPLANES: IMPROVING THE AERODYNAMIC PERFORMANCE THROUGH REDUNDANT LONGITUDINAL CONTROL | ICAS2024_0273 |
| Srivastava, V. | TRANSITION MODELING IN SUPPORT OF CFD VISION 2030 - HIGHLIGHTS OF RECENT EFFORTS AT THE NASA LANGLEY RESEARCH CENTER | ICAS2024_0081 |
| Staack, I. | LARGE LANGUAGE MODEL-DRIVEN SIMULATIONS FOR SYSTEM OF SYSTEMS ANALYSIS IN FIREFIGHTING AIRCRAFT CONCEPTUAL DESIGN | ICAS2024_0346 |
| Staack, I. | CONCEPT OF OPERATIONS IN AN AGENT-BASED SIMULATION: A SYSTEM-OF-SYSTEMS APPROACH | ICAS2024_0357 |
| Staack, I. | FRAMEWORK DEVELOPMENT FOR CONCEPTUAL DESIGN AND CONFIGURATION ANALYSIS OF EVTOL AIRCRAFT | ICAS2024_0557 |
| Stammel, S. | NUMERICAL METHOD TO DETERMINE STRUCTURAL ELEMENT REDUCED STIFFNESS FOR DESIRED COMPOSITE WING STRUCTURES CONFIGURATIONS | ICAS2024_0727 |
| Stamoulis, K.P. | TOWARDS TRUSTWORTHY DATA-DRIVEN GAS TURBINE PROGNOSTICS | ICAS2024_0793 |
| Standingford, D. | VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA | ICAS2024_0104 |
| Starek, J. | W-WING AEROELASTIC DEMONSTRATOR DESIGN MODIFICATION AND UPGRADE | ICAS2024_0054 |
| Stefana, E. | ENSURING THE NEXT GENERATION GREEN AIRCRAFT’ SUSTAINABILITY FROM THE DESIGN PHASE VIA A LIFE-CYCLE COST ANALYSIS | ICAS2024_0350 |
| Stefani, T. | APPLYING MODEL-BASED SYSTEM ENGINEERING AND DEVOPS ON THE IMPLEMENTATION OF AN AI-BASED COLLISION AVOIDANCE SYSTEM | ICAS2024_0869 |
| Steil, M.C. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Stella, F. | NUMERICAL INVESTIGATION ON THE LIQUID SLOSHING DAMPING INSIDE A TANK WITH A FLEXIBLE ANTI-SLOSHING DEVICE | ICAS2024_0930 |
| Stephan, A. | TOWARDS REFINED CONTRAIL SIMULATIONS OF FORMATION FLIGHT SCENARIOS | ICAS2024_0502 |
| Strafforello, T. | DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION | ICAS2024_0508 |
| Strauss, F. | RAMJET/SCRAMJET TEST BENCH WITH CAVITY INJECTION OF HYDROGEN | ICAS2024_0235 |
| Streit, T. | DESIGN OF A HIGHLY EFFICIENT TRANSPORT NLF AIRCRAFT WITH A BACKWARD SWEPT WING AND A LONG SINGLE-AISLE FUSELAGE | ICAS2024_0102 |
| Strokin, E. | SURFACE QUALITY CHALLENGE FOR TI-6AL-4V ADDITIVE MANUFACTURED TOPOLOGIC OPTIMIZED LIGHTWEIGHT STRUCTURE | ICAS2024_0025 |
| Stryczniewicz, W. | THERMAL HISTORY PAINT UNDER HIGH SUBSONIC FLOW | ICAS2024_0316 |
| Strzelecka, K. | AERODYNAMIC ANALYSIS OF CAMBER MORPHING AIRFOILS USING PARTICLE IMAGE VELOCIMETRY AND COMPUTATIONAL FLUID DYNAMICS METHODS | ICAS2024_0691 |
| Strömfeldt, H. | LOW-SPEED PROPELLER FOR UAV APPLICATIONS, FROM DESIGN TO EXPERIMENTAL EVALUATION | ICAS2024_1157 |
| Stuart, C. | CHARACTERISING THE ROLE OF FLEET RENEWAL ON THE PATHWAY TO 2050: A EUROPEAN AIRLINE CASE STUDY | ICAS2024_0126 |
| Stuart, C. | EVALUATION AND SIMULATION OF PARALLEL HYBRID ELECTRIC PROPULSION WITH REAL FLIGHT DATA | ICAS2024_0738 |
| Stumpf, E. | BIRD AND DRONE IMPACT DAMAGE PROGNOSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT ENGINE | ICAS2024_1162 |
| Stütz, P. | MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS | ICAS2024_0099 |
| Stütz, P. | SENSOR AND COVERAGE PATH PLANNING FOR THE MONITORING OF AIRCRAFT EMERGENCY LANDING SITES | ICAS2024_0706 |
| Städing, J. | SUSTAINABLE ENGINE MAINTENANCE: EVALUATING THE ECOLOGICAL IMPACT OF LIFE LIMITED PART REPLACEMENT | ICAS2024_0452 |
| Stöhr, C. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Subash, A. | EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR | ICAS2024_0518 |
| Sugioka, Y. | IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN | ICAS2024_0057 |
| Sultan, A. | NASA SUSTAINABLE FLIGHT NATIONAL PARTNERSHIP OPERATIONS RESEARCH | ICAS2024_1299 |
| Sumsurooah, S. | DUAL STAGE BATTERY SIZING AND PERFORMANCE ASSESSMENT ON-BOARD HYBRID ELECTRIC AIRCRAFT | ICAS2024_1072 |
| Sun, F. | HYDRODYNAMIC ANALYSIS OF STATIC WATER IMPACT ON WEDGE-SHAPED HULL WATERTIGHT TEST SPECIMEN THROUGH NUMERICAL ANALYSIS | ICAS2024_0904 |
| Sun, F. | ANALYTICAL STUDY ON HYDROSTATIC RESPONSE CHARACTERISTICS DURING WATER LANDINGS OF AMPHIBIOUS AIRCRAFT | ICAS2024_0905 |
| Sun, G. | A NOVEL DEEP MULTIMODAO INFORMATION FUSION MODEL FOR AERO-ENGINE STATE PREDICTION | ICAS2024_0159 |
| Sun, J. | STABILITY CHARACTERISTICS OF CROSSFLOW MODES IN HYPERSONIC BOUNDARY LAYER WITH EXPANSION CORNER | ICAS2024_0576 |
| Sun, M. | VALIDATION OF ENERGY CHARACTERISTICS IN FLIGHT CONTROL SYSTEM BASED ON A MULTIDISCIPLINARY VIRTUAL PLATFORM | ICAS2024_0646 |
| Sun, M. | RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS | ICAS2024_0674 |
| Sun, M.-W. | MODEL-BASED DESIGN OF ACTIVE/ACTIVE ELECTRO-HYDROSTATIC ACTUATION FOR HELICOPTER FLIGHT CONTROLS | ICAS2024_0735 |
| Sun, S. | INTEGRITY MONITORING OF TIGHTLY INTEGRATED BDS/SINS USING MULTI-HYPOTHESIS SOLUTION SEPARATION (MHSS) ALGORITHM | ICAS2024_0244 |
| Sun, S.-Y. | MODELING AND VALIDATION OF MORPHING WING TRAILING EDGE BASED ON ZERO POISSON'S RATIO HONEYCOMB | ICAS2024_1015 |
| Sun, X. | MULTI-DIMENTIONAL DESIGN AND THERMAL PROTECTION CAPABILITY OF A REGENERATIVE COOLED RBCC VARIABLE-GEOMETRY COMBUSTOR | ICAS2024_1012 |
| Sun, X.-Q. | NUMERICAL INVESTIGATION ON THE EFFECT OF REYNOLDS NUMBER ON TANDEM DROPLET | ICAS2024_0426 |
| Sun, Y. | FLIGHT CONTROL SYSTEM KNOWLEDGE GRAPH CONSTRUCTION BASED ON AERONAUTICAL DOMAIN KNOWLEDGE AUGMENTED LARGE LANGUAGE MODEL | ICAS2024_0610 |
| Sun, Y. | REVIEW ON NONLINEAR AEROELASTIC ANALYSIS WITH FREEPLAY | ICAS2024_0922 |
| Sun, Y. | PERFORMANCE ENHANCEMENTS BETWEEN DIFFERENT APPLICATIONS OF ALTERNATIVE FUELS AND NOVEL AIRCRAFT CONFIGURATIONS | ICAS2024_1046 |
| Sun, Z. | SYSTEM ARCHITECTURE AND EVALUATION METHOD OF HUMAN-MACHINE COLLABORATION IN FLIGHT CONTROL SYSTEM | ICAS2024_0185 |
| Sunzeri, E. | CONCEPTUAL DESIGN METHODOLOGY FOR LOW-SUPERSONIC LH2-POWERED PASSENGERS AIRCRAFT | ICAS2024_0927 |
| Suti, A. | PRELIMINARY DESIGN OF POWER CONTROL STRATEGIES FOR THE HYBRID-ELECTRIC PROPULSION SYSTEM OF A LIGHTWEIGHT FIXED-WING UAV | ICAS2024_1050 |
| Suzuki, W. | TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2024_1215 |
| Svensson, C. | MODELLING HYDROGEN FUEL CELL AIRCRAFT IN SUAVE | ICAS2024_1078 |
| Swaid, M. | DESIGN OF A UAM GROUND INFRASTRUCTURE NETWORK WITH RESPECT TO MAINTENANCE CAPACITY REQUIREMENTS | ICAS2024_0745 |
| Swannet, K. | LATENT SPACE CORRELATION FOR INTERPRETABLE AIRFOIL PARAMETERIZATION USING VARIATIONAL AUTOENCODERS | ICAS2024_0484 |
| Symeonidis, G. | EUROPEAN RESEARCH COUNCIL (ERC) - FUNDING OPPORTUNITIES AND REPRESENTATIVE PROJECT HIGHLIGHTS | ICAS2024_1226 |
| Synylo, K. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Szczechula, D. | ANALYSIS OF THE POSSIBILITY OF INCREASING THE THERMAL RESISTANCE OF EPOXY RESIN WITH CWNT AND MMT | ICAS2024_0275 |
| Szczepaniak, R. | ANALYSIS OF THE POSSIBILITY OF INCREASING THE THERMAL RESISTANCE OF EPOXY RESIN WITH CWNT AND MMT | ICAS2024_0275 |
| Szczepaniak, R. | EFFECT OF INFILL STYLE AND DENSITY ON SELECTED MECHANICAL PROPERTIES OF THE CARBON FIBRE REINFORCED ABS MFD FILAMENT | ICAS2024_0806 |
| Sziroczák, D. | ENHANCING PUBLIC GOOD MISSIONS AND DISASTER RESPONSE WITH ADVANCED AERIAL TECHNOLOGY: OPPORTUNITIES AND CHALLENGES | ICAS2024_1259 |
| Tahk, M.-J. | TRAJECTORY OPTIMIZATION FOR LONG-RANGE AIR-LAUNCHED GLIDING VEHICLES USING CONVEX PROGRAMMING | ICAS2024_0468 |
| Tahk, M.-J. | PURSUIT-BASED LONG-RANGE AIR-TO-AIR MISSILE MIDCOURSE GUIDANCE ROBUST TO CHANGES IN THE PREDICTED IMPACT POINT | ICAS2024_0828 |
| Tai, J. | PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS EXTRA | ICAS2024_1319 |
| Tai, J.C. | PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS | ICAS2024_1296 |
| Takaya, S. | DEVELOPMENT OF UNSTEADY PRESSURE-SENSITIVE PAINT FOR LOW REYNOLDS NUMBER WIND TUNNEL TESTS IN LOW-PRESSURE ENVIRONMENTS | ICAS2024_0840 |
| Takeichi, N. | FEASIBILITY STUDY ON OPERATIONAL FLIGHT PLANS ADAPTED FOR TRAJECTORY BASED OPERATION | ICAS2024_1177 |
| Tamaki, Y. | EVALUATING INSTALLATION EFFECTS IN SEMI-SPAN WIND TUNNEL EXPERIMENTS USING CARTESIAN-GRID-BASED FLOW SOLVER UTCART | ICAS2024_0293 |
| Tamayama, M. | EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) | ICAS2024_0549 |
| Tan, I. | FRICTION RIVETING OF THERMOPLASTIC COMPOSITE WITH A CNC MACHINE: EXPERIMENTAL WORK | ICAS2024_1127 |
| Tan, X.-T. | NUMERICAL INVESTIGATION OF THE FLOW FEATURES ON THE TURRET WITH DIFFERENT CYLINDER HEIGHT IN THE TRANSONIC FLOW | ICAS2024_0282 |
| Tan, Y. | STUDY OF THE SCAVENGE PUMP PERFORMANCE FOR TWO-PHASE FLOW IN AN AIRCRAFT ENGINE LUBRICATION SYSTEM | ICAS2024_0788 |
| Tanahashi, Y. | EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) | ICAS2024_0549 |
| Tanaka, H. | MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM | ICAS2024_0573 |
| Tang, A. | FLIGHT LOADS RESEARCH OF TWIN VERTICAL TAIL FOR BLENDED WING-BODY AIRCRAFT BASED ON STRAIN GAUGE CAILBRATION | ICAS2024_0072 |
| Tang, S. | HAWK-INSPIRED COOPERATIVE ENCIRCLEMENT GUIDANCE OF FIXED-WING UAV SWARM WITH LIMITED COMMUNICATION IN THREAT SCENARIO | ICAS2024_0084 |
| Tang, S. | A NOLINEAR MODEL PREDICTIVE CONTROL METHOD FOR AIRBREATHING HYPERSONIC VEHICLE BASED ON KOOPMAN OPERATOR | ICAS2024_1119 |
| Tang, X.H. | A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION | ICAS2024_0314 |
| Tang, Z. | SURFACE MORPHOLOGY AND MICROSTRUCTURAL FEATURES OF ELECTRON BEAM SURFI-SCULPTED TI-6AL-4V ALLOY | ICAS2024_0262 |
| Tang, Z.Y. | WALL TEMPERATURE EFFECTS ON AERODYNAMIC HEATING MECHANISMS IN SHOCK WAVE TURBULENT BOUNDARY LAYER INTERACTION | ICAS2024_0569 |
| Tanguy, G. | IDENTIFICATION METHOD OF LONGITUDINAL COEFFICIENTS BASED ON THE NUMERICAL STUDY OF THE FLOW TOPOLOGY AROUND THE SACCON GEOMETRY | ICAS2024_0506 |
| Tanimoto, J. | APPLICATION OF CONVOLUTIONAL NEURAL NETWORKS IN DETERMINING THE VELOCITY AND PRESSURE FIELDS AROUND AIRFOIL MODELS | ICAS2024_0197 |
| Tanimoto, J. | APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) FOR PREDICTION OF DRAG COEFFICIENT OF AXISYMMETRIC BOATTAIL MODELS | ICAS2024_0205 |
| Tao, J. | A NOVEL DEEP MULTIMODAO INFORMATION FUSION MODEL FOR AERO-ENGINE STATE PREDICTION | ICAS2024_0159 |
| Taouil, I. | A DIGITAL METHOD FOR THE COMPENSATED MOLD DESIGN OF COMPOSITE PARTS | ICAS2024_0487 |
| Tarnowski, A. | RAPID DESIGN OF UNCONVENTIONAL AIRCRAFT USING SOFTWARE TOOLS COUPLED IN OPTIMIZATION LOOP – LESSONS LEARNED | ICAS2024_0496 |
| Tarun, T. | COMPUTATIONAL ANALYSIS ON THE EFFECTS OF LEADING EDGE TUBERCLES ON THE PERFORMANCE OF ROTATING PROPELLER | ICAS2024_0581 |
| Tatsukawa, T. | VALIDATING FLOW-BASED EN ROUTE AMAN COUPLING ESCAPE LIGHT WITH AIRTOP SOFTWARE | ICAS2024_0968 |
| Taylor, S. | A PERFORMANCE COMPARISON OF HYDROGEN AIRCRAFT CONCEPTS | ICAS2024_0251 |
| Teixeira Da Silva, J.R. | INITIAL DEVELOPMENT OF A CFD ICING TOOL | ICAS2024_1112 |
| Tekkel, M. | DLR DESIGN CHALLENGE 2024: DESIGN OF A COST AND ENERGY EFFICIENT REGIONAL AIRCRAFT | ICAS2024_1264 |
| Teloli, R. | ON THE OPTIMIZATION OF (GENERALIZED) IMPEDANCE FOR ACOUSTIC LINERS | ICAS2024_1123 |
