| Aalmoes, R. | CHALLENGES IN ADVANCED AIR MOBILITY NOISE PREDICTION - FROM SOURCE TO PERCEPTION | ICAS2026_0345 |
| Abdelmoula, F. | DYN-MARS: A NEW CONCEPT ENABLING THE BEST APPROACH FLIGHT PROFILE | ICAS2026_0265 |
| Abdelrahman, M. | DESIGN AND TESTING OF A BUOYANT UAV FOR AGRICULTURAL SURVEILLANCE | ICAS2026_0594 |
| Abdulhak, S. | EXPLORING DETROIT METROPOLITAN WAYNE COUNTY AIRPORT AS A TESTBED FOR RESOLVING INTEGRATION CHALLENGES FOR AIR TAXI OPERATIONS | ICAS2026_0682 |
| Abe, H. | AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMI-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT THE JAXA 6.5M X 5.5M LOW SPEED WIND TUNNEL | ICAS2026_0256 |
| Abid, Hassan Ali | HIGH-FIDELITY NUMERICAL INVESTIGATION OF ROTOR-WING INTERACTIONS IN A MULTI-ROTOR DISTRIBUTED ELECTRIC PROPULSION CONFIGURATION | ICAS2026_0678 |
| Abid, Hassan Ali | HIGH-FIDELITY AEROACOUSTIC AND UNSTEADY FLOW ANALYSIS OF WIND TURBINE BLADES | ICAS2026_0693 |
| Abid, Hussain Ali | HIGH-FIDELITY NUMERICAL INVESTIGATION OF ROTOR-WING INTERACTIONS IN A MULTI-ROTOR DISTRIBUTED ELECTRIC PROPULSION CONFIGURATION | ICAS2026_0678 |
| Abou Khalil, J. | AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC | ICAS2026_0347 |
| Abouhamzeh, M. | INVERSE AEROELASTIC SIZING FOR STRUT-BRACED WINGS VIA PHYSICS-GUIDED GENERATIVE MODELING | ICAS2026_0100 |
| Abouhamzeh, M. | TOWARDS INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES: INSPECTABILITY ASSESSMENT OF HAT-STIFFENED PANELS | ICAS2026_0914 |
| Abrão S. Marques, V. | A SEMI-AUTONOMOUS DECISION SUPPORT TOOL FOR ATC IN EN-ROUTE REROUTING OPERATIONS | ICAS2026_0947 |
| Abratanski, A. | MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS | ICAS2026_0143 |
| Abu Salem, K. | ASSESSMENT OF LIQUID HYDROGEN-POWERED AIRCRAFT RANGE: A NOVEL BREGUET FORMULATION | ICAS2026_0285 |
| Abu Salem, K. | AN INTEGRATED CONCEPTUAL DESIGN WORKFLOW FOR LIQUID HYDROGEN-POWERED BOX-WING AIRCRAFT | ICAS2026_0400 |
| Abu Salem, K. | LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY | ICAS2026_0643 |
| Abu-Taa, K. | FLIGHT MISSION MODELING WITH VARYING BASELINE DATA: APPLICAITON IN BUSINESS AVIATION | ICAS2026_0315 |
| Abu-Zurayk, M. | A BENCHMARK FOR UNCERTAINTY QUANTIFICATION AND OPTIMIZATION UNDER UNCERTAINTY IN CONCEPTUAL AIRCRAFT DESIGN: THE F25-OUU CHALLENGE PROBLEM | ICAS2026_0320 |
| Abulawi, J. | PREPARING AERONAUTICAL ENGINEERING UNDERGRADUATES FOR WORKING IN GLOBAL TEAMS | ICAS2026_0453 |
| Abulawi, J. | DIGITAL ENGINEERING IN THE AGE OF AI AS BASIS FOR SYSTEM OF SYSTEMS ENGINEERING | ICAS2026_1108 |
| Abulela, M.S. | MACHINE LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION OF NACA AIRFOILS UNDER GEOMETRIC DESIGN CONSTRAINTS | ICAS2026_0530 |
