| Aaltonen, J. | FUEL CELLS AND NOVEL THERMAL MANAGEMENT ADVANCEMENTS REQUIRED FOR AVIATION | ICAS2022_0079 |
| Abdelmoula, F. | THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALE | ICAS2022_0328 |
| Abdelmoula, F. | IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT | ICAS2022_0627 |
| Abe, K. | COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHOD | ICAS2022_0416 |
| Abhyankar, K. | INVESTIGATION ON INTEGRATING RECYCLABILITY AS A FUNCTION AT THE DESIGN PHASE OF COMPLEX-LOADED STRUCTURAL COMPONENTS | ICAS2022_0125 |
| Abu Salem, K. | CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGE | ICAS2022_0148 |
| Abu-Zurayk, M. | APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT | ICAS2022_0892 |
| Adler, E.J. | AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0593 |
| Adler, E.J. | TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATION | ICAS2022_0905 |
| Ahn, S. | A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSB | ICAS2022_0222 |
| Ahn, H.J. | SAFE REINFORCEMENT LEARNING BASED MULTI-ROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLES | ICAS2022_0539 |
| Akatsuka, J. | FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLET | ICAS2022_0830 |
| Akman, T. | REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT | ICAS2022_0797 |
| Alaimo, A. | RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS | ICAS2022_0218 |
| Alarcon, D.S. | DEEP REINFORCEMENT LEARNING FOR EVTOL HOVERING CONTROL | ICAS2022_0291 |
| Alfredsson, J. | HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICS | ICAS2022_0707 |
| Allan, M. | VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA | ICAS2022_0124 |
| Allan, M. | COMPUTATIONALLY ECONOMICAL METHODS FOR LANDING GEAR NOISE SIMULATIONS | ICAS2022_0317 |
| Allegaert, E. | TEMPLATE-BASED SYNTHESIS OF 3D SYSTEMS FOR MBSE | ICAS2022_0724 |
| Allen, N.J. | IMPACT OF NASCENT TECHNOLOGIES ON THE SUSTAINABILITY ATTRIBUTES OF AN EVOLUTIONARY SINGLE-AISLE AIRCRAFT | ICAS2022_0543 |
| Allouis, C. | A NEW FACILITY FOR HYPERSONIC FLOW SIMULATION DRIVEN BY A HIGH VELOCITY OXYGEN FUEL GUN | ICAS2022_0437 |
| Almeida, S.F.M. | NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL | ICAS2022_0059 |
| Almeida, M.A. | USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION | ICAS2022_0389 |
| Almeida, L.E.N. | EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE | ICAS2022_0676 |
| Alonso, G. | IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONS | ICAS2022_0360 |
| Altar Inceer, A. | PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE | ICAS2022_0782 |
| Alves, L. | ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER | ICAS2022_0887 |
| Amadori, K. | ZERO-EMISSION REGIONAL AVIATION IN SWEDEN | ICAS2022_0650 |
| Amadori, K. | UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENT | ICAS2022_0659 |
| Ammann, N. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| An, Z. | HUMAN-MACHINE FUNCTION ALLOCATION METHOD FOR SINGLE PILOT OPERATION USING HESITANT FUZZY 2-TUPLE LINGUISTIC INFORMATION | ICAS2022_0493 |
| Anderini, U. | HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICS | ICAS2022_0707 |
| Andersson, J. | INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM ALLOY 780 | ICAS2022_0206 |
| Andersson, P. | DEMONSTRATING AN APPROACH FOR MULTIDISCIPLINARY SET BASED DESIGN WITHIN AN AEROSPACE RESEARCH PROJECT - DEFAINE | ICAS2022_0661 |
| Andreeva-Mori, A. | INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS | ICAS2022_0904 |
| Andreeva-Mori, A. | OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE | ICAS2022_0909 |
| Andreeva-Mori, A. | AN INTERNATIONAL RESEARCH PERSPECTIVE ON AIRSPACE INTEGRATION IN THE FRAMEWORK OF URBAN AIR MOBILITY | ICAS2022_0948 |
| Andrés, E. | AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGS | ICAS2022_0020 |
| Andrews, C. | HYBRID ELECTRIC PROPULSION DEVELOPMENT FOR COMMERCIAL AVIATION | ICAS2022_0944 |
| Andronikos, T. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Ansumali, S. | TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHOD | ICAS2022_0630 |
| Anvid, D.H. | A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT | ICAS2022_0453 |
| Anyu , B. | AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNEL | ICAS2022_0411 |
| Aprovitola, A. | AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLES | ICAS2022_0241 |
| Aprovitola, A. | AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE | ICAS2022_0259 |
| Arcidiacono, S. | TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHOD | ICAS2022_0630 |
| Ariaseta, A. | INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM ALLOY 780 | ICAS2022_0206 |
| Ariyarit, A. | AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION | ICAS2022_0413 |
| Arjoni, D. | HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICS | ICAS2022_0707 |
| Armani, U. | APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS | ICAS2022_0643 |
| Armanini, S.F. | URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH NON-COOPERATIVE AIRSPACE USERS | ICAS2022_0567 |
| Armanini, S.F. | EVALUATION AND QUANTIFICATION OF THE POTENTIAL CONSEQUENCES OF BIRD STRIKES IN URBAN AIR MOBILITY | ICAS2022_0629 |
| Arnoult, G. | OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACT | ICAS2022_0843 |
| Arthur, J.J. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Arvidson, S. | EFFECT OF LES LENGTH SCALE AND NUMERICAL SCHEME IN HYBRID RANS-LES OF FREE SHEAR LAYER FLOWS | ICAS2022_0684 |
| Asai, M. | EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETS | ICAS2022_0243 |
| Aschwanden, P. | POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORS | ICAS2022_0347 |
| Assato, M. | PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE | ICAS2022_0782 |
| Asseman, P. | OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN | ICAS2022_0550 |
| Atif, M. | HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS | ICAS2022_0894 |
| Atinault, O. | OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACT | ICAS2022_0843 |
| Atkin, C.J. | STABILITY OF A LAMINAR BOUNDARY LAYER OVER LOCALISED SURFACE INDENTATION | ICAS2022_0697 |
| Augello, R. | A GLOBAL/LOCAL ELEMENT-WISE APPROACH FOR THE BUCKLING AND POST-BUCKLING ANALYSIS OF THIN MULTILAYERED STRUCTURES | ICAS2022_0253 |
| Autenrieb, J. | COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACS | ICAS2022_0505 |
| Avanzini, G. | SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSIS | ICAS2022_0370 |
| Avellán, R. | ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR | ICAS2022_0382 |
| Avellan, R. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| Aydin, E. | CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACH | ICAS2022_0102 |
| Aydin, S.M. | AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPES | ICAS2022_0381 |
| Azevedo, J.L.F. | ON THE INFLUENCE OF GRADIENT RECONSTRUCTION PROCEDURES OVER THE ACCURACY OF FINITE VOLUME BASED SCHEMES | ICAS2022_0191 |
| Azevedo, J.L.F. | A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTS | ICAS2022_0672 |
| Azevedo, J.L.F. | STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWS | ICAS2022_0726 |
| Azevedo, J.L.F | AUTOMATIC FREE-FORM DEFORMATION AS GEOMETRIC PARAMETERIZATION FOR AERODYNAMIC DESIGN | ICAS2022_0749 |
| Azzara, R. | NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF UNSTIFFENED AND STIFFENED STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGS | ICAS2022_0220 |
| Baba, I. | DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES | ICAS2022_0448 |
| Babetto, L. | SORA-BASED RISK ASSESSMENT FOR CARGO UNMANNED AERIAL VEHICLES IN THE UAM FRAMEWORK | ICAS2022_0240 |
| Bae, J.-S. | ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION | ICAS2022_0827 |
| Bagassi, S. | VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTS | ICAS2022_0247 |
| Bagassi, S. | V/A-R AIR GESTURES HMI INTERACTION IN AIRPORT CONTROL TOWERS | ICAS2022_0452 |
| Bagassi, S. | AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACH | ICAS2022_0478 |
| Bagassi, S. | POTENTIAL OF EXTENDED REALITY IN ENGINEERING AND CHALLENGES OF UNCONVENTIONAL VEHICLE DESIGN | ICAS2022_0966 |
| Bagdatli, B. | SYSTEM LEVEL IDENTIFICATION OF CRITICAL UNCERTAINTIES TO ENABLE VALIDATION EXPERIMENTS | ICAS2022_0935 |
| Bahrami, F. | TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS | ICAS2022_0604 |
| Bai, J.Q. | AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK | ICAS2022_0199 |
| Balack, P. | IMPACT OF THE NUMBER OF WING STATIONS ON THE TWIST DISTRIBUTION OF A BWB CONCEPTUAL AIRCRAFT DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTION | ICAS2022_0854 |
| Balchanos, M. | A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT | ICAS2022_0453 |
| Baldochi, L. A. | USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION | ICAS2022_0389 |
| Bando, M. | ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOW | ICAS2022_0476 |
| Bando, M. | INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCE | ICAS2022_0796 |
| Bang, H. | INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFT | ICAS2022_0346 |
| Bang, H.-C. | FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSION | ICAS2022_0438 |
| Bang, H.C. | SAFE REINFORCEMENT LEARNING BASED MULTI-ROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLES | ICAS2022_0539 |
| Banks-Davies, L. | EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILTROTOR AIRCRAFT | ICAS2022_0530 |
| Bao, C. | AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNEL | ICAS2022_0411 |
| Barakos, G. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Barbarino, M. | COMPARISON OF ANALYTICAL SEMI-EMPIRICAL MODEL FOR JET NOISE PREDICTION | ICAS2022_0855 |
| Barbosa, D.F.C. | EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE | ICAS2022_0676 |
| Barbosa, L.M.F. | METHODOLOGIES AND EXAMPLE OF CONCEPTUAL DESIGN FOR A FOOT-LAUNCHABLE SPORT SAILPLANE | ICAS2022_0893 |
| Baron, C. | TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONES | ICAS2022_0655 |
| Barragan Montes, R. | DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELS | ICAS2022_0648 |
| Barrier, R. | AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTS | ICAS2022_0058 |
| Barrier, R. | LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES | ICAS2022_0339 |
| Bartasevicius, J. | COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAV | ICAS2022_0367 |
| Bartoli, N. | A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK | ICAS2022_0618 |
| Batra, A. | SERIES OR PARALLEL HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEMS? CASE STUDIES OF THE ATR42 AND ATR72 | ICAS2022_0163 |
| Batra, A. | KINETIC ENERGY RECOVERY FROM A LANDING AIRCRAFT: ENERGY ANALYSIS, ENVIRONMENTAL AND ECONOMIC PROSPECTS | ICAS2022_0821 |
| Bauer, T. | IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT | ICAS2022_0627 |
| Baumann, S. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Bayandor, J. | HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE STRIKE ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT | ICAS2022_0718 |
| Bayandor, J. | DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURES | ICAS2022_0734 |
| Bayram, K. | FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES | ICAS2022_0958 |
| Beamer, C. | LATEST DEVELOPMENTS IN HIGH PRESSURE HEAT TREATMENT OF AEROSPACE COMPONENTS | ICAS2022_0026 |
| Becker, D. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Beckert, F. | VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERING | ICAS2022_0063 |
| Beijer, B. | THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENT | ICAS2022_0615 |
| Ben Salah, N. | NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 | ICAS2022_0801 |
| Benad, J. | DESIGN OF A FLYING V SUBSONIC TRANSPORT | ICAS2022_0358 |
| Bénard, E. | SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES | ICAS2022_0084 |
| Benard, E. | OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN | ICAS2022_0550 |
| Benard, E. | AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS | ICAS2022_0560 |
| Bennehard, Q. | OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACT | ICAS2022_0843 |
| Berend, N. | FLIGHT EXPERIMENTS FOR THE ALTAIR SEMI-REUSABLE AIR-LAUNCH SYSTEM WITH THE DEMONSTRATOR EOLE | ICAS2022_0541 |
| Berlowitz, I. | ELECTRICALLY POWERED LANDING GEAR SYSTEM FOR TRANSPORT AIRCRAFT TAXIING | ICAS2022_0003 |
| Berlowitz, I. | TRANSPORT AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM AIR QUALITY IMPROVEMENT | ICAS2022_0055 |
| Bernardini, G. | SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSIS | ICAS2022_0370 |
| Berschik, M.C. | A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE | ICAS2022_0791 |
| Bertling Tjernberg, L. | MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACT | ICAS2022_0369 |
| Bertling-Tjernberg, L. | MORE ELECTRIC AIRPLANE: CASE STUDY STOCKHOLM - COPENHAGEN | ICAS2022_0506 |
| Bertram, O. | COUPLING OF MODEL-BASED SYSTEMS ENGINEERING AND SAFETY ANALYSIS IN CONCEPTUAL AIRCRAFT SYSTEM DESIGN | ICAS2022_0082 |
| Bhurat, S. | NUCLEAR POWERED AIR-BREATHING ELECTRIC THRUSTERS USED IN UAVS FOR EXTRA-TERRESTRIAL APPLICATIONS | ICAS2022_0019 |
| Bidinotto, J.H. | DEEP REINFORCEMENT LEARNING FOR EVTOL HOVERING CONTROL | ICAS2022_0291 |
| Bieber, P. | AVIATION SECURITY CONCERNS | ICAS2022_0918 |
| Biedermann, J. | VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERING | ICAS2022_0063 |
| Biedermann, J. | EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXT | ICAS2022_0254 |
| Bielsky, T. | SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGN | ICAS2022_0665 |
| Bil, C. | DOOR-TO-DOOR TRAVEL PLANNER FOR IMPROVED TRAVELER EXPERIENCE USING DIGITAL TWIN CONCEPT | ICAS2022_0011 |
| Bilger, M. | A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCE | ICAS2022_0332 |
| Billson, M. | STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT | ICAS2022_0480 |
| Billson, M. | IDENTIFICATION OF CRITICAL ACOUSTIC MODES FOR AN OPEN BOX CAVITY WITH ADJUSTABLE DEPTH | ICAS2022_0696 |
| Binante, V. | CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGE | ICAS2022_0148 |
| Binetti, T. | STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES | ICAS2022_0336 |
| Birberg, J. | REAL-TIME IDENTIFICATION OF USER ACTIONS IN COMPUTER-AIDED MANUFACTURING USING MACHINE LEARNING AND COMPUTER VISION | ICAS2022_0534 |
| Birch, D.M. | WALL INTERFERENCE CORRECTIONS USING NONLINEAR LEAST-SQUARES OPTIMISATION | ICAS2022_0378 |
| Biron, A. | VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGS | ICAS2022_0207 |
| Bisagni, C. | INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY | ICAS2022_0685 |
| Bischof, P.S. | DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK | ICAS2022_0677 |
| Bjursten Carlsson, C. | STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATION | ICAS2022_0903 |
| Bladh, P. | GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS | ICAS2022_0265 |
| Blecken, M. | A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE | ICAS2022_0791 |
| Bloise, N. | ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITION | ICAS2022_0085 |
| Boden, B. | RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORK | ICAS2022_0702 |
| Boggero, L. | METHODOLOGY FOR THE AUTOMATED PRELIMINARY CERTIFICATION OF ON-BOARD SYSTEMS ARCHITECTURES THROUGH REQUIREMENTS ANALYSIS | ICAS2022_0327 |
| Boggero, L. | SYSTEMS ARCHITECTING: A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0 PROJECT | ICAS2022_0365 |
| Boggero, L. | AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0593 |
| Boggero, L. | THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENT | ICAS2022_0615 |
| Boggero, L. | A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK | ICAS2022_0618 |
| Boggero, L. | POTENTIAL OF EXTENDED REALITY IN ENGINEERING AND CHALLENGES OF UNCONVENTIONAL VEHICLE DESIGN | ICAS2022_0966 |
| Bohnert, P. | DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFT | ICAS2022_0566 |
| Boisard, R. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Boni , I. | STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES | ICAS2022_0336 |
| Boni , L. | FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES | ICAS2022_0692 |
| Bonnin, V.O. | SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART I: INITIAL DESIGNS | ICAS2022_0248 |
| Bonnin, V.O. | SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART II: SENSITIVITY ANALYSIS | ICAS2022_0481 |
| Bontoft, E.K. | AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK | ICAS2022_0199 |
| Boogaart, T.E. | INSTALLATION PENALTY OF AERO-ENGINES ON NARROW BODY AIRCRAFT | ICAS2022_0246 |
| Bordeneuve-Guibe, J. | A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS | ICAS2022_0568 |
| Borghi, M. | “CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION | ICAS2022_0345 |
| Borodacz, K. | IMPACT OF MOTION-DEPENDENT ERRORS ON THE ACCURACY OF AN UNAIDED STRAPDOWN INERTIAL NAVIGATION SYSTEM | ICAS2022_0742 |
| Boscagli, L. | A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES | ICAS2022_0162 |
| Botero-Bolivar, L. | AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF THE NACA 0008 AIRFOIL | ICAS2022_0128 |
| Boucher, M.J. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Boussuge, J.-F. | LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES | ICAS2022_0339 |
| Bovecchi, F. | FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES | ICAS2022_0692 |
| Bowen Varela, J. | AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGS | ICAS2022_0020 |
| Boyer, J. | IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT | ICAS2022_0627 |
| Bramkamp, F. | ENHANCING CFD PREDICTIONS FOR THE GRIPEN AIRCRAFT | ICAS2022_0242 |
| Bramsiepe, K. | WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSES | ICAS2022_0663 |
| Brancalion, J.F.B. | COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMS | ICAS2022_0340 |
| Braune, M. | WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSES | ICAS2022_0663 |
| Bravo-Mosquera, P.D. | LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTION | ICAS2022_0088 |
| Bravo-Mosquera, P.D. | EXPERIMENTAL INVESTIGATION OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTION | ICAS2022_0431 |
| Bravo-Mosquera, P.D. | EXPLORATION OF BOX-WING AIRCRAFT CONCEPT USING HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION | ICAS2022_0446 |
| Bravo-Mosquera, P. | PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE | ICAS2022_0782 |
| Brazier, F. | ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEM | ICAS2022_0368 |
| Breitamter, C. | STRAKE SECTION IMPACT ON HYBRID-DELTA-WING AERODYNAMICS | ICAS2022_0075 |
| Breitsamter, C. | TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WING | ICAS2022_0037 |
| Breitsamter, C. | WING BUFFET PRESSURE LOAD PREDICTION BASED ON A HYBRID DEEP LEARNING MODEL | ICAS2022_0043 |
| Breitsamter, C. | WIND-TUNNEL TEST ON LEADING-EDGE VORTEX OF LOW-ASPECT-RATIO FLAPPING PLATES | ICAS2022_0154 |
| Breitsamter, C. | EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS | ICAS2022_0250 |
| Bremm, M. | EXPERIMENTS TO INVESTIGATE LIFT PRODUCTION MECHANISMS ON OSCILLATING TRAILING-EDGE FLAPS | ICAS2022_0780 |
| Bremmers, F. | VALIDATION OF SCALED FLIGHT TESTING | ICAS2022_0375 |
| Brentjes, A. | INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD | ICAS2022_0653 |
| Breviglieri, C. | STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWS | ICAS2022_0726 |
| Bringhenti, C. | EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE | ICAS2022_0676 |
| Bringhenti, C. | PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE | ICAS2022_0782 |
| Broatch, A. | NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINES | ICAS2022_0224 |
| Brodersen, O. | APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT | ICAS2022_0892 |
| Broehan, J. | SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGN | ICAS2022_0665 |
| Bronsvoort, J. | TRAJECTORY-BASED OPERATIONS TO IMPROVE LONG-RANGE AIR TRAFFIC FLOW MANAGEMENT | ICAS2022_0087 |
| Bronz, M. | A STUDY OF HIGH-LIFT DEVICES FOR LOW REYNOLDS NUMBER APPLICATIONS | ICAS2022_0312 |
| Brouckaert, J.-F. | THE CLEAN SKY 2 TECHNOLOGY EVALUATOR 1ST GLOBAL ASSESSMENT | ICAS2022_0927 |
| Bruno, M. | ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT | ICAS2022_0234 |
| Bu, C. | DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNEL | ICAS2022_0045 |
| Bu, C. | EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING | ICAS2022_0078 |
| Budinger, M. | STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS | ICAS2022_0151 |
| Budinger, M. | PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES | ICAS2022_0289 |
| Budinger, M. | A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONS | ICAS2022_0383 |
| Bura, R.O. | TURBULENCE MODELLING STUDIES OF SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE CYLINDER FLARE IN HYPERSONIC FLOWS | ICAS2022_0746 |
| Burger, U. | A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONS | ICAS2022_0030 |
| Burger, K. | DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFT | ICAS2022_0622 |
| Burschyk, T. | RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORK | ICAS2022_0702 |
| Buschhaus, M. | USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM | ICAS2022_0116 |
| Busse, D.O. | FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES | ICAS2022_0692 |
| Bussemaker, J.H. | SYSTEMS ARCHITECTING: A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0 PROJECT | ICAS2022_0365 |
| Bussemaker, J.H. | AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0593 |
| Busteros-Ramos, A. | FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFT | ICAS2022_0214 |
| Buszyk, M. | AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTS | ICAS2022_0058 |
| Buszyk, M. | LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES | ICAS2022_0339 |
| Byun, K.-H. | ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION | ICAS2022_0827 |
| Bĺng, M. | ATCO STRATEGIES IN TACTICAL TBO: A SIMULATOR STUDY | ICAS2022_0285 |
| Bĺng, M. | HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICS | ICAS2022_0707 |
| Cabac, Y. | RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORK | ICAS2022_0702 |
| Cabailero, C. | REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION | ICAS2022_0323 |
| Cabaleiro, C. | METHODOLOGY FOR THE AUTOMATED PRELIMINARY CERTIFICATION OF ON-BOARD SYSTEMS ARCHITECTURES THROUGH REQUIREMENTS ANALYSIS | ICAS2022_0327 |
| Cabaleiro, C. | CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT | ICAS2022_0350 |
| Caivano, A. | WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA | ICAS2022_0280 |
| Cakir, B.O. | HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS | ICAS2022_0572 |
| Calavera, L.R. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Calvo Blanco, M. | ULTRA-EFFICIENT AIRCRAFT AND PROPULSION ARCHITECTURES FOR LOW-EMISSION SHORT/MEDIUM RANGE [SMR] AIRCRAFT | ICAS2022_0929 |
| Cambertoni, R. | ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT | ICAS2022_0234 |
| Camilleri, R. | SERIES OR PARALLEL HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEMS? CASE STUDIES OF THE ATR42 AND ATR72 | ICAS2022_0163 |
| Camilleri, R. | KINETIC ENERGY RECOVERY FROM A LANDING AIRCRAFT: ENERGY ANALYSIS, ENVIRONMENTAL AND ECONOMIC PROSPECTS | ICAS2022_0821 |
| Campillo Borrás, E. | FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION | ICAS2022_0708 |
| Campos, L.M.B.C. | ON LATERAL-LONGITUDINAL CONTROL COUPLING FOR SHORT- AND LONG-FUSELAGE BWB AIRCRAFT CONFIGURATIONS | ICAS2022_0733 |
| Can, A.G. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Candell, O. | GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS | ICAS2022_0265 |
| Cantanna, G. | CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL | ICAS2022_0341 |
| Cao, M.-G. | RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE | ICAS2022_0510 |
| Capello, E. | ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITION | ICAS2022_0085 |
| Capitao, A. | EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT | ICAS2022_0788 |
| Capitao Patrao, A. | NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCT | ICAS2022_0236 |
| Caprdja, K. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Caramazza, A. | CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL | ICAS2022_0341 |
| Carbonneau, X. | ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEM | ICAS2022_0368 |
| Carbonneau, X. | UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLS | ICAS2022_0611 |
| Cardoso, M.M. | UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO | ICAS2022_0729 |
| Cardoso Júnior, M.M. | EXPLORATORY STUDY OF MENTAL WORKLOAD IN HELICOPTER AIR-TO-GROUND ROCKET FIRING | ICAS2022_0077 |
| Cardoso Junior, M.M. | A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY | ICAS2022_0723 |
| Carena, F. | A STUDENT TEAM BASED TEACHING APPROACH: THE TEAM S55 EXPERIENCE | ICAS2022_0315 |
| Carias, E.K.T. | VALIDATION STUDY OF BLUNTED AND SHARP CONES AT HYPERSONIC SPEED | ICAS2022_0147 |
| Carlsson, B. | FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE | ICAS2022_0028 |
| Carlsson, M. | EFFECT OF LES LENGTH SCALE AND NUMERICAL SCHEME IN HYBRID RANS-LES OF FREE SHEAR LAYER FLOWS | ICAS2022_0684 |
| Carreńo Ruiz, M. | ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITION | ICAS2022_0085 |
| Carrera, E. | NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF UNSTIFFENED AND STIFFENED STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGS | ICAS2022_0220 |
| Carrera, E. | A GLOBAL/LOCAL ELEMENT-WISE APPROACH FOR THE BUCKLING AND POST-BUCKLING ANALYSIS OF THIN MULTILAYERED STRUCTURES | ICAS2022_0253 |
| Carrera, E. | DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU) | ICAS2022_0295 |
| Carvalho, A.H.O. | COMPETITIVITY, STRATEGY AND VALUE ON AIRPORTS A METHOD OF DIAGNOSIS, SUGGESTIONS AND ACTIONS FOR INTERNATIONAL AIRPORTS WITH A CASE STUDY OF CNF | ICAS2022_0022 |
| Carvalho, L.O. | USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION | ICAS2022_0389 |
| Castańo, M. | GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS | ICAS2022_0265 |
| Castellanos, R. | AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGS | ICAS2022_0020 |
| Castino, F. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Castro, S.G.P. | OPTIMAL DESIGN OF STIFFENED PANELS UNDER BUCKLING CONSTRAINTS: A DESIGN METHODOLOGY CONSIDERING CAD-BASED PARAMETERIZATION WITH SIMULTANEOUS LAYOUT AND SIZING OPTIMIZATION | ICAS2022_0393 |
| Castro, B.M. | STUDY OF EFFECTS ON THE WING'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPAN | ICAS2022_0889 |
| Catalano, F.M. | EXPERIMENTAL STUDIES ON THE INTERACTION BETWEEN PROPELLERS AND WING | ICAS2022_0262 |
| Catalano, F.M. | EXPERIMENTAL INVESTIGATION OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTION | ICAS2022_0431 |
| Catalano, F.M. | EXPLORATION OF BOX-WING AIRCRAFT CONCEPT USING HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION | ICAS2022_0446 |
| Catalano, F.M. | PUSHER PROPELLER INFLUENCE ON A LAMINAR WING TRANSITION LOCATION USING INFRARED THERMOGRAPHY | ICAS2022_0678 |
| Caurin, G. | THE BENEFIT OF BILATERAL RESEARCH NETWORKS - THE SARC AND BARINET INITIATIVES AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICS | ICAS2022_0681 |
| Cavalieri, V. | DESIGN AND EXPERIMENTAL TESTING OF A DROOP NOSE MORPHING FOR ADVANCED REGIONAL AIRCRAFT | ICAS2022_0861 |
| Cecrdle, J. | UPDATING OF JET TRAINER AIRCRAFT DYNAMIC MODEL TO RESULTS OF GROUND VIBRATION TEST | ICAS2022_0044 |
| Celso Greco Junior, P. | VISCOUS CORRECTION FOR HIGH ORDER IMMERSED INTERFACE METHOD FOR COMPRESSIBLE TRANSONIC FLOWS | ICAS2022_0260 |
| Cerino, G. | REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION | ICAS2022_0323 |
| Cerón-Muńoz, H.D. | EXPERIMENTAL INVESTIGATION OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTION | ICAS2022_0431 |
| Cerulus, N. | ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER | ICAS2022_0887 |
| Cervenka, M. | TREND MONITORING OF TURBOPROP ENGINES | ICAS2022_0094 |
| Cestino, E. | WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA | ICAS2022_0280 |
| Cestino, E. | A STUDENT TEAM BASED TEACHING APPROACH: THE TEAM S55 EXPERIENCE | ICAS2022_0315 |
| Cestino, E. | CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL | ICAS2022_0341 |
| Cestino, E. | NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMS | ICAS2022_0396 |
| Cha, J.-H. | DOPAMINE-COATED UHMWPE/HYDROGEN-RICH BENZOXAZINE COMPOSITES FOR SPACE RADIATION SHIELDING | ICAS2022_0101 |