| Temme, M.-M. | ATM CONTROLLER SUPPORT IN CASE OF SPACIOUS SEVERE WEATHER CONSTELLATIONS ILLUSTRATED USING TWO AIRSPACE EXAMPLES | ICAS2024_0061 |
| Temme, M.-M. | SPEED GATED INTERCEPT PROCEDURE STUDY FOR INTEGRATION OF INCREASING DIVERSE OPERATIONS (IDO) AT EUROPEAN AIRPORTS | ICAS2024_0685 |
| Teng, Y. | SENSITIVITY ANALYSIS OF SAFETY FACTORS BASED ON MODEL OF AVIATION RECIPROCATING ENGINE TURBOCHARGING SYSTEM | ICAS2024_0599 |
| Teng, Y.-D. | A METHOD FOR AUTOMATIC GENERATING SAFETY ANALYSIS BASED ON AVIATION PISTON ENGINE MODEL | ICAS2024_0587 |
| Teofili, G. | ACCELERATING THE CLEAN FUTURE OF FLIGHT | ICAS2024_1314 |
| Terenzi, R. | PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION PLASMA THRUSTERS | ICAS2024_0649 |
| Terner, M. | THE JOURNEY TOWARDS CONDITION-BASED MAINTENANCE: A FRAMEWORK FOR THE HORIZONTAL TAIL ACTUATOR OF AN ADVANCED JET TRAINER AIRCRAFT | ICAS2024_0198 |
| Terrapon, V.E. | FAST TRANSONIC CORRECTIONS FOR PANEL METHODS USING VISCOUS-INVISCID INTERACTION | ICAS2024_0162 |
| Terrenoire, E. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Terrile, A. | AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) | ICAS2024_0575 |
| Terry, J. | X-57 TRACTION POWER AND COMMAND SYSTEMS DEVELOPMENT | ICAS2024_1288 |
| Tesser, R. | PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS | ICAS2024_1205 |
| Teubl, D. | RETROFITTING A JET DRIVEN UAV TO FORM A MULTI-PURPOSE TEST PLATFORM | ICAS2024_0036 |
| Teunisse, B. | APPLICATION OF NATURAL LANGUAGE PROCESSING FOR AIRCRAFT DEFECT TRACKING IN MAINTENANCE OPERATIONS | ICAS2024_0083 |
| Theochari, A. | A PROPOSAL TOWARDS A STEP CHANGE FROM ECO-DRIVEN TO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT COMPONENTS | ICAS2024_0088 |
| Theunissen, E. | SENSOR UNCERTAINTY MITIGATION FOR DETECT AND AVOID SYSTEMS | ICAS2024_1268 |
| Thiede, S. | BATTERY PERFORMANCE METRICS FOR LARGE ELECTRIC PASSENGER AIRCRAFT | ICAS2024_0636 |
| Thielecke, F. | TECHMAPS – TECHNOLOGY MANAGEMENT FOR THE ARCHITECTING PROCESS OF AIRCRAFT ON-BOARD SYSTEMS | ICAS2024_0053 |
| Thillays, B. | SENS4ICE EU PROJECT HYBRID ICE DETECTION ARCHITECTURES DEMONSTRATION RESULTS | ICAS2024_0178 |
| Thoeben, J. | ANALYSIS OF AN ELECTRICAL-POWERED-DUCTED-THRUST VECTORING-FLAP | ICAS2024_0412 |
| Thomas, R.H. | REFINED PREDICTIONS COMPARED WITH THE PROPULSION AIRFRAME AEROACOUSTICS AND AIRCRAFT SYSTEM NOISE FLIGHT RESEARCH TEST DATA | ICAS2024_0069 |
| Thomassin, J.M. | P&W APPROACH TO SUSTAINABILITY | ICAS2024_1303 |
| Thorvaldsen, T. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Tian, X. | DESIGN OF A BODY FREEDOM FLUTTER FLIGHT MODEL WITH CONVENTIONAL CONFIGURATION | ICAS2024_0565 |
| Tirschmann, R. | SIMULATION AND VERIFICATION OF HYDRAULIC ROTOR GAP PARAMETERS OF A NOVEL HIGH EFFICIENT WET ELECTRO MOTOR PUMP FOR AEROSPACE APPLICATIONS | ICAS2024_0123 |
| Todorov, V.T. | A MORPHOLOGICAL ANALYSIS OF METHODS FOR CONCEPTUAL AIRCRAFT DESIGN UNDER UNCERTAINTIES | ICAS2024_1169 |
| Toffol, F. | GUST LOAD PASSIVE ALLEVIATION BY MEANS ON NONLINEAR, BUCKLING DRIVEN, STRUCTURAL RESPONSE | ICAS2024_0147 |
| Toffol , F. | AEROELASTIC ISSUES IN THE DESIGN OF HIGH ASPECT RATIO STRUT-BRACED WING AIRCRAFT | ICAS2024_0874 |
| Tominaga, K. | TIME-BASED CONTROL TO REDUCE TRAJECTORY COMPLEXITY IN THE FLOW-CENTRIC AIR TRAFFIC CONTROL PARADIGM | ICAS2024_0966 |
| Tomita, N. | EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) | ICAS2024_0549 |
| Tong, M. | DAMAGE AND MECHANICAL REPAIR OF COMPOSITE LAMINATES: EFFECTS OF EMBEDDED DEFECTS AND LOW VELOCITY IMPACTS | ICAS2024_0748 |
| Tong, M. | SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT | ICAS2024_0925 |
| Tong, M.-B. | NUMERICAL SIMULATION OF THE RESPONSE CHARACTERISTICS OF THE WING STRUCTURE OF A SEAPLANE PLANING IN WAVE | ICAS2024_0901 |
| Tong, M.-B. | ANALYSIS OF SUCTION FORCE EFFECT ON DIFFERENT FUSELAGE SHAPE DURING THE WATER DITCHING | ICAS2024_0929 |
| Tong, M.-B. | RESEARCH ON AERODYNAMIC PERFORMANCE OF OVERSIZE MODULAR PARAFOIL IN RANDOM WIND FIELD | ICAS2024_0952 |
| Tong, Y. | RESEARCH ON MULTI-ATTRIBUTE DECISION MAKING AND VERIFICATION METHODS FOR SYSTEMS CONFRONTATION | ICAS2024_0561 |
| Tonti, J. | APPLICATION OF CLUSTERING TECHNIQUES IN OPTIMISATION-BASED FLIGHT CONTROL SYSTEM CLEARANCE | ICAS2024_0044 |
| Tornabene, R. | NASA HYBRID THERMALLY EFFICIENT CORE (HYTEC) PROJECT OVERVIEW | ICAS2024_1245 |
| Torresi, M. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF NOISE GENERATION IN HYDROGEN AND METHANE-HYDROGEN LAMINAR FLAMES | ICAS2024_1129 |
| Torrigiani, F. | PROCESSES, METHODS AND TOOLS SUPPORTING THE DEVELOPMENT OF AERONAUTICAL SYSTEMS | ICAS2024_0285 |
| Toussaint, C. | RESULTS OF THE SCALED FLIGHT DEMONSTRATOR FLIGHT TESTS | ICAS2024_1151 |
| Trainelli, L. | PRELIMINARY SIZING OF HYDROGEN-BURNING JETLINER FOR DIRECT OPERATING COST OPTIMIZATION | ICAS2024_0109 |
| Trainelli, L. | HYDROGEN TANKERING: TOOLS FOR ECONOMIC AND ENVIRONMENTAL IMPACT SCENARIO STUDIES | ICAS2024_0993 |
| Trainelli, L. | METHODOLOGIES FOR THE PRELIMINARY SIZING OF HYDROGEN-POWERED AIRCRAFT AND SUPPORTING AIRPORT INFRASTRUCTURES | ICAS2024_1002 |
| Trainelli, L. | CONCEPTUAL DESIGN OF A ZERO-EMISSION REGIONAL AIRCRAFT FOR ENHANCED SHORT-HAUL MOBILITY | ICAS2024_1085 |
| Trainelli, L. | IDENTIFICATION OF THE IMPACT OF BLOWING ON THE AERODYNAMIC MODEL OF AN AIRPLANE WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2024_1134 |
| Tran, N. | OPTIMIZING FLEET ASSIGNMENT DECISIONS FOR REGIONAL AIRLINES WITH HYBRID ELECTRIC AIRCRAFT UPTAKE | ICAS2024_0781 |
| Tran, T.H. | APPLICATION OF CONVOLUTIONAL NEURAL NETWORKS IN DETERMINING THE VELOCITY AND PRESSURE FIELDS AROUND AIRFOIL MODELS | ICAS2024_0197 |
| Tran, V. | PROBING AND MODELING LARGE-SCALE AIRLINE NETWORK DISRUPTIONS: 2022 SOUTHWEST AIRLINES SCHEDULING CRISIS | ICAS2024_0782 |
| Tran The, H. | APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) FOR PREDICTION OF DRAG COEFFICIENT OF AXISYMMETRIC BOATTAIL MODELS | ICAS2024_0205 |
| Travascio, L. | HYDROGEN SAFETY: A COMPARATIVE ANALYSIS OF LEAK DETECTION SENSORS | ICAS2024_0149 |
| Trovato, S. | PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION PLASMA THRUSTERS | ICAS2024_0649 |
| Tsentis, S. | BASE FLOW CHARACTERISTICS FOR A SUB-SCALE HIGH-SPEED EXHAUST AT OVER-EXPANDED MODE | ICAS2024_0512 |
| Tshabalala, L.C. | FATIGUE PROPERTIES OF ADDITIVELY MANUFACTURED TOOL STEEL | ICAS2024_0633 |
| Tsuchimoto, Y. | TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2024_1215 |
| Tsuchiya, T. | IN-FLIGHT MEASUREMENT OF WING SURFACE PRESSURE DISTRIBUTION ON A FIXED-WING UAV AND ITS APPLICATION TO FLIGHT CONTROL | ICAS2024_0980 |
| Tsushima, N. | EFFICIENT THERMOMECHANICAL SIMULATION FOR METALLIC LATTICE STRUCTURES FABRICATED BY ADDITIVE MANUFACTURING | ICAS2024_0908 |
| Tuccillo, M. | MULTIDISCIPLINARY PRELIMINARY DESIGN PROCESS OF HYBRID-ELECTRIC SEAPLANE | ICAS2024_0470 |
| Tuccillo, M. | A MODEL BASED SYSTEM ENGINEERING APPROACH TOWARDS AIRCRAFT DIGITAL CERTIFICATION | ICAS2024_0603 |
| Tuo, H. | A MOMENTUM-INTEGRAL METHOD TO CALCULATE WINDAGE LOSSES ON A ROTATING DRUM WITH SUPERPOSED FLOW | ICAS2024_0281 |
| Turazza, M.D. | HANDLING QUALITIES RATING SCALE: THE IMPACT OF THE PILOT SUBJECTIVITY IN WORKLOAD EVALUATION | ICAS2024_0848 |
| Turco, R. | PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS | ICAS2024_1205 |
| Turner, M. | VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA | ICAS2024_0104 |
| Turon, A. | ON AN EFFICIENT GLOBAL/LOCAL STOCHASTIC METHODOLOGY FOR FAILURE PREDICTION OF AIRCRAFT COMPOSITE STRUCTURES | ICAS2024_0250 |
| Türkyilmaz, B. | MODELLING AND INITIAL ASSESSMENT OF A FUEL CELL AUXILIARY PROPULSION AND POWER UNIT | ICAS2024_0261 |
| Türkyilmaz, B. | DESIGN OPTIMISATION OF A BOUNDARY LAYER INGESTION PROPULSOR FOR A MULTI-FUEL HYDROGEN AIRCRAFT | ICAS2024_1060 |
| Uellendahl, M. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Uenaka, A. | ELECTRIC FIELD MEASUREMENT IN GLOW DISCHARGE PLASMA INTERACTING WITH SHOCK WAVE IN HYPERSONIC FLOW | ICAS2024_0390 |
| Unterstrasser, S. | TOWARDS REFINED CONTRAIL SIMULATIONS OF FORMATION FLIGHT SCENARIOS | ICAS2024_0502 |
| Urso, G. | EFFICIENT SHAPE OPTIMIZATION IN AERONAUTICS: INTEGRATING PARAMETRIC CAD AND MESH MORPHING FOR ENHANCED AERODYNAMIC PERFORMANCE | ICAS2024_0824 |
| Usuelli, D. | PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION PLASMA THRUSTERS | ICAS2024_0649 |
| Vaghela, P. | BIRD AND DRONE IMPACT DAMAGE PROGNOSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT ENGINE | ICAS2024_1162 |
| Valente, M. | A PRELIMINARY METHODOLOGY TO ASSESS GUST SPECTRA VIA SATELLITE DATA | ICAS2024_1142 |
| Valentini, A. | AI-ASSISTED DESIGN OF UAV DOCKING STATION NETWORK FOR DUAL USE PURPOSES | ICAS2024_1133 |
| Vampola, T. | PREDICTION OF TRANSIENT DEFORMATION BY COUPLING CFD AND FEM ANALYSIS USING MACHINE LEARNING BASED CORRELATION FUNCTION | ICAS2024_1084 |
| Van Beeck, J. | DESIGN OF MEASUREMENT SETUP FOR HIGH-ALTITUDE IN-FLIGHT EXPERIMENTS ON DU89-134/14 AIRFOIL AT LOW REYNOLDS NUMBER | ICAS2024_0757 |
| Van Biert, L. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| van Dam, C.P. | SCOPING OF AN AIR SUPPLY CONFIGURATION FOR ACTIVE FLOW CONTROL ON A COMMERCIAL TRANSPORT AIRPLANE HIGH-LIFT SYSTEM | ICAS2024_0951 |
| Van der Laan, T. | VALUE-DRIVEN TRADESPACE EXPLORATION FOR AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN | ICAS2024_0589 |
| Van der Meulen, M.-J. | DUAL-STREAM JET NOISE TEST WITH INTERNAL MIXER DESIGN VARIATIONS FOR LTO NOISE OF SUPERSONIC AIRCRAFT | ICAS2024_0064 |
| van der Meulen, M.-J. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Van Eenige, M. | EU IMPACT MONITOR PROJECT - OVERVIEW AND APPROACH | ICAS2024_1114 |
| van Garrel, A. | FLYING WING CIRCULATION DISTRIBUTIONS, AERODYNAMIC PERFORMANCE AND WAKE ROLL-UP | ICAS2024_1153 |
| van Heerden, A.S.J. | SET-BASED DESIGN TECHNIQUES FOR EVOLVABILITY EXPLORATION DURING CONCEPTUAL AIRCRAFT DESIGN | ICAS2024_0233 |
| van Herden, A.S.J. | DIGITAL COLLABORATION FOR SUSTAINABLE AVIATION | ICAS2024_1326 |
| van Hoorn, N. | ELECTROMAGNETIC INDUCTION HEATING OF TP-CFRP LAMINATES: FEM MODELLING AND VALIDATION | ICAS2024_0032 |
| Vankan, W.J. | ELECTROMAGNETIC INDUCTION HEATING OF TP-CFRP LAMINATES: FEM MODELLING AND VALIDATION | ICAS2024_0032 |
| Vankan, W.J. | DESIGN AND ANALYSIS OF A SCALED COMPOSITE UHBR FAN BLADE FOR WIND TUNNEL TESTS | ICAS2024_0157 |
| Varriale, C. | A SYSTEM OF SYSTEMS AIRCRAFT DESIGN FRAMEWORK: DEMONSTRATION USING A SEAPLANE TRANSPORT NETWORK IN THE GREEK ISLANDS | ICAS2024_0402 |
| Varriale, C. | LATENT SPACE CORRELATION FOR INTERPRETABLE AIRFOIL PARAMETERIZATION USING VARIATIONAL AUTOENCODERS | ICAS2024_0484 |
| Varriale, C. | OPTIMAL APPROACH AND DEPARTURE TRAJECTORIES WITH ACOUSTIC FOOTPRINT ASSESSMENT FOR AN AIR MOBILITY QUAD-ROTOR | ICAS2024_1115 |