| Accardo, G. | EXPERIMENTAL VALIDATION OF A FUEL CELL SYSTEM DIGITAL TWIN FOR A FULL-ELECTRIC AIRCRAFT POWERTRAIN | ICAS2026_0303 |
| Ahamad, N.M. | CONCEPTUAL DESIGN OF A MIDDLE-OF-THE-MARKET AIRCRAFT FOR EDUCATIONAL PURPOSES | ICAS2026_0420 |
| Ahmed, N. | REBUILDING AGRICULTURAL STATISTICS IN POST-WAR SUDAN: A STRATEGIC FRAMEWORK FOR RECOVERY AND RESILIENCE | ICAS2026_0010 |
| Ahuja, V. | SIMULATION OF FIFTH-GENERATION HIGH-PERFORMANCE AIRCRAFT USING VISCOUS SURFACE-VORTICITY PANEL METHOD | ICAS2026_0119 |
| Ahuja, V. | SIMULATION OF AERODYNAMIC GROUND EFFECT FOR TILTED PROPELLERS USING VISCOUS SURFACE-VORTICITY PANEL METHOD | ICAS2026_0120 |
| Ai, X. | MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY | ICAS2026_0566 |
| Ai, X. | A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY | ICAS2026_0627 |
| Airoldi, A. | IMPACT TOLERANCE OF DRILLED THICK C/SIC CERAMIC MATRIX COMPOSITES | ICAS2026_0357 |
| Akatsuka, J. | SPILLAGE DRAG REDUCTION IN DIVERTERLESS SUPERSONIC INLET | ICAS2026_0418 |
| Akatsuka, J. | AN OVERVIEW OF JAXA’S HIGH-SPEED FLIGHT R&D: FROM SUPERSONIC FLIGHT TO HYPERSONIC TRANSPORTATION | ICAS2026_1067 |
| Akiyama, H. | FLIGHT DYNAMICS AND GUIDANCE CONTROL FOR AIRCRAFT IN TYPHOON ENVIRONMENTS FOR DELIVERY OF TYPHOON CONTROL SUBSTANCE | ICAS2026_0246 |
| Akiyama, H. | DESIGN AND FEASIBILITY ASSESSMENT OF TRANSPORT OPERATIONS FOR DELIVERING TYPHOON CONTROL SUBSTANCES | ICAS2026_0247 |
| Alaia, A. | GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION | ICAS2026_1011 |
| Alaimo, A. | HRV BASED PILOTS WORKLOAD PREDICTION FOR AN INTELLIGENT COCKPIT WARNING SYSTEM | ICAS2026_0422 |
| Alam, M. | STATIC AND DYNAMIC WIND-TUNNEL TESTING OF A TRANSPORT AIRCRAFT MODEL IN-STALL AND POST-STALL FLIGHT REGIMES | ICAS2026_0203 |
| Alam, M. | CRITICAL LOAD-CASE AND CONSTRAINT IDENTIFICATION FOR PRELIMINARY COMPOSITE WING SIZING USING RAPID DESIGN TOOLS | ICAS2026_0628 |
| Alam, M. | LATERAL-DIRECTIONAL HANDLING AND FLYING QUALITIES ASSESSMENT OF A BLENDED WING BODY (BWB) ACFA 2020 CONFIGURATION | ICAS2026_0630 |
| Alam, M. | PHYSICS-INFORMED MACHINE LEARNING FOR FLIGHT DYNAMICS IDENTIFICATION OF THE SAAB 340B USING FLIGHT TEST DATA | ICAS2026_0686 |
| Alam, M.I. | ENSEMBLE MACHINE LEARNING FOR UAV PROPELLER PERFORMANCE PREDICTION WITH UNCERTAINTY QUANTIFICATION | ICAS2026_0529 |
| Alam, M.I. | MACHINE LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION OF NACA AIRFOILS UNDER GEOMETRIC DESIGN CONSTRAINTS | ICAS2026_0530 |
| Aldèn, M. | KEY STAKEHOLDERS IN AEROSPACE FOR A SUSTAINABLE AND CIRCULAR PRODUCT DEVELOPMENT - A SYSTEMATIC APPROACH | ICAS2026_0222 |
| Alexander, M. | AN INVESTIGATION OF SAFETY-CRITICAL GROUND INTERFACE (TAKEOFF, LANDING) REGIME RECOGNITION FOR AUTOMATED AND AUTONOMOUS VERTICAL LIFT AIRCRAFT MISSION TASK DESIGN | ICAS2026_0680 |