| Chaitanya Munjulury, R. | ONTOLOGY-ASSISTED AIRCRAFT CONCEPT GENERATION | ICAS2022_0352 |
| Chalke, A.-P. | AEROELASTIC TAILORING OF COMPRESSOR BLADES | ICAS2022_0507 |
| Chalon Morgan, C. | DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELS | ICAS2022_0648 |
| Chalon Morgan, C. | FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES | ICAS2022_0958 |
| Chao, G. | RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION | ICAS2022_0760 |
| Chapman, J.W. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Chau, T. | EXPLORATION OF BOX-WING AIRCRAFT CONCEPT USING HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION | ICAS2022_0446 |
| Chau, T. | A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATION TO THE STRUT-BRACED-WING AND HYBRID-WING-BODY CONFIGURATIONS | ICAS2022_0748 |
| Chau, T. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Chen, Y. | DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK | ICAS2022_0032 |
| Chen, H. | EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING | ICAS2022_0078 |
| Chen, L. | DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT | ICAS2022_0321 |
| Chen, X. | SET-BASED DESIGN COORDINATION BETWEEN COUPLED SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVE | ICAS2022_0372 |
| Chen, Y.-H. | EXPERIMENTAL STUDY ON THE EFFECT OF INTERSTAGE BLEEDING ON THE PERFORMANCE OF FULL-SCALE MULTISTAGE AXIAL COMPRESSOR | ICAS2022_0495 |
| Chen, Y. | EXPERIMENTAL STUDY OF FLAT BAFFLE INLET TOTAL-PRESSURE DISTORTION IN A THREE-STAGE FAN | ICAS2022_0502 |
| Chen, B. | INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNEL | ICAS2022_0547 |
| Chen, Q. | A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT | ICAS2022_0584 |
| Chen, R. | TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS | ICAS2022_0604 |
| Chen, R. | DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATION | ICAS2022_0753 |
| Chen, Q. | COOPERATIVE PATH PLANNING AND ADJUSTING STRATEGY FOR UAVS WITH STRICT TIME CONSTRAINS | ICAS2022_0781 |
| Chen, H. | DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACE | ICAS2022_0785 |
| Chernoray, V. | THE INFLUENCE OF THE VANE LEAN ON THE FLOW IN A TURBINE REAR STRUCTURE | ICAS2022_0514 |
| Cheung, R.C.M. | LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPS | ICAS2022_0524 |
| Chiba, K. | INFLUENCES OF CHANGING THE INSTALLING POSITIONS OF MULTIPLE WINGLETS ON AERODYNAMIC CHARACTERISTICS | ICAS2022_0459 |
| Choi, H. | A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSB | ICAS2022_0222 |
| Christoffels, L. | THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION | ICAS2022_0268 |
| Chu, D.-L. | DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEM | ICAS2022_0818 |
| Chudý, P. | UNMANNED AERIAL VEHICLE\\\'S TRAJECTORY OPTIMIZATION IN CONSTRAINED ENVIRONMENTS | ICAS2022_0717 |
| Chudy, P. | LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFT | ICAS2022_0719 |
| Chudy, P. | PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELS | ICAS2022_0721 |
| Chunlei, Z. | NUMERICAL INVESTIGATION ON TURBINE SHROUD FILM COOLING HEAT TRANSFER PERFORMANCE OF TURBINE BLADE WITH GROOVE TIP | ICAS2022_0203 |
| Cicolini, P. | NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITCH ANGLE | ICAS2022_0355 |
| Cimini, C.A. | DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES USING NEURAL NETWORKS AND HYBRID DATA | ICAS2022_0705 |
| Cinefra, M. | VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTS | ICAS2022_0247 |
| Cinnela , P. | NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTS | ICAS2022_0349 |
| Cipolla, V. | CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGE | ICAS2022_0148 |
| Clair, V. | AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTS | ICAS2022_0058 |
| Clark, J.P. | REALISTIC HYDROGEN-BASED SOLUTIONS FOR SUSTAINABLE AVIATION | ICAS2022_0963 |
| Clifford, D. | COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMS | ICAS2022_0399 |
| Clinca, G. | “CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION | ICAS2022_0345 |
| Coelho Leite Fava, T. | DIRECT NUMERICAL SIMULATIONS OF A THICK, ROTATING AIRFOIL AT A LOW REYNOLDS NUMBER | ICAS2022_0680 |
| Coil, J. | FATIGUE CRACK PROPAGATION IN ADDITIVELY MANUFACTURED POLYMER PARTS | ICAS2022_0777 |
| Colli, A. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Condomines, J.-P. | PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY IMPLEMENTED UNDER ASWING | ICAS2022_0318 |
| Cooper, J.E. | LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPS | ICAS2022_0524 |
| Corcione, S. | REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION | ICAS2022_0323 |
| Corsi, M. | V/A-R AIR GESTURES HMI INTERACTION IN AIRPORT CONTROL TOWERS | ICAS2022_0452 |
| Cortes, R.G. | EXPLORATORY STUDY OF MENTAL WORKLOAD IN HELICOPTER AIR-TO-GROUND ROCKET FIRING | ICAS2022_0077 |
| Cortes, R.G. | DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY | ICAS2022_0662 |
| Coskun, S. | DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT – LIFE CYCLE ASSESSMENT ACTIVITIES AT ECOTECH / CLEANSKY 2 | ICAS2022_0895 |
| Couilleaux, A. | NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINES | ICAS2022_0224 |
| Coustols, P. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Coustols, E. | PROGRESS IN WING DESIGN, STATUS AND PERSPECTIVES | ICAS2022_0926 |
| Cristea, G.C. | TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINS | ICAS2022_0822 |
| Cubas, J. | IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONS | ICAS2022_0360 |
| Cuerno-Rejado, C. | ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORA | ICAS2022_0699 |
| Cui, Z. | A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTH | ICAS2022_0142 |
| Cui, Z. | DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION | ICAS2022_0143 |
| Cui, P. | DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATION | ICAS2022_0753 |
| Cumnuantip, S. | A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR | ICAS2022_0826 |
| Cusati, V. | TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASS | ICAS2022_0641 |
| Cutrone, L. | AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECT | ICAS2022_0235 |
| D'Alesio, P. | WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAP | ICAS2022_0232 |
| D'Amico, F.A. | “CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION | ICAS2022_0345 |
| Da Ronch, A. | COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMS | ICAS2022_0399 |
| da Silva, E.T. | A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY | ICAS2022_0723 |
| da Silva, R.G. | STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWS | ICAS2022_0726 |
| da Silva, E.T. | UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO | ICAS2022_0729 |
| da Silva, G.A.L. | LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP | ICAS2022_0869 |
| da Silva, R.G.A. | IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTING | ICAS2022_0873 |
| Dahlmann, K. | A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIES | ICAS2022_0853 |
| Dai, J.-H. | MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF 2D HIGH-LIFT DEVICE BASED ON DISTRIBUTED DEEP REINFORCEMENT LEARNING | ICAS2022_0219 |
| Danielson, L. | STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATION | ICAS2022_0903 |
| Daroukh, M. | STUDY OF THE IMPACT OF AZIMUTHAL FLOW DISTORTION ON IN-DUCT ACOUSTIC PROPAGATION USING A MULTIMODAL FORMULATION | ICAS2022_0666 |
| Das, S. | NUCLEAR POWERED AIR-BREATHING ELECTRIC THRUSTERS USED IN UAVS FOR EXTRA-TERRESTRIAL APPLICATIONS | ICAS2022_0019 |
| Das, R. | NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMS | ICAS2022_0396 |
| Das, T.S.G. | DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT – LIFE CYCLE ASSESSMENT ACTIVITIES AT ECOTECH / CLEANSKY 2 | ICAS2022_0895 |
| Datta, S. | A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT | ICAS2022_0453 |
| De Breuker, R. | OPTIMAL DESIGN OF STIFFENED PANELS UNDER BUCKLING CONSTRAINTS: A DESIGN METHODOLOGY CONSIDERING CAD-BASED PARAMETERIZATION WITH SIMULTANEOUS LAYOUT AND SIZING OPTIMIZATION | ICAS2022_0393 |
| De Crescenzio, F. | AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACH | ICAS2022_0478 |
| de Faria, A.R. | ASSESSMENT OF FAILURE UNDER LONGITUDINAL COMPRESSION OF UNIDIRECTIONAL COMPOSITES WITH IN-PLANE FIBER MISALIGNMENT | ICAS2022_0343 |
| De Felipe, P. | ECONOMICS OF SUSTAINABLE REGIONAL AIR MOBILITY | ICAS2022_0359 |
| De Franssu, H. | TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINE | ICAS2022_0006 |
| De Gaspari, A. | DESIGN AND EXPERIMENTAL TESTING OF A DROOP NOSE MORPHING FOR ADVANCED REGIONAL AIRCRAFT | ICAS2022_0861 |
| de Graaf, S. | DEVELOPMENT OF A CONTROLS APPROACH FOR FUEL CELL-POWERED ALL-ELECTRIC AERO ENGINES BASED ON AN FHA | ICAS2022_0366 |
| de Gruijl, W. | RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERS | ICAS2022_0489 |
| de Haan, W. | RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERS | ICAS2022_0489 |
| De Negri, V.J. | A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL | ICAS2022_0513 |
| de Negri, V.J. | THE BENEFIT OF BILATERAL RESEARCH NETWORKS - THE SARC AND BARINET INITIATIVES AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICS | ICAS2022_0681 |
| De Nicolas, B. | TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES | ICAS2022_0012 |
| de Oliveirra, G.L. | A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENT | ICAS2022_0523 |
| de Oliveirra, G. | EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMAS | ICAS2022_0526 |
| de Paula, L.G.L. | DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY | ICAS2022_0662 |
| De Paula, T.R. | PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING | ICAS2022_0694 |
| de Paula, T.R. | UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO | ICAS2022_0729 |
| De Rosa, S. | DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU) | ICAS2022_0295 |
| de Santana, L.D. | AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF THE NACA 0008 AIRFOIL | ICAS2022_0128 |
| de Santana, L.D. | INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD | ICAS2022_0653 |
| de Saqui-Sannes, P. | OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN | ICAS2022_0550 |
| de Saqui-Sannes, P. | TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONES | ICAS2022_0655 |
| De Simone, V. | COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION | ICAS2022_0342 |
| de Souza, T.M. | HYDRO ENVIRONMENTAL AND ELECTRICAL ASSETS MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV | ICAS2022_0017 |
| De Visscher, I. | DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELS | ICAS2022_0648 |
| De Visscher, I. | FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES | ICAS2022_0958 |
| De Wit, D. | CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM | ICAS2022_0606 |
| Debschütz, L. | EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATION | ICAS2022_0467 |
| Deck, K. | MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN | ICAS2022_0602 |
| Decours, J. | EXTERNAL-INTERNAL AERODYNAMIC COUPLING ON A TURBOPROP ENGINE USING THE BODY-FORCE METHOD | ICAS2022_0286 |
| Dedoussi, I. | MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN | ICAS2022_0602 |
| Defoort, S. | MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS | ICAS2022_0546 |
| Del Buono, A. | ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODY | ICAS2022_0385 |
| Delage, M. | ZERO-EMISSION REGIONAL AVIATION IN SWEDEN | ICAS2022_0650 |
| Delavenne, M. | AIRCRAFT FLEET MODELS USING A BOTTOM-UP APPROACH FOR SIMULATING AVIATION TECHNOLOGICAL PROSPECTIVE SCENARIOS | ICAS2022_0117 |
| Delbecq, S. | SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES | ICAS2022_0084 |
| Delbecq, S. | AIRCRAFT FLEET MODELS USING A BOTTOM-UP APPROACH FOR SIMULATING AVIATION TECHNOLOGICAL PROSPECTIVE SCENARIOS | ICAS2022_0117 |
| Delbecq, S. | A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONS | ICAS2022_0383 |
| Delbecq, S. | A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS | ICAS2022_0568 |
| Dell'Amico, A. | MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIES | ICAS2022_0575 |
| Dell'Amico, A. | AN EVALUATION METHOD FOR AIRCRAFT ACTUATION SYSTEMS OPERATIONAL COST | ICAS2022_0601 |
| Della Vecchia, P. | REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION | ICAS2022_0323 |
| Della Vecchia, P. | CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT | ICAS2022_0350 |
| Dell´Amico, A. | A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL | ICAS2022_0513 |
| Delmotte, H. | DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING | ICAS2022_0447 |
| Deng, J. | RESEARCH ON CROSSTALK CHARACTERISTICS OF AIRCRAFT ELECTRICAL CABLE | ICAS2022_0503 |
| Deng, S. | NUMERICAL INVESTIGATION ON THE AERO-PROPULSION EFFECT OF DISTRIBUTED PROPULSION FOR V/VTOL APPLICATION | ICAS2022_0674 |
| Denham, C.L. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Derra, M. | CONSIDERATIONS FOR MULTI-CRITERIA ROUTE DESIGN ON DIFFERENT ATMOSPHERIC SCALES | ICAS2022_0844 |
| Desgaches, D. | USE OF FRICTION STIR WELDING ON PRIMARY STRUCTURES OF AIRCRAFTS INSTEAD OF RIVETED JUNCTION | ICAS2022_0005 |
| Desmet, M. | CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM | ICAS2022_0606 |
| Dessena, G. | GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMP | ICAS2022_0644 |
| Deveerasetty, K.K. | CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H-INFINITY STRUCTURE WITH GWO | ICAS2022_0428 |
| Dever, T.P. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Devta, A. | EVALUATION AND QUANTIFICATION OF THE POTENTIAL CONSEQUENCES OF BIRD STRIKES IN URBAN AIR MOBILITY | ICAS2022_0629 |
| Dhake, M. | TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHOD | ICAS2022_0630 |
| Di Fabbio, T. | INVESTIGATION OF LEADING-EDGE VORTICES ON A TRIPLE-DELTA-WING CONFIGURATION USING SCALE-ADAPTIVE SIMULATION | ICAS2022_0528 |
| Di Mauro, G. | MECHANICAL CHARACTERIZATION OF A COMPOSITE STRUCTURAL BATTERY LAMINATE | ICAS2022_0690 |
| Di Stasio, M. | MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFT | ICAS2022_0649 |
| Di Vito, V. | A METHOD FOR EVALUATING AIRCRAFT DEPENDENCIES USING THE CLOSEST POINT OF APPROACH METHODOLOGY TO SUPPORT ATM OPERATIONS | ICAS2022_0798 |
| Diao, C. | MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING | ICAS2022_0176 |
| Dias, P.M. | A GENERALISED MULTI-OBJECTIVE ISLAND MODEL FOR FLIGHT CONTROL SYSTEM CLEARANCES | ICAS2022_0275 |
| Dickey, E.D. | TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATION | ICAS2022_0397 |
| Dietl, T. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Dietmüller, S. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Diette, C. | TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINE | ICAS2022_0006 |
| Diette, C. | OPEN FAN ENGINE ARCHITECTURE FOR NEXT GENERATION SMR | ICAS2022_0925 |
| Dilonardo, G. | CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL | ICAS2022_0341 |
| Ding, C. | RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAV | ICAS2022_0107 |
| Ding, J. | MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING | ICAS2022_0176 |
| Ding, S. | SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATION | ICAS2022_0386 |
| Ding, Y.-L. | A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT | ICAS2022_0584 |
| Ding, M. | OPTIMIZATION OF AIRCRAFT FLIGHT PATHS CONSIDERING THE CONFLICTING PARAMETERS OF ECONOMY AND SAFETY | ICAS2022_0652 |
| Diskin, A. | TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATION | ICAS2022_0036 |
| Docter, J. | CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM | ICAS2022_0606 |
| Doherty, J.J. | WALL INTERFERENCE CORRECTIONS USING NONLINEAR LEAST-SQUARES OPTIMISATION | ICAS2022_0378 |
| Donelli, G. | A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK | ICAS2022_0618 |
| Dong, W. | EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF COMPOSITE SHIELD ON THE ELECTROTHERMAL ANTI-ICING SYSTEMS | ICAS2022_0537 |
| dos Santos, F.L. | AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF THE NACA 0008 AIRFOIL | ICAS2022_0128 |
| Drego, A. | A SYSTEM INTEGRATOR’S PERSPECTIVE ON VEHICLE SYSTEM EVALUATION AT THE AIRCRAFT CONCEPT STAGE | ICAS2022_0856 |
| Du, Q. | DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK | ICAS2022_0032 |
| Du, W. | RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHP | ICAS2022_0200 |
| Du, K. | NUMERICAL SIMULATION ANALYSIS OF INFRARED RADIATION AND ELECTROMAGNETIC SCATTERING CHARACTERISTICS OF DIFFERENT MIXERS | ICAS2022_0223 |
| Du, H. | ELECTROMAGNETIC INTERFERENCE SHIELDING EFFECTIVENESS OF THE THIN CARBON NANOFIBERS/ SILICON CARBIDE FABRICS COMPOSITES | ICAS2022_0608 |
| Du, W. | DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATION | ICAS2022_0753 |
| Du, X.-B. | EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECK | ICAS2022_0847 |
| Dubois, S. | CLEAN SKY 2 PROGRAMME OVERVIEW | ICAS2022_0923 |
| Duval, M.N. | DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK | ICAS2022_0677 |
| Dziubinski, A. | THE USE OF COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A NEW GENERATION LIGHT COMBAT AIRPLANE | ICAS2022_0371 |
| Dziugiel, B. | AN INTERNATIONAL RESEARCH PERSPECTIVE ON AIRSPACE INTEGRATION IN THE FRAMEWORK OF URBAN AIR MOBILITY | ICAS2022_0948 |
| Döll, C. | HANDLING QUALITIES OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2022_0174 |
| Eek, M. | MODEL FIDELITY AND ITS INFLUENCE ON AIRCRAFT CONCEPTUAL DESIGN | ICAS2022_0477 |
| Effing, T. | COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN | ICAS2022_0149 |
| Eguea, J.P. | EXPERIMENTAL STUDIES ON THE INTERACTION BETWEEN PROPELLERS AND WING | ICAS2022_0262 |
| Eguea, J.P. | EXPERIMENTAL INVESTIGATION OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTION | ICAS2022_0431 |
| Eguea, J.P. | PUSHER PROPELLER INFLUENCE ON A LAMINAR WING TRANSITION LOCATION USING INFRARED THERMOGRAPHY | ICAS2022_0678 |
| Ehlers, T. | ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITY | ICAS2022_0233 |
| Ehlers, T. | CONSIDERATIONS FOR MULTI-CRITERIA ROUTE DESIGN ON DIFFERENT ATMOSPHERIC SCALES | ICAS2022_0844 |
| Eimer, E. | MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING | ICAS2022_0176 |
| Eitelberg, G. | RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERS | ICAS2022_0489 |
| Ekman, M. | TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS | ICAS2022_0604 |
| El Fazani, H. | FATIGUE CRACK PROPAGATION IN ADDITIVELY MANUFACTURED POLYMER PARTS | ICAS2022_0777 |
| El-Jabi, R. | NEW GENERATION SPACE VEHICLE OPERATIONS IN THE UNITED ARAB EMIRATES – AN AIRSPACE AND RISK ASSESSMENT | ICAS2022_0698 |
| Elfarra, M. | NUMERICAL INVESTIGATION OF ROTORCRAFT PRESSURE ERROR CORRECTION BY UTILIZATION OF AIR DAMS | ICAS2022_0357 |
| Elger, G. | IMAGE SEGMENTATION BASED EMERGENCY LANDING FOR AUTONOMOUS AND AUTOMATED UNMANNED AERIAL VEHICLES | ICAS2022_0725 |
| Elham, A. | A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTS | ICAS2022_0850 |
| Eliasson, P. | IMPROVING STALL CHARACTERISTICS OF UCAV WING WITH VORTEX GENERATORS | ICAS2022_0238 |
| Eliasson, P. | ENHANCING CFD PREDICTIONS FOR THE GRIPEN AIRCRAFT | ICAS2022_0242 |
| Eliasson, P. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Ellbrant, L. | STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT | ICAS2022_0480 |
| Eltgen, J. | TECHNICAL CONCEPTS FOR INSPECTING UAVS FOR DAMAGE | ICAS2022_0047 |
| Emeneth, M. | REGIONAL TRANSPORT AIRCRAFT DESIGN USING TURBO-ELECTRIC DISTRIBUTED PROPULSION (TEDIP) SYSTEM | ICAS2022_0609 |
| Emeneth, M. | UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENT | ICAS2022_0659 |
| Emori, K. | EXPERIMENTAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS OF DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATOR | ICAS2022_0877 |
| Enea, G. | TRAJECTORY-BASED OPERATIONS TO IMPROVE LONG-RANGE AIR TRAFFIC FLOW MANAGEMENT | ICAS2022_0087 |
| Enes, M.E.A. | A FAULT INTEGRATOR BASED VOTE&MONITOR DESIGN FOR GRACEFULL DEGRADATION IN MULTIPLE REDUNDANT SAFETY CRITICAL SYSTEMS | ICAS2022_0472 |
| Errico, A. | A METHOD FOR EVALUATING AIRCRAFT DEPENDENCIES USING THE CLOSEST POINT OF APPROACH METHODOLOGY TO SUPPORT ATM OPERATIONS | ICAS2022_0798 |
| Eschmann, C. | INTERNATIONAL SCIENTIFIC ASSESSMENT ON URBAN AIR MOBILITY AS A CONTRIBUTION TO FUTURE AVIATION STANDARDS | ICAS2022_0949 |
| Esposito, A. | A NEW FACILITY FOR HYPERSONIC FLOW SIMULATION DRIVEN BY A HIGH VELOCITY OXYGEN FUEL GUN | ICAS2022_0437 |
| Esposto, D. | NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITCH ANGLE | ICAS2022_0355 |
| Eto, R. | DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES | ICAS2022_0448 |
| Everaert, B. | CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM | ICAS2022_0606 |
| Fabianek, C. | AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTS | ICAS2022_0693 |
| Fan, L. | EXPERIMENTAL INVESTIGATION ON TRANSPORT AIRPLANE LONGITUDINAL STABILITY ENHANCEMENT IN CRITICAL ICING CONDITION | ICAS2022_0270 |
| Fan, J.-Z. | EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECK | ICAS2022_0847 |
| Fanteria, D. | FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES | ICAS2022_0692 |
| Faúndez Alarcón, J.M. | REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER | ICAS2022_0605 |
| Fay, A. | INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGION | ICAS2022_0840 |
| Fayez, K. | A STUDY OF HIGH-LIFT DEVICES FOR LOW REYNOLDS NUMBER APPLICATIONS | ICAS2022_0312 |
| Felgueroso, A. | NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINES | ICAS2022_0224 |
| Felux, M. | LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEM | ICAS2022_0144 |
| Feng, S. | EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING | ICAS2022_0078 |
| Feng, D. | STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATOR | ICAS2022_0313 |
| Feng, S. | FREE FLIGHT TEST IN HORIZONTAL WIND TUNNEL WITH POWERED AIRCRAFT | ICAS2022_0423 |
| Feng, S. | DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACE | ICAS2022_0785 |
| Fernandes, V.P. | PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING | ICAS2022_0694 |
| Fernberg, P. | FATIGUE DAMAGE MODEL OF HIGH TEMPERATURE POLYMER COMPOSITES IN AERO-ENGINES | ICAS2022_0831 |
| Ferrari, S. | DESIGNING SUSTAINABLE AVIATION SOLUTIONS WITH DIGITAL TWIN APPROACH | ICAS2022_0967 |
| Ferreira, L.P.S. | DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES USING NEURAL NETWORKS AND HYBRID DATA | ICAS2022_0705 |
| Ferreto, D. | MATHEMATICAL MODELLING AND ANALYSIS OF THERMAL MANAGEMENT SYSTEM ARCHITECTURE FOR HYPERSONIC AIRCRAFT | ICAS2022_0730 |
| Ferretto, D. | COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION | ICAS2022_0342 |
| Ferretto, D. | HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS | ICAS2022_0572 |
| Ferro, M. | LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP | ICAS2022_0869 |
| Feuerle, T. | FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES | ICAS2022_0958 |
| Feurich, P. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Fezans, N. | LANDING SIMULATION OF A HIGH-ALTITUDE PLATFORM WITH SKID-TYPE LANDING GEAR – FLIGHT PROCEDURE, CONTROLLER, AND LOADS | ICAS2022_0364 |
| Fezans, N. | COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACS | ICAS2022_0505 |
| Fezans, N. | EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERS | ICAS2022_0656 |
| Fidkowski, K.J. | DATA-DRIVEN ADAPTATION AND OPTIMIZATION OF TURBULENT FLOWS | ICAS2022_0914 |
| Figat, M. | PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLE | ICAS2022_0395 |
| Filho, A.J.D. | USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION | ICAS2022_0389 |
| Filippatos, A. | INVESTIGATION ON INTEGRATING RECYCLABILITY AS A FUNCTION AT THE DESIGN PHASE OF COMPLEX-LOADED STRUCTURAL COMPONENTS | ICAS2022_0125 |
| Filippi, M. | NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF UNSTIFFENED AND STIFFENED STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGS | ICAS2022_0220 |
| Finck, T. | DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORS | ICAS2022_0264 |
| Finzi Neto, R.M. | LATERAL-DIRECTIONAL AERODYNAMIC MODELLING FOR NUMERICAL RESULTS USING NEURO-FUZZY WITH DIFFERENTIAL EVOLUTION | ICAS2022_0870 |
| Fioriti, M. | REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION | ICAS2022_0323 |
| Fioriti, M. | METHODOLOGY FOR THE AUTOMATED PRELIMINARY CERTIFICATION OF ON-BOARD SYSTEMS ARCHITECTURES THROUGH REQUIREMENTS ANALYSIS | ICAS2022_0327 |
| Fioriti, M. | CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT | ICAS2022_0350 |
| Fischer, M. | FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION | ICAS2022_0708 |
| Fischer, O.J.P. | ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH | ICAS2022_0817 |
| Fischer, C. | IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTING | ICAS2022_0873 |
| Fitzgerald, L.K. | A STATIC STABILITY COMPARISON OF WIND TUNNEL AND COMPUTATIONAL FLUID DYNAMICS METHODS | ICAS2022_0384 |
| Flassig, P. | ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISK | ICAS2022_0532 |
| Flores-Peńa, P. | ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORA | ICAS2022_0699 |
| Fonseca, G.C. | NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL | ICAS2022_0059 |
| Fonte, F. | DESIGN OF AN INNOVATIVE WING TIP FOR AEROELASTIC CONTROL: FROM SCRATCH TO FLIGHT TEST | ICAS2022_0436 |
| Fornaseri, F. | “CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION | ICAS2022_0345 |
| Forsberg, H. | A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCE | ICAS2022_0332 |
| Forsyth, P. | NUMERICAL SIMULATION OF ICE ACCRETION ON A PITOT TUBE | ICAS2022_0130 |
| Forte, M. | STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE | ICAS2022_0583 |
| Fouda, M. | AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0593 |
| Francois, C. | OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACT | ICAS2022_0843 |
| Franke, F. | A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONS | ICAS2022_0030 |
| Freitas, A.C.S. | DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY | ICAS2022_0662 |
| Frezet, A. | TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINE | ICAS2022_0006 |
| Fridh, J. | IDENTIFICATION OF CRITICAL ACOUSTIC MODES FOR AN OPEN BOX CAVITY WITH ADJUSTABLE DEPTH | ICAS2022_0696 |
| Frigerio, L. | DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELS | ICAS2022_0648 |
| Frulla, G. | NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMS | ICAS2022_0396 |
| Fröhler, B. | IMPACT OF THE NUMBER OF WING STATIONS ON THE TWIST DISTRIBUTION OF A BWB CONCEPTUAL AIRCRAFT DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTION | ICAS2022_0854 |
| Fu, J. | AN INVESTIGATION ON THE IMPROVEMENT FOR TANDEM WING PITCHING MOMENT CHARACTERISTICS | ICAS2022_0050 |
| Fu, J.-C. | DESIGN AND EFFICIENCY ANALYSIS OF EVTOL CONTRA-ROTATING PROPELER | ICAS2022_0060 |
| Fu, J.-C. | RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAV | ICAS2022_0107 |
| Fuchs, M. | VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERING | ICAS2022_0063 |
| Fujii, K. | AIR TRAFFIC SIMULATION ACROSS FIR IN JAPAN USING CELLULAR AUTOMATON | ICAS2022_0401 |
| Fujii, K. | OPTIMIZATION OF AIRCRAFT FLIGHT PATHS CONSIDERING THE CONFLICTING PARAMETERS OF ECONOMY AND SAFETY | ICAS2022_0652 |
| Fukumine, Y. | ESTIMATION OF EVTOL FLIGHT PERFORMANCE USING ROTORCRAFT THEORY | ICAS2022_0408 |
| Funk, P. | GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS | ICAS2022_0265 |
| Funk, P. | USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION | ICAS2022_0389 |
| Fureby, C. | LARGE EDDY SIMULATION OF RAMJET TO SCRAMJET TRANSITION | ICAS2022_0188 |
| Fureby, C. | LES OF COMBUSTION DYNAMICS IN AN ETHYLENE-HYDROGEN-AIR RAMJET | ICAS2022_0786 |
| Furfari, D. | FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES | ICAS2022_0692 |
| Furse, G. | VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA | ICAS2022_0124 |
| Fusaro, R. | COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION | ICAS2022_0342 |
| Fusaro, R. | LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES | ICAS2022_0498 |
| Fusaro, R. | HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS | ICAS2022_0572 |
| Fusaro, R. | AERODATABASE DEVELOPMENT AND INTEGRATION OF SUPERSONIC/HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROJECT | ICAS2022_0596 |
| Fästh, O. | INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATION | ICAS2022_0245 |
| Gabard, G. | STUDY OF THE IMPACT OF AZIMUTHAL FLOW DISTORTION ON IN-DUCT ACOUSTIC PROPAGATION USING A MULTIMODAL FORMULATION | ICAS2022_0666 |