| Vashi, S. | EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS | ICAS2024_0464 |
| Vauquelin, P. | EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR | ICAS2024_0518 |
| Vaziry Zanjany, M.A. | APPLICATION OF LAMBDA FRAMEWORK FOR AIRCRAFT MULTIDISCIPLINARY DESIGN, ANALYSIS AND OPTIMIZATION | ICAS2024_0068 |
| Vehlhaber, F. | AIRPORT INFRASTRUCTURE SIZING FOR A REGIONAL ELECTRIC AVIATION NETWORK | ICAS2024_0686 |
| Veldhuis, L.L.M. | AERODYNAMIC PERFORMANCE AND INTERACTION EFFECTS OF AN OVER-THE-WING DISTRIBUTED-PROPELLER SYSTEM IN CRUISE CONDITIONS | ICAS2024_0632 |
| Venkatachari, B. | TRANSITION MODELING IN SUPPORT OF CFD VISION 2030 - HIGHLIGHTS OF RECENT EFFORTS AT THE NASA LANGLEY RESEARCH CENTER | ICAS2024_0081 |
| Venner, C.H. | FLYING WING CIRCULATION DISTRIBUTIONS, AERODYNAMIC PERFORMANCE AND WAKE ROLL-UP | ICAS2024_1153 |
| Ventura, S.S. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Venuti, J. | COMPARING CONVECTIVE WEATHER IMPACTS ON AIR TRAFFIC MANAGEMENT OPERATIONS IN UNITED STATES, CANADA & EUROPE | ICAS2024_0137 |
| Venuti, J. | WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES | ICAS2024_1137 |
| Vera Sepúlveda, D. | AERODYNAMIC ANALYSIS OF A FLAP-BASED DEPLOYABLE RE-ENTRY SYSTEM UNDER RAREFIED CONDITIONS | ICAS2024_1201 |
| Veraburenon, W. | LIFE CYCLE ASSESSMENT OF ALTERNATIVE LAUNCH METHODS | ICAS2024_0545 |
| Vercella, V. | HYDROGEN STORAGE SYSTEM DESIGN: CASE STUDIES FOR AIRBORNE APPLICATION | ICAS2024_0590 |
| Verde, N. | FLUIDODYNAMIC ANALYSIS OF LOW REYNOLDS NUMBER FLOWS | ICAS2024_0354 |
| Verhagen, W. | MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION | ICAS2024_0020 |
| Verhagen, W. | APPLICATION OF NATURAL LANGUAGE PROCESSING FOR AIRCRAFT DEFECT TRACKING IN MAINTENANCE OPERATIONS | ICAS2024_0083 |
| Verma, R. | AN AUTONOMOUS SYSTEM FOR DOCKING AND BATTERY SWAPPING IN UAVS | ICAS2024_1116 |
| Verstraete, D. | ON THE CHALLENGES OF SURROGATE-BASED AERODYNAMIC SHAPE OPTIMISATION | ICAS2024_0319 |
| Verstraete, D. | ON THE CHOICE OF TURBULENCE MODEL FOR THE SIMULATION OF AIRFOILS AT REYNOLDS NUMBER BELOW 200,000 | ICAS2024_0327 |
| Verstraete, D. | INFLUENCE OF MOTOR CHARACTERISTICS ON OPTIMAL PROPROTOR DESIGN | ICAS2024_0329 |
| Vertonghen, L. | STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT | ICAS2024_0855 |
| Vervliet, J. | NOVEL TEST RIG TO DEMONSTRATE A MULTI FUNCTIONAL FLAP MECHANISM OFFERING A 2ND DEGREE OF FREEDOM | ICAS2024_0299 |
| Vich, O. | W-WING AEROELASTIC DEMONSTRATOR DESIGN MODIFICATION AND UPGRADE | ICAS2024_0054 |
| Vieira da Fonseca, J.M. | HELICOPTER ACCIDENTS IN BRAZIL: AN ANALYSIS OF MAINTENANCE FROM THE PERSPECTIVE OF HUMAN FACTORS | ICAS2024_0416 |
| Viglietti, I. | HYBRID AIR DATA SYSTEM ARCHITECTURE: FROM DESIGN TO FLIGHT TEST VERIFICATION | ICAS2024_0056 |
| Viitanen, T. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Villani, E. | A SYSTEMATIC REVIEW OF HUMAN FACTORS AND AI INFLUENCING OPERATOR PERFORMANCE IN MUM-T ENVIRONMENTS | ICAS2024_0132 |
| Villani, E. | ASSESSING MENTAL WORKLOAD AND INTERFACE USABILITY IN MILITARY PILOTS: AN ADVANCED EYE-TRACKING METHODOLOGY | ICAS2024_0202 |
| Villani, E. | FAULT DETECTION FOR AN AIRCRAFT ELEVATOR | ICAS2024_0647 |
| Villani, E. | MULTIPLATFORM SIMULATION USING ROS | ICAS2024_0755 |
| Villas, F. | CONCEPT OF OPERATIONS IN AN AGENT-BASED SIMULATION: A SYSTEM-OF-SYSTEMS APPROACH | ICAS2024_0357 |
| Villegas, I.F. | CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS | ICAS2024_0091 |
| Villena Munoz, C. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Villena Muñoz, C. | DESIGN OF THE SENECA MACH 1.8 SUPERSONIC AIRLINER WITH MULTI-FIDELITY AERODYNAMIC ANALYSIS FOR NOISE-OPTIMISED TAKE-OFF TRAJECTORIES | ICAS2024_0758 |
| Vindigni, C.R. | ADAPTIVE WING FLUTTER SUPPRESSION BY MEANS OF MULTIPLE TRAILING EDGE CONTROL SURFACES - A COMPARATIVE STUDY | ICAS2024_0513 |
| Vio, G.A. | SURFACE VISUALISATION OF TIME AVERAGED FLOW BEHAVIOUR AROUND RIGID AND FLEXIBLE HEMISPHERES UTILISING UV SENSITIVE OIL | ICAS2024_0070 |
| Vio, G.A. | WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS | ICAS2024_0348 |
| Vio, G.A. | AEROACOUSTIC CAVITY FLOW ENERGY HARVESTING | ICAS2024_0558 |
| Viola, N. | THE FUTURE OF CIVIL SUPERSONIC TRANSPORT IN EUROPE: THE SENECA AND MORE&LESS PROJECTS | ICAS2024_0820 |
| Viola, N. | SONIC BOOM COMPARATIVE STUDY BETWEEN MACH 4.7 OUTDOOR EXPERIMENTAL TESTS AND NUMERICAL SIMULATIONS | ICAS2024_0882 |
| Viola, N. | COMPARISON OF LIFE CYCLE COST FOR MACH 8 AND MACH 5 HYPERSONIC PASSENGERS AIRCRAFT | ICAS2024_0924 |
| Viola, N. | CONCEPTUAL DESIGN METHODOLOGY FOR LOW-SUPERSONIC LH2-POWERED PASSENGERS AIRCRAFT | ICAS2024_0927 |
| Viola, N. | INTEGRATING ECO-EFFICIENT FLIGHT PLANNING IN AIRCRAFT CONCEPTUAL DESIGN: MINIMAL NOX ROUTES FOR HIGH-SPEED AIRCRAFT USING HYDROGEN | ICAS2024_0950 |
| Viola, N. | AERODYNAMIC NUMERICAL/EXPERIMENTAL COMPARISON OF A HYPERSONIC TEST VEHICLE IN MORE&LESS PROGRAM | ICAS2024_1026 |
| Viola, N. | ESATTO: THE HOLISTIC FRAMEWORK TO SUPPORT THE DESIGN OF SUSTAINABLE SUPERSONIC AVIATION | ICAS2024_1032 |
| Virdis, A. | NUMERICAL-THEORETICAL EVALUATION OF THE DITCHING OF A HULL WITH DIHEDRAL ANGLES BETWEEN -5 AND 20 DEGREES | ICAS2024_0665 |
| Viry, P. | AN EMPIRICAL AND CUSTOMISABLE FLEET RENEWAL MODEL FOR PROSPECTIVE SCENARIOS USING OPEN-ACCESS DATA | ICAS2024_0367 |
| Viscardi, M. | MODELING TECHNIQUE FOR THE EVALUTAION OF ENVIRONMENTAL EFFECT OF FLIGHT-PATH NEAR AIRPORTS: THE CASE STUDY OF A NEW ROUTE AT NAPLES AIRPORT | ICAS2024_0845 |
| Vitiello, F. | RESEARCH RESULTS AND PERSPECTIVES ON NON-COOPERATIVE SENSING FOR SAFE UAM OPERATIONS | ICAS2024_1267 |
| Viviani, A. | AERODYNAMICS AND AEROACOUSTIC ANALYSIS OF A SUPERSONIC SLENDER-BODY GEOMETRY | ICAS2024_0309 |
| Viviani, A. | WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS | ICAS2024_0348 |
| Viviani, A. | FLUIDODYNAMIC ANALYSIS OF LOW REYNOLDS NUMBER FLOWS | ICAS2024_0354 |
| Viviani, A. | SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT | ICAS2024_0361 |
| Viviani, A. | ENGINEERING-BASED TOOL FOR THREE-DIMENSIONAL ESTIMATIONS OF RE-ENTRY VEHICLES AEROTHERMODYNAMICS | ICAS2024_0859 |
| Viviani, A. | OPTIMIZATION PROCEDURE FOR THE WING OF A MARS EXPLORATION DRONE | ICAS2024_0862 |
| Viviani, A. | PRELIMINARY DESIGN OF A FIXED-WING DRONE FOR MARS EXPLORATION ACTIVITIES | ICAS2024_0863 |
| Viviani, A. | LOW SPEED AERODYNAMICS OF SIX OPTIMISED UNCONVENTIONAL RE-ENTRY VEHICLE AEROSHAPES | ICAS2024_0864 |
| Vlach, J. | W-WING AEROELASTIC DEMONSTRATOR DESIGN MODIFICATION AND UPGRADE | ICAS2024_0054 |
| Vogel, E. | TRANSITION MODELING IN SUPPORT OF CFD VISION 2030 - HIGHLIGHTS OF RECENT EFFORTS AT THE NASA LANGLEY RESEARCH CENTER | ICAS2024_0081 |
| Voigt, C. | RECENT FLIGHT EXPERIMENTS SHOW THE CLIMATE BENEFITS OF SUSTAINABLE AVIATION FUELS (SAF) AND ADVANCED ENGINE TECHNOLOGIES | ICAS2024_1252 |
| Vos, R. | FLYING V DIRECTIONAL FLIGHT CONTROL: AN EXPERIMENTAL INVESTIGATION | ICAS2024_1014 |
| Voth, V. | AIRCRAFT SYSTEM DESIGN: A MODEL-BASED AND COLLABORATIVE APPROACH | ICAS2024_0160 |
| Vozella, A. | HYDROGEN SAFETY: A COMPARATIVE ANALYSIS OF LEAK DETECTION SENSORS | ICAS2024_0149 |
| Voß, A. | CLOSED-LOOP GUST LOADS ANALYSIS OF A SUPERSONIC FIGHTER AIRCRAFT | ICAS2024_0011 |
| Voß, A. | FLIGHT MECHANICAL ANALYSIS OF A VERY FLEXIBLE HIGH-ALTITUDE PLATFORM UNDER UNCERTAINTY CONSIDERATIONS | ICAS2024_0310 |
| Vroon, J. | NOVEL TEST RIG TO DEMONSTRATE A MULTI FUNCTIONAL FLAP MECHANISM OFFERING A 2ND DEGREE OF FREEDOM | ICAS2024_0299 |
| Vukovic, D. | REVITALIZATION OF A FLOW-CELL DEVICE FOR AIR INTAKE TESTING AND ITS INTEGRATION WITH WIND TUNNEL SYSTEMS | ICAS2024_0218 |
| Wada, D. | EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) | ICAS2024_0549 |
| Wahls, R. | UNITED STATES' AIRCRAFT SUSTAINABILITY RESEARCH & DEVELOPMENT EFFORTS | ICAS2024_1229 |
| Waitman, S. | CONTROL ALLOCATION FOR A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT USING DIFFERENTIAL THRUST | ICAS2024_1182 |
| Wallace, R.D. | DISTRIBUTED THRUST TAKEOFF FOR THE NASA X-57 MOD IV FLIGHT DEMONSTRATOR | ICAS2024_1290 |
| Wallin, M. | PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES | ICAS2024_1222 |
| Walz, M. | A CALL TO ACTION TO ENGAGE THE COMMUNITY TO MEET THE CHALLENGES THAT MUST BE TACKLED TO MAKE ELECTRIFIED AIRCRAFT PROPULSION REAL | ICAS2024_0834 |
| Wan, B. | A PHASE FIELD BASED DEEP LEARNING APPROACH FOR MECHANICAL PROPERTY PREDICTION OF SINTERED SILVER IN POWER ELECTRONICS | ICAS2024_0351 |
| Wan, J. | HARDWARE-IN-THE-LOOP SIMULATION FRAMEWORK FOR THE EVALUATION OF AUTONOMOUS FLIGHT FUNCTIONS | ICAS2024_0897 |
| Wan, L. | PRESERVING HUMAN EXPERTISE: EXPLORING MIXED REALITY TRAJECTORY PLANNING FOR ROBOTIC BELT GRINDING | ICAS2024_0378 |
| Wan, X. | INVESTIGATION ON VARIABLE-HEIGHT PROTRUSION ARRANGEMENT OF METAL–COMPOSITE HYBRID JOINTS UNDER A TENSILE LOAD | ICAS2024_1099 |
| Wang, B. | SEPARATION SAFETY ANALYSIS IN VARIABLE LAUNCH CONDITION OF SMALL AIR-LAUNCHED UAVS BASED ON NUMERICAL SIMULATION AND FLIGHT TEST | ICAS2024_0311 |
| Wang, B. | FATIGUE CRACK LIFE PREDICTION BASED ON BAYESIAN DYNAMIC UPDATE | ICAS2024_0393 |
| Wang, B. | STUDY ON FATIGUE PROPERTIES OF TITANIUM ALLOY BASE MATERIAL AND WELDED STRUCTURE IN THERMAL COMBINED ENVIRONMENT | ICAS2024_0422 |
| Wang, B. | HIGH-VELOCITY DROPLET IMPACT STUDIES ON C/SIC AND C/C COMPOSITES | ICAS2024_0808 |
| Wang, B. | MULTI SENSOR AND MULTI TASK ALLOCATION BASED ON IMPROVED WHALE OPTIMIZATION ALGORITHM | ICAS2024_1028 |
| Wang, B.T. | EXPERIMENTAL INVESTIGATION AND NUMERICAL ANALYSIS OF THE EFFECT OF TEMPERATURE ON THE MECHANICAL PROPERTIES OF AEROSPACE COMPOSITE-METAL HYBRID JOINTS | ICAS2024_0530 |
| Wang, C. | EFFECTS OF PROCESSING STRATEGIES ON SURFACE QUALITY AND MECHANICAL PROPERTIES IN HYBRID ADDITIVE MANUFACTURING OF IN718 ALLOY | ICAS2024_0593 |
| Wang, C. | A HIGH-PRECESION PSEUDO ARC-LENGTH METHOD WITH POSITIVE VALUE PRESERVATION PROPERTIES BASED ON TV SPLITTING | ICAS2024_0694 |
| Wang, C. | FUZZING ON TARGET DETECTION SYSTEM OF UNMANNED AERIAL VEHICLE | ICAS2024_0794 |
| Wang, C.-S. | ANALYSIS ON COMPLEX HYPERSONIC FLOW DURING THE REENTRY OF EXPIRED SPACECRAFT | ICAS2024_0644 |
| Wang, C.Q. | ROBUST SLIDING MODE CONTROL FOR UAV FORMATION WITH EXTERNAL DISTURBANCES UNDER EVENT-TRIGGERED STRATEGY | ICAS2024_0013 |
| Wang, F. | DAMAGE AND MECHANICAL REPAIR OF COMPOSITE LAMINATES: EFFECTS OF EMBEDDED DEFECTS AND LOW VELOCITY IMPACTS | ICAS2024_0748 |
| Wang, F. | SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT | ICAS2024_0925 |
| Wang, G. | NUMERICAL STUDY OF FLOWS OVER LAUNCH VEHICLES WITH VARIOUS FAIRING BY SECOND-MOMENT CLOSURE DETACHED-EDDY SIMULATION | ICAS2024_0641 |
| Wang, G. | NUMERICAL INVESTIGATION OF THE INTERACTION OF OPPOSING JETS AND SUPERSONIC FREE FLOWS | ICAS2024_0783 |