| Ali, I. | EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY | ICAS2026_0080 |
| Alidadi, M. | IMPLICATIONS OF AAM OPERATIONS FOR FUTURE SHARED AIRSPACE IN VICTORIA, AUSTRALIA | ICAS2026_1083 |
| Allebrodt, P. | NUMERICAL PREDICTION OF CABIN NOISE FOR FUTURE SHORT-HAUL AIRCRAFT IN EARLY AIRCRAFT DESIGN | ICAS2026_0364 |
| Alonso-Rodrigo, G. | CHALLENGES AND BREAKTHROUGHS IN AIR TRANSPORT SYSTEM: VISION FROM EUROPE | ICAS2026_0976 |
| Alpfjord Wylde, H. | UNCERTAINTY ANALYSIS AND EYE-TRACKING-BASED CLUSTERING IN AIR TRAFFIC CONTROLLER WORKLOAD PREDICTION | ICAS2026_0118 |
| Alynur, K.K. | MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK | ICAS2026_0493 |
| Amadori, K. | THE CONFERENCE LOCATIONS: A QUANTITATIVE APPROACH TO REDUCING IMPACT GLOBAL TRAVEL | ICAS2026_0607 |
| Amano, M. | EXPLORING AIRWORTHINESS CBA: A STALL SPEED CASE STUDY BASED ON AERO-STRUCTURAL COUPLED ANALYSIS | ICAS2026_1052 |
| Amano, T. | HPC-BASED PARAMETER SPACE EXPLORATION FOR DENSE PICOSAT FORMATION FLYING TOWARD DIRECT-TO-DEVICE COMMUNICATIONS | ICAS2026_0869 |
| Ameduri, S. | ICE DETECTION: CORRELATION OF ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES TESTED IN ICING WIND TUNNEL | ICAS2026_0186 |
| Amoignon, O. | GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION | ICAS2026_1011 |
| Amoroso, F. | ICE DETECTION: CORRELATION OF ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES TESTED IN ICING WIND TUNNEL | ICAS2026_0186 |
| An, Z. | MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY | ICAS2026_0566 |
| Andreeva-Mori, A. | AIRCRAFT SEQUENCING UNDER UNCERTAINTY: GAME-THEORETIC OPTIMIZATION AND A COMPARATIVE ASSESSMENT OF GLOBAL AND INTRA-AIRLINE COOPERATIVE DECISION FRAMEWORKS | ICAS2026_0446 |
| Andrés Pérez, E. | GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION | ICAS2026_1011 |
| Andrews, C. | BEYOND 30,000 FEET: GE AEROSPACE AND THE FUTURE OF ELECTRIC FLIGHT | ICAS2026_1103 |
| Andrews, C.-A. | CFM INTERNATIONAL'S RISE PROGRAM: A STEP-CHANGE FOR DURABILITY AND EFFICIENCY | ICAS2026_1010 |
| Angioni, F. | INTERACTIVE NOTEBOOKS TO BRIDGE THE DIDACTIC GAP BETWEEN CALCULUS AND FLIGHT PERFORMANCE OPTIMIZATION | ICAS2026_0380 |
| Anilir, B. | INTERACTION OF COUNTER-PLUNGING BIPLANE AIRFOILS WITH A FLAT PLATE BOUNDARY LAYER AND WAKE | ICAS2026_0655 |
| Anilir, B. | THREE-DIMENSIONAL FLOW STRUCTURES OVER A LOW-ASPECT-RATIO PLUNGING WING | ICAS2026_0916 |
| Annes da Silva, R.G. | ASSESSING VORTEX BREAKDOWN AND COUPLING IN DELTA WING PLANFORMS THROUGH HIGH-FIDELITY DDES SIMULATIONS | ICAS2026_0939 |