| Gaitanis, A.D. | MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENT | ICAS2022_0943 |
| Galletti, A. | NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITCH ANGLE | ICAS2022_0355 |
| Galuppi, F. | V/A-R AIR GESTURES HMI INTERACTION IN AIRPORT CONTROL TOWERS | ICAS2022_0452 |
| Galvanetto, U. | DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU) | ICAS2022_0295 |
| Gan, C. | SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATION | ICAS2022_0386 |
| Gangoli Rao, A. | INSTALLATION PENALTY OF AERO-ENGINES ON NARROW BODY AIRCRAFT | ICAS2022_0246 |
| Gangoli Rao, A. | DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFT | ICAS2022_0622 |
| Gao, X. | NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR | ICAS2022_0165 |
| Gao, C.-H. | A NUMERICAL METHOD FOR STUDY ON THE AERO-ELASTICITY OF AIR-TO-AIR MISSILES IN OVER-THE-SHOULDER LAUNCH | ICAS2022_0311 |
| Gao, C.-H. | HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACK | ICAS2022_0555 |
| Gao, F. | ANALYSIS OF THE AERODYNAMIC CHARACTERISTICS AND ITS INFLUENCE OF TURBOMACHINERY IN TRANSITION STATE | ICAS2022_0603 |
| Garcia Crespillo, O. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| García-Tíscar, J. | NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINES | ICAS2022_0224 |
| Gardner, R. | UK-AEROSPACE RESEARCH CONSORTIUM - EXPANDING THE VALUE OF UK ACADEMIC RESEARCH | ICAS2022_0306 |
| Gardner, R. | MAXIMISING VALUE FROM UK ACADEMIC RESEARCH - THE UK-AEROSPACE RESEARCH CONSORTIUM THEME APPROACH | ICAS2022_0838 |
| Gardonio, P. | DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU) | ICAS2022_0295 |
| Garkun, A. | TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATION | ICAS2022_0036 |
| Garry, K.P. | EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILTROTOR AIRCRAFT | ICAS2022_0530 |
| Gastaldo, G. | STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS | ICAS2022_0151 |
| Gastaldo, G. | PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES | ICAS2022_0289 |
| Gatlin, G.M. | TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATION | ICAS2022_0397 |
| Gauci, J. | AN ENGINELESS TAXI OPERATIONS SYSTEM USING BATTERY-OPERATED AUTONOMOUS TOW TRUCKS | ICAS2022_0783 |
| Gauvrit-Ledogar, J. | FLIGHT EXPERIMENTS FOR THE ALTAIR SEMI-REUSABLE AIR-LAUNCH SYSTEM WITH THE DEMONSTRATOR EOLE | ICAS2022_0541 |
| Gauvrit-Ledogar, J. | MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS | ICAS2022_0546 |
| Gavel, H. | MODEL FIDELITY AND ITS INFLUENCE ON AIRCRAFT CONCEPTUAL DESIGN | ICAS2022_0477 |
| Ge, C.H. | NUMERICAL STUDY ON WATER DISPLACEMENT DRAG CHARACTERISTICS OF AIRCRAFT ELASTIC TIRE ON CONTAMINATED RUNWAYS | ICAS2022_0329 |
| Gehri, A. | USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC PERFORMANCE OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFT | ICAS2022_0251 |
| Geister, D. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Gelain, M. | NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINES | ICAS2022_0224 |
| Gemma, R. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Genito, N. | VALIDATION OF SCALED FLIGHT TESTING | ICAS2022_0375 |
| Genrup, M. | ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR | ICAS2022_0382 |
| Genrup, M. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| Gerber, M. | IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT | ICAS2022_0627 |
| Gerbeth, D. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Gerdes, I. | THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION | ICAS2022_0268 |
| Gessner, M. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Ghelani, R. | A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFT | ICAS2022_0703 |
| Ghika, S. | WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE | ICAS2022_0215 |
| Giacomossi, L. | COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMS | ICAS2022_0340 |
| Gibertini, G. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Gibertini, G. | EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING THE WIND TUNNEL: HELICOPTER SHIP LANDING CASE | ICAS2022_0625 |
| Gierszewski, D. | REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT | ICAS2022_0797 |
| Gierszewski, D. | AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT | ICAS2022_0835 |
| Giese, K. | THE NEW RESEARCH AIRCRAFT ISTAR - EXPERIMENTAL FLIGHT CONTROL SYSTEM | ICAS2022_0439 |
| Gijsman, F. | INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD | ICAS2022_0653 |
| Girard, G. | FUTURE COMBAT AIR SYSTEMS: REQUIREMENTS AND TECHNOLOGIES | ICAS2022_0940 |
| Gkoutzamanis, V.G. | MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENT | ICAS2022_0943 |
| Glabeke, G. | WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAP | ICAS2022_0232 |
| Glodic, N. | STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALL | ICAS2022_0351 |
| Glodic, N. | AEROELASTIC TAILORING OF COMPRESSOR BLADES | ICAS2022_0507 |
| Glodic, N. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| God, R. | A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE | ICAS2022_0791 |
| Góes, L.C.S. | SYNTHETIC AIR DATA - A COMPARATIVE PRACTICAL STUDY | ICAS2022_0536 |
| Góes, L.C.S. | PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING | ICAS2022_0694 |
| Góes, L.C.S. | IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTING | ICAS2022_0873 |
| Góes, L.C.S. | OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM | ICAS2022_0891 |
| Goetz, C. | VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERING | ICAS2022_0063 |
| Goetzendorf-Grabowski , T. | PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLE | ICAS2022_0395 |
| Goetzendorf-Grabowski, T. | MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIES | ICAS2022_0462 |
| Goetzendorf-Grabowski, T. | OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANE | ICAS2022_0576 |
| Golan, O. | TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATION | ICAS2022_0036 |
| Gollnick, V. | CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACH | ICAS2022_0102 |
| Gollnick, V. | ASSESSMENT OF REAL-TIME DATA TRANSMISSION VIA AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC OCEANIC AIRSPACE | ICAS2022_0168 |
| Gollnick, V. | ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITY | ICAS2022_0233 |
| Gollnick, V. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Gollnick, V. | INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGION | ICAS2022_0840 |
| Gomez-Escalonilla, J. | TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES | ICAS2022_0012 |
| Gong, R. | INTEGRATE ONLINE QUERY&DEFENSE INTO PROJECT BASED LEARNING TO PROMPT ENGINEERING AUTHENTIC EXPERIENCES | ICAS2022_0284 |
| Gonschorek, J. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| González, P.J. | DESIGN OF STABILITY AUGMENTATION SYSTEMS FOR A FLEXIBLE AIRCRAFT USING LQ OUTPUT-FEEDBACK CONTROL VIA LMI | ICAS2022_0623 |
| González, P.J. | TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONS | ICAS2022_0657 |
| González, P.J. | LPV/LFR CONTROL FOR ACTIVE FLUTTER SUPPRESSION OF A SMART AIRFOIL MODEL | ICAS2022_0816 |
| González, P.J. | A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR | ICAS2022_0826 |
| González Lozano, B. | NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCT | ICAS2022_0236 |
| Gorgues, A. | AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGS | ICAS2022_0020 |
| Gori, O. | SIMPLIFIED MODELS FOR THE PRELIMINARY AERODYNAMIC CHARACTERIZATION OF HIGH-SPEED VEHICLES TO SUPPORT MISSION ANALYSIS | ICAS2022_0551 |
| Gori, O. | HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS | ICAS2022_0572 |
| Gowree, E. | STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE | ICAS2022_0583 |
| Gowree, E.R. | UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLS | ICAS2022_0611 |
| Gowree, E.R. | STABILITY OF A LAMINAR BOUNDARY LAYER OVER LOCALISED SURFACE INDENTATION | ICAS2022_0697 |
| Graves, R. | CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIES | ICAS2022_0934 |
| Gray, I. | UK-AEROSPACE RESEARCH CONSORTIUM - EXPANDING THE VALUE OF UK ACADEMIC RESEARCH | ICAS2022_0306 |
| Gray, A.L. | A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATION TO THE STRUT-BRACED-WING AND HYBRID-WING-BODY CONFIGURATIONS | ICAS2022_0748 |
| Gray, A.C. | TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATION | ICAS2022_0905 |
| Graziani, S. | LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES | ICAS2022_0498 |
| Gregg, R. | TOWARDS CERTIFICATION BY ANALYSIS FOR FLIGHT CHARACTERISTICS | ICAS2022_0956 |
| Grendene, S. | STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES | ICAS2022_0336 |
| Grendysa, W. | A NEW APPROACH TO SHAPING THE PUSHROD TUBE AS THE MAIN COMPONENT OF THE CONTROL SYSTEM, OPTIMIZATION, AND MANUFACTURING TECHNOLOGY. | ICAS2022_0616 |
| Grewe, V. | MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN | ICAS2022_0602 |
| Griffin, P.C. | A STATIC STABILITY COMPARISON OF WIND TUNNEL AND COMPUTATIONAL FLUID DYNAMICS METHODS | ICAS2022_0384 |
| Grimaldi, G. | DEVELOPMENT OF A CONCEPTUAL DESIGN TOOL TO PREDICT PERFORMANCE OF HYDROGEN FUELLED PRECOOLED AIRBREATHING ROCKET ENGINES | ICAS2022_0152 |
| Grimme, W. | DESIGN AND ECO-EFFICIENCY ASSESSMENT OF A PEOPLE-MOVER AIRCRAFT IN COMPARISON TO STATE-OF-THE-ART NARROW BODY AIRCRAFT | ICAS2022_0304 |
| Gringinger, E. | AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTS | ICAS2022_0693 |
| Groot Koerkamp, L.H. | INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD | ICAS2022_0653 |
| Grundström, M. | DESIGNING SUSTAINABLE AVIATION SOLUTIONS WITH DIGITAL TWIN APPROACH | ICAS2022_0967 |
| Gryazev, V. | APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS | ICAS2022_0643 |
| Grün, G. | USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM | ICAS2022_0116 |
| Grünewald, M. | CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACH | ICAS2022_0102 |
| Grönstedt, T. | LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTION | ICAS2022_0088 |
| Grönstedt, T. | ENVIRONMENTAL ASSESSMENT OF NOISE ABATEMENT APPROACH TRAJECTORIES | ICAS2022_0671 |
| Grönstedt, T. | PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE | ICAS2022_0782 |
| Grönstedt, T. | SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045 | ICAS2022_0804 |
| Grönstedt, T. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| Gu, H. | LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPS | ICAS2022_0524 |
| Guagliardo, D. | NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITCH ANGLE | ICAS2022_0355 |
| Guarino, G. | TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHOD | ICAS2022_0427 |
| Guedes, M.J.M. | LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP | ICAS2022_0869 |
| Guenov, M.D. | SET-BASED DESIGN COORDINATION BETWEEN COUPLED SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVE | ICAS2022_0372 |
| Guerrero i Almirall, A. | ZONAL MODEL BASED AIRCRAFT PASSENGER THERMAL COMFORT COMPARATIVE STUDY | ICAS2022_0338 |
| Guglieri, G. | ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITION | ICAS2022_0085 |
| Guida, M. | MECHANICAL CHARACTERIZATION OF A COMPOSITE STRUCTURAL BATTERY LAMINATE | ICAS2022_0690 |
| Guiterrez Salas, M. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| Gulizzi, V. | TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHOD | ICAS2022_0427 |
| Gulizzi, V. | HIGH-ORDER ACCURATE EMBEDDED-BOUNDARY DISCONTINUOUS GALERKIN METHODS FOR INVISCID GAS DYNAMICS | ICAS2022_0735 |
| Guo, T. | EXPERIMENTAL INVESTIGATION ON TRANSPORT AIRPLANE LONGITUDINAL STABILITY ENHANCEMENT IN CRITICAL ICING CONDITION | ICAS2022_0270 |
| Guo, D. | DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIAL | ICAS2022_0290 |
| Guo, F. | MOTION STROKE DESIGN ON FLEXIBLE ASSEMBLY TOOLING FOR MULTIPLE AIRCRAFT COMPONENTS | ICAS2022_0314 |
| Guo, X. | EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF COMPOSITE SHIELD ON THE ELECTROTHERMAL ANTI-ICING SYSTEMS | ICAS2022_0537 |
| Guocheng, Z. | AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNEL | ICAS2022_0411 |
| Gupta, P. | CONCEPTUAL DESIGN AND SIZING FOR A FIXED WING UAV FOR EXPLORATION OVER MARS | ICAS2022_0210 |
| Gurtov, A. | A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATION | ICAS2022_0704 |
| Gustafsson, M. | GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS | ICAS2022_0265 |
| Gustafsson, B. | STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT | ICAS2022_0480 |
| Gutierrez Salas, M. | AEROELASTIC TAILORING OF COMPRESSOR BLADES | ICAS2022_0507 |
| Gürlük, H. | THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION | ICAS2022_0268 |
| Görtz, A. | THERMODYNAMIC POTENTIAL OF TURBOFAN ENGINES WITH DIRECT COMBUSTION OF HYDROGEN | ICAS2022_0499 |
| Görtz, S. | APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT | ICAS2022_0892 |
| Hackbarth, H. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Hackenberg, D.L. | INTERNATIONAL SCIENTIFIC ASSESSMENT ON URBAN AIR MOBILITY AS A CONTRIBUTION TO FUTURE AVIATION STANDARDS | ICAS2022_0949 |
| Hackström, M. | AERODYNAMIC DEVELOPMENT OF SAAB FCAS UNMANNED SUPERSONIC COMBAT AIRCRAFT | ICAS2022_0570 |
| Hagemann, S. | ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITY | ICAS2022_0233 |
| Hagström, M. | THE GROUP OF RESPONSABLES "FLIGHT MECHANICS, SYSTEMS AND INTEGRATION (GOR FM)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0912 |
| Hahn, S.H. | GENERATION OF TERRAIN PROFILE FOR TERRAIN FOLLOWING | ICAS2022_0538 |
| Haldar, D. | IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIES | ICAS2022_0334 |
| Haldar, D. | MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACT | ICAS2022_0369 |
| Halila, G.L.O. | A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTS | ICAS2022_0672 |
| Hallander, P. | SMART SKIN FOR AEW AIRCRAFT | ICAS2022_0048 |
| Hammer, S. | IDENTIFICATION OF CRITICAL ACOUSTIC MODES FOR AN OPEN BOX CAVITY WITH ADJUSTABLE DEPTH | ICAS2022_0696 |
| Han, Y.-J. | DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLE | ICAS2022_0108 |
| Han, J.-H. | DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLE | ICAS2022_0108 |
| Han, Y.-J. | OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNING | ICAS2022_0109 |
| Han, J.-H. | OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNING | ICAS2022_0109 |
| Han, J.-S. | WIND-TUNNEL TEST ON LEADING-EDGE VORTEX OF LOW-ASPECT-RATIO FLAPPING PLATES | ICAS2022_0154 |
| Han, S.-Q. | A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEME | ICAS2022_0157 |
| Han, Z.-H. | A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEME | ICAS2022_0157 |
| Han, S.-Q. | A NUMERICAL METHOD FOR STUDY ON THE AERO-ELASTICITY OF AIR-TO-AIR MISSILES IN OVER-THE-SHOULDER LAUNCH | ICAS2022_0311 |
| Han, Z.-H. | UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODEL | ICAS2022_0330 |
| Han, S. | NUMERICAL PREDICTION OF FOCUS BOOM GENERATED BY MANEUVERS | ICAS2022_0410 |
| Han, S. | IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT | ICAS2022_0421 |
| Han, Z.-H. | EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTOR GENERATION | ICAS2022_0548 |
| Han, S.-Q. | HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACK | ICAS2022_0555 |
| Han, Z.-H. | HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACK | ICAS2022_0555 |
| Han, Z.-H. | A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT | ICAS2022_0584 |
| Hanak, J. | PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELS | ICAS2022_0721 |
| Handal-Rivera, C.D. | DESIGN OF AN ADVANCED EMPENNAGE AND REAR FUSELAGE CONCEPT FOR A COMMERCIAL AIRCRAFT | ICAS2022_0227 |
| Handojo, V. | LOADS ANALYSIS AND STRUCTURAL OPTIMIZATION OF A LONG-RANGE TRANSPORT CONFIGURATION WITH HYBRID LAMINAR FLOW CONTROL | ICAS2022_0158 |
| Handojo, V. | XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEM | ICAS2022_0228 |
| Hang, H.-Y. | RESEARCH ON THE EFFECT OF THE PROCESS FIRST SHOT PEENING STRENGTHENING THEN SHOT PEENING FORMING ON FATIGUE STRENGTH OF 7050 HIGH-STRENGTH ALUMINUM ALLOY | ICAS2022_0316 |
| Hanifi, A. | PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFT | ICAS2022_0126 |
| Hanifi, A. | ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND DISTURBANCE LEVELS | ICAS2022_0571 |
| Hanifi, A. | REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER | ICAS2022_0605 |
| Hanifi, A. | ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATION | ICAS2022_0635 |
| Hanifi, A. | DIRECT NUMERICAL SIMULATIONS OF A THICK, ROTATING AIRFOIL AT A LOW REYNOLDS NUMBER | ICAS2022_0680 |
| Hanisch, L.V. | A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTS | ICAS2022_0850 |
| Hao, C. | NUMERICAL INVESTIGATION ON TURBINE SHROUD FILM COOLING HEAT TRANSFER PERFORMANCE OF TURBINE BLADE WITH GROOVE TIP | ICAS2022_0203 |
| Harada, A. | CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H-INFINITY STRUCTURE WITH GWO | ICAS2022_0428 |
| Harada, M. | STUDY ON THE APPLICATION OF EMULSIFIED FUEL IN SMALL JET ENGINES | ICAS2022_0751 |
| Harada, M. | EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENT | ICAS2022_0756 |
| Hardell, H. | PERFORMANCE EVALUATION OF THE ARRIVAL OPERATIONS IN TERMINAL AREA | ICAS2022_0825 |
| Harey, C. | DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURES | ICAS2022_0734 |
| Hariansyah, M.A. | DEEP LEARNING TECHNIQUES FOR HIGH-DIMENSIONAL SURROGATE-BASED AERODYNAMIC DESIGN | ICAS2022_0187 |
| Harrison, N.A. | TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATION | ICAS2022_0397 |
| Harrison, E.D. | A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT | ICAS2022_0453 |
| Harrison, N.A. | MDAO OF A TRANSONIC TRUSS-BRACED WING VISION VEHICLE | ICAS2022_0807 |
| Hartl, P. | EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS | ICAS2022_0250 |
| Hartman, S.A. | INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD | ICAS2022_0653 |
| Hartmann, J. | ELIMINATING CLIMATE IMPACT FROM AVIATION – REVIEW OF PROMISING AIRCRAFT CONCEPTS AND ENABLING TECHNOLOGY BRICKS | ICAS2022_0716 |
| Hasan, Y.J. | LANDING SIMULATION OF A HIGH-ALTITUDE PLATFORM WITH SKID-TYPE LANDING GEAR – FLIGHT PROCEDURE, CONTROLLER, AND LOADS | ICAS2022_0364 |
| Hatamoto, A. | EXPERIMENTAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS OF DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATOR | ICAS2022_0877 |
| Hausmann, P. | IMAGE SEGMENTATION BASED EMERGENCY LANDING FOR AUTONOMOUS AND AUTOMATED UNMANNED AERIAL VEHICLES | ICAS2022_0725 |
| Hayböck, S. | EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS | ICAS2022_0250 |
| He, P. | AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS | ICAS2022_0560 |
| He, Y.-B. | EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECK | ICAS2022_0847 |
| Healy, F. | LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPS | ICAS2022_0524 |
| Heberle, G. | EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMAS | ICAS2022_0526 |
| Hecker, P. | FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES | ICAS2022_0958 |
| Heersema, N. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Hegde, A. | INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT | ICAS2022_0326 |
| Heger, R. | THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0917 |
| Heidebrecht, A. | DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFT | ICAS2022_0622 |
| Heiets, I. | DOOR-TO-DOOR TRAVEL PLANNER FOR IMPROVED TRAVELER EXPERIENCE USING DIGITAL TWIN CONCEPT | ICAS2022_0011 |
| Helgesen, B. | FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE | ICAS2022_0028 |
| Henke, M. | A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTS | ICAS2022_0850 |
| Henne, U. | NUMERICAL AND EXPERIMENTAL INVESTIGATIONS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODEL | ICAS2022_0720 |
| Henningson, D. | AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES | ICAS2022_0104 |
| Henningson, D.S. | ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND DISTURBANCE LEVELS | ICAS2022_0571 |
| Henningson, D.S. | REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER | ICAS2022_0605 |
| Henningson, D.S. | ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATION | ICAS2022_0635 |
| Henningson, D. | DIRECT NUMERICAL SIMULATIONS OF A THICK, ROTATING AIRFOIL AT A LOW REYNOLDS NUMBER | ICAS2022_0680 |
| Henningson, D. | AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 2 | ICAS2022_0946 |
| Hermetz, J. | FLIGHT EXPERIMENTS FOR THE ALTAIR SEMI-REUSABLE AIR-LAUNCH SYSTEM WITH THE DEMONSTRATOR EOLE | ICAS2022_0541 |
| Herrmann, U. | NOVEL PATHWAYS TO SUSTAINABLE AVIATION | ICAS2022_0688 |
| Herzog, E. | HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENT | ICAS2022_0434 |
| Hesse, C. | EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXT | ICAS2022_0254 |
| Hesse, J.-T. | PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONS | ICAS2022_0820 |
| Higasa, K. | ASSESSMENT AND CONTROL OF ARRIVAL FLOW AND WAITING TIME APPLYING GT/GI/ST+GI TIME-VARYING QUEUING MODEL | ICAS2022_0132 |
| Hillebrecht, A. | ASSESSMENT OF REAL-TIME DATA TRANSMISSION VIA AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC OCEANIC AIRSPACE | ICAS2022_0168 |
| Hillebrecht, A. | CLUSTER STRUCTURE AND GATEWAY AVAILABILITY OF AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC AIRSPACE | ICAS2022_0293 |
| Hiraiwa, H. | ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOW | ICAS2022_0476 |
| Hjorth, J. | A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCE | ICAS2022_0332 |
| Hoarau, Y. | USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC PERFORMANCE OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFT | ICAS2022_0251 |
| Hoeijmakers, H.W.M. | INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD | ICAS2022_0653 |
| Hokamoto, S. | ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOW | ICAS2022_0476 |
| Hokamoto, S. | INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCE | ICAS2022_0796 |
| Holmgren, E. | IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIES | ICAS2022_0334 |
| Holmgren, E. | MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACT | ICAS2022_0369 |
| Holzapfel, F. | REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT | ICAS2022_0797 |
| Holzapfel, F. | AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT | ICAS2022_0835 |
| Holzapfel, F. | EXTENSION OF THE CAPABILITIES OF AN AUTOMATIC LANDING SYSTEM WITH PROCEDURES MOTIVATED BY VISUAL-FLIGHT-RULES | ICAS2022_0841 |
| Homan, J. | FATIGUE OF NOTCHED STANDARD SPECIMENS – THE INFLUENCE OF THE STRESS GRADIENT ON THE S-N CURVE IN AL2024 | ICAS2022_0561 |
| Homola, J. | INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS | ICAS2022_0904 |
| Homola, J. | OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE | ICAS2022_0909 |
| Honda, S. | AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION | ICAS2022_0192 |
| Hong, H. | REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT | ICAS2022_0797 |
| Hoogreef, M.F.M. | INSTALLATION PENALTY OF AERO-ENGINES ON NARROW BODY AIRCRAFT | ICAS2022_0246 |
| Hoogreef, M.F.M. | SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART I: INITIAL DESIGNS | ICAS2022_0248 |
| Hoogreef, M.F.M. | SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART II: SENSITIVITY ANALYSIS | ICAS2022_0481 |
| Hoogreef, M. | DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFT | ICAS2022_0622 |
| Hopkins, S. | FUTURE COMBAT AIRCRAFT SYSTEM THE COMPLEXITY OF THE SKILLS EQUATION | ICAS2022_0901 |
| Horak, M. | TREND MONITORING OF TURBOPROP ENGINES | ICAS2022_0094 |
| Horinouchi, S. | CONCEPT DESIGN OF A LOW BOOM SSBJ TO SATISFY SOCIAL ACCEPTANCE | ICAS2022_0762 |
| Hornung, M. | THE INFLUENCE OF THE MODEL PARAMETERS OF LI-ION BATTERIES ON THE WIRING HARNESS PERFORMANCE OF EVTOL AIRCRAFT | ICAS2022_0113 |
| Hornung, M. | MORPHING FORWARD WING SECTION SKIN DESIGN FOR A SAILPLANE CONSIDERING WING BENDING | ICAS2022_0178 |
| Hornung, M. | COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAV | ICAS2022_0367 |
| Hornung, M. | SUCCESSIVE KNOWLEDGE BUILDUP AND TRANSFER DURING THE ANALYSIS OF SCALED UAV WINGS BY MEANS OF MACHINE LEARNING | ICAS2022_0521 |
| Hosseini, S. | WING LOADING PROCESS IN KNOWLEDGE-BASED AIRCRAFT DESIGN AND OPTIMIZATION FRAMEWORK | ICAS2022_0519 |
| Hou, P. | TASK ALLOCATION METHOD FOR COMPLEX RECONNAISSANCE AREA BY MULTIPLE UAVS | ICAS2022_0195 |
| Hua, Y. | DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION | ICAS2022_0143 |
| Huang, Y.-L. | RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHP | ICAS2022_0200 |
| Huang, D.-Q. | RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHP | ICAS2022_0200 |
| Huang, H.Y. | STUDY ON MECHANICAL PROPERTIES OF CARBON FIBER RESIN MATRIX COMPOSITE BOLTED JOINT STRUCTURE AT HIGH TEMPERATURE | ICAS2022_0278 |
| Huang, H.Y. | DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIAL | ICAS2022_0290 |
| Huang, W. | DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT | ICAS2022_0321 |
| Huang, Y. | INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCE | ICAS2022_0796 |
| Hueso-Rebassa, J. | OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELS | ICAS2022_0167 |
| Huete, J. | PROPULSION SYSTEM INTEGRATION FOR A FIRST GENERATION HYDROGEN CIVIL AIRLINER? | ICAS2022_0950 |
| Hunger, R. | THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION | ICAS2022_0268 |
| Hyde, L. | ARRIVING AT CERTIFIABLE NOVEL AIRLINER USING LIQUID HYDROGEN & EFFICIENCY METRICS | ICAS2022_0373 |
| Hühne, C. | A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONS | ICAS2022_0030 |
| Hällqvist, R. | HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENT | ICAS2022_0434 |
| Hällqvist, R. | MODEL FIDELITY AND ITS INFLUENCE ON AIRCRAFT CONCEPTUAL DESIGN | ICAS2022_0477 |
| Häßy, J. | KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND MASS ESTIMATION OF RUBBER AERO ENGINES | ICAS2022_0497 |
| Häßy, J. | IMPACT OF THE NUMBER OF WING STATIONS ON THE TWIST DISTRIBUTION OF A BWB CONCEPTUAL AIRCRAFT DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTION | ICAS2022_0854 |
| Hörnschemeyer, R. | VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIR | ICAS2022_0083 |
| Hörnschemeyer, R. | EXPERIMENTS TO INVESTIGATE LIFT PRODUCTION MECHANISMS ON OSCILLATING TRAILING-EDGE FLAPS | ICAS2022_0780 |
| Iafrati, A. | ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODY | ICAS2022_0385 |
| Ibron, C. | LES OF COMBUSTION DYNAMICS IN AN ETHYLENE-HYDROGEN-AIR RAMJET | ICAS2022_0786 |
| Ignatyev, D. | FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIES | ICAS2022_0520 |
| Ignatyev, D.I. | GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMP | ICAS2022_0644 |
| Ikeda, T. | WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) | ICAS2022_0814 |
| Ilic, C. | APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT | ICAS2022_0892 |
| Ilina, S. | TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINS | ICAS2022_0822 |
| Imamura, T. | UNSTEADY TURBULENT FLOW SIMULATION OF ROTOR BLADES ON MOVING CARTESIAN GRIDS USING RECURSIVE FITTING APPROACH | ICAS2022_0790 |
| Inal, T. | A FAULT INTEGRATOR BASED VOTE&MONITOR DESIGN FOR GRACEFULL DEGRADATION IN MULTIPLE REDUNDANT SAFETY CRITICAL SYSTEMS | ICAS2022_0472 |
| Inasawa, A. | EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETS | ICAS2022_0243 |
| Iovieno, M. | HEAT TRANSFER ENHANCEMENT BY SUSPENDED PARTICLES IN A TURBULENT SHEARLESS FLOW | ICAS2022_0711 |
| Ireland, C.J. | A GLOBAL APPROACH TO ASSESSING THE CLIMATE RESILIENCE OF AIRPORTS | ICAS2022_0922 |
| Isikveren, A.T. | DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFT | ICAS2022_0622 |
| Ispir, A.C. | HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS | ICAS2022_0572 |
| Itoh, E. | DEVELOPING A DEPARTURE QUEUE MODEL FOR INTEGRATED ARRIVAL AND DEPARTURE OPERATION OF RUNWAYS | ICAS2022_0106 |
| Itoh, E. | ASSESSMENT AND CONTROL OF ARRIVAL FLOW AND WAITING TIME APPLYING GT/GI/ST+GI TIME-VARYING QUEUING MODEL | ICAS2022_0132 |
| Itoh, E. | APPLYING MACHINE LEARNING TO TAXI-TIME PREDICTION ATTOKYO INTERNATIONAL AIRPORT | ICAS2022_0267 |
| Itoh, E. | MACHINE LEARNING METHODS ENSURING BOTH PERFORMANCE AND INTERPRETABILITY OF ESTIMATING AIRCRAFT ARRIVAL TIMES | ICAS2022_0271 |
| Itoh, E. | AIR TRAFFIC SIMULATION ACROSS FIR IN JAPAN USING CELLULAR AUTOMATON | ICAS2022_0401 |
| Itoh, E. | REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMIC | ICAS2022_0486 |
| Iuspa, L. | AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLES | ICAS2022_0241 |
| Iuspa, L. | AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE | ICAS2022_0259 |