| Wang, H. | INTEGRITY MONITORING OF TIGHTLY INTEGRATED BDS/SINS USING MULTI-HYPOTHESIS SOLUTION SEPARATION (MHSS) ALGORITHM | ICAS2024_0244 |
| Wang, H. | SIMULATION STUDY ON AERODYNAMIC CHARACTERISTICS OF COMBINED LOW ASPECT RATIO UAV | ICAS2024_0449 |
| Wang, H. | DYNAMIC DROP SIMULATION OF THE MAIN LANDING GEAR OF A GENERAL AVIATION AIRCRAFT | ICAS2024_0588 |
| Wang, H.-Z. | MODELING AND VALIDATION OF MORPHING WING TRAILING EDGE BASED ON ZERO POISSON'S RATIO HONEYCOMB | ICAS2024_1015 |
| Wang, H.Y. | NUMERICAL STUDIES ON NOISE-SHIELDING EFFECTS OF A BLENDED-WING-BODY AIRCRAFT USING BOUNDARY ELEMENT METHOD | ICAS2024_0556 |
| Wang, J. | NUMERICAL SIMULATION STUDY ON THE INFLUENCE OF WING SPACING OF DRAGONFLY-INSPIRED FLAPPING WINGS | ICAS2024_0243 |
| Wang, J. | STUDY OF THE SCAVENGE PUMP PERFORMANCE FOR TWO-PHASE FLOW IN AN AIRCRAFT ENGINE LUBRICATION SYSTEM | ICAS2024_0788 |
| Wang, J. | A SEMANTIC MODEL-BASED SYSTEMS ENGINEERING APPROACH FOR SUPERSONIC BUSINESS JET CONCEPTUAL DESIGN | ICAS2024_0843 |
| Wang, J.C.-H. | SYSTEM OF SYSTEMS ANALYSIS OF AUTONOMOUS AIRCRAFT OPERATIONS IN AIR CARGO FEEDER NETWORKS | ICAS2024_0413 |
| Wang, J.C.-H. | MODELING CARGO DEMAND FOR REGIONAL AIR TRANSPORT NETWORKS IN CANADA AND THE UNITED STATES | ICAS2024_0729 |
| Wang, K.-K. | NOVEL GRADIENT-ENHANCED MULTI-FIDELITY SURROGATE MODEL ASSISTED ROBUST MULTIDISCIPLINARY DESIGN OPTIMIZATION OF TAILLESS FLYING WING | ICAS2024_0298 |
| Wang, L. | NUMERICAL SIMULATION STUDY ON THE INFLUENCE OF WING SPACING OF DRAGONFLY-INSPIRED FLAPPING WINGS | ICAS2024_0243 |
| Wang, L. | DESIGN OF ATTITUDE CONTROL SYSTEM FOR DRAGONFLY-INSPIRED FLAPPING WING AERIAL VEHICLE | ICAS2024_0578 |
| Wang, L.H. | ROBUST SLIDING MODE CONTROL FOR UAV FORMATION WITH EXTERNAL DISTURBANCES UNDER EVENT-TRIGGERED STRATEGY | ICAS2024_0013 |
| Wang, M. | NUMERICAL AND THEORETICAL INVESTIGATION OF HELICOPTER DITCHING WITH VARIOUS INITIAL VELOCITY AND PITCHING ANGLE | ICAS2024_0216 |
| Wang, M. | DESIGN OF DUAL-FUSELAGE FLIGHT PLATFORM FOR JET CONTROL FUNCTION VERIFICATION | ICAS2024_0812 |
| Wang, M. | MICKEY MOUSE AND A GIANT: COMPARISON OF AERONAUTICS EDUCATION IN FINLAND AND CHINA | ICAS2024_1263 |
| Wang, M.-Q. | LARGE-SCALE STRUCTURAL DYNAMIC TOPOLOGY OPTIMIZATION DESIGN FOR AIRCRAFT VIBRATION REDUCTION UNDER RANDOM EXCITING RESPONSE | ICAS2024_0365 |
| Wang, M.-X. | EXPERIMENTAL AND NUMERICAL INVESTIGATION ON SEPARATION CHARACTERISTICS OF SERPENTINE CONVERGENT-DIVERGENT NOZZLE | ICAS2024_0920 |
| Wang, P. | TRANSIENT SIMULATION CALCULATION FOR ELECTRIC THERMAL ANTI-ICING PERFORMANCE OF COMPOSITE WING IN ICING ENVIRONMENT | ICAS2024_0721 |
| Wang, P.-H. | EXPLORATION OF EFFICIENT HYPERPARAMETERS ADAPTION OF SUPPORT VECTOR REGRESSION FOR AERODYNAMIC DESIGN | ICAS2024_0625 |
| Wang, Q. | AN UAV MANEUVERING DECISION-MAKING ALGORITHM BASED ON DEEP TRANSFER REINFORCEMENT LEARNING | ICAS2024_1020 |
| Wang, S. | SPARSE POLYNOMIAL CHAOS-BASED SONIC BOOM UNCERTAINTY QUANTIFICATION AND AERODYNAMIC/SONIC BOOM ROBUST DESIGN OPTIMIZATION UNDER MULTI-PARAMETER UNCERTAINTIES | ICAS2024_0373 |
| Wang, S. | STUDY OF DROPLET MOTION AND WATER FILM FLOW CHARACTERISTICS ON SUPERHYDROPHOBIC SURFACES UNDER AIRFLOW SHEARING | ICAS2024_0934 |
| Wang, T. | EFFECTS OF PROCESSING STRATEGIES ON SURFACE QUALITY AND MECHANICAL PROPERTIES IN HYBRID ADDITIVE MANUFACTURING OF IN718 ALLOY | ICAS2024_0593 |
| Wang, T. | DEEP LEARNING BASED FAST PREDICTION OF AERODYNAMIC PARAMETERS FOR DUCTED PROPELLERS | ICAS2024_1011 |
| Wang, W. | THERMAL AND GRINDING PERFORMANCE OF 3D PRINTED COMPLIANCE GRINDING TOOLS WITH ROTARY-ENHANCED HEAT TRANSFER STRUCTURE | ICAS2024_0248 |
| Wang, W. | REDESIGN AND MACHINING OF LEADING EDGE OF TRANSONIC COMPRESSOR BLADE IN ROBOTIC GRINDING OPERATION | ICAS2024_0260 |
| Wang, W. | WEAR EVOLUTION OF PYRAMID-STRUCTURED ABRASIVE BELTS AND ITS EFFECT ON GRINDING OPERATIONS | ICAS2024_0368 |
| Wang, W. | INFLUENCE OF REINFORCED TRAILING EDGE ON FLAPPING WING AERODYNAMIC FORCE AND DEFORMATION | ICAS2024_0526 |
| Wang, W. | AEROELASTIC DIVERGENCE AND FLUTTER ANALYSIS OF A WING WITH ALL MOVING WING TIP | ICAS2024_0642 |
| Wang, W. | THE EFFECTS OF INITIAL STRESS ON AERODYNAMIC PERFORMANCE OF FLEXIBLE MEMBRANE-SKELETON WINGS WITH FSI SIMULATION | ICAS2024_0752 |
| Wang, W. | MULTI-FIDELITY SURROGATE MODELING BASED ON DATA EXTENSION USING POD AND ANN | ICAS2024_0957 |
| Wang, W. | IMPACT RESPONSES AND FAILURE MECHANISMS OF ALMGB14 UNDER DYNAMIC LOADS | ICAS2024_1006 |
| Wang, W. | INVESTIGATION ON VARIABLE-HEIGHT PROTRUSION ARRANGEMENT OF METAL–COMPOSITE HYBRID JOINTS UNDER A TENSILE LOAD | ICAS2024_1099 |
| Wang, W.-J. | COMPUTATIONAL/EXPERIMENTAL AEROELASTIC STUDY FOR AN ALL-MOVABLE HORIZONTAL TAIL WITH TORSION FREE-PLAY | ICAS2024_0728 |
| Wang, W.-X. | PRESERVING HUMAN EXPERTISE: EXPLORING MIXED REALITY TRAJECTORY PLANNING FOR ROBOTIC BELT GRINDING | ICAS2024_0378 |
| Wang, W.-X. | EFFECTS OF PROCESSING STRATEGIES ON SURFACE QUALITY AND MECHANICAL PROPERTIES IN HYBRID ADDITIVE MANUFACTURING OF IN718 ALLOY | ICAS2024_0593 |
| Wang, X. | LINEAR QUADRATIC PURSUIT AND EVASION DIFFERENTIAL GAME GUIDANCE STRATEGY WITH OBSTACLE AVOIDANCE | ICAS2024_0008 |
| Wang, X. | RESEARCH ON UNMANNED CLUSTER RECONNECTION DECISION-MAKING METHOD CONSIDERING RESOURCE SUPPLEMENTATION | ICAS2024_0343 |
| Wang, X. | RESEARCH ON UNMANNED CLUSTER RECONNECTION DECISION-MAKING METHOD CONSIDERING RESOURCE SUPPLEMENTATION | ICAS2024_0343 |
| Wang, X. | FLUID-STRUCTURE INTERACTION OF TWO-PHASE SCATTERER METAMATERIALS FOR VIBRATION SELF-SUPPRESSION | ICAS2024_0435 |
| Wang, X. | SUSTAINABLE FUELS SAFETY BOUNDARIES DEMARCATION METHOD | ICAS2024_0712 |
| Wang, X. | EFFICIENT MULTI-FIDELITY REDUCED-ORDER MODELING FOR FLUTTER PREDICTIONS ACROSS MULTIPLE MACH NUMBERS | ICAS2024_0900 |
| Wang, X. | DYNAMIC STALL PREDICTION THROUGH COMBINING PHYSICAL MODELS AND MACHINE LEARNING | ICAS2024_1080 |
| Wang, X.-Y. | ANALYSIS OF SUCTION FORCE EFFECT ON DIFFERENT FUSELAGE SHAPE DURING THE WATER DITCHING | ICAS2024_0929 |
| Wang, X.H. | A PHASE FIELD BASED DEEP LEARNING APPROACH FOR MECHANICAL PROPERTY PREDICTION OF SINTERED SILVER IN POWER ELECTRONICS | ICAS2024_0351 |
| Wang, X.H. | A PHASE FIELD BASED DEEP LEARNING APPROACH FOR MECHANICAL PROPERTY PREDICTION OF SINTERED SILVER IN POWER ELECTRONICS | ICAS2024_0351 |
| Wang, Y. | FAST PREDICTION METHOD FOR RADIAL GROWTH OF LABYRINTH SEAL CLEARANCE BASED ON TRANSIENT THERMAL-FLUID COUPLING NETWORK | ICAS2024_0450 |
| Wang, Y. | VALIDATION OF ENERGY CHARACTERISTICS IN FLIGHT CONTROL SYSTEM BASED ON A MULTIDISCIPLINARY VIRTUAL PLATFORM | ICAS2024_0646 |
| Wang, Y. | VIBRATION ANAYLYSIS AND INFLUENCING FACTOR STUTY OF HELICOPTER HYDRAULIC PIPELINNE | ICAS2024_0678 |
| Wang, Y.-F. | INFLUENCE OF REINFORCED TRAILING EDGE ON FLAPPING WING AERODYNAMIC FORCE AND DEFORMATION | ICAS2024_0526 |
| Wang, Y.-Q. | DATA MINING ANALYSIS ON AERODYNAMIC STEALTH DESIGN PRINCIPLES OF AIRFOIL PROFILES | ICAS2024_0448 |
| Wang, Y.-Z. | EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN | ICAS2024_0962 |
| Wang, Y.H. | DESIGN OPTIMIZATION OF A WIG CRAFT’S HIGH LIFT DEVICE CONSIDERING GROUND EFFECT | ICAS2024_0572 |
| Wang, Z. | RESEARCH ON TECHNOLOGICAL INNOVATION CAPABILITY EVALUATION INDEX FOR AVIATION INDUSTRIES | ICAS2024_0211 |
| Wang, Z. | SENSITIVITY ANALYSIS OF SAFETY FACTORS BASED ON MODEL OF AVIATION RECIPROCATING ENGINE TURBOCHARGING SYSTEM | ICAS2024_0599 |
| Wang, Z. | FUZZING ON TARGET DETECTION SYSTEM OF UNMANNED AERIAL VEHICLE | ICAS2024_0794 |
| Wang, Z.-L. | A METHOD FOR AUTOMATIC GENERATING SAFETY ANALYSIS BASED ON AVIATION PISTON ENGINE MODEL | ICAS2024_0587 |
| Wang, Z.-X. | AERODYNAMIC DEFORMATION EXPERIMENT OF SERPENTINE NOZZLE FOR TURBOFAN AND ANALYSIS OF FLUID-STRUCTURE INTERACTION METHOD | ICAS2024_0919 |
| Wang, Z.H. | DYNAMIC DROP SIMULATION OF THE MAIN LANDING GEAR OF A GENERAL AVIATION AIRCRAFT | ICAS2024_0588 |
| Wang, Z.J. | ANALYSIS OF THE R FAMILY OF LIMITERS APPLIED TO HIGH-ORDER FR/CPR SCHEMES FOR THE SIMULATION OF SUPERSONIC FLOWS | ICAS2024_1181 |
| Warsch, C. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Warwick, G. | A VIEW LOOKING IN - AVIATION WEEK'S ASSESSMENT OF SUSTAINABLE AVIATION R&D IN CHINA AND THE ASIA-PACIFIC REGION | ICAS2024_1255 |
| Watanabe, S. Watanabe | OVERVIEW OF JAPANESE R&D ACTIVITIES ON GREEN TRANSFORMATION AND DIGITAL TRANSFORMATION IN AVIATION | ICAS2024_1221 |
| Wauer, L. | DLR DESIGN CHALLENGE 2024: DESIGN OF A COST AND ENERGY EFFICIENT REGIONAL AIRCRAFT | ICAS2024_1264 |
| Wehrel, P. | KNOWLEDGE-BASED TURBINE DISK MODELING – A CONCEPTUAL DESIGN PROCESS CALIBRATED TO THE NASA ENERGY EFFICIENT ENGINE | ICAS2024_0272 |
| Wehrend, S. | DIGITALISATION AND SUSTAINABILITY IN CABIN DESIGN: SYNERGIES AND DEPENDENCIES | ICAS2024_0165 |
| Wehrend, S. | TOWARDS A HOLISTIC APPROACH TO INCREASE SUSTAINABILITY IN AIRCRAFT CABIN DESIGN | ICAS2024_0511 |
| Wei, C. | AERODYNAMIC OPTIMIZATION OF HIGH-ALTITUDE PROPELLER COMBINED WITH MACHINE LEARNING METHOD | ICAS2024_0342 |
| Wei, C. | AERO-KINEMATIC OPTIMIZATION OF HIGH-LIFT DEVICES WITH DOWNWARD DEFLECTION OF SPOILER | ICAS2024_0639 |
| Weigand, B. | VALIDATION OF MULTIPHASE FLOW SIMULATIONS BY EXPERIMENTAL MEASUREMENTS IN A CHANNEL FLOW | ICAS2024_0176 |
| Weigand, B. | EXPERIMENTAL SETUP FOR THE INVESTIGATION OF WATER SEPARATION IN ANNULAR FLOW WITHIN A CIRCULAR CHANNEL | ICAS2024_0969 |
| Weinerfelt, P. | ENHANCING EFFICIENCY FOR UNSTEADY CFD COMPUTATIONS IN AERONAUTICS | ICAS2024_0247 |
| Weinman, K. | APPLICATION OF DIFFERENT NUMERICAL TOOLS AND NUMERICAL METHODS FOR PREDICTION OF HEAT EXCHANGER RAMAIR-CONCEPTS FOR HYBRID ELECTRIC PROPULSION AIRCRAFT CONFIGURATIONS | ICAS2024_0062 |
| Weiss, F. | DRIVETRAIN INFLUENCE ON THE LEAD-LAG MOTION OF HELICOPTER ROTORS | ICAS2024_1241 |
| Wells, D.P. | NASA TRANSONIC TRUSS-BRACED WING STUDIES | ICAS2024_0108 |
| Welsch, T. | SPEED GATED INTERCEPT PROCEDURE STUDY FOR INTEGRATION OF INCREASING DIVERSE OPERATIONS (IDO) AT EUROPEAN AIRPORTS | ICAS2024_0685 |
| Wende, G. | MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION | ICAS2024_0020 |
| Wende, G. | TRANSLATING THE CONCEPT OF SUSTAINABILITY FOR THE DETERMINATION OF REQUIREMENTS FOR THE DESIGN OF FUTURE AIRCRAFT | ICAS2024_0042 |
| Wende, G. | CINNABAR PROJECT – COST-BENEFIT ANALYSIS OF DIGITAL PROCESSES FOR NON-DESTRUCTIVE INSPECTIONS OF AIRCRAFT STRUCTURES | ICAS2024_0125 |
| Wende, G. | CINNABAR PROJECT - AUGMENTED REALITY WORKFLOW FOR AIRCRAFT DENT & BUCKLE INSPECTION | ICAS2024_0152 |
| Wende, G. | CINNABAR PROJECT: EXAMINING REQUIREMENTS FOR USER ACCEPTANCE OF AIRCRAFT STRUCTURE INSPECTION IN AUGMENTED REALITY | ICAS2024_0164 |
| Wende, G. | TRAIN ON SYNTHETIC - TEST ON REAL: DOMAIN ADAPTATION FOR STRAIN-BASED DAMAGE DETECTION ON AN AIRCRAFT WING | ICAS2024_0169 |