| Annighoefer, B. | VLSEC: A CONCEPT FOR SECURING VIRTUAL LINKS IN AVIONICS NETWORKS THROUGH CENTRALIZED GROUP KEY MANAGEMENT | ICAS2026_0701 |
| Apostolidis, A. | FROM DATA TO DECISIONS: A CONCEPTUAL FRAMEWORK FOR DATA-DRIVEN AIRLINE OPERATIONS AND SUSTAINMENT | ICAS2026_0710 |
| Aprovitola, A. | NUMERICAL REBUILDING OF AERODYNAMIC WIND TUNNEL ANALYSES OF A CREW RETURN VEHICLE | ICAS2026_0572 |
| Arcand, X. | DESIGN AND OPERATION OF LOW-COST MULTI-SCALE TEST BEDS FOR BATTERY THERMAL RUNAWAY INITIATION AND PROPAGATION | ICAS2026_0030 |
| Aretskin-Hariton, E. | A BENCHMARK FOR UNCERTAINTY QUANTIFICATION AND OPTIMIZATION UNDER UNCERTAINTY IN CONCEPTUAL AIRCRAFT DESIGN: THE F25-OUU CHALLENGE PROBLEM | ICAS2026_0320 |
| Armanini, S.F. | KNOW YOUR LIMITS: ESTIMATING THE TILT-WING TRANSITION CORRIDOR UNDER FAILURE CONDITIONS | ICAS2026_0152 |
| Armanini, S.F. | DYNAMIC RECONFIGURABLE PATH PLANNING FOR FIRE-FIGHTING UAVS | ICAS2026_0217 |
| Armanini, S.F. | PROPULSION SYSTEM MODELING AND OPTIMIZATION FOR CONCEPTUAL DESIGN OF HYBRID-ELECTRIC VTOL AIRCRAFT | ICAS2026_0401 |
| Armanini, S.F. | AERODYNAMIC OPTIMISATION OF BIOINSPIRED CORRUGATED WINGS FOR HIGH-EFFICIENCY MAV GLIDING | ICAS2026_0665 |
| Armstrong, J. | A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. | ICAS2026_0041 |
| Arthur, J.J. (Trey) | X-59 EXTERNAL VISION SYSTEM FLIGHT TESTING | ICAS2026_0769 |
| Arts, E. | ONTOLOGY-BASED SENSOR HEALTH MONITORING: A DYNAMIC ONTOLOGY-BASED FAULT DETECTION AND CLASSIFICATION FOR TIMESERIES DATA | ICAS2026_0716 |
| Asadi, E. | REDUCING AIR TRAFFIC COMPLEXITY IN JAPANESE AIRSPACE THROUGH MINOR LATERAL TRAJECTORY ADJUSTMENTS | ICAS2026_0048 |
| Asadi, E. | SIMULATION-BASED EVALUATION OF SIGNALISED INTERSECTIONS FOR EMERGENCY SAFETY LANDINGS IN URBAN AIR MOBILITY | ICAS2026_0325 |
| Asadi, E. | RUNWAY-AWARE CAPACITY ENVELOPES FOR LONG-RANGE ARRIVAL METERING UNDER OPERATING-DIRECTION CHANGES AT SINGAPORE CHANGI | ICAS2026_0408 |
| Asensio Nieto, F. | ADAPTIVE FLIGHT CONTROL LAWS APPLIED TO AIR REFUELING WITH RECEIVERS EQUIPPED WITH RECEPTACLE OUT OF THE PLANE OF SYMMETRY | ICAS2026_0011 |
| Ashton, N. | THE ROLE OF NEXT-GENERATION HPC AND MACHINE LEARNING IN ACHIEVING THE 2030 VISION GOALS | ICAS2026_1022 |
| Asmer, L. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Atanasoaie, B. | ONTOLOGY-BASED SENSOR HEALTH MONITORING: A DYNAMIC ONTOLOGY-BASED FAULT DETECTION AND CLASSIFICATION FOR TIMESERIES DATA | ICAS2026_0716 |
| Atanasov, G. | INTEGRATION OF A SOLID OXIDE FUEL CELL PROPULSION SYSTEM: A TECHNOLOGY DEVELOPMENT GOAL FOR REGIONAL AIRCRAFT | ICAS2026_0319 |
| Atanasov, G. | A MULTI-RANGE HYBRID-ELECTRIC OPEN-ROTOR AIRCRAFT CONCEPT FOR THE WIDE-BODY PASSENGER CLASS | ICAS2026_0625 |
| Athanasiadou, M. | APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS | ICAS2026_0359 |