| Ivchenko, M. | DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING | ICAS2022_0447 |
| Iwami, Y. | WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) | ICAS2022_0814 |
| Iwanizki, M. | IMPACT OF THE NUMBER OF WING STATIONS ON THE TWIST DISTRIBUTION OF A BWB CONCEPTUAL AIRCRAFT DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTION | ICAS2022_0854 |
| Iwata, D. | DEVELOPING A DEPARTURE QUEUE MODEL FOR INTEGRATED ARRIVAL AND DEPARTURE OPERATION OF RUNWAYS | ICAS2022_0106 |
| Izuka, J.H. | EXPERIMENTAL AND NUMERICAL ANALYSIS OF A PRE-STRESSED TENSEGRITY MEMBRANE | ICAS2022_0038 |
| Jacob, M.C. | UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLS | ICAS2022_0611 |
| Jacobson, M. | DEMONSTRATING AN APPROACH FOR MULTIDISCIPLINARY SET BASED DESIGN WITHIN AN AEROSPACE RESEARCH PROJECT - DEFAINE | ICAS2022_0661 |
| Jameel, M. | DEMAND PATTERN INFLUENCE ON RELATION OF TURNAROUND DURATION AND GATE OCCUPATION DEPENDING ON AVAILABLE RESOURCES | ICAS2022_0122 |
| Jameel, M. | THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION | ICAS2022_0268 |
| Jan, R. | PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY IMPLEMENTED UNDER ASWING | ICAS2022_0318 |
| Jang, Y.H. | EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV | ICAS2022_0488 |
| Jansen, R. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Jaroslawski, T. | STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE | ICAS2022_0583 |
| Jax, T. | POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORS | ICAS2022_0347 |
| Jeaong, H.J. | EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV | ICAS2022_0488 |
| Jentink, H. | VALIDATION OF SCALED FLIGHT TESTING | ICAS2022_0375 |
| Jentys, M.M. | TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WING | ICAS2022_0037 |
| Jesudasan, R. | PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFT | ICAS2022_0126 |
| Jesus, L.D. | USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION | ICAS2022_0389 |
| Jeyarai, A. | CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT | ICAS2022_0350 |
| Jeyaraj, A.K. | SYSTEMS ARCHITECTING: A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0 PROJECT | ICAS2022_0365 |
| Jézégou, J. | FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFT | ICAS2022_0214 |
| Jezegou, J. | OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN | ICAS2022_0550 |
| Ji, Z. | A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTH | ICAS2022_0142 |
| Ji, Z. | DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION | ICAS2022_0143 |
| Ji, H.-B. | RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE | ICAS2022_0510 |
| Jia, D.S. | AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK | ICAS2022_0199 |
| Jia, Q. | EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONE | ICAS2022_0256 |
| Jia, B.-B. | SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSOR | ICAS2022_0589 |
| Jia, X. | ELECTROMAGNETIC INTERFERENCE SHIELDING EFFECTIVENESS OF THE THIN CARBON NANOFIBERS/ SILICON CARBIDE FABRICS COMPOSITES | ICAS2022_0608 |
| Jiang, X. | STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGER | ICAS2022_0072 |
| Jiang, X. | EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONE | ICAS2022_0256 |
| Jiang, T. | MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0544 |
| Jiang, L.-Y. | SAND EROSION MODELING IN GENERIC COMPRESSOR RIG TESTING | ICAS2022_0945 |
| Jiao, Y. | INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNEL | ICAS2022_0547 |
| Jin, T. | EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING | ICAS2022_0632 |
| Jochims Lau, C. | A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENT | ICAS2022_0523 |
| Jochims Lau, C. | EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMAS | ICAS2022_0526 |
| Johann, S. | USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM | ICAS2022_0116 |
| Johansson, A. | IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIES | ICAS2022_0334 |
| Johansson, A. | MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACT | ICAS2022_0369 |
| Johansson, E. | FLIGHT DYNAMICS SIMULATION AND FCS AUTO-GENERATION IN THE CONCEPTUAL DESIGN PHASE OF AN UNSTABLE SUPERSONIC AIRCRAFT | ICAS2022_0458 |
| Johansson, P. | STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT | ICAS2022_0480 |
| Johansson, U. | STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT | ICAS2022_0480 |
| Johansson, A. | MORE ELECTRIC AIRPLANE: CASE STUDY STOCKHOLM - COPENHAGEN | ICAS2022_0506 |
| Johansson, B. | HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICS | ICAS2022_0707 |
| Johnson, M. | INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS | ICAS2022_0904 |
| Johnson, M. | OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE | ICAS2022_0909 |
| Jokinen, J. | FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHOD | ICAS2022_0754 |
| Joksimovic, A. | AIRCRAFT FLEET MODELS USING A BOTTOM-UP APPROACH FOR SIMULATING AVIATION TECHNOLOGICAL PROSPECTIVE SCENARIOS | ICAS2022_0117 |
| Joksimovic, A. | ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEM | ICAS2022_0368 |
| Jonsson, I. | NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCT | ICAS2022_0236 |
| Jonsson, I. | EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT | ICAS2022_0788 |
| Jonsson, I. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| Jordao, R. | TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS | ICAS2022_0604 |
| Josefsson, B. | STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATION | ICAS2022_0903 |
| Jouannet, C. | ZERO-EMISSION REGIONAL AVIATION IN SWEDEN | ICAS2022_0650 |
| Jouannet, C. | UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENT | ICAS2022_0659 |
| Jouannet, C. | SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045 | ICAS2022_0804 |
| Jouannet, C. | ICAS DIGITAL PIONEERING INITIATIVE AND SYSTEM OF SYSTEM CHALLENGES | ICAS2022_0964 |
| Jung, C.-G. | CONVEX PROGRAMMING-BASED OPTIMAL THREE-DIMENSIONAL MID-COURSE GUIDANCE WITH LOSSLESS CONVEXIFICATION | ICAS2022_0810 |
| Jung, Y. | META-REINFORCEMENT LEARNING-BASED FAULT TOLERANT CONTROL FOR A QUADROTOR WITH A SEVERE LOSS OF ROTOR | ICAS2022_0879 |
| Júnior, M.M.C. | DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY | ICAS2022_0662 |
| Juracka, J. | TREND MONITORING OF TURBOPROP ENGINES | ICAS2022_0094 |
| Justin, C.Y. | ZERO-EMISSION REGIONAL AVIATION IN SWEDEN | ICAS2022_0650 |
| Justin, C.Y. | REGIONAL AIR MOBILITY MARKET STUDY | ICAS2022_0872 |
| Jäger, M. | LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEM | ICAS2022_0144 |
| Kacik, D. | OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANE | ICAS2022_0576 |
| Kahlo, H. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Kai, J.-M. | A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS | ICAS2022_0568 |
| Kalfas, A.I. | MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENT | ICAS2022_0943 |
| Kalra, R. | ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORA | ICAS2022_0699 |
| Kanazaki, M. | AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION | ICAS2022_0413 |
| Kanerva, M. | FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHOD | ICAS2022_0754 |
| Kang, M.-H. | INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX | ICAS2022_0417 |
| Kapidzic, Z. | INCREMENTAL FATIGUE DAMAGE MODEL: APPLICATION TO PLANE PROBLEMS WITH NON-PROPORTIONAL LOADING | ICAS2022_0111 |
| Karabasov, S.A. | APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS | ICAS2022_0643 |
| Karagoz, F. | A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT | ICAS2022_0453 |
| Kartal, M.R. | FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIES | ICAS2022_0520 |
| Kasemsri, R. | AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION | ICAS2022_0413 |
| Kashitani, M. | ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICES | ICAS2022_0145 |
| Katagiri, K. | WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) | ICAS2022_0814 |
| Kato, F. | APPLYING MACHINE LEARNING TO TAXI-TIME PREDICTION ATTOKYO INTERNATIONAL AIRPORT | ICAS2022_0267 |
| Kaya, M. | AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPES | ICAS2022_0381 |
| Kaysser-Pyzalla, A. | FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION | ICAS2022_0708 |
| Kazula, S. | DEVELOPMENT OF A CONTROLS APPROACH FOR FUEL CELL-POWERED ALL-ELECTRIC AERO ENGINES BASED ON AN FHA | ICAS2022_0366 |
| Kelly, M.A. | MODEL-BASED SYSTEMS ENGINEERING FOR FUTURE DIGITAL FLIGHT LINES | ICAS2022_0919 |
| Kerlin, U. | CERTIFICATION BY ANALYSIS - SOME THOUGHTS | ICAS2022_0954 |
| Kern, J.S. | ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND DISTURBANCE LEVELS | ICAS2022_0571 |
| Keye, S. | CAD DEFORMATION FOR THE CONSIDERATION OF AEROELASTIC EFFECTS | ICAS2022_0557 |
| Keßler, M. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Khan, S. | A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATION | ICAS2022_0704 |
| Khanal, P. | SMART SKIN FOR AEW AIRCRAFT | ICAS2022_0048 |
| Khankwa, K. | AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION | ICAS2022_0413 |
| Khorrami, M.R. | TOWARD A COMMUNITY NOISE ASSESSMENT OF SINGLE-AISLE AIRCRAFT WITH HYBRID-ELECTRIC PROPULSION | ICAS2022_0953 |
| Kiehn, D. | COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACS | ICAS2022_0505 |
| Kienberger, M. | USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM | ICAS2022_0116 |
| Kienberger, M. | ZONAL MODEL VALIDATION FOR AN ENVIRONMENTALLY FRIENDLY AIRCRAFT CARGO FIRE PROTECTION SYSTEM WITH CONTAINERIZED LOAD | ICAS2022_0159 |
| Kienitz, K.H. | FLIGHT CONTROLLABILITY ANALYSIS IN TIGHT FORMATION AND CRUISE FLIGHT FOR FUEL SAVING | ICAS2022_0273 |
| Kier, T. | EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERS | ICAS2022_0656 |
| Kierbel, D. | VALIDATION OF SCALED FLIGHT TESTING | ICAS2022_0375 |
| Kierbel, D. | CLEAN-SKY 2 LARGE PASSENGER AIRCRAFT PLATFORM 1 ADVANCED ENGINE AND AIRCRAFT CONFIGURATIONS | ICAS2022_0464 |
| Kierulf, B. | CRITICAL REVIEW OF SOUNDING ROCKET FLIGHT DATA AND COMPUTATIONAL FLUID DYNAMICS EFFORTS | ICAS2022_0414 |
| Kikura, I. | FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLET | ICAS2022_0830 |
| Kilian, T. | AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN | ICAS2022_0155 |
| Kim, C.-G. | DOPAMINE-COATED UHMWPE/HYDROGEN-RICH BENZOXAZINE COMPOSITES FOR SPACE RADIATION SHIELDING | ICAS2022_0101 |
| Kim, T.G. | PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTS | ICAS2022_0141 |
| Kim, Y.J. | PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTS | ICAS2022_0141 |
| Kim, S.K. | PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTS | ICAS2022_0141 |
| Kim, S. | A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSB | ICAS2022_0222 |
| Kim, J. | A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSB | ICAS2022_0222 |
| Kim, L. | INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFT | ICAS2022_0346 |
| Kim, Y.J. | FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTER | ICAS2022_0420 |
| Kim, T.G. | FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTER | ICAS2022_0420 |
| Kim, S.K. | FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTER | ICAS2022_0420 |
| Kim, L.-S. | FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSION | ICAS2022_0438 |
| Kim, D. | A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT | ICAS2022_0453 |
| Kim, S.K. | EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV | ICAS2022_0488 |
| Kim, Y. | NEURAL-NETWORK ADAPTIVE DECENTRALIZED FORMATION CONTROL | ICAS2022_0490 |
| Kim, B.S. | NEURAL-NETWORK ADAPTIVE DECENTRALIZED FORMATION CONTROL | ICAS2022_0490 |
| Kim, J. | OPENVSP BASED AERODYNAMIC DESIGN OPTIMIZATION TOOL BUILDING METHOD AND ITS APPLICATION TO TAILLESS UAV | ICAS2022_0858 |
| Kim, S.-H. | META-REINFORCEMENT LEARNING-BASED FAULT TOLERANT CONTROL FOR A QUADROTOR WITH A SEVERE LOSS OF ROTOR | ICAS2022_0879 |
| Kim, Y. | META-REINFORCEMENT LEARNING-BASED FAULT TOLERANT CONTROL FOR A QUADROTOR WITH A SEVERE LOSS OF ROTOR | ICAS2022_0879 |
| Kimura, K. | HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA | ICAS2022_0444 |
| Kiris, C.C. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Kishimoto, N. | WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) | ICAS2022_0814 |
| Kiszkowiak, L. | THE USE OF COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A NEW GENERATION LIGHT COMBAT AIRPLANE | ICAS2022_0371 |
| Klaproth, T. | SUCCESSIVE KNOWLEDGE BUILDUP AND TRANSFER DURING THE ANALYSIS OF SCALED UAV WINGS BY MEANS OF MACHINE LEARNING | ICAS2022_0521 |
| Klein, M. | OPEN CAVITY SIMULATIONS UNDER SIDESLIP FLOW CONDITIONS | ICAS2022_0173 |
| Klein, M. | INVESTIGATION OF LEADING-EDGE VORTICES ON A TRIPLE-DELTA-WING CONFIGURATION USING SCALE-ADAPTIVE SIMULATION | ICAS2022_0528 |
| Klein, C. | NUMERICAL AND EXPERIMENTAL INVESTIGATIONS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODEL | ICAS2022_0720 |
| Kleine, V.G. | ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATION | ICAS2022_0635 |
| Kleineberg, M. | DESIGN,MANUFACTURING & CERTIFICATION STRATEGIES FOR INNOVATIVE HYDROGEN STORAGE SYSTEMS TO ENABLE ZERO EMISSION AVIATION | ICAS2022_0962 |
| Klimczyk, W. | PROPELLER AEROACOUSTIC MODELS IN VARIABLE-FIDELITY DESIGN OPTIMIZATION | ICAS2022_0710 |
| Klimmek, T. | LOADS ANALYSIS AND STRUCTURAL OPTIMIZATION OF A LONG-RANGE TRANSPORT CONFIGURATION WITH HYBRID LAMINAR FLOW CONTROL | ICAS2022_0158 |
| Klimmek, T. | AEROELASTIC MODELING, LOADS ANALYSIS AND STRUCTURAL DESIGN OF A FIGHTER AIRCRAFT | ICAS2022_0161 |
| Klimmek, T. | A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR | ICAS2022_0826 |
| Kloock-Schreiber, D. | INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGION | ICAS2022_0840 |
| Kluenker, C. | DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORS | ICAS2022_0264 |
| Klöckner, A. | FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION | ICAS2022_0708 |
| Kniebel, B. | SORA-BASED RISK ASSESSMENT FOR CARGO UNMANNED AERIAL VEHICLES IN THE UAM FRAMEWORK | ICAS2022_0240 |
| Knoblauch, B. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Knöös Franzén, L. | ONTOLOGY-ASSISTED AIRCRAFT CONCEPT GENERATION | ICAS2022_0352 |
| Kobayashi, E. | INFLUENCES OF CHANGING THE INSTALLING POSITIONS OF MULTIPLE WINGLETS ON AERODYNAMIC CHARACTERISTICS | ICAS2022_0459 |
| Kobayashi, K. | INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS | ICAS2022_0904 |
| Kobayashi, K. | OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE | ICAS2022_0909 |
| Kobiki, N. | HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA | ICAS2022_0444 |
| Kong, G. | DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATION | ICAS2022_0753 |
| Kontos, G. | PILOT TRAINING CHALLENGES FOR ADVANCED AIR MOBILITY | ICAS2022_0675 |
| Kopardekar, P. | INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS | ICAS2022_0904 |
| Kopardekar, P. | OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE | ICAS2022_0909 |
| Korn, B. | THE GROUP OF RESPONSABLES "FLIGHT MECHANICS, SYSTEMS AND INTEGRATION (GOR FM)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0912 |
| Kos, J. | NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 | ICAS2022_0801 |
| Koschel, S. | AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATION | ICAS2022_0747 |
| Koschlik, A.-K. | DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTS | ICAS2022_0868 |
| Kostek, A. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Koyama, T. | DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES | ICAS2022_0448 |
| Kraft, T. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Krammer, C. | REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT | ICAS2022_0797 |
| Kratz, J.L. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Krause, D. | A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE | ICAS2022_0791 |
| Krause, D. | PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONS | ICAS2022_0820 |
| Krawczyk, K. | TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINS | ICAS2022_0822 |
| Krishnaswamy, S. | MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING | ICAS2022_0176 |
| Krus, P. | ONTOLOGY-ASSISTED AIRCRAFT CONCEPT GENERATION | ICAS2022_0352 |
| Krus, P. | A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL | ICAS2022_0513 |
| Krus, P. | MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIES | ICAS2022_0575 |
| Krus, P. | ENVIRONMENTAL AGENT-BASED MODELLING FOR A FIREFIGHTING SYSTEM OF SYSTEMS | ICAS2022_0645 |
| Krus, P. | THE BENEFIT OF BILATERAL RESEARCH NETWORKS - THE SARC AND BARINET INITIATIVES AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICS | ICAS2022_0681 |
| Krus, P. | SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045 | ICAS2022_0804 |
| Krus, P. | HYBRID ELECTRIC PROPULSION SYSTEM OPTIMIZATION FOR A COMMUTER AIRCRAFT | ICAS2022_0874 |
| Krus, P. | CRITICALITY AND COMFORT ZONE SUPPORTING DESIGN CHOICES TO ACHIEVE SUSTAINABLE REQUIREMENTS: THE CASE OF ELECTRIC AIRCRAFT | ICAS2022_0875 |
| Kruse, M. | AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN | ICAS2022_0155 |
| Krüger, W. | WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSES | ICAS2022_0663 |
| Krüger, W.R. | A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR | ICAS2022_0826 |
| Kuchar, R. | EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATION | ICAS2022_0467 |
| Kuelper, N. | SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGN | ICAS2022_0665 |
| Kuenz, A. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Kumawat, H. | A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE | ICAS2022_0791 |
| Kurita, M. | EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETS | ICAS2022_0243 |
| Kurka, P.R.G. | EXPERIMENTAL AND NUMERICAL ANALYSIS OF A PRE-STRESSED TENSEGRITY MEMBRANE | ICAS2022_0038 |
| Kurtulus, D.F. | AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0593 |
| Kusunose, K. | ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICES | ICAS2022_0145 |
| Kwiecien, A. | COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS OBTAINED BY ANALYTICAL, PANEL AND CFD METHOD | ICAS2022_0353 |
| Kwiek, A. | PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLE | ICAS2022_0395 |
| Kwiek, A. | MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIES | ICAS2022_0462 |
| Kügler, D. | FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION | ICAS2022_0708 |
| Kyriakopoulos, M. | EUROPEAN AVIATION RESEARCH AND INNOVATION TOWARDS CLIMATE NEUTRALITY | ICAS2022_0959 |
| Kĺllberg, F. | AERODYNAMIC DEVELOPMENT OF SAAB FCAS UNMANNED SUPERSONIC COMBAT AIRCRAFT | ICAS2022_0570 |
| Kötter, A. | DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT – LIFE CYCLE ASSESSMENT ACTIVITIES AT ECOTECH / CLEANSKY 2 | ICAS2022_0895 |
| La, J. | DOOR-TO-DOOR TRAVEL PLANNER FOR IMPROVED TRAVELER EXPERIENCE USING DIGITAL TWIN CONCEPT | ICAS2022_0011 |
| Labans, E. | INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY | ICAS2022_0685 |
| Laliberté, J. | FATIGUE CRACK PROPAGATION IN ADDITIVELY MANUFACTURED POLYMER PARTS | ICAS2022_0777 |
| Lamkin, A.H.R. | COUPLED AEROPROPULSIVE ANALYSIS AND OPTIMIZATION OF A HIGH BYPASS TURBOFAN ENGINE | ICAS2022_0390 |
| Lammen, W. | NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 | ICAS2022_0801 |
| Lammering, T. | DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK | ICAS2022_0677 |
| Langer, M. | FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES | ICAS2022_0958 |
| Langer, M. | FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES | ICAS2022_0961 |
| Lappa, M. | A NEW FACILITY FOR HYPERSONIC FLOW SIMULATION DRIVEN BY A HIGH VELOCITY OXYGEN FUEL GUN | ICAS2022_0437 |
| Larsson, R. | ANALYSIS OF THE EFFECT OF FLOW TRANSITION OVER THE WINGS OF THE BLADE DEMONSTRATOR | ICAS2022_0150 |
| Larsson, R. | RAPID PROTOTYPING IN AIRCRAFT DESIGN USING CFD, WIND TUNNEL AND FLIGHT TESTING | ICAS2022_0441 |
| Larsson, J. | THE INFLUENCE OF THE VANE LEAN ON THE FLOW IN A TURBINE REAR STRUCTURE | ICAS2022_0514 |
| Larsson, F. | MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIES | ICAS2022_0575 |
| Larsson, F. | AN EVALUATION METHOD FOR AIRCRAFT ACTUATION SYSTEMS OPERATIONAL COST | ICAS2022_0601 |
| Larsson, R. | REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER | ICAS2022_0605 |
| Lau, K.A. | DOOR-TO-DOOR TRAVEL PLANNER FOR IMPROVED TRAVELER EXPERIENCE USING DIGITAL TWIN CONCEPT | ICAS2022_0011 |
| Lau, A. | CONSIDERATIONS FOR MULTI-CRITERIA ROUTE DESIGN ON DIFFERENT ATMOSPHERIC SCALES | ICAS2022_0844 |
| Lazzara, D.S. | MDAO OF A TRANSONIC TRUSS-BRACED WING VISION VEHICLE | ICAS2022_0807 |
| Le Garrec, T. | LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES | ICAS2022_0339 |
| Le Lamer, Y. | AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS | ICAS2022_0560 |
| Le Pape, A. | THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0917 |
| Lecce, M. | ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITION | ICAS2022_0085 |
| Lee, S.-G. | DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLE | ICAS2022_0108 |
| Lee, S.-G. | OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNING | ICAS2022_0109 |
| Lee, D. | INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFT | ICAS2022_0346 |
| Lee, S. | AIRCRAFT DESIGN PARAMETER ESTIMATION USING DATA-DRIVEN MACHINE LEARNING MODELS | ICAS2022_0435 |
| Lee, D.-W. | FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSION | ICAS2022_0438 |
| Lee, H.J. | GENERATION OF TERRAIN PROFILE FOR TERRAIN FOLLOWING | ICAS2022_0538 |
| Lee, S.C. | GENERATION OF TERRAIN PROFILE FOR TERRAIN FOLLOWING | ICAS2022_0538 |
| Lee, D.W. | SAFE REINFORCEMENT LEARNING BASED MULTI-ROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLES | ICAS2022_0539 |
| Lee, J.-J. | DESIGN STUDY OF BRAKE MECHANICAL CONTROL SYSTEM OF UAV | ICAS2022_0778 |
| Lee, J.-H. | DESIGN STUDY OF BRAKE MECHANICAL CONTROL SYSTEM OF UAV | ICAS2022_0778 |
| Lee, C.-H. | CONVEX PROGRAMMING-BASED OPTIMAL THREE-DIMENSIONAL MID-COURSE GUIDANCE WITH LOSSLESS CONVEXIFICATION | ICAS2022_0810 |
| Lefebvre, T. | REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION | ICAS2022_0323 |
| Lefebvre, T. | CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT | ICAS2022_0350 |
| Lefčbvre, T. | THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENT | ICAS2022_0615 |
| Lefebvre, T. | A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK | ICAS2022_0618 |
| Lefevre, L. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Lehmann, O. | PILOT TRAINING CHALLENGES FOR ADVANCED AIR MOBILITY | ICAS2022_0675 |
| Lehmann, O. | NEW GENERATION SPACE VEHICLE OPERATIONS IN THE UNITED ARAB EMIRATES – AN AIRSPACE AND RISK ASSESSMENT | ICAS2022_0698 |
| Lei, Z. | ESTIMATION OF EVTOL FLIGHT PERFORMANCE USING ROTORCRAFT THEORY | ICAS2022_0408 |
| Lei, Z. | OPERATIONAL FEASIBILITY STUDY OF AIR TAXI SERVICE USING EVTOL | ICAS2022_0474 |
| Leißling, D. | THE NEW RESEARCH AIRCRAFT ISTAR - EXPERIMENTAL FLIGHT CONTROL SYSTEM | ICAS2022_0439 |
| Lejon , M. | MULTIPOINT AERODYNAMIC DESIGN OF A NACELLE FOR AN ELECTRIC FAN | ICAS2022_0138 |
| Lejon, M. | DEMONSTRATING AN APPROACH FOR MULTIDISCIPLINARY SET BASED DESIGN WITHIN AN AEROSPACE RESEARCH PROJECT - DEFAINE | ICAS2022_0661 |
| Lejon, M. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| Lemetti, A. | PERFORMANCE EVALUATION OF THE ARRIVAL OPERATIONS IN TERMINAL AREA | ICAS2022_0825 |
| Lemmens, Y. | INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT | ICAS2022_0326 |
| Lemmens, Y. | TEMPLATE-BASED SYNTHESIS OF 3D SYSTEMS FOR MBSE | ICAS2022_0724 |
| Leng, Y. | A STUDY OF HIGH-LIFT DEVICES FOR LOW REYNOLDS NUMBER APPLICATIONS | ICAS2022_0312 |
| Lepage, A. | VALIDATION OF SCALED FLIGHT TESTING | ICAS2022_0375 |
| Lery, J. | PROGRESS IN WING DESIGN, STATUS AND PERSPECTIVES | ICAS2022_0926 |
| Levinski, O. | AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATION | ICAS2022_0747 |
| Leweke, T. | VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIR | ICAS2022_0083 |
| Li, L. | DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNEL | ICAS2022_0045 |
| Li, W. | THREE DIMENSIONAL PATH FOLLOWING CONTROL FOR A FIXED-WING UAV ON SO(3) WITH INPUT SATURATION | ICAS2022_0049 |
| Li, L. | MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF 2D HIGH-LIFT DEVICE BASED ON DISTRIBUTED DEEP REINFORCEMENT LEARNING | ICAS2022_0219 |
| Li, G.W. | STUDY ON MECHANICAL PROPERTIES OF CARBON FIBER RESIN MATRIX COMPOSITE BOLTED JOINT STRUCTURE AT HIGH TEMPERATURE | ICAS2022_0278 |
| Li, H. | RESEARCH ON PRESSURE LOAD OF AN EMBEDDED JET NOZZLE | ICAS2022_0302 |
| Li, G.-W. | RESEARCH ON THE EFFECT OF THE PROCESS FIRST SHOT PEENING STRENGTHENING THEN SHOT PEENING FORMING ON FATIGUE STRENGTH OF 7050 HIGH-STRENGTH ALUMINUM ALLOY | ICAS2022_0316 |
| Li, X. | DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT | ICAS2022_0321 |
| Li, Y. | DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT | ICAS2022_0321 |
| Li, H.-Y. | INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX | ICAS2022_0417 |
| Li, H.-Y. | A FAST PREDICTION METHOD FOR DROPPING WATER OF FIRE FIGHTING AIRCRAFT BASED ON EXTERNAL BALLISTICS OF PARTICLES | ICAS2022_0422 |
| Li, Z.-P. | REDESIGNING AND SIMULATION EVALUATION ON LARGE-FLOW HIGH-TEMPERATURE HIGH-PRESSURE BYPASS SURGE-OUT SYSTEM | ICAS2022_0487 |
| Li, M. | MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0544 |
| Li, H.-X. | SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSOR | ICAS2022_0589 |
| Li, J. | ANALYSIS OF THE AERODYNAMIC CHARACTERISTICS AND ITS INFLUENCE OF TURBOMACHINERY IN TRANSITION STATE | ICAS2022_0603 |
| Li, L. | EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING | ICAS2022_0632 |
| Li, Q. | NUMERICAL INVESTIGATION ON THE AERO-PROPULSION EFFECT OF DISTRIBUTED PROPULSION FOR V/VTOL APPLICATION | ICAS2022_0674 |
| Li, Z.-K. | RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION | ICAS2022_0760 |
| Li, Z.-Y. | RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION | ICAS2022_0760 |
| Li, F.-R. | RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION | ICAS2022_0760 |
| Li, H. | AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT | ICAS2022_0795 |
| Li, Y. | HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS | ICAS2022_0894 |
| Liaboeuf, R. | MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS | ICAS2022_0546 |
| Liang, C. | TWO-PHASE NUMERICAL SIMULATION INVESTIGATION ON THE EFFECTS OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCE | ICAS2022_0029 |
| Lieb, J. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Lim, C.S. | SAFE REINFORCEMENT LEARNING BASED MULTI-ROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLES | ICAS2022_0539 |
| Lim, N. | NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 | ICAS2022_0801 |
| Lima, L.Z. | DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK | ICAS2022_0677 |
| Lin, H. | TWO-PHASE NUMERICAL SIMULATION INVESTIGATION ON THE EFFECTS OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCE | ICAS2022_0029 |
| Lindgren, B. | A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCE | ICAS2022_0332 |
| Lindner, A. | MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHT | ICAS2022_0115 |
| Lindner, A. | USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM | ICAS2022_0116 |
| Lindström, S.B. | INCREMENTAL FATIGUE DAMAGE MODEL: APPLICATION TO PLANE PROBLEMS WITH NON-PROPORTIONAL LOADING | ICAS2022_0111 |
| Link, A. | ASSESSMENT OF A SERIAL COOLING CONCEPT FOR HTPEM FUEL CELL SYSTEMS FOR AVIATION APPLICATIONS | ICAS2022_0456 |
| Linke, F. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Linke, F. | MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN | ICAS2022_0602 |
| Linke, F. | A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIES | ICAS2022_0853 |
| Liscouët, J. | A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONS | ICAS2022_0383 |
| Liscouët-Hanke, S. | CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT | ICAS2022_0350 |
| Liscouët-Hanke, S. | SYSTEMS ARCHITECTING: A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0 PROJECT | ICAS2022_0365 |
| Litt, J.S. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Liu, Y. | TWO-PHASE NUMERICAL SIMULATION INVESTIGATION ON THE EFFECTS OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCE | ICAS2022_0029 |
| Liu, Y. | DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK | ICAS2022_0032 |
| Liu, G. | STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGER | ICAS2022_0072 |
| Liu, F. | A NOVEL EMBEDDED INLET BASED ON THE INTEGRATED DESIGN CONCEPT OF FUSELAGE AND INLET | ICAS2022_0092 |