| Wende, G. | SUSTAINABLE ENGINE MAINTENANCE: EVALUATING THE ECOLOGICAL IMPACT OF LIFE LIMITED PART REPLACEMENT | ICAS2024_0452 |
| Wendt, K. | ADVANCING URBAN AIR MOBILITY: COLLABORATIVE EXCELLENCE AND INFRASTRUCTURE INITIATIVES BY DLR | ICAS2024_1223 |
| Wenz, L. | DLR DESIGN CHALLENGE 2024: DESIGN OF A COST AND ENERGY EFFICIENT REGIONAL AIRCRAFT | ICAS2024_1264 |
| Westman, E.-L. | DESIGN OF A SUSTAINABLE FLEXFORMING PROCEDURE FOR AERO ENGINE COMPONENTS IS ALLOY 718 | ICAS2024_1194 |
| Wheatley, M. | ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD | ICAS2024_1280 |
| Wicke, K. | SUSTAINABLE ENGINE MAINTENANCE: EVALUATING THE ECOLOGICAL IMPACT OF LIFE LIMITED PART REPLACEMENT | ICAS2024_0452 |
| Wickramasinghe, N.K. | ESTIMATING THE IMPACT OF NUMERICAL WEATHER PREDICTION DATA MODELS ON SHORT-HAUL MINIMUM COST TRACKS | ICAS2024_0142 |
| Wieczorek, U. | MRO FOR VTOLS IN A FUNCTIONAL SEQUENCES SOLUTION SPACE | ICAS2024_0705 |
| Wild, J. | THE CRM-HL ECOSYSTEM - DLR CONTRIBUTIONS | ICAS2024_1214 |
| Wildermuth, S. | LIFE CYCLE ASSESSMENT OF ALTERNATIVE LAUNCH METHODS | ICAS2024_0545 |
| Wilke, H. | AILERON-FLAP-INTEGRATED ROLL CONTROL LAW BY OPTIMIZED CONTROL ALLOCATION FOR FLEXIBLE TRANSPORT AIRCRAFT | ICAS2024_0613 |
| Wille, E. | COMPARING THE CAPACITY OF DIFFERENT VERTIPORT TOPOLOGIES USING DISCRETE EVENT SIMULATION | ICAS2024_0155 |
| Williams, T.L. | DISTRIBUTED THRUST TAKEOFF FOR THE NASA X-57 MOD IV FLIGHT DEMONSTRATOR | ICAS2024_1290 |
| Willrodt, L. | AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS | ICAS2024_1139 |
| Wilson, G. | NUMERICAL INVESTIGATION OF PASSIVE AND ACTIVE ALLEVIATION OF DYNAMIC LOADS ON HIGH-ASPECT-RATIO-WING VEHICLES | ICAS2024_0740 |
| Winter, F. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Wise, A. | DUAL STAGE BATTERY SIZING AND PERFORMANCE ASSESSMENT ON-BOARD HYBRID ELECTRIC AIRCRAFT | ICAS2024_1072 |
| Wolleswinkel, R.E. | BATTERY PERFORMANCE METRICS FOR LARGE ELECTRIC PASSENGER AIRCRAFT | ICAS2024_0636 |
| Woo, C.J. | OPERATIONAL LIMITS ASSESSMENT FOR HIGH-ALTITUDE LONG-ENDURANCE UAVS CONSIDERING PROPELLER ICING EFFECT | ICAS2024_0507 |
| Wood, N. | A PERFORMANCE COMPARISON OF HYDROGEN AIRCRAFT CONCEPTS | ICAS2024_0251 |
| Woodrow, K.C. | WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES | ICAS2024_1137 |
| Woroniak, G. | ANALYSIS OF THE POSSIBILITY OF INCREASING THE THERMAL RESISTANCE OF EPOXY RESIN WITH CWNT AND MMT | ICAS2024_0275 |
| Worris, M. | WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES | ICAS2024_1137 |
| Woszidlo, R. | THE PATH TO TRANSITION ACTIVE FLOW CONTROL TECHNOLOGY | ICAS2024_1262 |
| Wu, B. | NUMERICAL SIMULATION OF THE RESPONSE CHARACTERISTICS OF THE WING STRUCTURE OF A SEAPLANE PLANING IN WAVE | ICAS2024_0901 |
| Wu, D. | AN EXPERIMENTAL SIMULATION ON THE INFLUENCE OF DIFFERENT FILM COOLING HOLE SHAPES ON PARTICLE DEPOSITION ON TURBINE VANE | ICAS2024_0341 |
| Wu, G. | SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT | ICAS2024_0925 |
| Wu, H. | THE RESISTANCE TO THE HIGH-VELOCITY IMPACT OF THE INTRA-LAYER HYBRID PLAIN WEAVE COMPOSITES | ICAS2024_0212 |
| Wu, H. | BOUNDARY-LAYER SUCTION AND AERODYNAMIC SHAPE OPTIMIZATION FOR HYBRID LAMINAR FLOW CONTROL ON A FIN | ICAS2024_0681 |
| Wu, H. | OPTIMIZING FLEET ASSIGNMENT DECISIONS FOR REGIONAL AIRLINES WITH HYBRID ELECTRIC AIRCRAFT UPTAKE | ICAS2024_0781 |
| Wu, J.M. | EFFECTS OF SHAPE AND STREAMWISE SPACING OF PIN-FINS ARRAYS ON FLOW AND HEAT TRANSFER | ICAS2024_0720 |
| Wu, L. | RESEARCH ON AIRSPEED CORRECTION TECHNOLOGY OF EJECTION SEAT BASED ON CFD | ICAS2024_0709 |
| Wu, N. | STUDY OF THE SCAVENGE PUMP PERFORMANCE FOR TWO-PHASE FLOW IN AN AIRCRAFT ENGINE LUBRICATION SYSTEM | ICAS2024_0788 |
| Wu, S. | NOVEL SOFTWARE-DRIVEN VARIABLE-PITCH AND LEVEL FLIGHT CONTROL SYSTEM: PRINCIPLES AND APPLICATIONS FOR SMALL AIRCRAFT WITH A QUADROTOR CASE STUDY | ICAS2024_0940 |
| Wu, Y. | STUDY OF DROPLET MOTION AND WATER FILM FLOW CHARACTERISTICS ON SUPERHYDROPHOBIC SURFACES UNDER AIRFLOW SHEARING | ICAS2024_0934 |
| Wu, Z. | REVIEW ON NONLINEAR AEROELASTIC ANALYSIS WITH FREEPLAY | ICAS2024_0922 |
| Wunderlich, T.F. | OPTIMAL WING ASPECT RATIO OF HIGHLY EFFICIENT LONG-RANGE AIRCRAFT | ICAS2024_1225 |
| Wykes, K. | DESIGN OF MEASUREMENT SETUP FOR HIGH-ALTITUDE IN-FLIGHT EXPERIMENTS ON DU89-134/14 AIRFOIL AT LOW REYNOLDS NUMBER | ICAS2024_0757 |
| Wöhler, S. | ESTABLISHING THE DLR-F25 AS A RESEARCH BASELINE AIRCRAFT FOR THE SHORT-MEDIUM RANGE MARKET IN 2035 | ICAS2024_0398 |
| Wöhler, S. | CLIMATE IMPACT AND ECONOMIC ASSESSMENT OF LIQUID HYDROGEN AND SYNTHETIC KEROSENE LONG-RANGE AIRCRAFT CONCEPTS | ICAS2024_0399 |
| Wöhler, S. | CONCEPTUAL AIRCRAFT DESIGN OF A RESEARCH BASELINE WITH DIRECT LIQUID HYDROGEN COMBUSTION | ICAS2024_0503 |
| Xi, X.-L. | IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM | ICAS2024_1186 |
| Xi, Y. | CROSSFLOW AND GÖRTLER INSTABILITIES IN HYPERSONIC BOUNDARY LAYERS | ICAS2024_0574 |
| Xi, Y. | STABILITY CHARACTERISTICS OF CROSSFLOW MODES IN HYPERSONIC BOUNDARY LAYER WITH EXPANSION CORNER | ICAS2024_0576 |
| Xiang, J.-W. | IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM | ICAS2024_1186 |
| Xiao, H. | EXPERIMENTAL AND NUMERICAL INVESTIGATION ON SEPARATION CHARACTERISTICS OF SERPENTINE CONVERGENT-DIVERGENT NOZZLE | ICAS2024_0920 |
| Xiao, J. | EXPERIMENTAL AND NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF A MARS ROTOR SYSTEM | ICAS2024_0790 |
| Xiao, Q. | AN IMPROVED END-TO-END STAR MAP RECOGNITION METHOD FOR AEROSPACE VEHICLE | ICAS2024_0697 |
| Xiao, S. | LARGE-SCALE STRUCTURAL DYNAMIC TOPOLOGY OPTIMIZATION DESIGN FOR AIRCRAFT VIBRATION REDUCTION UNDER RANDOM EXCITING RESPONSE | ICAS2024_0365 |
| Xiao, T. | NUMERICAL AND THEORETICAL INVESTIGATION OF HELICOPTER DITCHING WITH VARIOUS INITIAL VELOCITY AND PITCHING ANGLE | ICAS2024_0216 |
| Xiao, Y. | CONJUGATED HEAT TRANSFER SIMULATION OF BUOYANCY-INDUCED FLOW AND HEAT TRANSFER MECHANISMS IN A COMPRESSOR CAVITY | ICAS2024_0531 |
| Xie, J. | INVESTIGATION ON THE MECHANISM OF THERMAL CYCLING FAILURE IN C/SIC COATING COMPOSITE MATERIALS | ICAS2024_0796 |
| Xie, J.-W. | VOID FRACTION CALCULATION MODEL BASED ON TWO-PHASE FLOW PATTERNS IN THE SCAVENGE PIPE | ICAS2024_1010 |
| Xie, W.-T. | THE DESIGN FOR TESTABILITY OF CIVIL AIRCRAFT AVIONICS SYSTEMS | ICAS2024_0033 |
| Xing, C. | TECHNICAL RISK MANAGEMENT OF SYSTEM OF SYSTEMS BASED ON TECHNOLOGY READINESS ASSESSMENT | ICAS2024_0041 |
| Xing, K.-A. | EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN | ICAS2024_0962 |
| Xiong, X. | NOVEL SOFTWARE-DRIVEN VARIABLE-PITCH AND LEVEL FLIGHT CONTROL SYSTEM: PRINCIPLES AND APPLICATIONS FOR SMALL AIRCRAFT WITH A QUADROTOR CASE STUDY | ICAS2024_0940 |
| Xisto, C. | LESSONS LEARNED FROM PROJECT BASED TEACHING IN AEROSPACE AT CHALMERS | ICAS2024_0867 |
| Xisto, C. | MODELLING A HYDROGEN FUELLED COMPOSITE CYCLE AEROENGINE | ICAS2024_1103 |
| Xu, B. | SIMULATION STUDY ON AERODYNAMIC CHARACTERISTICS OF COMBINED LOW ASPECT RATIO UAV | ICAS2024_0449 |
| Xu, B.Z. | NUMERICAL STUDY ON ACOUSTIC RECEPTIVITY OF COMPRESSIBLE LAMINAR FLOW OVER A FLAT PLATE WITH MODIFIED SUPER-ELLIPSE LEADING EDGE | ICAS2024_0553 |
| Xu, C. | MECHANISM STUDY ON THE IMPACT OF PULSED JET AT THE BLADE TIP LEADING EDGE ON THE FLOW FIELD IN COMPRESSOR | ICAS2024_0849 |
| Xu, C.-Z. | A SEQUENTIAL LOCAL ENUMERATION-BASED IMPROVED LATIN HYPERCUBE SAMPLING METHOD FOR BALLISTIC CONSTRAINT DESIGN SPACE | ICAS2024_0618 |
| Xu, C.-Z. | EFFICIENT AEROSTRUCTURAL DESIGN OPTIMIZATION COMBINING GRADIENT-ENHANCED KRIGING WITH COUPLED ADJOINT METHOD | ICAS2024_0651 |
| Xu, D. | ATTITUDE ESTIMATION USING KALMAN FILTERING FOR SPACEBORNE SAR SYSTEMS | ICAS2024_0866 |
| Xu, H.-Y. | NUMERICAL INVESTIGATION OF THE FLOW FEATURES ON THE TURRET WITH DIFFERENT CYLINDER HEIGHT IN THE TRANSONIC FLOW | ICAS2024_0282 |
| Xu, H.-Y. | FAULT DIAGNOSIS AND TOLERANCE SYSTEM OF FLIGHT STATE PERCEPTION MODEL BASED ON MACHINE LEARNING FOR CO-FLOW JET AIRFOIL | ICAS2024_0662 |
| Xu, H.N. | WALL TEMPERATURE EFFECTS ON AERODYNAMIC HEATING MECHANISMS IN SHOCK WAVE TURBULENT BOUNDARY LAYER INTERACTION | ICAS2024_0569 |
| Xu, J. | RESEARCH ON TECHNOLOGICAL INNOVATION CAPABILITY EVALUATION INDEX FOR AVIATION INDUSTRIES | ICAS2024_0211 |
| Xu, J. | THERMAL AND MECHANICAL CYCLING OF THIN-PLY COMPOSITES FOR CRYOGENIC APPLICATIONS | ICAS2024_1052 |
| Xu, J.-H. | RESEARCH ON AERODYNAMIC DESIGN OF ENGINE NACELLE UNDER THE INFLUENCE OF PROPELLER SLIPSTREAM FOR THE TURBOPROP AIRCRAFT | ICAS2024_0605 |
| Xu, J.-H. | NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF HOVERING ROTOR IN GROUND EFFECT | ICAS2024_0655 |
| Xu, J.-H. | RESEARCH ON MULTI-OBJECTIVE AERODYNAMIC/STRUCTURAL DESIGN OPTIMIZATION METHOD FOR LARGE THICKNESS FLATBACK AIRFOILS | ICAS2024_0690 |
| Xu, J.H. | INVESTIGATION ON AERODYNAMIC DESIGN OF VTOL AIRCRAFT PROPELLER | ICAS2024_0643 |
| Xu, L. | NUMERICAL STUDY OF FLOWS OVER LAUNCH VEHICLES WITH VARIOUS FAIRING BY SECOND-MOMENT CLOSURE DETACHED-EDDY SIMULATION | ICAS2024_0641 |
| Xu, L. | DESIGN OF DUAL-FUSELAGE FLIGHT PLATFORM FOR JET CONTROL FUNCTION VERIFICATION | ICAS2024_0812 |
| Xu, P. | OPTIMIZATION DESIGN OF MULTI-SCALE ACTIVE COOLING STRUCTURE FOR AIRCRAFT | ICAS2024_0375 |
| Xu, R.-F. | RESEARCH ON AERODYNAMIC DESIGN OF ENGINE NACELLE UNDER THE INFLUENCE OF PROPELLER SLIPSTREAM FOR THE TURBOPROP AIRCRAFT | ICAS2024_0605 |
| Xu, S.-R. | TILT-DUCT AIRCRAFT WING AERODYNAMIC DESIGN AND OPTIMIZATION BASED ON ADJOINT METHOD | ICAS2024_0332 |
| Xu, S.-R. | OPTIMIZATION OF COMPOSITE WING STRUCTURE FOR TILT-DUCT AIRCRAFT CONSIDERING DISCRETE AND CONTINUOUS DESIGN VARIABLES | ICAS2024_0405 |
| Xu, T. | SENSITIVITY ANALYSIS OF SAFETY FACTORS BASED ON MODEL OF AVIATION RECIPROCATING ENGINE TURBOCHARGING SYSTEM | ICAS2024_0599 |
| Xu, T.-G. | A METHOD FOR AUTOMATIC GENERATING SAFETY ANALYSIS BASED ON AVIATION PISTON ENGINE MODEL | ICAS2024_0587 |
| Xu, X. | INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF WINGS UNDER ICING CONDITIONS AT VARIOUS SWEEP ANGLES | ICAS2024_0287 |
| Xu, X. | SIMULATION STUDY ON AERODYNAMIC CHARACTERISTICS OF COMBINED LOW ASPECT RATIO UAV | ICAS2024_0449 |
| Xu, Y. | EXPERIMENTAL STUDY ON MULTI-ATTITUDE OIL SUPPLY STRUCTURE | ICAS2024_0817 |
| Xu, Y. | LIGHT WEIGHT DESIGN AND LASER ADDITIVE MANUFACTURING OF METAL BIPOLAR PLATES FOR THE APPLICATION OF AIRCRAFT FUEL CELL | ICAS2024_0964 |
| Xu, Z. | LONG-WAVE INSTABILITY OF AIRCRAFT WAKE VORTEX UNDER SHEAR CROSSWIND | ICAS2024_0551 |
| Xu, Z. | AN IMPROVED END-TO-END STAR MAP RECOGNITION METHOD FOR AEROSPACE VEHICLE | ICAS2024_0697 |
| Xu, Z. | MULTI-DIMENTIONAL DESIGN AND THERMAL PROTECTION CAPABILITY OF A REGENERATIVE COOLED RBCC VARIABLE-GEOMETRY COMBUSTOR | ICAS2024_1012 |
| Xu, Z.-M. | ON THE INFLUENCE OF BASE FLOW CHARACTERISTICS ON CROSSFLOW INSTABILITY IN SWEPT BOUNDARY LAYERS | ICAS2024_0918 |