| Athanasiadou, M. | AI IN THE COCKPIT: THE JARVIS STORY | ICAS2026_0547 |
| Atinault, O. | AERODYNAMIC TRANSONIC DESIGN OF A STRUT-BRACED WING | ICAS2026_0223 |
| Atinault, O. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Atkinson, C. | PASSIVE FLOW CONTROL OF A TURBULENT BOUNDARY LAYER AT THE VERGE OF SEPARATION USING SURFACE ROUGHNESS | ICAS2026_1085 |
| Atkinson, Z. | EXPERIMENTAL CHARACTERIZATION OF PROPELLER-WING INTERACTIONS FOR A SUBSCALE LIFT + CRUISE VTOL UAV | ICAS2026_0689 |
| Austin, T. | A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. | ICAS2026_0041 |
| Avadiar, T. | CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS | ICAS2026_0749 |
| Avellan, R. | CURRENT AND ALTERNATIVE PROPULSION SYSTEMS IN EUROPE | ICAS2026_0981 |
| Avirovic, M. | CONTINUOUS UNSTEADY ADJOINT VARIATIONAL MULTISCALE METHOD FOR AIRFOILS SHAPE OPTIMIZATION | ICAS2026_0105 |
| Avirovic, M. | INFLUENCE OF ZIGZAG TAPE–INDUCED TRANSITION ON THE DU89-134 AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBER | ICAS2026_0221 |
| Avoni, L. | A STALL EXTENSION TO LIFTING-LINE THEORY: IMPLEMENTATION AND VALIDATION IN ASWING | ICAS2026_0720 |
| Axten, C.J. | MULTIPOINT INVERSE DESIGN FOR TRANSONIC, SLOTTED, NATURAL-LAMINAR-FLOW WINGS | ICAS2026_0934 |
| Azevedo, J.L.F. | A STUDY ON THE CELL REYNOLDS NUMBER AS A PARAMETER FOR MESH QUALITY ON HYPERSONIC FLOWS | ICAS2026_0065 |
| B. S. de Andrade, E. | A FORMALLY VERIFIED, EVENT-DRIVEN ROS SCADA SUPERVISORY SYSTEM ARCHITECTURE FOR SAFETY-CRITICAL ROBOTIC CELLS IN AEROSPACE MANUFACTURING | ICAS2026_0945 |
| Babunaidu, G. | IMPACT OF DIFFERENT PROPELLER CONFIGURATIONS ON THE FLIGHT DYNAMICS AND STABILITY OF A SMALL REGIONAL ELECTRIC AIRCRAFT | ICAS2026_0837 |
| Baciu, T.D. | ADVANCES IN NON-DESTRUCTIVE BUCKLING PREDICTION OF THIN-WALLED STRUCTURES BY VIBRATIONS | ICAS2026_0313 |
| Baczynski, C. | ENTRY INTO SERVICE REQUIRES CERTIFICATION FOR NOVEL TECHNOLOGY | ICAS2026_0398 |
| Badea, A. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Bagassi, S. | AUGMENTED REALITY SAFETY NETS FOR INCREASED AIRPORT SAFETY | ICAS2026_0811 |
| Bagassi, S. | DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY | ICAS2026_0827 |
| Bagassi, S. | AURAL DIGITAL TWIN FOR AIRCRAFT CABIN DESIGN | ICAS2026_0899 |
| Bagdahn, A. | A MULTIDIMENSIONAL FRAMEWORK FOR DEMONSTRATION AND V&V CAPABILITIES FOR NEXT-GENERATION FLIGHT CONTROL SYSTEMS | ICAS2026_0093 |
| Bahm, C. | X-59: THE FIRST CHAPTER IN THE QUESST FOR QUIET COMMERICAL SUPERSONIC FLIGHT | ICAS2026_0758 |
| Bahm, C. | X-59: PART 2 BY C.M.BAHM AND P.G.COEN | ICAS2026_1007 |
| Bai, J.Q. | QUASI-STEADY AERODYNAMIC AND MBD COUPLED FLIGHT SIMULATION OF FOLDING MORPHING UAV | ICAS2026_0237 |