| Liu, L. | STRUCTURAL DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WING | ICAS2022_0139 |
| Liu, H. | A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTH | ICAS2022_0142 |
| Liu, H. | DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION | ICAS2022_0143 |
| Liu, J. | RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHP | ICAS2022_0200 |
| Liu, Y. | INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN THE V103 CASCADE | ICAS2022_0204 |
| Liu, P.-Q. | MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF 2D HIGH-LIFT DEVICE BASED ON DISTRIBUTED DEEP REINFORCEMENT LEARNING | ICAS2022_0219 |
| Liu, G. | EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONE | ICAS2022_0256 |
| Liu, F. | RESEARCH ON PRESSURE LOAD OF AN EMBEDDED JET NOZZLE | ICAS2022_0302 |
| Liu, P.Q. | NUMERICAL STUDY ON WATER DISPLACEMENT DRAG CHARACTERISTICS OF AIRCRAFT ELASTIC TIRE ON CONTAMINATED RUNWAYS | ICAS2022_0329 |
| Liu, P. | SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATION | ICAS2022_0386 |
| Liu, Y. | MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0544 |
| Liu, Q.-H. | EQUIVALENT CALCULATION METHOD OF FLYOVER NOISE LEVEL OF CUTBACK TAKE-OFF FOR CIVIL JET AIRPLANE AIRWORTHINESS CERTIFICATION | ICAS2022_0626 |
| Liu, Y.J. | RESEARCH ON THE DUCTILE FRACTURE OF AL7085 AND TC11 UNDER COMPLEX STRESS STATE | ICAS2022_0862 |
| Llamas-Sandin, R.C. | DESIGN OF AN ADVANCED EMPENNAGE AND REAR FUSELAGE CONCEPT FOR A COMMERCIAL AIRCRAFT | ICAS2022_0227 |
| Loiodice, L. | STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES | ICAS2022_0336 |
| Lombardi , S. | WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA | ICAS2022_0280 |
| Lopez Pereira, R. | CERTIFICATION ASPECTS OF AN EARTH OBSERVATION PAYLOAD INSTALLED ON COMMERCIAL TRANSPORT AIRCRAFT | ICAS2022_0354 |
| Loruenser, T. | AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTS | ICAS2022_0693 |
| Lovaco, J.L. | ENVIRONMENTAL AGENT-BASED MODELLING FOR A FIREFIGHTING SYSTEM OF SYSTEMS | ICAS2022_0645 |
| Lovero , F. | STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES | ICAS2022_0336 |
| Loxton, B. | A ROADMAP TOWARDS ENVIRONMENTALLY SUSTAINABLE AVIATION | ICAS2022_0398 |
| Lozano, M. | TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES | ICAS2022_0012 |
| Lu, K. | A NUMERICAL METHOD FOR STUDY ON THE AERO-ELASTICITY OF AIR-TO-AIR MISSILES IN OVER-THE-SHOULDER LAUNCH | ICAS2022_0311 |
| Lu, Y. | ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODY | ICAS2022_0385 |
| Lu, S.-G. | FREE FLIGHT TEST IN HORIZONTAL WIND TUNNEL WITH POWERED AIRCRAFT | ICAS2022_0423 |
| Lu, Z. | EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTOR GENERATION | ICAS2022_0548 |
| Lu, K. | HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACK | ICAS2022_0555 |
| Lu, Y. | NUMERICAL INVESTIGATION ON THE AERO-PROPULSION EFFECT OF DISTRIBUTED PROPULSION FOR V/VTOL APPLICATION | ICAS2022_0674 |
| Lu, Y. | COOPERATIVE PATH PLANNING AND ADJUSTING STRATEGY FOR UAVS WITH STRICT TIME CONSTRAINS | ICAS2022_0781 |
| Luckring, J.M. | CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIES | ICAS2022_0934 |
| Ludena Cervantes, T.J. | NEURAL-NETWORK ADAPTIVE DECENTRALIZED FORMATION CONTROL | ICAS2022_0490 |
| Luderer, O. | VALIDATION OF A HYBRID LOADS OBSERVER FOR A SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2022_0080 |
| Ludowicy, J. | ASSESSMENT OF A SERIAL COOLING CONCEPT FOR HTPEM FUEL CELL SYSTEMS FOR AVIATION APPLICATIONS | ICAS2022_0456 |
| Luehrs, B. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Lundberg, J. | ATCO STRATEGIES IN TACTICAL TBO: A SIMULATOR STUDY | ICAS2022_0285 |
| Lundberg, R. | STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT | ICAS2022_0480 |
| Lundbladh, A. | MULTIPOINT AERODYNAMIC DESIGN OF A NACELLE FOR AN ELECTRIC FAN | ICAS2022_0138 |
| Lundbladh, A. | DESIGN AND PERFORMANCE OF LIQUID HYDROGEN FUELLED AIRCRAFT FOR YEAR 2050 EIS | ICAS2022_0496 |
| Lundbladh, A. | SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045 | ICAS2022_0804 |
| Lundgren, J. | INCREMENTAL FATIGUE DAMAGE MODEL: APPLICATION TO PLANE PROBLEMS WITH NON-PROPORTIONAL LOADING | ICAS2022_0111 |
| Lundström, D. | RAPID PROTOTYPING IN AIRCRAFT DESIGN USING CFD, WIND TUNNEL AND FLIGHT TESTING | ICAS2022_0441 |
| Lunghitano , A. | WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA | ICAS2022_0280 |
| Luo, R. | SMART SKIN FOR AEW AIRCRAFT | ICAS2022_0048 |
| Luo, M. | A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTH | ICAS2022_0142 |
| Luo, M. | DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION | ICAS2022_0143 |
| Luo, T.-H. | RESEARCH ON THE EFFECT OF THE PROCESS FIRST SHOT PEENING STRENGTHENING THEN SHOT PEENING FORMING ON FATIGUE STRENGTH OF 7050 HIGH-STRENGTH ALUMINUM ALLOY | ICAS2022_0316 |
| Lutz, F. | FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFT | ICAS2022_0214 |
| Luu, H.S. | ESTIMATION OF STEPWISE VARYING WIND BASED ON DERIVATIVE ESTIMATION OF AIRCRAFT USING SLIDING WINDOW RECURSIVE LEAST SQUARES METHOD | ICAS2022_0110 |
| Lübbe, S.M. | COUPLING OF MODEL-BASED SYSTEMS ENGINEERING AND SAFETY ANALYSIS IN CONCEPTUAL AIRCRAFT SYSTEM DESIGN | ICAS2022_0082 |
| Lübker, J. | SOME EXPERIMENTAL RESULTS ON DYNAMIC AEROELASTICITY OF PLATES AND SHELLS IN SUBSONIC AND SUPERSONIC FLOW. | ICAS2022_0016 |
| Lührs, B. | MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN | ICAS2022_0602 |
| Lührs, B. | CONSIDERATIONS FOR MULTI-CRITERIA ROUTE DESIGN ON DIFFERENT ATMOSPHERIC SCALES | ICAS2022_0844 |
| Lütjens, K. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Lütjens, K. | ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITY | ICAS2022_0233 |
| Lynde, M.N. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Lyrio, J.A.A. | STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWS | ICAS2022_0726 |
| Lyu, S. | A DAMAGE RECOGNITION METHOD OF COMPOSITE STRUCTURES USING ARTIFICIAL DEFECTIONS | ICAS2022_0052 |
| Lößle, F. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Ma, Z. | DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNEL | ICAS2022_0045 |
| Ma, T. | AN INVESTIGATION ON THE IMPROVEMENT FOR TANDEM WING PITCHING MOMENT CHARACTERISTICS | ICAS2022_0050 |
| Ma, T.-L. | DESIGN AND EFFICIENCY ANALYSIS OF EVTOL CONTRA-ROTATING PROPELER | ICAS2022_0060 |
| Ma, T.-L. | RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAV | ICAS2022_0107 |
| Ma, N. | STRUCTURAL DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WING | ICAS2022_0139 |
| Ma, Q. | SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATION | ICAS2022_0386 |
| Mabboux, J. | A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS | ICAS2022_0568 |
| Machado, L. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Machado, R.C. | OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM | ICAS2022_0891 |
| Machado Cardoso Junior, M. | LONG TOUCHDOWN THROUGH A SAFETY-II PERSPECTIVE | ICAS2022_0185 |
| MacManus, D.G. | A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKE | ICAS2022_0127 |
| MacManus, D. | A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES | ICAS2022_0162 |
| MacManus, D. | OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELS | ICAS2022_0167 |
| MacManus, D.G. | TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINES | ICAS2022_0380 |
| Mader, C.A. | LARGE-SCALE MULTIFIDELITY AEROSTRUCTURAL OPTIMIZATION OF A TRANSPORT AIRCRAFT | ICAS2022_0186 |
| Magnusson, A. | LATEST DEVELOPMENTS IN HIGH PRESSURE HEAT TREATMENT OF AEROSPACE COMPONENTS | ICAS2022_0026 |
| Mahavier, K. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Maitelli, A.L. | HYDRO ENVIRONMENTAL AND ELECTRICAL ASSETS MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV | ICAS2022_0017 |
| Maki, A. | VISION-BASED LOCALISATION FOR AUTONOMOUS AERIAL NAVIGATION IN GNSS-DENIED SITUATIONS | ICAS2022_0485 |
| Malatesta, V. | STUDY OF EFFECTS ON THE WING'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPAN | ICAS2022_0889 |
| Mallet, M. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Mallwitz, R. | A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTS | ICAS2022_0850 |
| Malone, A.M. | TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATION | ICAS2022_0397 |
| Mancini, S. | MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING | ICAS2022_0176 |
| Mancini, A. | TOWARDS A SEAMLESS SIMULATION OF THE AIR TRANSPORT SYSTEM | ICAS2022_0732 |
| Mandorino, M. | REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION | ICAS2022_0323 |
| Mandorino, M. | CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT | ICAS2022_0350 |
| Mandry, N. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Mangin, B. | STUDY OF THE IMPACT OF AZIMUTHAL FLOW DISTORTION ON IN-DUCT ACOUSTIC PROPAGATION USING A MULTIMODAL FORMULATION | ICAS2022_0666 |
| Manikar, S.S. | OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN | ICAS2022_0550 |
| Mansfield, N. | MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHT | ICAS2022_0115 |
| Mantegna, G. | RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS | ICAS2022_0218 |
| Marciello, V. | TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASS | ICAS2022_0641 |
| Marciello, V. | MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFT | ICAS2022_0649 |
| Mariani, R. | PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFT | ICAS2022_0126 |
| Mariani, R. | WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE | ICAS2022_0215 |
| Mariani, R. | DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING | ICAS2022_0447 |
| Marini, M. | AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECT | ICAS2022_0235 |
| Marini, M. | COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION | ICAS2022_0342 |
| Marini, M. | HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS | ICAS2022_0572 |
| Marini, M. | AERODATABASE DEVELOPMENT AND INTEGRATION OF SUPERSONIC/HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROJECT | ICAS2022_0596 |
| Marini, M. | HIGH PRESSURE HYDROGEN OXYGEN COMBUSTION KINETIC ASSESSMENT FOR AIR-BREATHING PROPULSION SUPERSONIC GREEN AVIATION | ICAS2022_0845 |
| Marino, A. | HYBRID-ELECTRIC AND FULL ELECTRIC ARCHITECTURES FOR LOW-EMISSION HYBRID-ELECTRIC REGIONAL [REG] AIRCRAFT | ICAS2022_0930 |
| Marion, G. | TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINE | ICAS2022_0006 |
| Markatos, D.N. | ASSESSMENT OF THE SUSTAINABILITY OF THE IMPLEMENTATION OF CIRCULAR ECONOMY PRINCIPLES IN PRODUCING AIRCRAFT STRUCTURES | ICAS2022_0056 |
| Markesteijn, A.P. | APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS | ICAS2022_0643 |
| Markiewicz, R. | THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0917 |
| Marks, T. | ASSESSMENT OF REAL-TIME DATA TRANSMISSION VIA AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC OCEANIC AIRSPACE | ICAS2022_0168 |
| Marks, T. | CLUSTER STRUCTURE AND GATEWAY AVAILABILITY OF AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC AIRSPACE | ICAS2022_0293 |
| Marouf, A. | USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC PERFORMANCE OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFT | ICAS2022_0251 |
| Marques, H.C. | A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY | ICAS2022_0723 |
| Marques, H.C. | UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO | ICAS2022_0729 |
| Marques, J.M.G. | ON LATERAL-LONGITUDINAL CONTROL COUPLING FOR SHORT- AND LONG-FUSELAGE BWB AIRCRAFT CONFIGURATIONS | ICAS2022_0733 |
| Martin, N. | TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES | ICAS2022_0012 |
| Martina, F. | MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING | ICAS2022_0176 |
| Martini Catalano, F. | LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTION | ICAS2022_0088 |
| Martins, J.R.R.A. | LARGE-SCALE MULTIFIDELITY AEROSTRUCTURAL OPTIMIZATION OF A TRANSPORT AIRCRAFT | ICAS2022_0186 |
| Martins, W. M. | USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION | ICAS2022_0389 |
| Martins, J.R.R.A. | COUPLED AEROPROPULSIVE ANALYSIS AND OPTIMIZATION OF A HIGH BYPASS TURBOFAN ENGINE | ICAS2022_0390 |
| Martins, J.R.R.A. | AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0593 |
| Martins, J.R.R.A. | TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATION | ICAS2022_0905 |
| Marzocca, P. | NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMS | ICAS2022_0396 |
| Marzocca, P. | AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATION | ICAS2022_0747 |
| Massegur, D. | COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMS | ICAS2022_0399 |
| Matayoshi, N. | NEW ENTRANTS’ AIRSPACE INTEGRATION IN JAPAN: JAXA’S ONGOING CONTRIBUTION | ICAS2022_0907 |
| Matesanz-Garcia, J. | A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES | ICAS2022_0162 |
| Matias, C. | TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATION | ICAS2022_0036 |
| Matoses Gimenez, A. | DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING | ICAS2022_0447 |
| Matthes, S. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Matunaga, M.A.L. | AUTOMATIC FREE-FORM DEFORMATION AS GEOMETRIC PARAMETERIZATION FOR AERODYNAMIC DESIGN | ICAS2022_0749 |
| Maulana, F.A. | TURBULENCE MODELLING STUDIES OF SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE CYLINDER FLARE IN HYPERSONIC FLOWS | ICAS2022_0746 |
| Mavris, D.N. | A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT | ICAS2022_0453 |
| Mavris, D.N. | ZERO-EMISSION REGIONAL AVIATION IN SWEDEN | ICAS2022_0650 |
| Mavris, D.N. | ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH | ICAS2022_0817 |
| Mavris, D.N. | REGIONAL AIR MOBILITY MARKET STUDY | ICAS2022_0872 |
| Mavris, D.N. | SYSTEM LEVEL IDENTIFICATION OF CRITICAL UNCERTAINTIES TO ENABLE VALIDATION EXPERIMENTS | ICAS2022_0935 |
| Mavris, D. | NEXT STEPS TOWARDS CERTIFICATION BY ANALYSIS - A DIGITAL THREAD PERSPECTIVE | ICAS2022_0955 |
| Maximo, M.R.O.A. | COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMS | ICAS2022_0340 |
| May, M. | EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONS | ICAS2022_0860 |
| Mayer, F. | USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM | ICAS2022_0116 |
| Meddaikar, Y.M. | A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR | ICAS2022_0826 |
| Meeß, H. | IMAGE SEGMENTATION BASED EMERGENCY LANDING FOR AUTONOMOUS AND AUTOMATED UNMANNED AERIAL VEHICLES | ICAS2022_0725 |
| Mčge, R. | TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONES | ICAS2022_0655 |
| Méheut, M. | MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS | ICAS2022_0546 |
| Méheut, M. | OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACT | ICAS2022_0843 |
| Meissner, D. | VALIDATION OF SCALED FLIGHT TESTING | ICAS2022_0375 |
| Meister, J. | IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT | ICAS2022_0627 |
| Mello, J.M.G.D. | A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK | ICAS2022_0618 |
| Mendiguchia Meuser, M. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Mendonca, W.R.P. | APPLICATION OF THE VIRTUAL CRACK CLOSURE TECHNIQUE FOR CRACKS IN BUILT-UP PANELS | ICAS2022_0799 |
| Meng, F.-M. | STRUCTURAL DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WING | ICAS2022_0139 |
| Meng, J.-H. | STRUCTURAL DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WING | ICAS2022_0139 |
| Meng, D. | STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATOR | ICAS2022_0313 |
| Metz, I.C. | AN OPERATIONAL CONCEPT FOR THE INTEGRATION OF URBAN AIR MOBILITY VEHICLES INTO THE AIR TRAFFIC CONTROL PROCESSES | ICAS2022_0451 |
| Metz, I.C. | URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH NON-COOPERATIVE AIRSPACE USERS | ICAS2022_0567 |
| Metz, I.C. | EVALUATION AND QUANTIFICATION OF THE POTENTIAL CONSEQUENCES OF BIRD STRIKES IN URBAN AIR MOBILITY | ICAS2022_0629 |
| Metzler, D. | DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK | ICAS2022_0677 |
| Meyer, M. | ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISK | ICAS2022_0532 |
| Meyer, H. | DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTS | ICAS2022_0868 |
| Meyer, L. | STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATION | ICAS2022_0903 |
| Miao, Z. | THREE DIMENSIONAL PATH FOLLOWING CONTROL FOR A FIXED-WING UAV ON SO(3) WITH INPUT SATURATION | ICAS2022_0049 |
| Michler, O. | REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMIC | ICAS2022_0486 |
| Mieloszyk, J. | MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIES | ICAS2022_0462 |
| Mieloszyk, J. | OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANE | ICAS2022_0576 |
| Migliorini, M. | A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKE | ICAS2022_0127 |
| Miki, H. | FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLET | ICAS2022_0830 |
| Milazzo, A. | DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU) | ICAS2022_0295 |
| Milazzo, A. | TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHOD | ICAS2022_0427 |
| Milz, D. | EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONS | ICAS2022_0860 |
| Mingione, G. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Mirhashemi, A. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Mishra, C. | AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT | ICAS2022_0835 |
| Mishra, C. | EXTENSION OF THE CAPABILITIES OF AN AUTOMATIC LANDING SYSTEM WITH PROCEDURES MOTIVATED BY VISUAL-FLIGHT-RULES | ICAS2022_0841 |
| Miura, T. | VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGS | ICAS2022_0207 |
| Miyake, T. | NUMERICAL INVESTIGATION ON THE DOUBLE TRANSONIC DIP OF SUPERCRITICAL AIRFOIL FLUTTER | ICAS2022_0545 |
| Miyazaki, S. | COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHOD | ICAS2022_0416 |
| Mizukaki, T. | NUMERICAL ANALYSIS OF PROPAGATION OF DETONATION WAVE PLUNGING ENTRY THE FUEL JET TRAIN INSIDE ROTATING DETONATION COMBUSTOR | ICAS2022_0409 |
| Mo, D. | TWO-PHASE NUMERICAL SIMULATION INVESTIGATION ON THE EFFECTS OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCE | ICAS2022_0029 |
| Mo, D. | DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK | ICAS2022_0032 |
| Modi, P. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Moens, F. | MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS | ICAS2022_0546 |
| Moerland, E. | A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONS | ICAS2022_0700 |
| Moerland, E. | TOWARDS A SEAMLESS SIMULATION OF THE AIR TRANSPORT SYSTEM | ICAS2022_0732 |
| Monge, F. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Monnier, V. | A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKE | ICAS2022_0127 |
| Montella, N. | AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLES | ICAS2022_0241 |
| Montella, N. | AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE | ICAS2022_0259 |
| Moraes, L. | PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE | ICAS2022_0782 |
| Morel, F. | MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS | ICAS2022_0546 |
| Moretti, R. | EXTERNAL-INTERNAL AERODYNAMIC COUPLING ON A TURBOPROP ENGINE USING THE BODY-FORCE METHOD | ICAS2022_0286 |
| Moretti, S. | SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSIS | ICAS2022_0370 |
| Mori, R. | AIRCRAFT MASS ESTIMATION USING CRUISE FLIGHT PROFILE | ICAS2022_0105 |
| Moriai, H. | STUDY ON THE APPLICATION OF EMULSIFIED FUEL IN SMALL JET ENGINES | ICAS2022_0751 |
| Moriai, H. | EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENT | ICAS2022_0756 |
| Morikawa, N. | MACHINE LEARNING METHODS ENSURING BOTH PERFORMANCE AND INTERPRETABILITY OF ESTIMATING AIRCRAFT ARRIVAL TIMES | ICAS2022_0271 |
| Morita, N. | DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES | ICAS2022_0448 |
| Morlier, J. | AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS | ICAS2022_0560 |
| Morrison, J. | NATO AVT-297 DEVELOPMENT OF A FRAMEWORK FOR VALIDATION OF COMPUTATIONAL TOOLS FOR ANALYSIS OF AIR VEHICLES | ICAS2022_0933 |
| Moruzzi, M.C. | VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTS | ICAS2022_0247 |
| Moruzzi, M.C. | AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACH | ICAS2022_0478 |
| Moschetta, J.-M. | A STUDY OF HIGH-LIFT DEVICES FOR LOW REYNOLDS NUMBER APPLICATIONS | ICAS2022_0312 |
| Moschetta, J.-M. | PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY IMPLEMENTED UNDER ASWING | ICAS2022_0318 |
| Moschetta, J.-M. | A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONS | ICAS2022_0383 |
| Moschetta, J.-M. | STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE | ICAS2022_0583 |
| Moura, E.A. | IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTING | ICAS2022_0873 |
| Mu, W. | EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING | ICAS2022_0078 |
| Muchla, G. | COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS OBTAINED BY ANALYTICAL, PANEL AND CFD METHOD | ICAS2022_0353 |
| Mulder, J.L. | INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD | ICAS2022_0653 |
| Murali, A.R. | APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS | ICAS2022_0643 |
| Muraoka, K. | FLIGHT VERIFICATION OF AUTOMATIC TRANSITION FOR QUAD TILT WING SMALL UAV | ICAS2022_0740 |
| Muth, B. | CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACH | ICAS2022_0102 |
| Muth, K. | REAL-TIME CALCULATION AND ADAPTION OF CONFLICT-FREE AIRCRAFT GROUND TRAJECTORIES | ICAS2022_0213 |
| Müller, B. | MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHT | ICAS2022_0115 |
| Müller, P. | LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEM | ICAS2022_0144 |
| Müller, J. | POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORS | ICAS2022_0347 |
| Mĺnsson, P. | FLIGHT DYNAMICS SIMULATION AND FCS AUTO-GENERATION IN THE CONCEPTUAL DESIGN PHASE OF AN UNSTABLE SUPERSONIC AIRCRAFT | ICAS2022_0458 |
| Mĺrtensson, H. | STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALL | ICAS2022_0351 |
| Mĺrtensson, H. | ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR | ICAS2022_0382 |
| Mĺrtensson, H. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| Mönig, R. | FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION | ICAS2022_0708 |
| Nadjm-Tehrani, S. | CONCEPT LEVEL EXPLORATION OF IMA-BASED NETWORKED PLATFORMS WITH MIXED TIME-SENSITIVE COMMUNICATION REQUIREMENTS | ICAS2022_0660 |
| Naeser, J. | HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENT | ICAS2022_0434 |
| Nagashima, T. | OPTIMIZATION OF AIRCRAFT FLIGHT PATHS CONSIDERING THE CONFLICTING PARAMETERS OF ECONOMY AND SAFETY | ICAS2022_0652 |
| Nagel, B. | VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERING | ICAS2022_0063 |
| Nagel, B. | EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXT | ICAS2022_0254 |
| Nagel, B. | AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0593 |
| Nagel, B. | THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENT | ICAS2022_0615 |
| Nagel, B. | A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK | ICAS2022_0618 |
| Nagel, B. | A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONS | ICAS2022_0700 |
| Nagel, B. | RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORK | ICAS2022_0702 |
| Nagel, B. | FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION | ICAS2022_0708 |
| Nagel, B. | TOWARDS A SEAMLESS SIMULATION OF THE AIR TRANSPORT SYSTEM | ICAS2022_0732 |
| Nagel, B. | SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045 | ICAS2022_0804 |
| Nagel, B. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Nagel, N. | ICAS DIGITAL PIONEERING INITIATIVE AND SYSTEM OF SYSTEM CHALLENGES | ICAS2022_0964 |
| Nagele-Renzl, A. | USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM | ICAS2022_0116 |
| Naghibi, S.E. | APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS | ICAS2022_0643 |
| Nairus, J.G. | POWER/THERMAL 2030 VISION - AIR PLATFORM ELECTRIFICATION | ICAS2022_0960 |
| Nakasuka, S. | DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES | ICAS2022_0448 |
| Nalianda, D. | PROPULSION SYSTEM INTEGRATION FOR A FIRST GENERATION HYDROGEN CIVIL AIRLINER? | ICAS2022_0950 |
| Nambiar, S. | MATHEMATICAL MODELLING AND ANALYSIS OF THERMAL MANAGEMENT SYSTEM ARCHITECTURE FOR HYPERSONIC AIRCRAFT | ICAS2022_0730 |
| Nan Fernandez-Ayala, V. | DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING | ICAS2022_0447 |
| Nangia, R.K. | ARRIVING AT CERTIFIABLE NOVEL AIRLINER USING LIQUID HYDROGEN & EFFICIENCY METRICS | ICAS2022_0373 |
| Naruoka, M. | STATISTICAL DATA SELECTION FOR BETTER FLIGHT CHARACTERISTIC MODELING | ICAS2022_0430 |
| Navarro, P. | PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES | ICAS2022_0289 |
| Nepomuceno, L.M. | IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTING | ICAS2022_0873 |
| Névir, M.-C. | DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORS | ICAS2022_0264 |
| Nghiem, Q.-H. | DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEM | ICAS2022_0818 |
| Nguyen, T.D. | ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICES | ICAS2022_0145 |
| Nguyen, Q.-H. | MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES | ICAS2022_0813 |
| Nguyen, N.-V. | MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES | ICAS2022_0813 |
| Nguyen, T.-G. | DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEM | ICAS2022_0818 |
| Nguyen, Q.-H. | DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEM | ICAS2022_0818 |
| Nguyen, N.-V. | DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEM | ICAS2022_0818 |
| Nguyen, P.-M. | DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEM | ICAS2022_0818 |
| Nguyen, P.A. | ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION | ICAS2022_0827 |
| Nicolosi, G. | WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA | ICAS2022_0280 |
| Nicolosi, F. | REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION | ICAS2022_0323 |
| Nicolosi, F. | TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASS | ICAS2022_0641 |
| Nicolosi, F. | MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFT | ICAS2022_0649 |
| Niedermeier, D. | THE NEW RESEARCH AIRCRAFT ISTAR - EXPERIMENTAL FLIGHT CONTROL SYSTEM | ICAS2022_0439 |
| Nieto, A. | IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONS | ICAS2022_0360 |
| Nikbay, M. | NATO AVT-297 DEVELOPMENT OF A FRAMEWORK FOR VALIDATION OF COMPUTATIONAL TOOLS FOR ANALYSIS OF AIR VEHICLES | ICAS2022_0933 |
| Niklaß, M. | MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN | ICAS2022_0602 |
| Niklaß, M. | INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGION | ICAS2022_0840 |
| Nilsson, T. | LARGE EDDY SIMULATION OF RAMJET TO SCRAMJET TRANSITION | ICAS2022_0188 |
| Nilsson, J. | ATCO STRATEGIES IN TACTICAL TBO: A SIMULATOR STUDY | ICAS2022_0285 |
| Nilsson, S. | EFFECT OF LES LENGTH SCALE AND NUMERICAL SCHEME IN HYBRID RANS-LES OF FREE SHEAR LAYER FLOWS | ICAS2022_0684 |
| Ninomiya, T. | STATISTICAL DATA SELECTION FOR BETTER FLIGHT CHARACTERISTIC MODELING | ICAS2022_0430 |
| Nishida, R. | AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION | ICAS2022_0192 |
| Nishida, H. | EXPERIMENTAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS OF DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATOR | ICAS2022_0877 |
| Nishijima, Y. | VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGS | ICAS2022_0207 |
| Nitzsche, F. | STRUCTURAL ANALYSIS OF TWISTED/CURVED BEAMS USING A HYBRID METHOD | ICAS2022_0802 |
| Niven, A.J. | A STATIC STABILITY COMPARISON OF WIND TUNNEL AND COMPUTATIONAL FLUID DYNAMICS METHODS | ICAS2022_0384 |
| Noakes, I. | FUTURE COMBAT AIRCRAFT SYSTEM THE COMPLEXITY OF THE SKILLS EQUATION | ICAS2022_0901 |
| Noel, S. | WALL INTERFERENCE CORRECTIONS USING NONLINEAR LEAST-SQUARES OPTIMISATION | ICAS2022_0378 |
| Nordin-Bates, K. | LES OF COMBUSTION DYNAMICS IN AN ETHYLENE-HYDROGEN-AIR RAMJET | ICAS2022_0786 |
| Nordström, P. | AERODYNAMIC DEVELOPMENT OF SAAB FCAS UNMANNED SUPERSONIC COMBAT AIRCRAFT | ICAS2022_0570 |
| Norrefeldt, V. | MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHT | ICAS2022_0115 |
| Norrefeldt, V. | USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM | ICAS2022_0116 |
| Norrefeldt, V. | ZONAL MODEL VALIDATION FOR AN ENVIRONMENTALLY FRIENDLY AIRCRAFT CARGO FIRE PROTECTION SYSTEM WITH CONTAINERIZED LOAD | ICAS2022_0159 |
| Nostrani, M.P. | A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL | ICAS2022_0513 |
| Novák , J. | UNMANNED AERIAL VEHICLE\\\'S TRAJECTORY OPTIMIZATION IN CONSTRAINED ENVIRONMENTS | ICAS2022_0717 |
| Nylin, M. | ATCO STRATEGIES IN TACTICAL TBO: A SIMULATOR STUDY | ICAS2022_0285 |