| Xuan, J. | DYNAMICS ANALYSIS AND CONTROL OF A LARGE WINGSPAN FLAPPING-WING VEHICLE | ICAS2024_0621 |
| Xuan, J.-L. | THE EFFECTS OF INITIAL STRESS ON AERODYNAMIC PERFORMANCE OF FLEXIBLE MEMBRANE-SKELETON WINGS WITH FSI SIMULATION | ICAS2024_0752 |
| Xuan, J.X. | ATTITUDE CONTROL DESIGN FOR A FLYING-CRAWLING INTEGRATED FLAPPING-WING MICRO AIR VEHICLE | ICAS2024_0478 |
| Xue, D. | RESEARCH ON OPTIMAL TORSIONAL DEFORMATION OF FLAPPING WING | ICAS2024_0473 |
| Xue, D. | THE EFFECTS OF INITIAL STRESS ON AERODYNAMIC PERFORMANCE OF FLEXIBLE MEMBRANE-SKELETON WINGS WITH FSI SIMULATION | ICAS2024_0752 |
| Xue, H.-M. | LARGE-SCALE STRUCTURAL DYNAMIC TOPOLOGY OPTIMIZATION DESIGN FOR AIRCRAFT VIBRATION REDUCTION UNDER RANDOM EXCITING RESPONSE | ICAS2024_0365 |
| Yahata, T. | DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY | ICAS2024_0325 |
| Yakimenko, O. | DIGITAL TWIN OF AN AIRCRAFT LANDING GEAR TO ENHANCE FAILURE ANALYSIS AND MANAGE PREDICTIVE MAINTENANCE | ICAS2024_0065 |
| Yamada, K. | MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM | ICAS2024_0573 |
| Yamaguchi, Y. | AIRCRAFT DX IN COMMERCIAL AVIATION SYSTEMS | ICAS2024_0856 |
| Yamamoto, K. | EFFICIENT THERMOMECHANICAL SIMULATION FOR METALLIC LATTICE STRUCTURES FABRICATED BY ADDITIVE MANUFACTURING | ICAS2024_0908 |
| Yamane, T. | JAXA EN-CORE PROJECT OVERVIEW AND ACHIEVEMENTS | ICAS2024_1265 |
| Yamashita, R. | NUMERICAL SIMULATION OF FLOWS AROUND AN AIRFOIL DURING ACCELERATED AND DECELERATED FLIGHT | ICAS2024_0034 |
| Yan, B. | DAMAGE AND MECHANICAL REPAIR OF COMPOSITE LAMINATES: EFFECTS OF EMBEDDED DEFECTS AND LOW VELOCITY IMPACTS | ICAS2024_0748 |
| Yan, C.-L. | ANALYSIS OF SUCTION FORCE EFFECT ON DIFFERENT FUSELAGE SHAPE DURING THE WATER DITCHING | ICAS2024_0929 |
| Yan, H. | NUMERICAL INVESTIGATION ON THE EFFECT OF REYNOLDS NUMBER ON TANDEM DROPLET | ICAS2024_0426 |
| Yan, J.-Q. | ENERGY PREDICTION DURING APPROACH AND LANDING BASED ON LONG SHORT-TERM MEMORY MODEL | ICAS2024_0890 |
| Yan, K. | THE IMPACT OF PIEZOELECTRIC STACK HEATING ON AIRCRAFT DEICING | ICAS2024_0279 |
| Yan, S. | THERMAL AND GRINDING PERFORMANCE OF 3D PRINTED COMPLIANCE GRINDING TOOLS WITH ROTARY-ENHANCED HEAT TRANSFER STRUCTURE | ICAS2024_0248 |
| Yanev, R.Y. | FRAMEWORK DEVELOPMENT FOR CONCEPTUAL DESIGN AND CONFIGURATION ANALYSIS OF EVTOL AIRCRAFT | ICAS2024_0557 |
| Yang, A. | DATA-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION AND MULTI-FIDELITY DESIGN EXPLORATION USING CONDITIONAL DIFFUSION-BASED GEOMETRY SAMPLING METHOD | ICAS2024_0431 |
| Yang, B.R. | A PHASE FIELD BASED DEEP LEARNING APPROACH FOR MECHANICAL PROPERTY PREDICTION OF SINTERED SILVER IN POWER ELECTRONICS | ICAS2024_0351 |
| Yang, C. | REVIEW ON NONLINEAR AEROELASTIC ANALYSIS WITH FREEPLAY | ICAS2024_0922 |
| Yang, G. | JET NOISE ABATEMENT VIA SURROGATE MODEL-BASED AEROACOUSTIC OPTIMISATION USING LARGE EDDY SIMULATION | ICAS2024_0583 |
| Yang, H.-H. | DEVELOPMENT OF A SERVO-DRIVEN FLAPPING-WING AIR VEHICLE WITH FOLDING-WING MECHANISM | ICAS2024_0477 |
| Yang, L. | AERODYNAMIC OPTIMIZATION OF HIGH-ALTITUDE PROPELLER COMBINED WITH MACHINE LEARNING METHOD | ICAS2024_0342 |
| Yang, L. | AERO-KINEMATIC OPTIMIZATION OF HIGH-LIFT DEVICES WITH DOWNWARD DEFLECTION OF SPOILER | ICAS2024_0639 |
| Yang, M. | LINEAR QUADRATIC PURSUIT AND EVASION DIFFERENTIAL GAME GUIDANCE STRATEGY WITH OBSTACLE AVOIDANCE | ICAS2024_0008 |
| Yang, R. | MODELING AND VALIDATION OF MORPHING WING TRAILING EDGE BASED ON ZERO POISSON'S RATIO HONEYCOMB | ICAS2024_1015 |
| Yang, S. | VIBRATION ANAYLYSIS AND INFLUENCING FACTOR STUTY OF HELICOPTER HYDRAULIC PIPELINNE | ICAS2024_0678 |
| Yang, S. | EXPLORING A CATEGORY OF LIMIT CYCLE OSCILLATIONS IN AIRCRAFT HYDRAULIC SYSTEMS | ICAS2024_0932 |
| Yang, W.-Q. | THE EFFECTS OF INITIAL STRESS ON AERODYNAMIC PERFORMANCE OF FLEXIBLE MEMBRANE-SKELETON WINGS WITH FSI SIMULATION | ICAS2024_0752 |
| Yang, W.Y. | ATTITUDE CONTROL DESIGN FOR A FLYING-CRAWLING INTEGRATED FLAPPING-WING MICRO AIR VEHICLE | ICAS2024_0478 |
| Yang, X. | NUMERICAL SIMULATION STUDY ON THE INFLUENCE OF WING SPACING OF DRAGONFLY-INSPIRED FLAPPING WINGS | ICAS2024_0243 |
| Yang, X. | KINETIC MONTE CARLO BASED CATALYTIC VISCOUS WALL BOUNDARY MODELING IN CFD SIMULATION OF HIGH-ENTHALPY NON-EQUILIBRIUM FLOW | ICAS2024_0276 |
| Yang, X. | DESIGN OF ATTITUDE CONTROL SYSTEM FOR DRAGONFLY-INSPIRED FLAPPING WING AERIAL VEHICLE | ICAS2024_0578 |
| Yang, X. | ANALYSIS OF BATTERY WEIGHT REQUIREMENTS IN THE DESIGN OF HYBRID ELECTRIC POWERED AIRCRAFT | ICAS2024_0813 |
| Yang, X.W. | FLUID-STRUCTURE INTERACTION OF TWO-PHASE SCATTERER METAMATERIALS FOR VIBRATION SELF-SUPPRESSION | ICAS2024_0435 |
| Yang, Y. | AN IMPROVED END-TO-END STAR MAP RECOGNITION METHOD FOR AEROSPACE VEHICLE | ICAS2024_0697 |
| Yang, Y. | MECHANISM STUDY ON THE IMPACT OF PULSED JET AT THE BLADE TIP LEADING EDGE ON THE FLOW FIELD IN COMPRESSOR | ICAS2024_0849 |
| Yang, Y.J. | AIRFOIL PRESSURE PREDICTION BASED ON PHYSICS-INFORMED DEEP LEARNING APPROACH | ICAS2024_1036 |
| Yang, Z. | DESIGN OF A BODY FREEDOM FLUTTER FLIGHT MODEL WITH CONVENTIONAL CONFIGURATION | ICAS2024_0565 |
| Yao, J. | RESEARCH ON UNMANNED CLUSTER RECONNECTION DECISION-MAKING METHOD CONSIDERING RESOURCE SUPPLEMENTATION | ICAS2024_0343 |
| Yao, J. | A PHASE FIELD BASED DEEP LEARNING APPROACH FOR MECHANICAL PROPERTY PREDICTION OF SINTERED SILVER IN POWER ELECTRONICS | ICAS2024_0351 |
| Yao, J. | CLASSIFICATION OF COGNITIVE LOAD BASED ON THE PILOT’ VISUAL SCAN PATTERNS | ICAS2024_0955 |
| Yao, M. | RESEARCH ON UNMANNED CLUSTER RECONNECTION DECISION-MAKING METHOD CONSIDERING RESOURCE SUPPLEMENTATION | ICAS2024_0343 |
| Yao, Z.X. | INNOVATIVE UAVS WITH CONFIGURATION OF LIKING BOTH PLANE AND KITE FOR WIND POWER | ICAS2024_0284 |
| Yasuda, A. | FEASIBILITY STUDY ON OPERATIONAL FLIGHT PLANS ADAPTED FOR TRAJECTORY BASED OPERATION | ICAS2024_1177 |
| Yasuda, H. | TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2024_1215 |
| Yawata, M. | DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY | ICAS2024_0325 |
| Ye, N.-H. | SURROGATE-ASSISTED HIERARCHICAL OPTIMIZATION METHOD FOR VARIABLE SWEEP FLIGHT VEHICLE TRAJECTORY | ICAS2024_0825 |
| Ye, Z. | INTELLIGENT RECONSTRUCTION METHOD OF AIRFOIL FLOW FIELD BASED ON DEEP ATTENTION NETWORK | ICAS2024_0852 |
| Yee, K.J. | OPERATIONAL LIMITS ASSESSMENT FOR HIGH-ALTITUDE LONG-ENDURANCE UAVS CONSIDERING PROPELLER ICING EFFECT | ICAS2024_0507 |
| Yeoh, S. | DUAL STAGE BATTERY SIZING AND PERFORMANCE ASSESSMENT ON-BOARD HYBRID ELECTRIC AIRCRAFT | ICAS2024_1072 |
| Yildirim, A. | AERODYNAMIC SHAPE OPTIMIZATION OF FILLETED INTERSECTIONS WITH SURFACE MESH DEFORMATION | ICAS2024_0227 |
| Yildirim, A. | SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION | ICAS2024_0465 |
| Yildirim, A. | ROBUST SCHUR-COMPLEMENT SOLVERS AND LARGE-SCALE MULTIDISCIPLINARY DESIGN OPTIMIZATION | ICAS2024_0687 |
| Yin, F. | HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION | ICAS2024_0161 |
| Yin, Q. | ANGLE AND DISTANCE EFFECT ON PHOSPHOR THERMOMETRY | ICAS2024_0529 |
| Yin, Y.-L. | FAST PARAMETRIC STRUCTURE MODELING FOR VARIETY OF AIRCRAFT CONFIGURATIONS | ICAS2024_0614 |
| Ying, S. | A CALL TO ACTION TO ENGAGE THE COMMUNITY TO MEET THE CHALLENGES THAT MUST BE TACKLED TO MAKE ELECTRIFIED AIRCRAFT PROPULSION REAL | ICAS2024_0834 |
| Yokoyama, N. | DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY | ICAS2024_0325 |
| Yokoyama, Y. | EVALUATING INSTALLATION EFFECTS IN SEMI-SPAN WIND TUNNEL EXPERIMENTS USING CARTESIAN-GRID-BASED FLOW SOLVER UTCART | ICAS2024_0293 |
| Yondo Mine, R. | MICKEY MOUSE AND A GIANT: COMPARISON OF AERONAUTICS EDUCATION IN FINLAND AND CHINA | ICAS2024_1263 |
| Yoshida, H. | DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY | ICAS2024_0325 |
| Yoshida, M. | A FAST INFORMATION THEORETICALLY SECURE RADIO COMMUNICATION PROTOCOL BASED ON GNSS POSITIONING | ICAS2024_0559 |
| Yoshikawa, N. | PAIRWISE SWAPPING SEQUENCE OPTIMIZATION BY METROPOLIS-HASTING ALGORITHM WITH QUANTUM ANNEALING FOR AIR TRAFFIC CONTROL | ICAS2024_0763 |
| Youhanna, V. | PRELIMINARY DESIGN EXPLORATION OF PROSPECTIVE MULTIROTOR AEROBOTS FOR MARS | ICAS2024_0536 |
| Young, R. | NASA HI-RATE COMPOSITE AIRCRAFT MANUFACTURING (HICAM) PROJECT OVERVIEW | ICAS2024_1237 |
| Yu, J. | FLOW CHARACTERISTICS OF THE INLET IN TURBOPROP ENGINE WITH THE INFLUENCE OF SANDS | ICAS2024_0143 |
| Yu, L. | STUDY OF DROPLET MOTION AND WATER FILM FLOW CHARACTERISTICS ON SUPERHYDROPHOBIC SURFACES UNDER AIRFLOW SHEARING | ICAS2024_0934 |
| Yu, S. | AERODYNAMIC PERFORMANCE OF BLADELESS DUCTED FAN BASED ON EJECTION EFFECT WITH DIFFERENT DESIGN VARIABLES | ICAS2024_0419 |
| Yu, S. | EFFECT OF FREESTREAM DISTURBANCES ON BOUNDARY LAYER TRANSITION IN HYPERSONIC WIND TUNNEL | ICAS2024_0540 |
| Yu, T. | MODELING AND ANALYSIS OF ELECTRO-HYDROSTATIC ACTUATORS EFFICIENCY | ICAS2024_1043 |
| Yu, Z. | ROTOR DYNAMIC LOADS CHARACTERISTIC ANALYSIS WITH BLADE TIP TWIST DISTRIBUTION | ICAS2024_0418 |
| Yuan, B. | MULTI SENSOR AND MULTI TASK ALLOCATION BASED ON IMPROVED WHALE OPTIMIZATION ALGORITHM | ICAS2024_1028 |
| Yuan, J. | EFFECT OF FREESTREAM DISTURBANCES ON BOUNDARY LAYER TRANSITION IN HYPERSONIC WIND TUNNEL | ICAS2024_0540 |
| Yuan, L. | THE IMPACT OF PIEZOELECTRIC STACK HEATING ON AIRCRAFT DEICING | ICAS2024_0279 |
| Yuan, W.H. | FLUID-STRUCTURE INTERACTION OF TWO-PHASE SCATTERER METAMATERIALS FOR VIBRATION SELF-SUPPRESSION | ICAS2024_0435 |
| Yuan, X. | INTELLIGENT RECONSTRUCTION METHOD OF AIRFOIL FLOW FIELD BASED ON DEEP ATTENTION NETWORK | ICAS2024_0852 |
| Yuan, Z. | DYNAMIC AND STABILITY ANALYSES OF ROTATING THIN-WALLED FILAMENT WOUND GLASS FIBRE COMPOSITE CYLINDERS WITH METAL LINER | ICAS2024_0296 |
| Yuan, Z.Y. | ATTITUDE CONTROL DESIGN FOR A FLYING-CRAWLING INTEGRATED FLAPPING-WING MICRO AIR VEHICLE | ICAS2024_0478 |
| Yue, N. | STUDY ON THE BALLISTIC-RESISTANT AIRWORTHINESS STANDARDS FOR COMMERCIAL AIRCRAFT COCKPIT DOOR | ICAS2024_0074 |
| Yue, Y. | HIGH-VELOCITY DROPLET IMPACT STUDIES ON C/SIC AND C/C COMPOSITES | ICAS2024_0808 |
| Yumusak, M. | NUMERICAL INVESTIGATION OF HYPERSONIC FLOWS | ICAS2024_0907 |
| Yun, G.J. | MICROMECHANICAL MODELING OF THE VISCOELASTIC-VISCOPLASTIC RESPONSE OF FIBER-REINFORCED COMPOSITES | ICAS2024_0213 |
| Yun, S.-H. | DATA-DRIVEN MODEL DISCOVERY AND CONTROL OF HIGH-PERFORMANCE TRAINER AIRCRAFT VIA SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS | ICAS2024_0627 |
| Yunus, F. | OPTIMAL APPROACH AND DEPARTURE TRAJECTORIES WITH ACOUSTIC FOOTPRINT ASSESSMENT FOR AN AIR MOBILITY QUAD-ROTOR | ICAS2024_1115 |
| Yury, Z. | ROBUST SLIDING MODE CONTROL FOR UAV FORMATION WITH EXTERNAL DISTURBANCES UNDER EVENT-TRIGGERED STRATEGY | ICAS2024_0013 |
| Ywet, N.L. | ENHANCED AIRCRAFT TAKEOFF/LANDING SAFETY USING DEEP LEARNING MODEL IN RUNWAY ASSISTANCE SYSTEM | ICAS2024_0786 |