| Bai, S. | POWER FLOW DYNAMICS AND COUPLING MECHANISMS IN POWER-BY-WIRE ACTUATION: A COMPREHENSIVE MODELING AND ANALYSIS APPROACH | ICAS2026_0561 |
| Bai, S. | INTEGRATED CONTROL STRATEGY BASED ON PHYSICS-INFORMED MODEL-BASED REINFORCEMENT LEARNING FOR AIRBORNE HIGH-ENERGY SYSTEMS | ICAS2026_0621 |
| Bai, X. | MODELING AND ANALYSIS OF ACTIVE FLUTTER SUPPRESSION OF THE PREPOSITIVE ELLIPTICAL WING-MAIN WING COMPOSITE CONFIGURATION | ICAS2026_0494 |
| Baier Schmelcher, M. | HEAT EXCHANGER MODELING METHODS FOR HYDROGEN POWERED AERO ENGINES DURING THERMODYNAMIC CYCLE DESIGN | ICAS2026_0574 |
| Bailey, R.E. | X-59 EXTERNAL VISION SYSTEM FLIGHT TESTING | ICAS2026_0769 |
| Bakhshi, S.A. | A MIXED-FIDELITY VISCOUS-INVISCID INTERACTION APPROACH FOR WING AERODYNAMIC DESIGN OPTIMIZATION | ICAS2026_0469 |
| Balchanos, M. | FEATURE MODEL CREATION THROUGH MISSION ANALYSIS IN THE CONTEXT OF VEHICLE FAMILIES | ICAS2026_0918 |
| Baluch, A.H. | ENSEMBLE MACHINE LEARNING FOR UAV PROPELLER PERFORMANCE PREDICTION WITH UNCERTAINTY QUANTIFICATION | ICAS2026_0529 |
| Baluch, A.H. | IMPACT RESISTANCE ENHANCEMENT IN FIBER-REINFORCED COMPOSITES USING CARBON/BASALT HYBRIDIZATION APPROACHES | ICAS2026_0885 |
| Bando, M. | ROBUST MOTION ESTIMATION FOR INDOOR MAVS USING WIDE-FIELD-INTEGRATION OF OPTIC FLOW | ICAS2026_0163 |
| Bang, H. | LEARNING-BASED CONTROL ALLOCATION FOR OVER-ACTUATED VTOL AIRCRAFT WITH NONLINEAR DYNAMICS | ICAS2026_0567 |
| Bang, H. | PHYSICS-INFORMED LEARNING-BASED RECOVERY TRAJECTORY PREDICTION FOR AUTOMATIC GROUND COLLISION AVOIDANCE | ICAS2026_0865 |
| Bang, H.-C. | TRAJECTORY OPTIMIZATION OF HIT-TO-KILL INTERCEPTORS VIA SEQUENTIAL CONVEX PROGRAMMING APPROACH | ICAS2026_0534 |
| Baraniello, V.R. | MULTIDISCIPLINARY APPROACH FOR THE AERODYNAMIC CHARACTERIZATION OF AN INFLATABLE CLOSED-WING HYBRID HIGH-ALTITUDE PSEUDO-SATELLITE | ICAS2026_0371 |
| Barba, V. | EXPERIMENTAL VALIDATION OF A FUEL CELL SYSTEM DIGITAL TWIN FOR A FULL-ELECTRIC AIRCRAFT POWERTRAIN | ICAS2026_0303 |
| Barber, C. | DESIGN ASSESSMENT OF A HELICOPTER BLADE | ICAS2026_0225 |
| Bardenhagen, A. | EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT | ICAS2026_0274 |
| Bardera, R. | WIND TUNNEL INVESTIGATION OF HELICOPTER LOADS DURING URBAN OPERATIONS ON A BUILDING WITH COLUMNAR VORTEX GENERATORS | ICAS2026_0049 |
| Bardera, R. | CFD ANALYSIS OF MMRTG THERMAL PLUME ON THE EXTERNAL AERODYNAMICS OF A MARS ROVER | ICAS2026_0054 |
| Bardera, R. | DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE. | ICAS2026_0427 |
| Barroso, E. | WIND TUNNEL INVESTIGATION OF HELICOPTER LOADS DURING URBAN OPERATIONS ON A BUILDING WITH COLUMNAR VORTEX GENERATORS | ICAS2026_0049 |