| Nöhren, L. | REAL-TIME CALCULATION AND ADAPTION OF CONFLICT-FREE AIRCRAFT GROUND TRAJECTORIES | ICAS2022_0213 |
| Oberdieck, F. | NUMERICAL AND EXPERIMENTAL INVESTIGATIONS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODEL | ICAS2022_0720 |
| Oberkampf, W.L. | CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIES | ICAS2022_0934 |
| Oberschwendtner, S. | THE INFLUENCE OF THE MODEL PARAMETERS OF LI-ION BATTERIES ON THE WIRING HARNESS PERFORMANCE OF EVTOL AIRCRAFT | ICAS2022_0113 |
| Obert, E. | TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINE | ICAS2022_0006 |
| Occhipinti, G. | CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL | ICAS2022_0341 |
| Ochi, Y. | ESTIMATION OF STEPWISE VARYING WIND BASED ON DERIVATIVE ESTIMATION OF AIRCRAFT USING SLIDING WINDOW RECURSIVE LEAST SQUARES METHOD | ICAS2022_0110 |
| Ochi, Y. | FLIGHT TESTS AND SIMULATION OF A HANG GLIDER | ICAS2022_0135 |
| Odaguil, F.I.K. | A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK | ICAS2022_0618 |
| Ohlenforst, B. | THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0917 |
| Oka, K. | CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H-INFINITY STRUCTURE WITH GWO | ICAS2022_0428 |
| Okoro, O.C. | DATA-DRIVEN APPROACH TO OPTIMAL AIRCRAFT MAINTENANCE | ICAS2022_0871 |
| Okuno, Y. | INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS | ICAS2022_0904 |
| Okuno, Y. | OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE | ICAS2022_0909 |
| Olejnik, A. | THE USE OF COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A NEW GENERATION LIGHT COMBAT AIRPLANE | ICAS2022_0371 |
| Olivares, G. | INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT | ICAS2022_0326 |
| Oliveira, F.B. | ON THE INFLUENCE OF GRADIENT RECONSTRUCTION PROCEDURES OVER THE ACCURACY OF FINITE VOLUME BASED SCHEMES | ICAS2022_0191 |
| Oliveira, A.S. | A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY | ICAS2022_0723 |
| Oliveira, A.S. | UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO | ICAS2022_0729 |
| Oliveira, A.A.M. | HYBRID ELECTRIC PROPULSION SYSTEM OPTIMIZATION FOR A COMMUTER AIRCRAFT | ICAS2022_0874 |
| Oliveira e Silva, D. | A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL | ICAS2022_0513 |
| Olivier, P. | PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES | ICAS2022_0289 |
| Olsson, S. | FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE | ICAS2022_0028 |
| Olsson, E. | GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS | ICAS2022_0265 |
| Ongut, E. | TEMPLATE-BASED SYNTHESIS OF 3D SYSTEMS FOR MBSE | ICAS2022_0724 |
| Oppelstrup, J. | IMPROVING STALL CHARACTERISTICS OF UCAV WING WITH VORTEX GENERATORS | ICAS2022_0238 |
| Oprea, A. | MODEL FIDELITY AND ITS INFLUENCE ON AIRCRAFT CONCEPTUAL DESIGN | ICAS2022_0477 |
| Orefice, F. | TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASS | ICAS2022_0641 |
| Orell, O. | FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHOD | ICAS2022_0754 |
| Orisamolu, W. | AN INNOVATIVE HYDROGEN-POWERED PROPULSION SYSTEM FOR SINGLE-AISLE AIRCRAFT | ICAS2022_0952 |
| Orlando, C. | RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS | ICAS2022_0218 |
| Osawa, N. | EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENT | ICAS2022_0756 |
| Osund-Ireland, M.P.P. | A GLOBAL APPROACH TO ASSESSING THE CLIMATE RESILIENCE OF AIRPORTS | ICAS2022_0922 |
| Otero Sola, E. | ENVIRONMENTAL ASSESSMENT OF NOISE ABATEMENT APPROACH TRAJECTORIES | ICAS2022_0671 |
| Ovesy, H.R. | WING LOADING PROCESS IN KNOWLEDGE-BASED AIRCRAFT DESIGN AND OPTIMIZATION FRAMEWORK | ICAS2022_0519 |
| Paek, S.-K. | KARI-DLR DIGITAL COLLABORATION TO BUILD A MDAO SYSTEM FOR THE PRELIMINARY DESIGN OF HYBRID EVTOL AIRCRAFT | ICAS2022_0947 |
| Pagan, D. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Pagani, A. | NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF UNSTIFFENED AND STIFFENED STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGS | ICAS2022_0220 |
| Pagani, A. | A GLOBAL/LOCAL ELEMENT-WISE APPROACH FOR THE BUCKLING AND POST-BUCKLING ANALYSIS OF THIN MULTILAYERED STRUCTURES | ICAS2022_0253 |
| Page, M. | JETZERO BWB ENABLING TECHNOLOGIES | ICAS2022_0392 |
| Page, M. | JETZERO BWB ENABLING TECHNOLOGIES | ICAS2022_0951 |
| Pagone, E. | MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING | ICAS2022_0176 |
| Pahlke, K. | THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0917 |
| Paiva, F.R.V. | COMPETITIVITY, STRATEGY AND VALUE ON AIRPORTS A METHOD OF DIAGNOSIS, SUGGESTIONS AND ACTIONS FOR INTERNATIONAL AIRPORTS WITH A CASE STUDY OF CNF | ICAS2022_0022 |
| Paiva, V.A.S. | EXPERIMENTAL AND NUMERICAL ANALYSIS OF A PRE-STRESSED TENSEGRITY MEMBRANE | ICAS2022_0038 |
| Pakkam Gabriel, V.R. | FATIGUE DAMAGE MODEL OF HIGH TEMPERATURE POLYMER COMPOSITES IN AERO-ENGINES | ICAS2022_0831 |
| Palaia, G. | CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGE | ICAS2022_0148 |
| Palanque, V. | SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES | ICAS2022_0084 |
| Palanque, V. | STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS | ICAS2022_0151 |
| Palmeros-Parada, M. | NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 | ICAS2022_0801 |
| Palomar, A. | TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES | ICAS2022_0012 |
| Paluch, B. | MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS | ICAS2022_0546 |
| Panchal, I. | URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH NON-COOPERATIVE AIRSPACE USERS | ICAS2022_0567 |
| panel, op | OPEN PANEL DISCUSSION | ICAS2022_0936 |
| Pang, X. | STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGER | ICAS2022_0072 |
| Pant, R.S. | CONCEPTUAL DESIGN AND SIZING FOR A FIXED WING UAV FOR EXPLORATION OVER MARS | ICAS2022_0210 |
| Pantelakis, S.G. | ASSESSMENT OF THE SUSTAINABILITY OF THE IMPLEMENTATION OF CIRCULAR ECONOMY PRINCIPLES IN PRODUCING AIRCRAFT STRUCTURES | ICAS2022_0056 |
| Papageorgiou, A. | UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENT | ICAS2022_0659 |
| Parello, R.C. | ZERO-EMISSION REGIONAL AVIATION IN SWEDEN | ICAS2022_0650 |
| Park, S.-H. | ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION | ICAS2022_0827 |
| Pascazio, G. | NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTS | ICAS2022_0349 |
| Passiatore, D. | NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTS | ICAS2022_0349 |
| Pastor, P. | HANDLING QUALITIES OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2022_0174 |
| Pathak, A. | USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM | ICAS2022_0116 |
| Pathak, A. | ZONAL MODEL VALIDATION FOR AN ENVIRONMENTALLY FRIENDLY AIRCRAFT CARGO FIRE PROTECTION SYSTEM WITH CONTAINERIZED LOAD | ICAS2022_0159 |
| Pauly, P. | ASSESSMENT OF ENERGY-EFFICIENT APPROACHES WITH INCREASED GLIDESLOPE ANGLES | ICAS2022_0054 |
| Peerlings, B. | NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 | ICAS2022_0801 |
| Pei, Y. | TASK ALLOCATION METHOD FOR COMPLEX RECONNAISSANCE AREA BY MULTIPLE UAVS | ICAS2022_0195 |
| Peklar, G. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Pelin, C.-E. | TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINS | ICAS2022_0822 |
| Pellegrino, A. | ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT | ICAS2022_0234 |
| Pendry, S. | FLYZERO: THE UK VISION FOR ZERO-CARBON EMISSION AIR TRAVEL | ICAS2022_0908 |
| Penela, L.A. | WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE | ICAS2022_0215 |
| Peng, S.-H. | DEVELOPMENT OF AN AERODYNAMIC ANALYSIS TOOL FOR BOUNDARY LAYER INGESTION CONCEPT DESIGN | ICAS2022_0362 |
| Peng, S.-H. | HYBRID RANS-LES MODELLING: SOME RECENT DEVELOPMENT AND AERODYNAMIC APPLICATIONS | ICAS2022_0376 |
| Perdolt, D. | EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONS | ICAS2022_0860 |
| Pereira, J. | OPTIMIZATION OF AN ACTIVE DAMPING SYSTEM FOR USE WITH A SINGLE STRUT MOUNT | ICAS2022_0024 |
| Pereira, R.L. | DESIGN OF STABILITY AUGMENTATION SYSTEMS FOR A FLEXIBLE AIRCRAFT USING LQ OUTPUT-FEEDBACK CONTROL VIA LMI | ICAS2022_0623 |
| Pereira, L. | THE BENEFIT OF BILATERAL RESEARCH NETWORKS - THE SARC AND BARINET INITIATIVES AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICS | ICAS2022_0681 |
| Pereira, R.L. | LPV/LFR CONTROL FOR ACTIVE FLUTTER SUPPRESSION OF A SMART AIRFOIL MODEL | ICAS2022_0816 |
| Pereira, L. | CRITICALITY AND COMFORT ZONE SUPPORTING DESIGN CHOICES TO ACHIEVE SUSTAINABLE REQUIREMENTS: THE CASE OF ELECTRIC AIRCRAFT | ICAS2022_0875 |
| Persson, M. | INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATION | ICAS2022_0245 |
| Pertz, J. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Peter, F. | COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN | ICAS2022_0149 |
| Petersson, T. | THE SWEDISH AIR FORCE INTO THE FUTURE – AIMING FOR A HIGHER GROUND AND A SHARPER EDGE | ICAS2022_0937 |
| Petrachi, P. | ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT | ICAS2022_0234 |
| Petrolo, M. | A GLOBAL/LOCAL ELEMENT-WISE APPROACH FOR THE BUCKLING AND POST-BUCKLING ANALYSIS OF THIN MULTILAYERED STRUCTURES | ICAS2022_0253 |
| Petropoulos, I. | AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN | ICAS2022_0155 |
| Petrosino, F. | COMPARISON OF ANALYTICAL SEMI-EMPIRICAL MODEL FOR JET NOISE PREDICTION | ICAS2022_0855 |
| Peukert, B. | REAL-TIME IDENTIFICATION OF USER ACTIONS IN COMPUTER-AIDED MANUFACTURING USING MACHINE LEARNING AND COMPUTER VISION | ICAS2022_0534 |
| Peukert, M. | STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATION | ICAS2022_0903 |
| Pezzella, G. | AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLES | ICAS2022_0241 |
| Pezzella, G. | AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE | ICAS2022_0259 |
| Pfeiffer, H. | SIGMOIDAL SENSING DEVICES FOR MONITORING TO IMPROVE MAINTENANCE OPERATIONS IN AERONAUTICS | ICAS2022_0454 |
| Pham, C.-A. | MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES | ICAS2022_0813 |
| Phiboon, T. | AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION | ICAS2022_0413 |
| Piani, R. | STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES | ICAS2022_0336 |
| Piccirillo, G. | LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES | ICAS2022_0498 |
| Pilidis, P. | PROPULSION SYSTEM INTEGRATION FOR A FIRST GENERATION HYDROGEN CIVIL AIRLINER? | ICAS2022_0950 |
| Pimenta, T.C. | USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION | ICAS2022_0389 |
| Pinon Fischer, O. | NEXT STEPS TOWARDS CERTIFICATION BY ANALYSIS - A DIGITAL THREAD PERSPECTIVE | ICAS2022_0955 |
| Pinter, Z. | MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING | ICAS2022_0176 |
| Pio, D.M. | LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP | ICAS2022_0869 |
| Piprek, P. | A GENERALISED MULTI-OBJECTIVE ISLAND MODEL FOR FLIGHT CONTROL SYSTEM CLEARANCES | ICAS2022_0275 |
| Pla Guerrero, D. | INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT | ICAS2022_0326 |
| Planas, D. | HANDLING QUALITIES OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2022_0174 |
| Plančs, T. | SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES | ICAS2022_0084 |
| Plančs, T. | AIRCRAFT FLEET MODELS USING A BOTTOM-UP APPROACH FOR SIMULATING AVIATION TECHNOLOGICAL PROSPECTIVE SCENARIOS | ICAS2022_0117 |
| Planquart, P. | WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAP | ICAS2022_0232 |
| Pobikrowska, K. | OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANE | ICAS2022_0576 |
| Poirel, D. | NUMERICAL MODELLING OF PITCHING WINGS FOR GUST MITIGATION | ICAS2022_0406 |
| Polacsek, C. | AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTS | ICAS2022_0058 |
| Polacsek, C. | LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES | ICAS2022_0339 |
| Polepeddi, V. | REGIONAL TRANSPORT AIRCRAFT DESIGN USING TURBO-ELECTRIC DISTRIBUTED PROPULSION (TEDIP) SYSTEM | ICAS2022_0609 |
| Polishchuk, T. | PERFORMANCE EVALUATION OF THE ARRIVAL OPERATIONS IN TERMINAL AREA | ICAS2022_0825 |
| Polla, A. | NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMS | ICAS2022_0396 |
| Pollet, F. | A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONS | ICAS2022_0383 |
| Pommier-Budinger, V. | SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES | ICAS2022_0084 |
| Pommier-Budinger, V. | AIRCRAFT FLEET MODELS USING A BOTTOM-UP APPROACH FOR SIMULATING AVIATION TECHNOLOGICAL PROSPECTIVE SCENARIOS | ICAS2022_0117 |
| Pommier-Budinger, V. | STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS | ICAS2022_0151 |
| Pommier-Budinger, V. | FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFT | ICAS2022_0214 |
| Pommier-Budinger, V. | PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES | ICAS2022_0289 |
| Pommier-Budinger, V. | A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS | ICAS2022_0568 |
| Pontillo, A. | GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMP | ICAS2022_0644 |
| Porcarelli, A. | DEVELOPMENT OF A CFD MODEL AND METHODOLOGY FOR THE INTERNAL FLOW SIMULATION IN A HYDROGEN-POWERED UAV | ICAS2022_0051 |
| Posada-Duque, J. | NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 | ICAS2022_0801 |
| Possamai, J. | A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY | ICAS2022_0723 |
| Possamai, J. | UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO | ICAS2022_0729 |
| Powell, A.J. | A GLOBAL APPROACH TO ASSESSING THE CLIMATE RESILIENCE OF AIRPORTS | ICAS2022_0922 |
| Pradas, A. | DEMONSTRATING AN APPROACH FOR MULTIDISCIPLINARY SET BASED DESIGN WITHIN AN AEROSPACE RESEARCH PROJECT - DEFAINE | ICAS2022_0661 |
| Prado, L.A.S.A | DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT – LIFE CYCLE ASSESSMENT ACTIVITIES AT ECOTECH / CLEANSKY 2 | ICAS2022_0895 |
| Prince, S.A. | VALIDATION STUDY OF BLUNTED AND SHARP CONES AT HYPERSONIC SPEED | ICAS2022_0147 |
| Prince, S.A. | EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILTROTOR AIRCRAFT | ICAS2022_0530 |
| Proenca, A.R. | EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILTROTOR AIRCRAFT | ICAS2022_0530 |
| Proesmans, P. | MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN | ICAS2022_0602 |
| Proesmans, P. | PROPELLER AIRCRAFT DESIGN OPTIMIZATION FOR CLIMATE IMPACT REDUCTION | ICAS2022_0819 |
| Prustomersky, M. | LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFT | ICAS2022_0719 |
| Pschirer, M. | USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAM | ICAS2022_0116 |
| Pschirer, M. | ZONAL MODEL VALIDATION FOR AN ENVIRONMENTALLY FRIENDLY AIRCRAFT CARGO FIRE PROTECTION SYSTEM WITH CONTAINERIZED LOAD | ICAS2022_0159 |
| Pülm, S. | XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEM | ICAS2022_0228 |
| Qiao, N. | AN INVESTIGATION ON THE IMPROVEMENT FOR TANDEM WING PITCHING MOMENT CHARACTERISTICS | ICAS2022_0050 |
| Qiao, N.-X. | DESIGN AND EFFICIENCY ANALYSIS OF EVTOL CONTRA-ROTATING PROPELER | ICAS2022_0060 |
| Qiao, J.-L. | A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT | ICAS2022_0584 |
| Qiao, H. | NUMERICAL INVESTIGATION ON THE AERO-PROPULSION EFFECT OF DISTRIBUTED PROPULSION FOR V/VTOL APPLICATION | ICAS2022_0674 |
| Qiu, T. | SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATION | ICAS2022_0386 |
| Qu, F. | AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK | ICAS2022_0199 |
| Qu, Q.L. | NUMERICAL STUDY ON WATER DISPLACEMENT DRAG CHARACTERISTICS OF AIRCRAFT ELASTIC TIRE ON CONTAMINATED RUNWAYS | ICAS2022_0329 |
| Qu, L. | IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT | ICAS2022_0421 |
| Quaranta, G. | EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING THE WIND TUNNEL: HELICOPTER SHIP LANDING CASE | ICAS2022_0625 |
| Qudus, S. | DATA-DRIVEN APPROACH TO OPTIMAL AIRCRAFT MAINTENANCE | ICAS2022_0871 |
| Quintanilha Jr, H. | ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER | ICAS2022_0887 |
| Quix, H. | RECENT ACTIVITIES ON FLOW QUALITY ASSESSMENT AT THE EUROPEAN TRANSONIC WINDTUNNEL | ICAS2022_0061 |
| Rachdi, A. | NEW GENERATION SPACE VEHICLE OPERATIONS IN THE UNITED ARAB EMIRATES – AN AIRSPACE AND RISK ASSESSMENT | ICAS2022_0698 |
| Raddatz, F. | DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTS | ICAS2022_0868 |
| Rade, D.A. | STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWS | ICAS2022_0726 |
| Radhakrishnan, K. | MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN | ICAS2022_0602 |
| Radomsky, L. | A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTS | ICAS2022_0850 |
| Radtke, J. | OPEN CAVITY SIMULATIONS UNDER SIDESLIP FLOW CONDITIONS | ICAS2022_0173 |
| Rafael, C.F. | LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP | ICAS2022_0869 |
| Rafik, Y. | PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES | ICAS2022_0289 |
| Rahman, H. | OPTIMAL DESIGN OF STIFFENED PANELS UNDER BUCKLING CONSTRAINTS: A DESIGN METHODOLOGY CONSIDERING CAD-BASED PARAMETERIZATION WITH SIMULTANEOUS LAYOUT AND SIZING OPTIMIZATION | ICAS2022_0393 |
| Raj, P. | REGIONAL TRANSPORT AIRCRAFT DESIGN USING TURBO-ELECTRIC DISTRIBUTED PROPULSION (TEDIP) SYSTEM | ICAS2022_0609 |
| Rajaram, D. | ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH | ICAS2022_0817 |
| Rajkumar, K. | OPEN CAVITY SIMULATIONS UNDER SIDESLIP FLOW CONDITIONS | ICAS2022_0173 |
| Rameshbabu, R. | ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH | ICAS2022_0817 |
| Rammos, L. | CERTIFICATION ASPECTS OF AN EARTH OBSERVATION PAYLOAD INSTALLED ON COMMERCIAL TRANSPORT AIRCRAFT | ICAS2022_0354 |
| Ramos, P.G. | EXPERIMENTAL AND NUMERICAL ANALYSIS OF A PRE-STRESSED TENSEGRITY MEMBRANE | ICAS2022_0038 |
| Ramos, A.C.B. | USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION | ICAS2022_0389 |
| Ramos, B.M. | A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENT | ICAS2022_0523 |
| Ramos, B.M. | EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMAS | ICAS2022_0526 |
| Rangel, R.K. | HYDRO ENVIRONMENTAL AND ELECTRICAL ASSETS MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV | ICAS2022_0017 |
| Ranman, R. | EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT | ICAS2022_0788 |
| Raposo, C.L.S. | COMPUTATIONAL STUDY OF AIRFLOW AND DISPERSION OF AIRBORNE PATHOGENS INSIDE AN AIRCRAFT CABIN | ICAS2022_0911 |
| Rapp, M. | NOVEL PATHWAYS TO SUSTAINABLE AVIATION | ICAS2022_0688 |
| Ratei, P. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Rath, J.-E. | A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE | ICAS2022_0791 |
| Rauscher, F. | VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERING | ICAS2022_0063 |
| Raute, R. | SERIES OR PARALLEL HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEMS? CASE STUDIES OF THE ATR42 AND ATR72 | ICAS2022_0163 |
| Raza, H. | HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE STRIKE ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT | ICAS2022_0718 |
| Raza, H. | DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURES | ICAS2022_0734 |
| Raza, M.A. | HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS | ICAS2022_0894 |
| Razafimahazo, E. | TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONES | ICAS2022_0655 |
| Rebollo, M. | TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES | ICAS2022_0012 |
| Reckzeh, D. | TECHNOLOGY INTEGRATION FOR FUTURE AIRCRAFT CONFIGURATIONS | ICAS2022_0129 |
| Reichenwallner, C. | MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIES | ICAS2022_0575 |
| Reichenwallner, C. | AN EVALUATION METHOD FOR AIRCRAFT ACTUATION SYSTEMS OPERATIONAL COST | ICAS2022_0601 |
| Reimer, L. | APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT | ICAS2022_0892 |
| Reinap, A. | ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR | ICAS2022_0382 |
| Reinap, A. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| Reiser, C. | LONG TOUCHDOWN THROUGH A SAFETY-II PERSPECTIVE | ICAS2022_0185 |
| Reist, T.A. | A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATION TO THE STRUT-BRACED-WING AND HYBRID-WING-BODY CONFIGURATIONS | ICAS2022_0748 |
| Renzoni, P. | GARTEUR: NEARLY HALF A CENTURY OF EUROPEAN COLLABORATION IN AERONAUTICS | ICAS2022_0910 |
| Resende, G.J. | STUDY OF EFFECTS ON THE WING'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPAN | ICAS2022_0889 |
| Reysset, A. | FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFT | ICAS2022_0214 |
| Rezgui, D. | LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPS | ICAS2022_0524 |
| Rho, H.-G. | ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION | ICAS2022_0827 |
| Riabov, V. | APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS | ICAS2022_0643 |
| Riaz, A. | SET-BASED DESIGN COORDINATION BETWEEN COUPLED SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVE | ICAS2022_0372 |
| Ribeiro, M. | URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH NON-COOPERATIVE AIRSPACE USERS | ICAS2022_0567 |
| Ribeiro, M.Y.D. | DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY | ICAS2022_0662 |
| Ricardo Jr, J.A. | COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMS | ICAS2022_0340 |
| Ricci, S. | DESIGN OF AN INNOVATIVE WING TIP FOR AEROELASTIC CONTROL: FROM SCRATCH TO FLIGHT TEST | ICAS2022_0436 |
| Ricci, S. | DESIGN AND EXPERIMENTAL TESTING OF A DROOP NOSE MORPHING FOR ADVANCED REGIONAL AIRCRAFT | ICAS2022_0861 |
| Richter, K. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Rider, C. | VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA | ICAS2022_0124 |
| Righi, A.R.S. | A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTS | ICAS2022_0672 |
| Ringertz, U. | RAPID PROTOTYPING IN AIRCRAFT DESIGN USING CFD, WIND TUNNEL AND FLIGHT TESTING | ICAS2022_0441 |
| Rispoli, A. | VALIDATION OF SCALED FLIGHT TESTING | ICAS2022_0375 |
| Ritter, J. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Rivero, I. | TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES | ICAS2022_0012 |
| Rizzi, A. | AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES | ICAS2022_0104 |
| Rizzi, A. | IMPROVING STALL CHARACTERISTICS OF UCAV WING WITH VORTEX GENERATORS | ICAS2022_0238 |
| Rizzi, A. | AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 2 | ICAS2022_0946 |
| Rodrigues, V.A. | HYDRO ENVIRONMENTAL AND ELECTRICAL ASSETS MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV | ICAS2022_0017 |
| Rodrigues, M.R.B. | APPLICATION OF THE VIRTUAL CRACK CLOSURE TECHNIQUE FOR CRACKS IN BUILT-UP PANELS | ICAS2022_0799 |
| Roh, C. | EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV | ICAS2022_0488 |
| Romero, J. | TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES | ICAS2022_0012 |
| Romero-Ramirez, R. | EFFECT OF NITRIDING ON MICROSTRUCTURE AND MECHANICAL PROPERTIES ON A TI64 ALLOY FOR AEROSPACE APPLICATIONS | ICAS2022_0607 |
| Roncioni, P. | AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECT | ICAS2022_0235 |
| Roncioni, P. | HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS | ICAS2022_0572 |
| Roncioni, P. | AERODATABASE DEVELOPMENT AND INTEGRATION OF SUPERSONIC/HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROJECT | ICAS2022_0596 |
| Rooseleer, F. | FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURES | ICAS2022_0958 |
| Rosado, T. | OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM | ICAS2022_0891 |
| Rosado de Paula, T. | A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY | ICAS2022_0723 |
| Rosell, D. | LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTION | ICAS2022_0088 |
| Rosell, D. | PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE | ICAS2022_0782 |
| Rossato, D.B. | FLIGHT CONTROLLABILITY ANALYSIS IN TIGHT FORMATION AND CRUISE FLIGHT FOR FUEL SAVING | ICAS2022_0273 |
| Rossow, C.-C. | FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION | ICAS2022_0708 |
| Roth, Y.C. | SUSTAINABLE TECHNOLOGIES FOR COMMERCIAL AIRCRAFT OF TOMORROW - INTEGRATED MULTIFUNCTIONAL FUSELAGE DEMONSTRATOR | ICAS2022_0924 |
| Roumeliotis, I. | A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFT | ICAS2022_0703 |
| Roush, K. | DESIGNING FOR SECURITY: A CYBERSECURITY INTRODUCTION FOR AEROSPACE EDUCATION | ICAS2022_0180 |
| Rudolph, M. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Ruiz, S. | AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTS | ICAS2022_0693 |
| Ruocco, M. | MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFT | ICAS2022_0649 |
| Russo, P. | MECHANICAL CHARACTERIZATION OF A COMPOSITE STRUCTURAL BATTERY LAMINATE | ICAS2022_0690 |
| Ryu, H. | A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSB | ICAS2022_0222 |
| Rönnberg, N. | EXPECTED TEAMWORK ATTRIBUTES BETWEEN HUMAN OPERATOR AND AUTOMATION IN AIR TRAFFIC CONTROL | ICAS2022_0504 |
| Saar de Moraes, R. | CONCEPT LEVEL EXPLORATION OF IMA-BASED NETWORKED PLATFORMS WITH MIXED TIME-SENSITIVE COMMUNICATION REQUIREMENTS | ICAS2022_0660 |
| Sabel, D. | INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATION | ICAS2022_0245 |
| Sabel, D. | VISION-BASED LOCALISATION FOR AUTONOMOUS AERIAL NAVIGATION IN GNSS-DENIED SITUATIONS | ICAS2022_0485 |
| Saccone, G. | HIGH PRESSURE HYDROGEN OXYGEN COMBUSTION KINETIC ASSESSMENT FOR AIR-BREATHING PROPULSION SUPERSONIC GREEN AVIATION | ICAS2022_0845 |
| Sachs, F. | THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALE | ICAS2022_0328 |
| Sadeghinia, N. | INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM ALLOY 780 | ICAS2022_0206 |
| Saluzzi, V. | THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENT | ICAS2022_0615 |
| Salze, E. | AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTS | ICAS2022_0058 |
| Sanchez-Carmona, A. | ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORA | ICAS2022_0699 |
| Sánchez-Moreno, F. | OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELS | ICAS2022_0167 |
| Sanchez-Moreno, F. | TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINES | ICAS2022_0380 |
| Sander, I. | TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS | ICAS2022_0604 |
| Sanders, D. | A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFT | ICAS2022_0703 |
| Sant'Ana, V.T. | LATERAL-DIRECTIONAL AERODYNAMIC MODELLING FOR NUMERICAL RESULTS USING NEURO-FUZZY WITH DIFFERENTIAL EVOLUTION | ICAS2022_0870 |
| Santhosh, S. | AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACH | ICAS2022_0478 |
| Santos, D.A. | COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMS | ICAS2022_0340 |
| Santos, R. | ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER | ICAS2022_0887 |
| Sapienza, V. | WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA | ICAS2022_0280 |
| Sapienza, V. | A STUDENT TEAM BASED TEACHING APPROACH: THE TEAM S55 EXPERIENCE | ICAS2022_0315 |
| Sapienza, S. | A STUDENT TEAM BASED TEACHING APPROACH: THE TEAM S55 EXPERIENCE | ICAS2022_0315 |
| Saracoglu, B.H. | HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS | ICAS2022_0572 |
| Sarmento, A.G.P. | PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING | ICAS2022_0694 |
| Sarmento, A.G.P. | A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY | ICAS2022_0723 |
| Sarmento, A.G.P. | UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO | ICAS2022_0729 |
| Sarperi, L. | LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEM | ICAS2022_0144 |
| Sasaki, D. | COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHOD | ICAS2022_0416 |
| Sasaki, K. | REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER | ICAS2022_0605 |
| Sasamori, M. | EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETS | ICAS2022_0243 |
| Sasi, S. | A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFT | ICAS2022_0703 |
| Sato, M. | AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION | ICAS2022_0192 |
| Sato, M. | FLIGHT VERIFICATION OF AUTOMATIC TRANSITION FOR QUAD TILT WING SMALL UAV | ICAS2022_0740 |
| Sato, A. | STUDY ON THE APPLICATION OF EMULSIFIED FUEL IN SMALL JET ENGINES | ICAS2022_0751 |
| Savio, M.C. | STUDY OF EFFECTS ON THE WING'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPAN | ICAS2022_0889 |
| Scagnellato, L. | ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITION | ICAS2022_0085 |
| Scarano, F. | UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLS | ICAS2022_0611 |
| Schagerl, M. | FATIGUE OF NOTCHED STANDARD SPECIMENS – THE INFLUENCE OF THE STRESS GRADIENT ON THE S-N CURVE IN AL2024 | ICAS2022_0561 |
| Schalk, L. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Schaper, M. | REAL-TIME CALCULATION AND ADAPTION OF CONFLICT-FREE AIRCRAFT GROUND TRAJECTORIES | ICAS2022_0213 |
| Scheibe, K. | CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACH | ICAS2022_0102 |
| Scherer, S.P. | REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT | ICAS2022_0797 |