| Yüksel, M.-N. | NUMERICAL INVESTIGATION OF HYPERSONIC FLOWS | ICAS2024_0907 |
| Zahorski, T. | EFFECT OF INFILL STYLE AND DENSITY ON SELECTED MECHANICAL PROPERTIES OF THE CARBON FIBRE REINFORCED ABS MFD FILAMENT | ICAS2024_0806 |
| Zaidi, T. | REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS | ICAS2024_1172 |
| Zalewski, P. | STUDY ON CONFIGURATIONS OF AIRBORNE LAUNCH SYSTEM FOR DELIVERY OF SMALL PAYLOAD TO LOW EARTH ORBIT | ICAS2024_0355 |
| Zammit, B. | A GENETIC ALGORITHM FOR TRAJECTORY GENERATION IN ENGINE-OUT EMERGENCY LANDING SCENARIOS OF COMMERCIAL AIRCRAFT | ICAS2024_0364 |
| Zammit-Mangion, D. | ENHANCED SAFETY THROUGH AI: AN ASSESSMENT OF ADVERSARIAL REINFORCEMENT LEARNING FOR CONTROL OF COMPLEX AIRCRAFT | ICAS2024_0440 |
| Zanoni, A. | SIMPLIFIED MODELS OF PILOT BIOMECHANICS FOR ROTORCRAFT VERTICAL BOUNCE ANALYSIS | ICAS2024_0520 |
| Zanotti, A. | UNCERTAINTY ANALYSIS OF THE AERODYNAMIC PERFORMANCE OF EVTOL PROPELLERS VIA REYNOLDS STRESS TENSOR PERTURBATION | ICAS2024_1197 |
| Zaporozhets, O. | DUAL-STREAM JET NOISE TEST WITH INTERNAL MIXER DESIGN VARIATIONS FOR LTO NOISE OF SUPERSONIC AIRCRAFT | ICAS2024_0064 |
| Zaporozhets, O. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Zaporozhets, O. | SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL | ICAS2024_0975 |
| Zappino, E. | NUMERICAL ANALYSIS OF PROCESS-INDUCED DEFORMATIONS AND STRESSES IN AERONAUTICAL COMPOSITE COMPONENTS | ICAS2024_0818 |
| Zappino, E. | HIGHER-ORDER 1D STICK MODELS FOR THE FLUTTER ANALYSIS OF AIRCRAFT STRUCTURES | ICAS2024_1001 |
| Zazzaro, G. | A SUPPORTING FRAMEWORK FOR AIRCRAFT MRO OPERATIONS. CAPACITY PLANNING, TASKS TRACEABILITY AND DISEMBARKED ITEMS TRACKING | ICAS2024_0100 |
| Zeitz, D. | THERMODYNAMIC DESIGN AND EMISSIONS MODEL OF A MACH 1.8 SUPERSONIC AIRLINER ENGINE | ICAS2024_0129 |
| Zeng, H. | A SEQUENTIAL LOCAL ENUMERATION-BASED IMPROVED LATIN HYPERCUBE SAMPLING METHOD FOR BALLISTIC CONSTRAINT DESIGN SPACE | ICAS2024_0618 |
| Zeng, L. | DEEP LEARNING BASED FAST PREDICTION OF AERODYNAMIC PARAMETERS FOR DUCTED PROPELLERS | ICAS2024_1011 |
| Zeng, Y. | TIME-BASED CONTROL TO REDUCE TRAJECTORY COMPLEXITY IN THE FLOW-CENTRIC AIR TRAFFIC CONTROL PARADIGM | ICAS2024_0966 |
| Zengerling, Z.L. | MITIGATING THE CLIMATE IMPACT OF AVIATION BY OPERATIONAL MEANS - A COMPARATIVE STUDY FOR DIFFERENT WEATHER SITUATIONS | ICAS2024_0096 |
| Zenkner, S. | LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT | ICAS2024_0121 |
| Zenkner, S. | THERMODYNAMIC DESIGN AND EMISSIONS MODEL OF A MACH 1.8 SUPERSONIC AIRLINER ENGINE | ICAS2024_0129 |
| Zha, X. | INVESTIGATION ON THE MECHANISM OF THERMAL CYCLING FAILURE IN C/SIC COATING COMPOSITE MATERIALS | ICAS2024_0796 |
| Zhai, C. | DYNAMICS ANALYSIS AND CONTROL OF A LARGE WINGSPAN FLAPPING-WING VEHICLE | ICAS2024_0621 |
| Zhan, H. | FLOW CHARACTERISTICS OF THE INLET IN TURBOPROP ENGINE WITH THE INFLUENCE OF SANDS | ICAS2024_0143 |
| Zhan, H. | INVESTIGATION ON INFLUENCE PARAMETER OF AIRCRAFT-MISSILE SEPARATION BY CONSIDERING AEROELASTICITY | ICAS2024_0445 |
| Zhan, H. | ANALYSIS AND STUDY ON FLUTTER CHARACTERISTICS OF WINGS UNDER TYPICAL FRAGMENT DAMAGE | ICAS2024_0446 |
| Zhan, H. | FAULT DIAGNOSIS AND TOLERANCE SYSTEM OF FLIGHT STATE PERCEPTION MODEL BASED ON MACHINE LEARNING FOR CO-FLOW JET AIRFOIL | ICAS2024_0662 |
| Zhang, B. | SURFACE MORPHOLOGY AND MICROSTRUCTURAL FEATURES OF ELECTRON BEAM SURFI-SCULPTED TI-6AL-4V ALLOY | ICAS2024_0262 |
| Zhang, C. | STUDY ON LOW-VELOCITY IMPACT BEHAVIOR AND RESIDUAL PERFORMANCE PREDICTION OF CFRP T-JOINTS | ICAS2024_0045 |
| Zhang, C. | THE RESISTANCE TO THE HIGH-VELOCITY IMPACT OF THE INTRA-LAYER HYBRID PLAIN WEAVE COMPOSITES | ICAS2024_0212 |
| Zhang, C. | MICROMECHANICAL MODELING OF THE VISCOELASTIC-VISCOPLASTIC RESPONSE OF FIBER-REINFORCED COMPOSITES | ICAS2024_0213 |
| Zhang, C. | MODELING THE TEMPERATURE-RISE BEHAVIOR OF 2D TRIAXIAL BRAIDED COMPOSITES UNDER IMPACT LOADS | ICAS2024_0215 |
| Zhang, C. | THE EFFECT OF TARGET THICKNESS ON THE BALLISTIC BEHAVIOR OF HYBRID CFRP/KFRP COMPOSITES | ICAS2024_0225 |
| Zhang, C. | A MESO-SCALED SIMULATION ON THE THICKNESS EFFECT OF TWO-DIMENSIONAL TRIAXIALLY BRAIDED COMPOSITES UNDER TENSILE LOADS | ICAS2024_0259 |
| Zhang, C. | DYNAMIC AND STABILITY ANALYSES OF ROTATING THIN-WALLED FILAMENT WOUND GLASS FIBRE COMPOSITE CYLINDERS WITH METAL LINER | ICAS2024_0296 |
| Zhang, C. | A DYNAMIC TEST METHODOLOGY FOR DETERMINING THE LONGITUDINAL COMPRESSIVE RESPONSE OF CARBON FIBER COMPOSITE TOWS | ICAS2024_0584 |
| Zhang, C. | HIGH TEMPERATURE BALLISTIC IMPACT TEST TECHNOLOGY BASED ON ELECTROMAGNETIC LAUNCH | ICAS2024_0841 |
| Zhang, C. | MECHANISM STUDY ON THE IMPACT OF PULSED JET AT THE BLADE TIP LEADING EDGE ON THE FLOW FIELD IN COMPRESSOR | ICAS2024_0849 |
| Zhang, C. | TRAJECTORY DESIGN FOR ASTEROID SAMPLE RETURN COMBINING BALLISTIC CAPTURE AND AEROBRAKING | ICAS2024_1070 |
| Zhang, D. | HAWK-INSPIRED COOPERATIVE ENCIRCLEMENT GUIDANCE OF FIXED-WING UAV SWARM WITH LIMITED COMMUNICATION IN THREAT SCENARIO | ICAS2024_0084 |
| Zhang, G. | NUMERICAL SIMULATION OF HEAT TRANSFER IN MINIATURE RADIALLY ROTATING SODIUM/POTASSIUM HEAT PIPES | ICAS2024_0323 |
| Zhang, G. | DAMAGE AND MECHANICAL REPAIR OF COMPOSITE LAMINATES: EFFECTS OF EMBEDDED DEFECTS AND LOW VELOCITY IMPACTS | ICAS2024_0748 |
| Zhang, G. | DESIGN OF DUAL-FUSELAGE FLIGHT PLATFORM FOR JET CONTROL FUNCTION VERIFICATION | ICAS2024_0812 |
| Zhang, G. | SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT | ICAS2024_0925 |
| Zhang, H. | RESEARCH ON TECHNOLOGICAL INNOVATION CAPABILITY EVALUATION INDEX FOR AVIATION INDUSTRIES | ICAS2024_0211 |
| Zhang, H. | DAMAGE AND MECHANICAL REPAIR OF COMPOSITE LAMINATES: EFFECTS OF EMBEDDED DEFECTS AND LOW VELOCITY IMPACTS | ICAS2024_0748 |
| Zhang, H. | MECHANISM STUDY ON THE IMPACT OF PULSED JET AT THE BLADE TIP LEADING EDGE ON THE FLOW FIELD IN COMPRESSOR | ICAS2024_0849 |
| Zhang, H. | ATTITUDE ESTIMATION USING KALMAN FILTERING FOR SPACEBORNE SAR SYSTEMS | ICAS2024_0866 |
| Zhang, H. | SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT | ICAS2024_0925 |
| Zhang, J. | APPLICATION OF NATURAL LANGUAGE PROCESSING FOR AIRCRAFT DEFECT TRACKING IN MAINTENANCE OPERATIONS | ICAS2024_0083 |
| Zhang, J. | RESEARCH ON UNSTEADY AERODYNAMIC MODELING METHOD OF PREPOSITIVE WING - MAIN WING COMPOSITE SYSTEM AT HIGH ATTACK ANGLE | ICAS2024_0239 |
| Zhang, J. | A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION | ICAS2024_0314 |
| Zhang, J. | DATA-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION AND MULTI-FIDELITY DESIGN EXPLORATION USING CONDITIONAL DIFFUSION-BASED GEOMETRY SAMPLING METHOD | ICAS2024_0431 |
| Zhang, J. | LOW ENERGY CONSUMPTION DESIGN METHOD AND STRATEGY FOR HIGH-ALTITUDE PROPELLERS BASED ON FLIGHT PROFILE | ICAS2024_0865 |
| Zhang, J.-F. | OPTIMIZATION OF COMPOSITE WING STRUCTURE FOR TILT-DUCT AIRCRAFT CONSIDERING DISCRETE AND CONTINUOUS DESIGN VARIABLES | ICAS2024_0405 |
| Zhang, J.-H. | REDUCED ORDER MODELLING OF UNSTEADY AERODYNAMICS FOR GROUND FLUTTER TEST SYSTEM | ICAS2024_0430 |
| Zhang, K. | AN UAV MANEUVERING DECISION-MAKING ALGORITHM BASED ON DEEP TRANSFER REINFORCEMENT LEARNING | ICAS2024_1020 |
| Zhang, K. | MULTI SENSOR AND MULTI TASK ALLOCATION BASED ON IMPROVED WHALE OPTIMIZATION ALGORITHM | ICAS2024_1028 |
| Zhang, K.-S. | EFFICIENT MULTI-OBJECTIVE DESIGN OPTIMIZATION OF ROTOR AIRFOILS FOR IMPROVING DYNAMIC STALL CHARACTERISTICS | ICAS2024_0420 |
| Zhang, K.-S. | AERODYNAMIC DESIGN OF A SUPERSONIC TRANSPORT CONFIGURATION CONSIDERING AVERAGE LOUDNESS IN THE WHOLE BOOM CARPET | ICAS2024_0597 |
| Zhang, K.-S. | FAST PARAMETRIC STRUCTURE MODELING FOR VARIETY OF AIRCRAFT CONFIGURATIONS | ICAS2024_0614 |
| Zhang, K.-S. | EXPLORATION OF EFFICIENT HYPERPARAMETERS ADAPTION OF SUPPORT VECTOR REGRESSION FOR AERODYNAMIC DESIGN | ICAS2024_0625 |
| Zhang, K.-S. | EFFICIENT AEROSTRUCTURAL DESIGN OPTIMIZATION COMBINING GRADIENT-ENHANCED KRIGING WITH COUPLED ADJOINT METHOD | ICAS2024_0651 |
| Zhang, K.F. | THERMAL AND GRINDING PERFORMANCE OF 3D PRINTED COMPLIANCE GRINDING TOOLS WITH ROTARY-ENHANCED HEAT TRANSFER STRUCTURE | ICAS2024_0248 |
| Zhang, L. | ANGLE AND DISTANCE EFFECT ON PHOSPHOR THERMOMETRY | ICAS2024_0529 |
| Zhang, L. | MULTI-DIMENTIONAL DESIGN AND THERMAL PROTECTION CAPABILITY OF A REGENERATIVE COOLED RBCC VARIABLE-GEOMETRY COMBUSTOR | ICAS2024_1012 |
| Zhang, M. | INVESTIGATION ON INFLUENCE PARAMETER OF AIRCRAFT-MISSILE SEPARATION BY CONSIDERING AEROELASTICITY | ICAS2024_0445 |
| Zhang, M. | ANALYSIS AND STUDY ON FLUTTER CHARACTERISTICS OF WINGS UNDER TYPICAL FRAGMENT DAMAGE | ICAS2024_0446 |
| Zhang, M. | LOW ENERGY CONSUMPTION DESIGN METHOD AND STRATEGY FOR HIGH-ALTITUDE PROPELLERS BASED ON FLIGHT PROFILE | ICAS2024_0865 |
| Zhang, M.-X. | MODELING AND FLIGHT CONTROL LAW DESIGN FOR A SEAPLANE DURING WATER SURFACE TAKEOFF | ICAS2024_0977 |
| Zhang, Q. | A HYBRID APPROACH FOR RECONSTRUCTION OF TRANSONIC BUFFET AERODYNAMIC NOISE: INTEGRATING RANDOM FOREST AND COMPRESSIVE SENSING ALGORITHM | ICAS2024_0857 |
| Zhang, S. | MULTI SENSOR AND MULTI TASK ALLOCATION BASED ON IMPROVED WHALE OPTIMIZATION ALGORITHM | ICAS2024_1028 |
| Zhang, S. | A STUDY ON THE AIRLOCK MECHANISM OF THE OIL SUPPLY PUMP IN AERO-ENGINE LUBRICATING OIL SYSTEM | ICAS2024_1030 |
| Zhang, S.-Q. | RESEARCH ON MULTI-OBJECTIVE AERODYNAMIC/STRUCTURAL DESIGN OPTIMIZATION METHOD FOR LARGE THICKNESS FLATBACK AIRFOILS | ICAS2024_0690 |
| Zhang, T. | AERO-KINEMATIC OPTIMIZATION OF HIGH-LIFT DEVICES WITH DOWNWARD DEFLECTION OF SPOILER | ICAS2024_0639 |
| Zhang, T. | TRAJECTORY DESIGN FOR ASTEROID SAMPLE RETURN COMBINING BALLISTIC CAPTURE AND AEROBRAKING | ICAS2024_1070 |
| Zhang, T. | REENTRY TRAJECTORY DESIGN FOR DEFORMABLE HYPERSONIC VEHICLES BASED ON NEURAL NETWORKS | ICAS2024_1087 |
| Zhang, W. | FAST PREDICTION OF PRESSURE DISTRIBUTION FOR 3D CONFIGURATION BASED ON LARGE LANGRAGE MODEL | ICAS2024_0679 |
| Zhang, W. | INTELLIGENT RECONSTRUCTION METHOD OF AIRFOIL FLOW FIELD BASED ON DEEP ATTENTION NETWORK | ICAS2024_0852 |
| Zhang, W. | A HYBRID APPROACH FOR RECONSTRUCTION OF TRANSONIC BUFFET AERODYNAMIC NOISE: INTEGRATING RANDOM FOREST AND COMPRESSIVE SENSING ALGORITHM | ICAS2024_0857 |
| Zhang, W. | EFFICIENT MULTI-FIDELITY REDUCED-ORDER MODELING FOR FLUTTER PREDICTIONS ACROSS MULTIPLE MACH NUMBERS | ICAS2024_0900 |
| Zhang, W. | CORRELATION MODELLING OF SURFACE INVISCID FLOW CHARACTERISTICS AND FRICTION DISTRIBUTION BASED ON MACHINE LEARNING | ICAS2024_0958 |
| Zhang, W. | DYNAMIC STALL PREDICTION THROUGH COMBINING PHYSICAL MODELS AND MACHINE LEARNING | ICAS2024_1080 |
| Zhang, W. | TRANSFER LEARNING FOR REDUCED-ORDER MODELING OF TRANSONIC FLOWS USING MULTIFIDELITY DATA | ICAS2024_1110 |
| Zhang, W.-N. | OPTIMIZATION DESIGN OF MULTI-SCALE ACTIVE COOLING STRUCTURE FOR AIRCRAFT | ICAS2024_0375 |