| Scherer, S. | AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT | ICAS2022_0835 |
| Scherer, S. | EXTENSION OF THE CAPABILITIES OF AN AUTOMATIC LANDING SYSTEM WITH PROCEDURES MOTIVATED BY VISUAL-FLIGHT-RULES | ICAS2022_0841 |
| Schier-Morgenthal, S. | AN OPERATIONAL CONCEPT FOR THE INTEGRATION OF URBAN AIR MOBILITY VEHICLES INTO THE AIR TRAFFIC CONTROL PROCESSES | ICAS2022_0451 |
| Schmeink, J. | KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND MASS ESTIMATION OF RUBBER AERO ENGINES | ICAS2022_0497 |
| Schminder, J. | ZONAL MODEL BASED AIRCRAFT PASSENGER THERMAL COMFORT COMPARATIVE STUDY | ICAS2022_0338 |
| Schmitz, V. | COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN | ICAS2022_0149 |
| Schmollgruber, P. | VALIDATION OF SCALED FLIGHT TESTING | ICAS2022_0375 |
| Schmollgruber, P. | CHALLENGES OF MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR GREEN AVIATION | ICAS2022_0965 |
| Schneider, J. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Schofield, M.R. | IMPACT OF NASCENT TECHNOLOGIES ON THE SUSTAINABILITY ATTRIBUTES OF AN EVOLUTIONARY SINGLE-AISLE AIRCRAFT | ICAS2022_0543 |
| Schreiner, B.D.J. | TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINES | ICAS2022_0380 |
| Schröder, D. | VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIR | ICAS2022_0083 |
| Schröder, B.-O. | TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONS | ICAS2022_0657 |
| Schuetz, C.G. | AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTS | ICAS2022_0693 |
| Schultz, M. | DEVELOPING A DEPARTURE QUEUE MODEL FOR INTEGRATED ARRIVAL AND DEPARTURE OPERATION OF RUNWAYS | ICAS2022_0106 |
| Schultz, M. | REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMIC | ICAS2022_0486 |
| Schulz, S. | EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERS | ICAS2022_0656 |
| Schwalb, D. | A GENERALISED MULTI-OBJECTIVE ISLAND MODEL FOR FLIGHT CONTROL SYSTEM CLEARANCES | ICAS2022_0275 |
| Schwalb, D. | EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATION | ICAS2022_0467 |
| Schwarz, F. | MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING | ICAS2022_0176 |
| Schwarz, C.W. | THE SENS4ICE EU PROJECT – SENSORS AND CERTIFIABLE HYBRID ARCHITECTURES FOR SAFER AVIATION IN ICING ENVIRONMENT – PROJECT OVERVIEW AND INITIAL RESULTS | ICAS2022_0794 |
| Schweighofer, F. | REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFT | ICAS2022_0797 |
| Schültke, F. | COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN | ICAS2022_0149 |
| Schüppstuhl, T. | TECHNICAL CONCEPTS FOR INSPECTING UAVS FOR DAMAGE | ICAS2022_0047 |
| Schüppstuhl, T. | A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE | ICAS2022_0791 |
| Schäfer, M. | COUPLING OF MODEL-BASED SYSTEMS ENGINEERING AND SAFETY ANALYSIS IN CONCEPTUAL AIRCRAFT SYSTEM DESIGN | ICAS2022_0082 |
| Sciacovelli, L. | NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTS | ICAS2022_0349 |
| Scigliano, R. | COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION | ICAS2022_0342 |
| Scott, M.J. | AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATION | ICAS2022_0747 |
| Sedlacek, D. | STRAKE SECTION IMPACT ON HYBRID-DELTA-WING AERODYNAMICS | ICAS2022_0075 |
| Seefried, A. | EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATION | ICAS2022_0467 |
| Seidler, R.B. | XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEM | ICAS2022_0228 |
| Seidler, R. | CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM | ICAS2022_0606 |
| Sekine, K. | AIR TRAFFIC SIMULATION ACROSS FIR IN JAPAN USING CELLULAR AUTOMATON | ICAS2022_0401 |
| Sekler, H. | SIGMOIDAL SENSING DEVICES FOR MONITORING TO IMPROVE MAINTENANCE OPERATIONS IN AERONAUTICS | ICAS2022_0454 |
| Selegĺrd, L. | EFFECT OF NITRIDING ON MICROSTRUCTURE AND MECHANICAL PROPERTIES ON A TI64 ALLOY FOR AEROSPACE APPLICATIONS | ICAS2022_0607 |
| Selier, M. | DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFT | ICAS2022_0566 |
| Sequeira, C. | VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA | ICAS2022_0124 |
| Serafini, J. | SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSIS | ICAS2022_0370 |
| Serhii , D. | DATA-DRIVEN APPROACH TO OPTIMAL AIRCRAFT MAINTENANCE | ICAS2022_0871 |
| Sever, N. | A FAULT INTEGRATOR BASED VOTE&MONITOR DESIGN FOR GRACEFULL DEGRADATION IN MULTIPLE REDUNDANT SAFETY CRITICAL SYSTEMS | ICAS2022_0472 |
| Sezer, A.-O. | NUMERICAL INVESTIGATION OF ROTORCRAFT PRESSURE ERROR CORRECTION BY UTILIZATION OF AIR DAMS | ICAS2022_0357 |
| Shah, H. | INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT | ICAS2022_0326 |
| Shahi, H. | A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR | ICAS2022_0826 |
| Shang, Y. | DESIGN OF AERO-ENGINE FADEC POWER SUPPLY CONTROL SYSTEM BASED ON FORWARD DESIGN | ICAS2022_0023 |
| Shang, S. | TWO-PHASE NUMERICAL SIMULATION INVESTIGATION ON THE EFFECTS OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCE | ICAS2022_0029 |
| Sharma, S. | AN INTERNATIONAL RESEARCH PERSPECTIVE ON AIRSPACE INTEGRATION IN THE FRAMEWORK OF URBAN AIR MOBILITY | ICAS2022_0948 |
| Sharpe, J. | VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA | ICAS2022_0124 |
| Shaw, S. | CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIES | ICAS2022_0934 |
| Sheaf, C. | A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES | ICAS2022_0162 |
| Sheaf, C. | OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELS | ICAS2022_0167 |
| Sheaf, C. | TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINES | ICAS2022_0380 |
| Sheikh, M.Z. | HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS | ICAS2022_0894 |
| Shen, Y. | EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING | ICAS2022_0078 |
| Shen, J. | HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS | ICAS2022_0894 |
| Shetty, N.K. | NUCLEAR POWERED AIR-BREATHING ELECTRIC THRUSTERS USED IN UAVS FOR EXTRA-TERRESTRIAL APPLICATIONS | ICAS2022_0019 |
| Shi, Y.-Q. | EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECK | ICAS2022_0847 |
| Shi, X.Z. | HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS | ICAS2022_0894 |
| Shibasaki, S. | STUDY ON THE APPLICATION OF EMULSIFIED FUEL IN SMALL JET ENGINES | ICAS2022_0751 |
| Shima, E. | AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION | ICAS2022_0192 |
| Shimoyama, K. | DEEP LEARNING TECHNIQUES FOR HIGH-DIMENSIONAL SURROGATE-BASED AERODYNAMIC DESIGN | ICAS2022_0187 |
| Shin, S. | AIRCRAFT DESIGN PARAMETER ESTIMATION USING DATA-DRIVEN MACHINE LEARNING MODELS | ICAS2022_0435 |
| Shipley, J. | LATEST DEVELOPMENTS IN HIGH PRESSURE HEAT TREATMENT OF AEROSPACE COMPONENTS | ICAS2022_0026 |
| Shiva Prakasha, P. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Siami, A. | STRUCTURAL ANALYSIS OF TWISTED/CURVED BEAMS USING A HYBRID METHOD | ICAS2022_0802 |
| Sieberer, S. | FATIGUE OF NOTCHED STANDARD SPECIMENS – THE INFLUENCE OF THE STRESS GRADIENT ON THE S-N CURVE IN AL2024 | ICAS2022_0561 |
| Sieradzki, A. | PROPELLER AEROACOUSTIC MODELS IN VARIABLE-FIDELITY DESIGN OPTIMIZATION | ICAS2022_0710 |
| Silberhorn, D. | THERMODYNAMIC POTENTIAL OF TURBOFAN ENGINES WITH DIRECT COMBUSTION OF HYDROGEN | ICAS2022_0499 |
| Silberhorn, D. | IMPACT OF THE NUMBER OF WING STATIONS ON THE TWIST DISTRIBUTION OF A BWB CONCEPTUAL AIRCRAFT DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTION | ICAS2022_0854 |
| Silva, V.T. | MULTIPOINT AERODYNAMIC DESIGN OF A NACELLE FOR AN ELECTRIC FAN | ICAS2022_0138 |
| Silva, G.P.G. | EXPERIMENTAL STUDIES ON THE INTERACTION BETWEEN PROPELLERS AND WING | ICAS2022_0262 |
| Silva, M.V.R.J. | EXPERIMENTAL STUDIES ON THE INTERACTION BETWEEN PROPELLERS AND WING | ICAS2022_0262 |
| Silva, G.P.G. | PUSHER PROPELLER INFLUENCE ON A LAMINAR WING TRANSITION LOCATION USING INFRARED THERMOGRAPHY | ICAS2022_0678 |
| Silva, R.G.A. | PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING | ICAS2022_0694 |
| Silva, S. | DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES USING NEURAL NETWORKS AND HYBRID DATA | ICAS2022_0705 |
| Silvestre, F.J. | DESIGN OF STABILITY AUGMENTATION SYSTEMS FOR A FLEXIBLE AIRCRAFT USING LQ OUTPUT-FEEDBACK CONTROL VIA LMI | ICAS2022_0623 |
| Silvestre, F.J. | TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONS | ICAS2022_0657 |
| Silvestre, F.J. | LPV/LFR CONTROL FOR ACTIVE FLUTTER SUPPRESSION OF A SMART AIRFOIL MODEL | ICAS2022_0816 |
| Silvestre, F.J. | A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR | ICAS2022_0826 |
| Simőes Lopes Junior, R. | A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL | ICAS2022_0513 |
| Simone, N. | WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA | ICAS2022_0280 |
| Simorgh, A. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Simpson, A. | HYBRID ELECTRIC PROPULSION DEVELOPMENT FOR COMMERCIAL AVIATION | ICAS2022_0944 |
| Singh Gaba, G. | A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATION | ICAS2022_0704 |
| Sinisi, M. | CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL | ICAS2022_0341 |
| Sinnige, T. | RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERS | ICAS2022_0489 |
| Sjunnesson, A. | TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINE | ICAS2022_0006 |
| Sjöberg, P. | FLIGHT DYNAMICS SIMULATION AND FCS AUTO-GENERATION IN THE CONCEPTUAL DESIGN PHASE OF AN UNSTABLE SUPERSONIC AIRCRAFT | ICAS2022_0458 |
| Slongo, A.G. | A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENT | ICAS2022_0523 |
| Slongo, A.G. | EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMAS | ICAS2022_0526 |
| Sobron, A. | RAPID PROTOTYPING IN AIRCRAFT DESIGN USING CFD, WIND TUNNEL AND FLIGHT TESTING | ICAS2022_0441 |
| Sohlberg, R. | GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS | ICAS2022_0265 |
| Soler, M. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Son, C. | AIRCRAFT DESIGN PARAMETER ESTIMATION USING DATA-DRIVEN MACHINE LEARNING MODELS | ICAS2022_0435 |
| Song, Y. | MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHT | ICAS2022_0115 |
| Song, W.-P. | A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEME | ICAS2022_0157 |
| Song, W.-P. | A NUMERICAL METHOD FOR STUDY ON THE AERO-ELASTICITY OF AIR-TO-AIR MISSILES IN OVER-THE-SHOULDER LAUNCH | ICAS2022_0311 |
| Song, C. | MOTION STROKE DESIGN ON FLEXIBLE ASSEMBLY TOOLING FOR MULTIPLE AIRCRAFT COMPONENTS | ICAS2022_0314 |
| Song, W.-P. | UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODEL | ICAS2022_0330 |
| Song, Y. | IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT | ICAS2022_0421 |
| Song, W.-P. | EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTOR GENERATION | ICAS2022_0548 |
| Song, W.-P. | HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACK | ICAS2022_0555 |
| Song, W.-P. | A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT | ICAS2022_0584 |
| Song, Y.-H. | EQUIVALENT CALCULATION METHOD OF FLYOVER NOISE LEVEL OF CUTBACK TAKE-OFF FOR CIVIL JET AIRPLANE AIRWORTHINESS CERTIFICATION | ICAS2022_0626 |
| Song, S. | NUMERICAL INVESTIGATION ON THE AERO-PROPULSION EFFECT OF DISTRIBUTED PROPULSION FOR V/VTOL APPLICATION | ICAS2022_0674 |
| Soolaki, M. | REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMIC | ICAS2022_0486 |
| Sorrentino, R.T. | ZERO-EMISSION REGIONAL AVIATION IN SWEDEN | ICAS2022_0650 |
| Soula, J. | TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONES | ICAS2022_0655 |
| Sousa, J.M.M. | COMPUTATIONAL STUDY OF AIRFLOW AND DISPERSION OF AIRBORNE PATHOGENS INSIDE AN AIRCRAFT CABIN | ICAS2022_0911 |
| Souza, A.G. | PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING | ICAS2022_0694 |
| Souza, A. | OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM | ICAS2022_0891 |
| Spampinato, C. | ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT | ICAS2022_0234 |
| Speckmaier, M. | AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT | ICAS2022_0835 |
| Spencer, R. | COMPUTATIONALLY ECONOMICAL METHODS FOR LANDING GEAR NOISE SIMULATIONS | ICAS2022_0317 |
| Splichal, M. | TREND MONITORING OF TURBOPROP ENGINES | ICAS2022_0094 |
| Staack, I. | MODEL FIDELITY AND ITS INFLUENCE ON AIRCRAFT CONCEPTUAL DESIGN | ICAS2022_0477 |
| Staack, I. | ENVIRONMENTAL AGENT-BASED MODELLING FOR A FIREFIGHTING SYSTEM OF SYSTEMS | ICAS2022_0645 |
| Staack, I. | SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045 | ICAS2022_0804 |
| Staack, I. | LATERAL-DIRECTIONAL AERODYNAMIC MODELLING FOR NUMERICAL RESULTS USING NEURO-FUZZY WITH DIFFERENTIAL EVOLUTION | ICAS2022_0870 |
| Staack, I. | HYBRID ELECTRIC PROPULSION SYSTEM OPTIMIZATION FOR A COMMUTER AIRCRAFT | ICAS2022_0874 |
| Staack, I. | CHALLENGES OF MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR GREEN AVIATION | ICAS2022_0965 |
| Staggat, M. | ASSESSMENT OF A SERIAL COOLING CONCEPT FOR HTPEM FUEL CELL SYSTEMS FOR AVIATION APPLICATIONS | ICAS2022_0456 |
| Stalcup, E.J. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Stalewski, W. | PRELIMINARY STUDY ON A FLUIDIC DEVICE SUPPORTING AIRCRAFT-FLIGHT CONTROL | ICAS2022_0403 |
| Standingford, D. | VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA | ICAS2022_0124 |
| Staub, F. | DESIGN AND WIND TUNNEL TESTING OF A GENERAL AVIATION BLENDED WING BODY AIRCRAFT | ICAS2022_0269 |
| Stavorinus, G. | A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR | ICAS2022_0826 |
| Stefan, A. | TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINS | ICAS2022_0822 |
| Stefes, B. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Steffen, J. | VIKA - CONCEPT OF A DIGITAL PLATFORM FOR IMPLICIT KNOWLEDGE AND VIRTUAL ASSISTANCE FOR ADDITIVE MANUFACTURED PARTS | ICAS2022_0053 |
| Steffensen, R. | AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT | ICAS2022_0835 |
| Stegmüller, J. | EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS | ICAS2022_0250 |
| Steiling, D. | POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORS | ICAS2022_0347 |
| Steinert, A. | AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT | ICAS2022_0835 |
| Steinkellner, S. | A SYSTEM INTEGRATOR’S PERSPECTIVE ON VEHICLE SYSTEM EVALUATION AT THE AIRCRAFT CONCEPT STAGE | ICAS2022_0856 |
| Stekovic, S. | EFFECT OF NITRIDING ON MICROSTRUCTURE AND MECHANICAL PROPERTIES ON A TI64 ALLOY FOR AEROSPACE APPLICATIONS | ICAS2022_0607 |
| Stempfel, G. | DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELS | ICAS2022_0648 |
| Stepchuk, I. | NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 | ICAS2022_0801 |
| Stepien, H. | A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCE | ICAS2022_0332 |
| Stramigioli, S. | INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD | ICAS2022_0653 |
| Streit, T. | AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN | ICAS2022_0155 |
| Streit, T. | LOADS ANALYSIS AND STRUCTURAL OPTIMIZATION OF A LONG-RANGE TRANSPORT CONFIGURATION WITH HYBRID LAMINAR FLOW CONTROL | ICAS2022_0158 |
| Strokin, E. | TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATION | ICAS2022_0036 |
| Stromayer, A. | DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFT | ICAS2022_0921 |
| Stumpf, E. | VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIR | ICAS2022_0083 |
| Stumpf, E. | COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN | ICAS2022_0149 |
| Stumpf, E. | SORA-BASED RISK ASSESSMENT FOR CARGO UNMANNED AERIAL VEHICLES IN THE UAM FRAMEWORK | ICAS2022_0240 |
| Stumpf, E. | HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE STRIKE ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT | ICAS2022_0718 |
| Stumpf, E. | EXPERIMENTS TO INVESTIGATE LIFT PRODUCTION MECHANISMS ON OSCILLATING TRAILING-EDGE FLAPS | ICAS2022_0780 |
| Sturm, F. | MORPHING FORWARD WING SECTION SKIN DESIGN FOR A SAILPLANE CONSIDERING WING BENDING | ICAS2022_0178 |
| Su, S.-G. | RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION | ICAS2022_0760 |
| Suewatanakul, S. | WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE | ICAS2022_0215 |
| Sugawara, H. | HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA | ICAS2022_0444 |
| Sugaya, K. | UNSTEADY TURBULENT FLOW SIMULATION OF ROTOR BLADES ON MOVING CARTESIAN GRIDS USING RECURSIVE FITTING APPROACH | ICAS2022_0790 |
| Sugiura, M. | HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA | ICAS2022_0444 |
| Sui, H. | STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGER | ICAS2022_0072 |
| Suk, J.Y | EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV | ICAS2022_0488 |
| Sun, X. | A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTH | ICAS2022_0142 |
| Sun, X. | DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION | ICAS2022_0143 |
| Sun, S. | INTEGRATE ONLINE QUERY&DEFENSE INTO PROJECT BASED LEARNING TO PROMPT ENGINEERING AUTHENTIC EXPERIENCES | ICAS2022_0284 |
| Sun, P. | AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT | ICAS2022_0795 |
| Sun, F.Z. | INFLUENCE OF MANEUVERING PROCESS ON PERFORMANCE CHARACTERISTICS OF BELLY INLET OF AIRCRAFT | ICAS2022_0834 |
| Suzuki, K. | DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES | ICAS2022_0448 |
| Svensson, Ĺ. | EXPECTED TEAMWORK ATTRIBUTES BETWEEN HUMAN OPERATOR AND AUTOMATION IN AIR TRAFFIC CONTROL | ICAS2022_0504 |
| Svensson, Ĺ. | STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATION | ICAS2022_0903 |
| Swaid, M. | INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGION | ICAS2022_0840 |
| Swarthout, A. | A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES | ICAS2022_0162 |
| Symon, S. | COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMS | ICAS2022_0399 |
| Szczepanski, C. | IMPACT OF MOTION-DEPENDENT ERRORS ON THE ACCURACY OF AN UNAIDED STRAPDOWN INERTIAL NAVIGATION SYSTEM | ICAS2022_0742 |
| Szilder, K. | NUMERICAL SIMULATION OF ICE ACCRETION ON A PITOT TUBE | ICAS2022_0130 |
| Sziroczak, D. | AN INTERNATIONAL RESEARCH PERSPECTIVE ON AIRSPACE INTEGRATION IN THE FRAMEWORK OF URBAN AIR MOBILITY | ICAS2022_0948 |
| Söderquist, I. | TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS | ICAS2022_0604 |
| Taguchi, M. | ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICES | ICAS2022_0145 |
| Taguchi, Y. | DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES | ICAS2022_0448 |
| Tahk, M.-J. | CONVEX PROGRAMMING-BASED OPTIMAL THREE-DIMENSIONAL MID-COURSE GUIDANCE WITH LOSSLESS CONVEXIFICATION | ICAS2022_0810 |
| Tai, J. | SYSTEM LEVEL STUDIES FOR NASA - MODEL DEVELOPMENT TOWARD ZERO EMISSIONS | ICAS2022_0322 |
| Takachi Tomita, J. | PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE | ICAS2022_0782 |
| Takahashi, S. | COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHOD | ICAS2022_0416 |
| Takamatsu, T. | FLIGHT TESTS AND SIMULATION OF A HANG GLIDER | ICAS2022_0135 |
| Takashima, K. | DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES | ICAS2022_0448 |
| Takeda, K. | OPTIMIZATION OF AIRCRAFT FLIGHT PATHS CONSIDERING THE CONFLICTING PARAMETERS OF ECONOMY AND SAFETY | ICAS2022_0652 |
| Takizawa, H. | OPERATIONAL FEASIBILITY STUDY OF AIR TAXI SERVICE USING EVTOL | ICAS2022_0474 |
| Talamucci, T. | WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA | ICAS2022_0280 |
| Tamayama, M. | WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) | ICAS2022_0814 |
| Tamkan, A. | ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISK | ICAS2022_0532 |
| Tan, H. | EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING | ICAS2022_0078 |
| Tan, H. | DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACE | ICAS2022_0785 |
| Tanabe, Y. | HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA | ICAS2022_0444 |
| Tanahashi, Y. | WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) | ICAS2022_0814 |
| Tanaka, H. | VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGS | ICAS2022_0207 |
| Tang, J.P. | INFLUENCE OF MANEUVERING PROCESS ON PERFORMANCE CHARACTERISTICS OF BELLY INLET OF AIRCRAFT | ICAS2022_0834 |
| Tangermann, E. | OPEN CAVITY SIMULATIONS UNDER SIDESLIP FLOW CONDITIONS | ICAS2022_0173 |
| Tangermann, E. | INVESTIGATION OF LEADING-EDGE VORTICES ON A TRIPLE-DELTA-WING CONFIGURATION USING SCALE-ADAPTIVE SIMULATION | ICAS2022_0528 |
| Taniguchi, R. | EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETS | ICAS2022_0243 |
| Tarnowski, A. | MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIES | ICAS2022_0462 |
| Tarraga Prieto, J.I. | ZONAL MODEL BASED AIRCRAFT PASSENGER THERMAL COMFORT COMPARATIVE STUDY | ICAS2022_0338 |
| Tarroc Gil, S. | ZONAL MODEL BASED AIRCRAFT PASSENGER THERMAL COMFORT COMPARATIVE STUDY | ICAS2022_0338 |
| Tatsukawa, T. | AIR TRAFFIC SIMULATION ACROSS FIR IN JAPAN USING CELLULAR AUTOMATON | ICAS2022_0401 |
| Tavera Guerrero, C. | STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALL | ICAS2022_0351 |
| Taymourtash, N. | EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING THE WIND TUNNEL: HELICOPTER SHIP LANDING CASE | ICAS2022_0625 |
| Tegner, J. | ANALYSIS OF THE OPERATION OF THE PULSEJET ENGINE | ICAS2022_0120 |
| Teirlink, C. | INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT | ICAS2022_0326 |
| Teixeira, L.H.S. | EXPERIMENTAL AND NUMERICAL ANALYSIS OF A PRE-STRESSED TENSEGRITY MEMBRANE | ICAS2022_0038 |
| Teixeira, B.R. | DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY | ICAS2022_0662 |
| Tejero, F. | A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES | ICAS2022_0162 |
| Tejero, F. | OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELS | ICAS2022_0167 |
| Tejero, F. | TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINES | ICAS2022_0380 |
| Terashima, H. | NUMERICAL INVESTIGATION ON THE DOUBLE TRANSONIC DIP OF SUPERCRITICAL AIRFOIL FLUTTER | ICAS2022_0545 |
| Thang, Y.-L. | EQUIVALENT CALCULATION METHOD OF FLYOVER NOISE LEVEL OF CUTBACK TAKE-OFF FOR CIVIL JET AIRPLANE AIRWORTHINESS CERTIFICATION | ICAS2022_0626 |
| Thantanapally, C. | TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHOD | ICAS2022_0630 |
| Theofilis, V. | ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER | ICAS2022_0887 |
| Thiele, M. | EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONS | ICAS2022_0860 |
| Thielecke, F. | VALIDATION OF A HYBRID LOADS OBSERVER FOR A SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2022_0080 |
| Thielecke, F. | SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGN | ICAS2022_0665 |
| Thielecke, F. | DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK | ICAS2022_0677 |
| Thijssen, R. | PROPELLER AIRCRAFT DESIGN OPTIMIZATION FOR CLIMATE IMPACT REDUCTION | ICAS2022_0819 |
| Thoma, E.M. | ENVIRONMENTAL ASSESSMENT OF NOISE ABATEMENT APPROACH TRAJECTORIES | ICAS2022_0671 |
| Thuis, H.G.S.J. | THE GROUP OF RESPONSABLES "STRUCTURES AND MATERIALS (GOR SM)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0916 |
| Tichy, L. | WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSES | ICAS2022_0663 |
| Timmermans, L. | VALIDATION OF SCALED FLIGHT TESTING | ICAS2022_0375 |
| Tipnis, T. | WALL INTERFERENCE CORRECTIONS USING NONLINEAR LEAST-SQUARES OPTIMISATION | ICAS2022_0378 |
| Toffol, F. | DESIGN OF AN INNOVATIVE WING TIP FOR AEROELASTIC CONTROL: FROM SCRATCH TO FLIGHT TEST | ICAS2022_0436 |
| Tomita, J.T. | EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE | ICAS2022_0676 |
| Tomita, N. | WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) | ICAS2022_0814 |
| Tong, W.-T. | RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE | ICAS2022_0510 |
| Tong, M. | EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING | ICAS2022_0632 |
| Tonon, D.S. | EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE | ICAS2022_0676 |
| Topolewski, R. | MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIES | ICAS2022_0462 |
| Torga, E.M.M. | COMPETITIVITY, STRATEGY AND VALUE ON AIRPORTS A METHOD OF DIAGNOSIS, SUGGESTIONS AND ACTIONS FOR INTERNATIONAL AIRPORTS WITH A CASE STUDY OF CNF | ICAS2022_0022 |
| Tormalm, M. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| Toropov, V.V. | AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK | ICAS2022_0199 |
| Toropov, V. | APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS | ICAS2022_0643 |
| Toussaint, C. | VALIDATION OF SCALED FLIGHT TESTING | ICAS2022_0375 |
| Travostino, G. | WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAP | ICAS2022_0232 |
| Tremolet, A. | MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS | ICAS2022_0546 |
| Trifari, V. | REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION | ICAS2022_0323 |
| Trinchieri, P. | DISRUPTIVE TECHNOLOGIES TO ENABLE ZERO-CARBON HYDROGEN–POWERED [HPA] SHORT RANGE AIRCRAFT | ICAS2022_0931 |
| Trochelmann, N. | DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK | ICAS2022_0677 |
| Truc-Hermel, A. | A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS | ICAS2022_0568 |
| Truong, H. | USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC PERFORMANCE OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFT | ICAS2022_0251 |
| Tschida, C. | TOWARD DIRECT DRIVE ELECTRIFIED PROPULSION CONCEPTS FOR SUSTAINABLE AVIATION | ICAS2022_0736 |
| Tsentis, S.E. | MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENT | ICAS2022_0943 |
| Tsuchiya, T. | DESIGN AND WIND TUNNEL TESTING OF A GENERAL AVIATION BLENDED WING BODY AIRCRAFT | ICAS2022_0269 |
| Tsuchiya, T. | DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES | ICAS2022_0448 |
| Tsuchiya, T. | OPENVSP BASED AERODYNAMIC DESIGN OPTIMIZATION TOOL BUILDING METHOD AND ITS APPLICATION TO TAILLESS UAV | ICAS2022_0858 |
| Tugrul, E. | A FAULT INTEGRATOR BASED VOTE&MONITOR DESIGN FOR GRACEFULL DEGRADATION IN MULTIPLE REDUNDANT SAFETY CRITICAL SYSTEMS | ICAS2022_0472 |
| Tumino, D. | RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS | ICAS2022_0218 |
| Turner, M.G. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Tyburzy, L. | REAL-TIME CALCULATION AND ADAPTION OF CONFLICT-FREE AIRCRAFT GROUND TRAJECTORIES | ICAS2022_0213 |
| Tzortzinis, G. | INVESTIGATION ON INTEGRATING RECYCLABILITY AS A FUNCTION AT THE DESIGN PHASE OF COMPLEX-LOADED STRUCTURAL COMPONENTS | ICAS2022_0125 |
| v. Geyr, J. | AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN | ICAS2022_0155 |
| Vaghela, P. | HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE STRIKE ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT | ICAS2022_0718 |
| Vaghela, P. | DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURES | ICAS2022_0734 |
| Valpiani, F. | NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITCH ANGLE | ICAS2022_0355 |
| van der Laan, T. | A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORK | ICAS2022_0618 |
| van der Sman, E. | NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050 | ICAS2022_0801 |
| van der Ven, H. | THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0915 |
| van Heerden, A.S.J. | A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFT | ICAS2022_0703 |
| van Manen, R. | CLEAN AVIATION PROGRAMME RATIONALE AND OVERVIEW | ICAS2022_0928 |
| Vankan, J. | THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENT | ICAS2022_0615 |
| Vassberg, J. | JETZERO BWB ENABLING TECHNOLOGIES | ICAS2022_0392 |
| Vassberg, J. | JETZERO BWB ENABLING TECHNOLOGIES | ICAS2022_0951 |
| Vaz Linn, R. | ZONAL MODEL BASED AIRCRAFT PASSENGER THERMAL COMFORT COMPARATIVE STUDY | ICAS2022_0338 |
| Vaziri-Zanjani, M.A. | WING LOADING PROCESS IN KNOWLEDGE-BASED AIRCRAFT DESIGN AND OPTIMIZATION FRAMEWORK | ICAS2022_0519 |
| Vechtel, D. | ASSESSMENT OF ENERGY-EFFICIENT APPROACHES WITH INCREASED GLIDESLOPE ANGLES | ICAS2022_0054 |
| Vechtel, D. | THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALE | ICAS2022_0328 |
| Velandia Luis, L.P. | VISCOUS CORRECTION FOR HIGH ORDER IMMERSED INTERFACE METHOD FOR COMPRESSIBLE TRANSONIC FLOWS | ICAS2022_0260 |
| Venkatesh, A. | MULTIPOINT AERODYNAMIC DESIGN OF A NACELLE FOR AN ELECTRIC FAN | ICAS2022_0138 |
| Venner, C.H. | AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF THE NACA 0008 AIRFOIL | ICAS2022_0128 |
| Venner, C.H. | INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRD | ICAS2022_0653 |
| Veras, V.L.M. | SYNTHETIC AIR DATA - A COMPARATIVE PRACTICAL STUDY | ICAS2022_0536 |
| Verhagen, W. | AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATION | ICAS2022_0747 |
| Verma, S. | AN INTERNATIONAL RESEARCH PERSPECTIVE ON AIRSPACE INTEGRATION IN THE FRAMEWORK OF URBAN AIR MOBILITY | ICAS2022_0948 |
| Vermeersch, O. | STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE | ICAS2022_0583 |
| Versino, E. | “CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION | ICAS2022_0345 |
| Vervliet, J. | CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM | ICAS2022_0606 |
| Vescovini, R. | DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU) | ICAS2022_0295 |
| Vesterberg, J. | REAL-TIME IDENTIFICATION OF USER ACTIONS IN COMPUTER-AIDED MANUFACTURING USING MACHINE LEARNING AND COMPUTER VISION | ICAS2022_0534 |
| Vidal, C. | INTERNATIONAL SCIENTIFIC ASSESSMENT ON URBAN AIR MOBILITY AS A CONTRIBUTION TO FUTURE AVIATION STANDARDS | ICAS2022_0949 |
| Vidal de Saint Jean, F. | TOWARD A GREENER AIRCRAFT ARCHITECTURE | ICAS2022_0484 |
| Vienne, L. | LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES | ICAS2022_0339 |
| Vikhorev, V. | THE INFLUENCE OF THE VANE LEAN ON THE FLOW IN A TURBINE REAR STRUCTURE | ICAS2022_0514 |
| Vilani, E. | DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY | ICAS2022_0662 |
| Villani, E. | EXPLORATORY STUDY OF MENTAL WORKLOAD IN HELICOPTER AIR-TO-GROUND ROCKET FIRING | ICAS2022_0077 |
| Villani, E. | LONG TOUCHDOWN THROUGH A SAFETY-II PERSPECTIVE | ICAS2022_0185 |
| Villani, E. | THE BENEFIT OF BILATERAL RESEARCH NETWORKS - THE SARC AND BARINET INITIATIVES AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICS | ICAS2022_0681 |
| Villani, E. | HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICS | ICAS2022_0707 |
| Villani, E. | A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY | ICAS2022_0723 |
| Villani, E. | UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO | ICAS2022_0729 |
| Villela, P.S.C. | LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP | ICAS2022_0869 |
| Vimláti, L. | DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING | ICAS2022_0447 |
| Vindigni, C.R. | RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS | ICAS2022_0218 |
| Vingerhoeds, R. | ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEM | ICAS2022_0368 |
| Vingerhoeds, R.A. | TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONES | ICAS2022_0655 |
| Vink, P. | MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHT | ICAS2022_0115 |
| Viola, N. | COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION | ICAS2022_0342 |
| Viola, N. | LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES | ICAS2022_0498 |
| Viola, N. | HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS | ICAS2022_0572 |
| Viola, N. | AERODATABASE DEVELOPMENT AND INTEGRATION OF SUPERSONIC/HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROJECT | ICAS2022_0596 |
| Visingardi, A. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Visingardi, A. | THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0917 |
| Viviani, A. | AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE | ICAS2022_0259 |
| Vlk, J. | LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFT | ICAS2022_0719 |
| Vlk, J. | PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELS | ICAS2022_0721 |
| Voigt, C. | NOVEL PATHWAYS TO SUSTAINABLE AVIATION | ICAS2022_0688 |
| Volkert, A. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Volkman, T.B. | A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENT | ICAS2022_0523 |
| Volkmann, T.B. | EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMAS | ICAS2022_0526 |
| Vos, J.B. | USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC PERFORMANCE OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFT | ICAS2022_0251 |
| Vos, R. | DESIGN OF A FLYING V SUBSONIC TRANSPORT | ICAS2022_0358 |
| Vos, R. | MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN | ICAS2022_0602 |
| Vos, R. | DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFT | ICAS2022_0622 |
| Vos, R. | PROPELLER AIRCRAFT DESIGN OPTIMIZATION FOR CLIMATE IMPACT REDUCTION | ICAS2022_0819 |
| Vozella, A. | AVIATION SECURITY CONCERNS | ICAS2022_0918 |
| Voß, A. | AEROELASTIC MODELING, LOADS ANALYSIS AND STRUCTURAL DESIGN OF A FIGHTER AIRCRAFT | ICAS2022_0161 |
| Voß, A. | LANDING SIMULATION OF A HIGH-ALTITUDE PLATFORM WITH SKID-TYPE LANDING GEAR – FLIGHT PROCEDURE, CONTROLLER, AND LOADS | ICAS2022_0364 |
| Voß, A. | A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATOR | ICAS2022_0826 |
| Vu, T.-A. | MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES | ICAS2022_0813 |
| Wada, D. | WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS) | ICAS2022_0814 |
| Wahler, N.F.M. | A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTS | ICAS2022_0850 |
| Walker, E. | NATO AVT-297 DEVELOPMENT OF A FRAMEWORK FOR VALIDATION OF COMPUTATIONAL TOOLS FOR ANALYSIS OF AIR VEHICLES | ICAS2022_0933 |
| Wall, A. | NUMERICAL MODELLING OF PITCHING WINGS FOR GUST MITIGATION | ICAS2022_0406 |
| Wallace, C. | EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERS | ICAS2022_0656 |
| Wallén Axehill, J. | HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENT | ICAS2022_0434 |
| Walther, B. | TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINE | ICAS2022_0006 |
| Walther, J.-N. | EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXT | ICAS2022_0254 |
| Walther, H. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Walther, J.-N. | DESIGN AND ECO-EFFICIENCY ASSESSMENT OF A PEOPLE-MOVER AIRCRAFT IN COMPARISON TO STATE-OF-THE-ART NARROW BODY AIRCRAFT | ICAS2022_0304 |
| Wan, Z. | AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT | ICAS2022_0795 |
| Wang, K.-L. | INVESTIGATION ON CRUISE PERFORMANCE OF A HAND-LAUNCHED SOLAR-POWERED UAV FOR ENVIRONMENTAL MONITORING IN TIBET | ICAS2022_0033 |
| Wang, X. | AN INVESTIGATION ON THE IMPROVEMENT FOR TANDEM WING PITCHING MOMENT CHARACTERISTICS | ICAS2022_0050 |
| Wang, X.-S. | DESIGN AND EFFICIENCY ANALYSIS OF EVTOL CONTRA-ROTATING PROPELER | ICAS2022_0060 |
| Wang, R. | USING DEEP REINFORCEMENT LEARNING TO IMPROVE THE ROBUSTNESS OF UAV LATERAL-DIRECTIONAL CONTROL | ICAS2022_0065 |
| Wang, Y. | EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING | ICAS2022_0078 |
| Wang, X.-S. | RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAV | ICAS2022_0107 |
| Wang, L. | OPTIMIZATION STUDY ON THE FLOW SEPARATION CONTROL USING A SAWTOOTH PLASMA ACTUATOR | ICAS2022_0156 |
| Wang, D. | INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN THE V103 CASCADE | ICAS2022_0204 |
| Wang, R. | NUMERICAL SIMULATION ANALYSIS OF INFRARED RADIATION AND ELECTROMAGNETIC SCATTERING CHARACTERISTICS OF DIFFERENT MIXERS | ICAS2022_0223 |
| Wang, D. | STUDY ON MECHANICAL PROPERTIES OF CARBON FIBER RESIN MATRIX COMPOSITE BOLTED JOINT STRUCTURE AT HIGH TEMPERATURE | ICAS2022_0278 |
| Wang, X. | RESEARCH ON PRESSURE LOAD OF AN EMBEDDED JET NOZZLE | ICAS2022_0302 |
| Wang, J. | STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATOR | ICAS2022_0313 |
| Wang, Y. | UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODEL | ICAS2022_0330 |
| Wang, F. | NUMERICAL ANALYSIS OF PROPAGATION OF DETONATION WAVE PLUNGING ENTRY THE FUEL JET TRAIN INSIDE ROTATING DETONATION COMBUSTOR | ICAS2022_0409 |
| Wang, Y. | IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT | ICAS2022_0421 |
| Wang, J.-F. | FREE FLIGHT TEST IN HORIZONTAL WIND TUNNEL WITH POWERED AIRCRAFT | ICAS2022_0423 |
| Wang, M.-H. | FREE FLIGHT TEST IN HORIZONTAL WIND TUNNEL WITH POWERED AIRCRAFT | ICAS2022_0423 |
| Wang, A. | EXPERIMENTAL STUDY OF FLAT BAFFLE INLET TOTAL-PRESSURE DISTORTION IN A THREE-STAGE FAN | ICAS2022_0502 |
| Wang, Z. | RESEARCH ON CROSSTALK CHARACTERISTICS OF AIRCRAFT ELECTRICAL CABLE | ICAS2022_0503 |
| Wang, Y. | HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACK | ICAS2022_0555 |
| Wang, H. | EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING | ICAS2022_0632 |
| Wang, Y. | COOPERATIVE PATH PLANNING AND ADJUSTING STRATEGY FOR UAVS WITH STRICT TIME CONSTRAINS | ICAS2022_0781 |
| Wang, J.-F. | DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACE | ICAS2022_0785 |
| Wang, M.-H. | DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACE | ICAS2022_0785 |
| Watanabe, Y. | FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLET | ICAS2022_0830 |
| Weber, T. | CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACH | ICAS2022_0102 |
| Weber, G. | EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERS | ICAS2022_0656 |
| Webster, K. | NEW GENERATION SPACE VEHICLE OPERATIONS IN THE UNITED ARAB EMIRATES – AN AIRSPACE AND RISK ASSESSMENT | ICAS2022_0698 |
| Weder, C. | A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIES | ICAS2022_0853 |
| Wegener, P. | CAD DEFORMATION FOR THE CONSIDERATION OF AEROELASTIC EFFECTS | ICAS2022_0557 |
| Wei, Z. | RESEARCH ON THE INFLUENCE OF FLIGHT ATTITUDE ON UNILATERAL MISSILE SEPARATION FROM EMBEDDED BAY | ICAS2022_0319 |
| Weiner, A. | WING BUFFET PRESSURE LOAD PREDICTION BASED ON A HYBRID DEEP LEARNING MODEL | ICAS2022_0043 |
| Weinerfelt, P. | ENHANCING CFD PREDICTIONS FOR THE GRIPEN AIRCRAFT | ICAS2022_0242 |
| Weixiang, W. | HUMAN-MACHINE FUNCTION ALLOCATION METHOD FOR SINGLE PILOT OPERATION USING HESITANT FUZZY 2-TUPLE LINGUISTIC INFORMATION | ICAS2022_0493 |
| Wenhao, B. | HUMAN-MACHINE FUNCTION ALLOCATION METHOD FOR SINGLE PILOT OPERATION USING HESITANT FUZZY 2-TUPLE LINGUISTIC INFORMATION | ICAS2022_0493 |
| Wennhage, P. | WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE | ICAS2022_0215 |
| Werner, M. | PROGRESS IN WING DESIGN, STATUS AND PERSPECTIVES | ICAS2022_0926 |
| Westermeier, T. | EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATION | ICAS2022_0467 |
| Westin, T. | VISION-BASED LOCALISATION FOR AUTONOMOUS AERIAL NAVIGATION IN GNSS-DENIED SITUATIONS | ICAS2022_0485 |
| Wevers, M. | SIGMOIDAL SENSING DEVICES FOR MONITORING TO IMPROVE MAINTENANCE OPERATIONS IN AERONAUTICS | ICAS2022_0454 |
| Whidborne, J.F. | GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMP | ICAS2022_0644 |
| Whitacker, L.H.L. | EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE | ICAS2022_0676 |
| White, M. | THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2022_0917 |
| Wickersheim, R. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Wiedemann, M. | FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATION | ICAS2022_0708 |
| Wiedemann, M. | DESIGN,MANUFACTURING & CERTIFICATION STRATEGIES FOR INNOVATIVE HYDROGEN STORAGE SYSTEMS TO ENABLE ZERO EMISSION AVIATION | ICAS2022_0962 |
| Wilckens, D. | DESIGN,MANUFACTURING & CERTIFICATION STRATEGIES FOR INNOVATIVE HYDROGEN STORAGE SYSTEMS TO ENABLE ZERO EMISSION AVIATION | ICAS2022_0962 |
| Willberg, C. | PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONS | ICAS2022_0820 |
| Williams, S. | MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING | ICAS2022_0176 |
| Wishart, J.M. | UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATION | ICAS2022_0774 |
| Wong, C.W. | OPTIMIZATION STUDY ON THE FLOW SEPARATION CONTROL USING A SAWTOOTH PLASMA ACTUATOR | ICAS2022_0156 |
| Wright, M.C.N. | RECENT ACTIVITIES ON FLOW QUALITY ASSESSMENT AT THE EUROPEAN TRANSONIC WINDTUNNEL | ICAS2022_0061 |
| Wright, S.J. | FUEL CELLS AND NOVEL THERMAL MANAGEMENT ADVANCEMENTS REQUIRED FOR AVIATION | ICAS2022_0079 |
| Wu, Y. | DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK | ICAS2022_0032 |
| Wu, N. | LARGE-SCALE MULTIFIDELITY AEROSTRUCTURAL OPTIMIZATION OF A TRANSPORT AIRCRAFT | ICAS2022_0186 |
| Wu, R. | DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT | ICAS2022_0321 |
| Wu, B. | HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACK | ICAS2022_0555 |
| Wu, Z. | EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING | ICAS2022_0632 |
| Wu, C.J. | INFLUENCE OF MANEUVERING PROCESS ON PERFORMANCE CHARACTERISTICS OF BELLY INLET OF AIRCRAFT | ICAS2022_0834 |
| Wu, X. | SAND EROSION MODELING IN GENERIC COMPRESSOR RIG TESTING | ICAS2022_0945 |
| Wulf, S. | AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT | ICAS2022_0835 |
| Wunderli, J.M. | IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT | ICAS2022_0627 |
| Wunderlich, T. | APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT | ICAS2022_0892 |
| Wöhler, S. | DESIGN AND ECO-EFFICIENCY ASSESSMENT OF A PEOPLE-MOVER AIRCRAFT IN COMPARISON TO STATE-OF-THE-ART NARROW BODY AIRCRAFT | ICAS2022_0304 |
| Xia, J. | TWO-PHASE NUMERICAL SIMULATION INVESTIGATION ON THE EFFECTS OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCE | ICAS2022_0029 |
| Xia, Z.-X. | A FAST PREDICTION METHOD FOR DROPPING WATER OF FIRE FIGHTING AIRCRAFT BASED ON EXTERNAL BALLISTICS OF PARTICLES | ICAS2022_0422 |
| Xiangnan, L. | AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNEL | ICAS2022_0411 |
| Xiao, Q. | MOTION STROKE DESIGN ON FLEXIBLE ASSEMBLY TOOLING FOR MULTIPLE AIRCRAFT COMPONENTS | ICAS2022_0314 |
| Xiao, T. | ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODY | ICAS2022_0385 |
| Xiao, C. | INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNEL | ICAS2022_0547 |
| Xiong, W.T. | INFLUENCE OF MANEUVERING PROCESS ON PERFORMANCE CHARACTERISTICS OF BELLY INLET OF AIRCRAFT | ICAS2022_0834 |
| Xisto, C. | MULTIPOINT AERODYNAMIC DESIGN OF A NACELLE FOR AN ELECTRIC FAN | ICAS2022_0138 |
| Xisto, C. | NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCT | ICAS2022_0236 |
| Xisto, C. | DEVELOPMENT OF AN AERODYNAMIC ANALYSIS TOOL FOR BOUNDARY LAYER INGESTION CONCEPT DESIGN | ICAS2022_0362 |
| Xisto, C. | DESIGN AND PERFORMANCE OF LIQUID HYDROGEN FUELLED AIRCRAFT FOR YEAR 2050 EIS | ICAS2022_0496 |
| Xisto, C. | EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT | ICAS2022_0788 |
| Xisto, C. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| Xu, K. | DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK | ICAS2022_0032 |
| Xu, H. | INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN THE V103 CASCADE | ICAS2022_0204 |
| Xu, J. | ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODY | ICAS2022_0385 |
| Xu, Y. | NUMERICAL PREDICTION OF FOCUS BOOM GENERATED BY MANEUVERS | ICAS2022_0410 |
| Xu, Y. | IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT | ICAS2022_0421 |
| Xu, L. | AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT | ICAS2022_0795 |
| XU, B.-B. | INFLUENCE OF MANEUVERING PROCESS ON PERFORMANCE CHARACTERISTICS OF BELLY INLET OF AIRCRAFT | ICAS2022_0834 |
| Yamada, G. | COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHOD | ICAS2022_0416 |
| Yan, P. | A NOVEL EMBEDDED INLET BASED ON THE INTEGRATED DESIGN CONCEPT OF FUSELAGE AND INLET | ICAS2022_0092 |
| Yan, B. | EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING | ICAS2022_0632 |
| Yang, Y. | A DAMAGE RECOGNITION METHOD OF COMPOSITE STRUCTURES USING ARTIFICIAL DEFECTIONS | ICAS2022_0052 |
| Yang, H.-H. | DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLE | ICAS2022_0108 |
| Yang, H.-H. | OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNING | ICAS2022_0109 |
| Yang, G.-Q. | NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR | ICAS2022_0165 |
| Yang, Q. | NUMERICAL SIMULATION ANALYSIS OF INFRARED RADIATION AND ELECTROMAGNETIC SCATTERING CHARACTERISTICS OF DIFFERENT MIXERS | ICAS2022_0223 |
| Yang, D. | ECONOMICS OF SUSTAINABLE REGIONAL AIR MOBILITY | ICAS2022_0359 |
| Yang, Q. | EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF COMPOSITE SHIELD ON THE ELECTROTHERMAL ANTI-ICING SYSTEMS | ICAS2022_0537 |
| Yang, Q.-Z. | EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECK | ICAS2022_0847 |
| Yang, H.-Q. | EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECK | ICAS2022_0847 |
| Yang, Q. | SAND EROSION MODELING IN GENERIC COMPRESSOR RIG TESTING | ICAS2022_0945 |
| Yano, M.O. | DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES USING NEURAL NETWORKS AND HYBRID DATA | ICAS2022_0705 |
| Yao, L. | RESEARCH ON SERVO CONTROL METHOD AND DAMPING CHARACTERISTICS OF ACTIVE CONTROL DEVICE | ICAS2022_0348 |
| Yao, R. | INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX | ICAS2022_0417 |
| Yarbasi, E.Y. | SYSTEM LEVEL IDENTIFICATION OF CRITICAL UNCERTAINTIES TO ENABLE VALIDATION EXPERIMENTS | ICAS2022_0935 |
| Yasuda, R. | STUDY ON THE APPLICATION OF EMULSIFIED FUEL IN SMALL JET ENGINES | ICAS2022_0751 |
| Yates, D.C. | BOEING/SAAB CO-DEVELOPMENT PROGRAMME OF T-7A TRAINER - A JOINT DIGITAL JOURNEY | ICAS2022_0764 |
| Yavuz, A.G. | AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPES | ICAS2022_0381 |
| Ye, K. | A NUMERICAL METHOD FOR STUDY ON THE AERO-ELASTICITY OF AIR-TO-AIR MISSILES IN OVER-THE-SHOULDER LAUNCH | ICAS2022_0311 |
| Yee, K. | AIRCRAFT DESIGN PARAMETER ESTIMATION USING DATA-DRIVEN MACHINE LEARNING MODELS | ICAS2022_0435 |
| Yi, L. | NUMERICAL INVESTIGATION ON TURBINE SHROUD FILM COOLING HEAT TRANSFER PERFORMANCE OF TURBINE BLADE WITH GROOVE TIP | ICAS2022_0203 |
| Yigit, E. | A FAULT INTEGRATOR BASED VOTE&MONITOR DESIGN FOR GRACEFULL DEGRADATION IN MULTIPLE REDUNDANT SAFETY CRITICAL SYSTEMS | ICAS2022_0472 |
| Yildirim, A. | COUPLED AEROPROPULSIVE ANALYSIS AND OPTIMIZATION OF A HIGH BYPASS TURBOFAN ENGINE | ICAS2022_0390 |
| Yildiz, M. | MORE ELECTRIC AIRPLANE: CASE STUDY STOCKHOLM - COPENHAGEN | ICAS2022_0506 |
| Yin, F. | MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE | ICAS2022_0574 |
| Yin, F. | MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGN | ICAS2022_0602 |
| Ying, S.X. | DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFT | ICAS2022_0566 |
| Ying, S. | AMPAIRE AND THE ELECTRIFIED PROPULSION JOURNEY | ICAS2022_0957 |
| Ünlü, H.-I. | NUMERICAL INVESTIGATION OF ROTORCRAFT PRESSURE ERROR CORRECTION BY UTILIZATION OF AIR DAMS | ICAS2022_0357 |
| Yonezawa, K. | AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION | ICAS2022_0192 |
| Yoshikawa, N. | QUANTUM ARRIVAL AND DEPARTURE MANAGEMENT | ICAS2022_0728 |
| You, J.H. | RECENT ACTIVITIES ON FLOW QUALITY ASSESSMENT AT THE EUROPEAN TRANSONIC WINDTUNNEL | ICAS2022_0061 |
| Yu, D. | RESEARCH ON PRESSURE LOAD OF AN EMBEDDED JET NOZZLE | ICAS2022_0302 |
| Yu, H. | RESEARCH ON SERVO CONTROL METHOD AND DAMPING CHARACTERISTICS OF ACTIVE CONTROL DEVICE | ICAS2022_0348 |
| Yu, F. | COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAV | ICAS2022_0367 |
| Yu, B.-W. | RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE | ICAS2022_0510 |
| Yu, X. | RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE | ICAS2022_0510 |
| Yu, D. | EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING | ICAS2022_0632 |
| Yuan, W. | NUMERICAL MODELLING OF PITCHING WINGS FOR GUST MITIGATION | ICAS2022_0406 |
| Yuce, M. | A FAULT INTEGRATOR BASED VOTE&MONITOR DESIGN FOR GRACEFULL DEGRADATION IN MULTIPLE REDUNDANT SAFETY CRITICAL SYSTEMS | ICAS2022_0472 |
| Yue, Y. | TASK ALLOCATION METHOD FOR COMPLEX RECONNAISSANCE AREA BY MULTIPLE UAVS | ICAS2022_0195 |
| Yuhui, L. | HUMAN-MACHINE FUNCTION ALLOCATION METHOD FOR SINGLE PILOT OPERATION USING HESITANT FUZZY 2-TUPLE LINGUISTIC INFORMATION | ICAS2022_0493 |
| Zaccariotto, M. | DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU) | ICAS2022_0295 |
| Zachos, P.K. | A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKE | ICAS2022_0127 |
| Zahn, R. | WING BUFFET PRESSURE LOAD PREDICTION BASED ON A HYBRID DEEP LEARNING MODEL | ICAS2022_0043 |
| Zaliskyi, M. | DATA-DRIVEN APPROACH TO OPTIMAL AIRCRAFT MAINTENANCE | ICAS2022_0871 |
| Zamboni, J. | A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONS | ICAS2022_0700 |
| Zamfir, A. | A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONS | ICAS2022_0700 |
| Zammit, B. | AN ENGINELESS TAXI OPERATIONS SYSTEM USING BATTERY-OPERATED AUTONOMOUS TOW TRUCKS | ICAS2022_0783 |
| Zandi Pour, H.R. | HEAT TRANSFER ENHANCEMENT BY SUSPENDED PARTICLES IN A TURBULENT SHEARLESS FLOW | ICAS2022_0711 |
| Zanetti, D. | CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGE | ICAS2022_0148 |
| Zang, B. | WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE | ICAS2022_0215 |
| Zaninotto, S. | AN ENGINELESS TAXI OPERATIONS SYSTEM USING BATTERY-OPERATED AUTONOMOUS TOW TRUCKS | ICAS2022_0783 |
| Zanotti, A. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Zanotti, A. | EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING THE WIND TUNNEL: HELICOPTER SHIP LANDING CASE | ICAS2022_0625 |
| Zanotti Fragonara, L. | GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMP | ICAS2022_0644 |
| Zantner, T. | DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK | ICAS2022_0677 |
| Zappino, E. | VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTS | ICAS2022_0247 |
| Zastrow, J. | NUMERICAL AND EXPERIMENTAL INVESTIGATIONS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODEL | ICAS2022_0720 |
| Zengerling, Z. | A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIES | ICAS2022_0853 |
| Zettervall, N. | LES OF COMBUSTION DYNAMICS IN AN ETHYLENE-HYDROGEN-AIR RAMJET | ICAS2022_0786 |
| Zhang, Y. | DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNEL | ICAS2022_0045 |
| Zhang, B. | THREE DIMENSIONAL PATH FOLLOWING CONTROL FOR A FIXED-WING UAV ON SO(3) WITH INPUT SATURATION | ICAS2022_0049 |
| Zhang, Y. | THREE DIMENSIONAL PATH FOLLOWING CONTROL FOR A FIXED-WING UAV ON SO(3) WITH INPUT SATURATION | ICAS2022_0049 |
| Zhang, Y. | AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK | ICAS2022_0199 |
| Zhang, S. | NUMERICAL SIMULATION ANALYSIS OF INFRARED RADIATION AND ELECTROMAGNETIC SCATTERING CHARACTERISTICS OF DIFFERENT MIXERS | ICAS2022_0223 |
| Zhang, M. | IMPROVING STALL CHARACTERISTICS OF UCAV WING WITH VORTEX GENERATORS | ICAS2022_0238 |
| Zhang, L. | EXPERIMENTAL INVESTIGATION ON TRANSPORT AIRPLANE LONGITUDINAL STABILITY ENHANCEMENT IN CRITICAL ICING CONDITION | ICAS2022_0270 |
| Zhang, H. | EXPERIMENTAL INVESTIGATION ON TRANSPORT AIRPLANE LONGITUDINAL STABILITY ENHANCEMENT IN CRITICAL ICING CONDITION | ICAS2022_0270 |
| Zhang, X.J. | DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIAL | ICAS2022_0290 |
| Zhang, X. | MOTION STROKE DESIGN ON FLEXIBLE ASSEMBLY TOOLING FOR MULTIPLE AIRCRAFT COMPONENTS | ICAS2022_0314 |
| Zhang, Z. | DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT | ICAS2022_0321 |
| Zhang, S.-Q. | UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODEL | ICAS2022_0330 |
| Zhang, T. | ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUP | ICAS2022_0335 |
| Zhang, X. | NUMERICAL MODELLING OF PITCHING WINGS FOR GUST MITIGATION | ICAS2022_0406 |
| Zhang, Y. | IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT | ICAS2022_0421 |
| Zhang, Z.-B. | EXPERIMENTAL STUDY ON THE EFFECT OF INTERSTAGE BLEEDING ON THE PERFORMANCE OF FULL-SCALE MULTISTAGE AXIAL COMPRESSOR | ICAS2022_0495 |
| Zhang, Y.-H. | EXPERIMENTAL STUDY ON THE EFFECT OF INTERSTAGE BLEEDING ON THE PERFORMANCE OF FULL-SCALE MULTISTAGE AXIAL COMPRESSOR | ICAS2022_0495 |
| Zhang, Z. | EXPERIMENTAL STUDY OF FLAT BAFFLE INLET TOTAL-PRESSURE DISTORTION IN A THREE-STAGE FAN | ICAS2022_0502 |
| Zhang, L. | RESEARCH ON CROSSTALK CHARACTERISTICS OF AIRCRAFT ELECTRICAL CABLE | ICAS2022_0503 |
| Zhang, K. | RESEARCH ON CROSSTALK CHARACTERISTICS OF AIRCRAFT ELECTRICAL CABLE | ICAS2022_0503 |
| Zhang, X.-Z. | RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE | ICAS2022_0510 |
| Zhang, C.-L. | RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTURE | ICAS2022_0510 |
| Zhang, Y. | EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTOR GENERATION | ICAS2022_0548 |
| Zhang, L.-W. | A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT | ICAS2022_0584 |
| Zhang, Z.-B. | SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSOR | ICAS2022_0589 |
| Zhang, Z. | ANALYSIS OF THE AERODYNAMIC CHARACTERISTICS AND ITS INFLUENCE OF TURBOMACHINERY IN TRANSITION STATE | ICAS2022_0603 |
| Zhang, L. | ELECTROMAGNETIC INTERFERENCE SHIELDING EFFECTIVENESS OF THE THIN CARBON NANOFIBERS/ SILICON CARBIDE FABRICS COMPOSITES | ICAS2022_0608 |
| Zhang, X. | ELECTROMAGNETIC INTERFERENCE SHIELDING EFFECTIVENESS OF THE THIN CARBON NANOFIBERS/ SILICON CARBIDE FABRICS COMPOSITES | ICAS2022_0608 |
| Zhang, X.-L. | EQUIVALENT CALCULATION METHOD OF FLYOVER NOISE LEVEL OF CUTBACK TAKE-OFF FOR CIVIL JET AIRPLANE AIRWORTHINESS CERTIFICATION | ICAS2022_0626 |
| Zhang, G. | EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING | ICAS2022_0632 |
| Zhao, Y. | INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN THE V103 CASCADE | ICAS2022_0204 |
| Zhao, W. | THE CONVERSATION ANALYSIS OF AVIATION ENGLISH FROM SYSTEMIC FUNCTIONAL LINGUISTICS PERSPECTIV | ICAS2022_0209 |
| Zhao, Q. | STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATOR | ICAS2022_0313 |
| Zhao, Z. | RESEARCH ON SERVO CONTROL METHOD AND DAMPING CHARACTERISTICS OF ACTIVE CONTROL DEVICE | ICAS2022_0348 |
| Zhao, X. | DEVELOPMENT OF AN AERODYNAMIC ANALYSIS TOOL FOR BOUNDARY LAYER INGESTION CONCEPT DESIGN | ICAS2022_0362 |
| Zhao, X. | INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX | ICAS2022_0417 |
| Zhao, X. | A FAST PREDICTION METHOD FOR DROPPING WATER OF FIRE FIGHTING AIRCRAFT BASED ON EXTERNAL BALLISTICS OF PARTICLES | ICAS2022_0422 |
| Zhao, X. | ENVIRONMENTAL ASSESSMENT OF NOISE ABATEMENT APPROACH TRAJECTORIES | ICAS2022_0671 |
| Zhao, Z. | AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT | ICAS2022_0795 |
| Zhao, S. | AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT | ICAS2022_0795 |
| Zhao, X. | SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045 | ICAS2022_0804 |
| Zhao, X. | MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM | ICAS2022_0832 |
| Zheng, L. | USING DEEP REINFORCEMENT LEARNING TO IMPROVE THE ROBUSTNESS OF UAV LATERAL-DIRECTIONAL CONTROL | ICAS2022_0065 |
| Zheng, J. | RESEARCH ON SERVO CONTROL METHOD AND DAMPING CHARACTERISTICS OF ACTIVE CONTROL DEVICE | ICAS2022_0348 |
| Zheng, H. | EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF COMPOSITE SHIELD ON THE ELECTROTHERMAL ANTI-ICING SYSTEMS | ICAS2022_0537 |
| Zheng, Y. | MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATION | ICAS2022_0544 |
| Zhong, Z. | ELECTROMAGNETIC INTERFERENCE SHIELDING EFFECTIVENESS OF THE THIN CARBON NANOFIBERS/ SILICON CARBIDE FABRICS COMPOSITES | ICAS2022_0608 |
| Zhou, Z. | INVESTIGATION ON CRUISE PERFORMANCE OF A HAND-LAUNCHED SOLAR-POWERED UAV FOR ENVIRONMENTAL MONITORING IN TIBET | ICAS2022_0033 |
| Zhou, Z. | USING DEEP REINFORCEMENT LEARNING TO IMPROVE THE ROBUSTNESS OF UAV LATERAL-DIRECTIONAL CONTROL | ICAS2022_0065 |
| Zhou, Y. | OPTIMIZATION STUDY ON THE FLOW SEPARATION CONTROL USING A SAWTOOTH PLASMA ACTUATOR | ICAS2022_0156 |
| Zhou, W.-Y. | NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR | ICAS2022_0165 |
| Zhou, B.-X. | NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR | ICAS2022_0165 |
| Zhou, J. | EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONE | ICAS2022_0256 |
| Zhou, Z. | EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTOR GENERATION | ICAS2022_0548 |
| Zhu, X. | USING DEEP REINFORCEMENT LEARNING TO IMPROVE THE ROBUSTNESS OF UAV LATERAL-DIRECTIONAL CONTROL | ICAS2022_0065 |
| Zhu, X.-Y. | NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR | ICAS2022_0165 |
| Zhu, S. | INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN THE V103 CASCADE | ICAS2022_0204 |
| Zhu, C. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Zhu, S. | EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRING | ICAS2022_0632 |
| Zhukov, D. | CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREAS | ICAS2022_0300 |
| Zingg, D.W. | EXPLORATION OF BOX-WING AIRCRAFT CONCEPT USING HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION | ICAS2022_0446 |
| Zingg, D.W. | A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATION TO THE STRUT-BRACED-WING AND HYBRID-WING-BODY CONFIGURATIONS | ICAS2022_0748 |
| Zolotas, A. | FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIES | ICAS2022_0520 |
| Zou, H. | INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNEL | ICAS2022_0547 |
| Zuher, A.M. | THE INFLUENCE OF THE VANE LEAN ON THE FLOW IN A TURBINE REAR STRUCTURE | ICAS2022_0514 |
| Zuńiga, D.F.C. | PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WING | ICAS2022_0694 |
| Zúniga, D.F.C. | OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM | ICAS2022_0891 |
| Ĺhlander, A. | TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS | ICAS2022_0604 |
| Ĺkerblom, A. | THE IMPACT OF REACTION MECHANISM COMPLEXITY IN LES MODELING OF LIQUID KEROSENE SPRAY COMBUSTION | ICAS2022_0274 |
| Ĺkerman, D. | INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATION | ICAS2022_0245 |
| Ĺsvärn, D. | INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATION | ICAS2022_0245 |
| Ĺsvärn, D. | VISION-BASED LOCALISATION FOR AUTONOMOUS AERIAL NAVIGATION IN GNSS-DENIED SITUATIONS | ICAS2022_0485 |