| Zhang, W.L. | LIGHT WEIGHT DESIGN AND LASER ADDITIVE MANUFACTURING OF METAL BIPOLAR PLATES FOR THE APPLICATION OF AIRCRAFT FUEL CELL | ICAS2024_0964 |
| Zhang, W.W. | ACTIVE-PASSIVE HYBRID CONTROL OF SHOCK BUFFET | ICAS2024_0792 |
| Zhang, X. | TRANSFORMATIVE PEDAGOGY: CO-TEACHING COURSE CLUSTERS THROUGH COMPETITIVE TEAM DESIGNS FOR INNOVATIVE TALENT DEVELOPMENT IN AEROSPACE EDUCATION | ICAS2024_0324 |
| Zhang, X.-B. | AERODYNAMIC DEFORMATION EXPERIMENT OF SERPENTINE NOZZLE FOR TURBOFAN AND ANALYSIS OF FLUID-STRUCTURE INTERACTION METHOD | ICAS2024_0919 |
| Zhang, Y. | STUDY ON THE BALLISTIC-RESISTANT AIRWORTHINESS STANDARDS FOR COMMERCIAL AIRCRAFT COCKPIT DOOR | ICAS2024_0074 |
| Zhang, Y. | INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF WINGS UNDER ICING CONDITIONS AT VARIOUS SWEEP ANGLES | ICAS2024_0287 |
| Zhang, Y. | NUMERICAL SIMULATION OF HEAT TRANSFER IN MINIATURE RADIALLY ROTATING SODIUM/POTASSIUM HEAT PIPES | ICAS2024_0323 |
| Zhang, Y. | AN EXPERIMENTAL SIMULATION ON THE INFLUENCE OF DIFFERENT FILM COOLING HOLE SHAPES ON PARTICLE DEPOSITION ON TURBINE VANE | ICAS2024_0341 |
| Zhang, Y. | FATIGUE CRACK LIFE PREDICTION BASED ON BAYESIAN DYNAMIC UPDATE | ICAS2024_0393 |
| Zhang, Y. | STUDY ON FATIGUE PROPERTIES OF TITANIUM ALLOY BASE MATERIAL AND WELDED STRUCTURE IN THERMAL COMBINED ENVIRONMENT | ICAS2024_0422 |
| Zhang, Y. | INVESTIGATION ON INFLUENCE PARAMETER OF AIRCRAFT-MISSILE SEPARATION BY CONSIDERING AEROELASTICITY | ICAS2024_0445 |
| Zhang, Y. | ANALYSIS AND STUDY ON FLUTTER CHARACTERISTICS OF WINGS UNDER TYPICAL FRAGMENT DAMAGE | ICAS2024_0446 |
| Zhang, Y. | SENSITIVITY ANALYSIS OF SAFETY FACTORS BASED ON MODEL OF AVIATION RECIPROCATING ENGINE TURBOCHARGING SYSTEM | ICAS2024_0599 |
| Zhang, Y. | A SEQUENTIAL LOCAL ENUMERATION-BASED IMPROVED LATIN HYPERCUBE SAMPLING METHOD FOR BALLISTIC CONSTRAINT DESIGN SPACE | ICAS2024_0618 |
| Zhang, Y. | AN IMPROVED END-TO-END STAR MAP RECOGNITION METHOD FOR AEROSPACE VEHICLE | ICAS2024_0697 |
| Zhang, Y. | DESIGN OF DUAL-FUSELAGE FLIGHT PLATFORM FOR JET CONTROL FUNCTION VERIFICATION | ICAS2024_0812 |
| Zhang, Y. | IMPACT RESPONSES AND FAILURE MECHANISMS OF ALMGB14 UNDER DYNAMIC LOADS | ICAS2024_1006 |
| Zhang, Y. | MICKEY MOUSE AND A GIANT: COMPARISON OF AERONAUTICS EDUCATION IN FINLAND AND CHINA | ICAS2024_1263 |
| Zhang, Y.-J. | RESEARCH ON AERODYNAMIC DESIGN OF ENGINE NACELLE UNDER THE INFLUENCE OF PROPELLER SLIPSTREAM FOR THE TURBOPROP AIRCRAFT | ICAS2024_0605 |
| Zhang, Y.-T. | TILT-DUCT AIRCRAFT WING AERODYNAMIC DESIGN AND OPTIMIZATION BASED ON ADJOINT METHOD | ICAS2024_0332 |
| Zhang, Y.-T. | OPTIMIZATION OF COMPOSITE WING STRUCTURE FOR TILT-DUCT AIRCRAFT CONSIDERING DISCRETE AND CONTINUOUS DESIGN VARIABLES | ICAS2024_0405 |
| Zhang, Y.F. | AIRFOIL PRESSURE PREDICTION BASED ON PHYSICS-INFORMED DEEP LEARNING APPROACH | ICAS2024_1036 |
| Zhang, Z. | STUDY ON THE BALLISTIC-RESISTANT AIRWORTHINESS STANDARDS FOR COMMERCIAL AIRCRAFT COCKPIT DOOR | ICAS2024_0074 |
| Zhang, Z. | LOW ENERGY CONSUMPTION DESIGN METHOD AND STRATEGY FOR HIGH-ALTITUDE PROPELLERS BASED ON FLIGHT PROFILE | ICAS2024_0865 |
| Zhang, Z. | IMPACT RESPONSES AND FAILURE MECHANISMS OF ALMGB14 UNDER DYNAMIC LOADS | ICAS2024_1006 |
| Zhao, G. | MEASUREMENT OF WING BENDING IN-FLIGHT FROM A T67 SLINGSBY FIREFLY LIGHT AIRCRAFT | ICAS2024_0140 |
| Zhao, H. | NOVEL GRADIENT-ENHANCED MULTI-FIDELITY SURROGATE MODEL ASSISTED ROBUST MULTIDISCIPLINARY DESIGN OPTIMIZATION OF TAILLESS FLYING WING | ICAS2024_0298 |
| Zhao, H. | SPARSE POLYNOMIAL CHAOS-BASED SONIC BOOM UNCERTAINTY QUANTIFICATION AND AERODYNAMIC/SONIC BOOM ROBUST DESIGN OPTIMIZATION UNDER MULTI-PARAMETER UNCERTAINTIES | ICAS2024_0373 |
| Zhao, H. | FAST PREDICTION OF PRESSURE DISTRIBUTION FOR 3D CONFIGURATION BASED ON LARGE LANGRAGE MODEL | ICAS2024_0679 |
| Zhao, H. | STUDY OF DROPLET MOTION AND WATER FILM FLOW CHARACTERISTICS ON SUPERHYDROPHOBIC SURFACES UNDER AIRFLOW SHEARING | ICAS2024_0934 |
| Zhao, J. | WEAR EVOLUTION OF PYRAMID-STRUCTURED ABRASIVE BELTS AND ITS EFFECT ON GRINDING OPERATIONS | ICAS2024_0368 |
| Zhao, J. | RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS | ICAS2024_0674 |
| Zhao, R. | HIGH-VELOCITY DROPLET IMPACT STUDIES ON C/SIC AND C/C COMPOSITES | ICAS2024_0808 |
| Zhao, S. | THE EFFECT OF TARGET THICKNESS ON THE BALLISTIC BEHAVIOR OF HYBRID CFRP/KFRP COMPOSITES | ICAS2024_0225 |
| Zhao, S. | RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS | ICAS2024_0674 |
| Zhao, S. | CORRELATION MODELLING OF SURFACE INVISCID FLOW CHARACTERISTICS AND FRICTION DISTRIBUTION BASED ON MACHINE LEARNING | ICAS2024_0958 |
| Zhao, X. | ANALYSIS OF AERODYNAMIC INTERFERENCE CHARACTERISTICS AND AEROACOUSTICS FOR HIGH-SPEED COMPOSITE HELICOPTER IN HOVER | ICAS2024_0704 |
| Zhao, Y. | INVESTIGATION ON VARIABLE-HEIGHT PROTRUSION ARRANGEMENT OF METAL–COMPOSITE HYBRID JOINTS UNDER A TENSILE LOAD | ICAS2024_1099 |
| Zhao, Y.-R. | FAULT DIAGNOSIS AND TOLERANCE SYSTEM OF FLIGHT STATE PERCEPTION MODEL BASED ON MACHINE LEARNING FOR CO-FLOW JET AIRFOIL | ICAS2024_0662 |
| Zhao, Z. | A DYNAMIC TEST METHODOLOGY FOR DETERMINING THE LONGITUDINAL COMPRESSIVE RESPONSE OF CARBON FIBER COMPOSITE TOWS | ICAS2024_0584 |
| Zhao, Z.-Q. | THE RESISTANCE TO THE HIGH-VELOCITY IMPACT OF THE INTRA-LAYER HYBRID PLAIN WEAVE COMPOSITES | ICAS2024_0212 |
| Zhao, Z.-Q. | A MESO-SCALED SIMULATION ON THE THICKNESS EFFECT OF TWO-DIMENSIONAL TRIAXIALLY BRAIDED COMPOSITES UNDER TENSILE LOADS | ICAS2024_0259 |
| Zheng, K.F. | DESIGN OPTIMIZATION OF A WIG CRAFT’S HIGH LIFT DEVICE CONSIDERING GROUND EFFECT | ICAS2024_0572 |
| Zheng, L. | NUMERICAL AND THEORETICAL INVESTIGATION OF HELICOPTER DITCHING WITH VARIOUS INITIAL VELOCITY AND PITCHING ANGLE | ICAS2024_0216 |
| Zheng, Y. | TILT-DUCT AIRCRAFT WING AERODYNAMIC DESIGN AND OPTIMIZATION BASED ON ADJOINT METHOD | ICAS2024_0332 |
| Zheng, Y. | OPTIMIZATION OF COMPOSITE WING STRUCTURE FOR TILT-DUCT AIRCRAFT CONSIDERING DISCRETE AND CONTINUOUS DESIGN VARIABLES | ICAS2024_0405 |
| Zheng, Y.-H. | ANALYTICAL STUDY ON HYDROSTATIC RESPONSE CHARACTERISTICS DURING WATER LANDINGS OF AMPHIBIOUS AIRCRAFT | ICAS2024_0905 |
| Zheng, Z.-J. | TILT-DUCT AIRCRAFT WING AERODYNAMIC DESIGN AND OPTIMIZATION BASED ON ADJOINT METHOD | ICAS2024_0332 |
| Zhong, Z. | CLASSIFICATION OF COGNITIVE LOAD BASED ON THE PILOT’ VISUAL SCAN PATTERNS | ICAS2024_0955 |
| Zhou, C.-K. | REENTRY TRAJECTORY DESIGN FOR DEFORMABLE HYPERSONIC VEHICLES BASED ON NEURAL NETWORKS | ICAS2024_1087 |
| Zhou, J. | STUDY ON LOW-VELOCITY IMPACT BEHAVIOR AND RESIDUAL PERFORMANCE PREDICTION OF CFRP T-JOINTS | ICAS2024_0045 |
| Zhou, K.-Y. | EFFICIENT MULTI-OBJECTIVE DESIGN OPTIMIZATION OF ROTOR AIRFOILS FOR IMPROVING DYNAMIC STALL CHARACTERISTICS | ICAS2024_0420 |
| Zhou, K.-Y. | RESEARCH ON MULTI-OBJECTIVE AERODYNAMIC/STRUCTURAL DESIGN OPTIMIZATION METHOD FOR LARGE THICKNESS FLATBACK AIRFOILS | ICAS2024_0690 |
| Zhou, L. | AERODYNAMIC DEFORMATION EXPERIMENT OF SERPENTINE NOZZLE FOR TURBOFAN AND ANALYSIS OF FLUID-STRUCTURE INTERACTION METHOD | ICAS2024_0919 |
| Zhou, L. | EXPERIMENTAL AND NUMERICAL INVESTIGATION ON SEPARATION CHARACTERISTICS OF SERPENTINE CONVERGENT-DIVERGENT NOZZLE | ICAS2024_0920 |
| Zhou, T.-Y. | PRESERVING HUMAN EXPERTISE: EXPLORING MIXED REALITY TRAJECTORY PLANNING FOR ROBOTIC BELT GRINDING | ICAS2024_0378 |
| Zhou, X. | ON THE DEVELOPMENT OF THE STRUCTURAL DIGITAL TWIN OF AN UNMANNED AERIAL VEHICLE | ICAS2024_0724 |
| Zhou, Y. | MANNED AND UNMANNED AERIAL VEHICLES COOPERATIVE COMBAT FRAMEWORK BASED ON LARGE LANGUAGE MODELS | ICAS2024_0231 |
| Zhou, Y.M. | A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION | ICAS2024_0314 |
| Zhou, Z. | SIMULATION STUDY ON AERODYNAMIC CHARACTERISTICS OF COMBINED LOW ASPECT RATIO UAV | ICAS2024_0449 |
| Zhu, B. | ANALYSIS OF BATTERY WEIGHT REQUIREMENTS IN THE DESIGN OF HYBRID ELECTRIC POWERED AIRCRAFT | ICAS2024_0813 |
| Zhu, C.L. | THE IMPACT OF PIEZOELECTRIC STACK HEATING ON AIRCRAFT DEICING | ICAS2024_0279 |
| Zhu, D. | STUDY OF DROPLET MOTION AND WATER FILM FLOW CHARACTERISTICS ON SUPERHYDROPHOBIC SURFACES UNDER AIRFLOW SHEARING | ICAS2024_0934 |
| Zhu, H. | DYNAMIC BUCKLING ANALYSIS OF THIN-SHELL COMPOSITE STRUCTURES BASED ON ISOGEOMETRIC ANALYSIS | ICAS2024_0389 |
| Zhu, L. | ENHANCING THE PERFORMANCE OF SLENDER STRUCTURES WITH GEOMETRIC CONSTRAINTS: A CASE STUDY WITH THE ROORDA FRAME | ICAS2024_0192 |
| Zhu, P.-F. | VOID FRACTION CALCULATION MODEL BASED ON TWO-PHASE FLOW PATTERNS IN THE SCAVENGE PIPE | ICAS2024_1010 |
| Zhu, P.-F. | A STUDY ON THE AIRLOCK MECHANISM OF THE OIL SUPPLY PUMP IN AERO-ENGINE LUBRICATING OIL SYSTEM | ICAS2024_1030 |
| Zhu, Q. | SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT | ICAS2024_0925 |
| Zhu, S.-S. | ANALYTICAL STUDY ON HYDROSTATIC RESPONSE CHARACTERISTICS DURING WATER LANDINGS OF AMPHIBIOUS AIRCRAFT | ICAS2024_0905 |
| Zhu, Z.X. | EXPERIMENTAL INVESTIGATION AND NUMERICAL ANALYSIS OF THE EFFECT OF TEMPERATURE ON THE MECHANICAL PROPERTIES OF AEROSPACE COMPOSITE-METAL HYBRID JOINTS | ICAS2024_0530 |
| Ziaja, K. | DESIGN APPROACH FOR HYBRID ELECTRIC PROPULSION CONCEPTS OF MID-RANGE AIRCRAFT INCLUDING SUSTAINABLE AVIATION FUELS | ICAS2024_1069 |
| Ziegler, M. | MRO FOR VTOLS IN A FUNCTIONAL SEQUENCES SOLUTION SPACE | ICAS2024_0705 |
| Zieher, M. | ASSESSMENT OF AN ADAPTIVE ONE-EQUATION TURBULENCE MODEL FOR LEADING-EDGE VORTEX FLOWS ON MULTIPLE SWEPT DELTA WINGS | ICAS2024_0822 |
| Zill, T. | GLOBAL SENSITIVITY ANALYSIS OF LIQUID HYDROGEN STORAGE DESIGN PARAMETERS FOR OVERALL AIRCRAFT DESIGN | ICAS2024_0092 |
| Zill, T. | CONCEPTUAL AIRCRAFT DESIGN OF A RESEARCH BASELINE WITH DIRECT LIQUID HYDROGEN COMBUSTION | ICAS2024_0503 |
| Zilli, A. | CORUS-XUAM: TACKLING URBAN AIR MOBILITY AIRSPACE INTEGRATION CHALLENGES | ICAS2024_0347 |
| Zmijanovic, V. | BASE FLOW CHARACTERISTICS FOR A SUB-SCALE HIGH-SPEED EXHAUST AT OVER-EXPANDED MODE | ICAS2024_0512 |
| Zobeiry, N. | NUMERICAL ANALYSIS OF PROCESS-INDUCED DEFORMATIONS AND STRESSES IN AERONAUTICAL COMPOSITE COMPONENTS | ICAS2024_0818 |
| Zou, L. | THERMAL AND GRINDING PERFORMANCE OF 3D PRINTED COMPLIANCE GRINDING TOOLS WITH ROTARY-ENHANCED HEAT TRANSFER STRUCTURE | ICAS2024_0248 |
| Zou, L. | REDESIGN AND MACHINING OF LEADING EDGE OF TRANSONIC COMPRESSOR BLADE IN ROBOTIC GRINDING OPERATION | ICAS2024_0260 |
| Zou, L. | WEAR EVOLUTION OF PYRAMID-STRUCTURED ABRASIVE BELTS AND ITS EFFECT ON GRINDING OPERATIONS | ICAS2024_0368 |
| Zozulya, V.V. | VIBRATION OF COMPOSITE SHELLS OF REVOLUTION USING EQUIVALENT SINGLE LAYER APPROACH | ICAS2024_1203 |
| Zumach, K. | TOWARDS A HOLISTIC APPROACH TO INCREASE SUSTAINABILITY IN AIRCRAFT CABIN DESIGN | ICAS2024_0511 |
| Zuo, K. | INTELLIGENT RECONSTRUCTION METHOD OF AIRFOIL FLOW FIELD BASED ON DEEP ATTENTION NETWORK | ICAS2024_0852 |
| Zwane, L. | DECOUPLING STORE AND PARENT AERODYNAMICS FOR FAST PREDICTION OF SUBSONIC STORE TRAJECTORIES | ICAS2024_0189 |