| Barroso, E. | CFD ANALYSIS OF MMRTG THERMAL PLUME ON THE EXTERNAL AERODYNAMICS OF A MARS ROVER | ICAS2026_0054 |
| Barroso, E. | DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE. | ICAS2026_0427 |
| Barry, N. | INVESTIGATION OF DECARBONISATION PATHWAYS FOR SHORT HAUL AVIATION USING A DISCRETE OPTIMISATION DECISION-MAKING ALGORITHM | ICAS2026_0396 |
| Barter, S. | DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS | ICAS2026_0250 |
| Barys, K. | MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS | ICAS2026_0143 |
| Bashir, M. | EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION | ICAS2026_0673 |
| Battaglia, M. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Batty, T. | MULTI-OBJECTIVE OPTIMISATION OF AERIAL VEHICLES USING REINFORCEMENT LEARNING | ICAS2026_0034 |
| Bayandor, J. | PROGRESSIVE FAILURE TIMELINE RECOUNT OF AN ATMOSPHERIC REENTRY TRAGEDY - IN MEMORY OF STS-107 CREW, AND DR. FRANK ABDI | ICAS2026_1100 |
| Becker, K. | TOWARDS AN ONTOLOGY-BASED APPROACH FOR DISCIPLINE-SPECIFIC ENGINEERING VIEWS IN ENGINE DESIGN | ICAS2026_0353 |
| Becker, T.H. | LASER SCANNING STRATEGIES TO INVESTIGATE THE EFFECTS OF OXIDATION IN PURE TANTALUM | ICAS2026_0507 |
| Behr, M. | PHYSICS-INFORMED NEURAL NETWORKS FOR ULTRASONIC LAMB WAVE RECONSTRUCTION IN NON-DESTRUCTIVE TESTING | ICAS2026_0573 |
| Bejarano Espada, C. | APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS | ICAS2026_0359 |
| Bejarano Espada, C. | AI IN THE COCKPIT: THE JARVIS STORY | ICAS2026_0547 |
| Bekemeyer, P. | GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION | ICAS2026_1011 |
| Ben Simon, M. | DIGITAL TWIN FOR AIR DEFENSE: LIVE-VIRTUAL-CONSTRUCTIVE INTEGRATION AND DECISION SUPPORT | ICAS2026_0076 |
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| Bierig, A. | MODEL-BASED FUNCTIONAL HAZARD ASSESSMENT BASED ON ARP4761A USING SYSML V1 AND SYSML V2 | ICAS2026_0674 |
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| Bliemetsrieder, W. | HARDWARE-IN-THE-LOOP VERIFICATION OF A SAFETY-CRITICAL RECONFIGURABLE BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIRCRAFT | ICAS2026_0557 |
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| Blom, P.H.L. | REDUCED-ORDER MODELLING OF MINI-TAB SPOILER DYNAMICS FOR GUST LOAD ALLEVIATION | ICAS2026_0374 |
| Boggero, L. | VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS | ICAS2026_0336 |
| Boggero, L. | AIRCRAFT AND INDUSTRIAL SYSTEMS CO-ARCHITECTING BASED ON VALUE-DRIVEN MBPLE APPROACH | ICAS2026_0337 |
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| Budinger, M. | POWER-HIL TESTING OF LI-PO BATTERY PACKS FOR LIGHTWEIGHT EVTOL UAVS | ICAS2026_0619 |
| Budinger, M. | A MPC–MHE STRATEGY FOR FREQUENCY TRACKING AND PARAMETERS ESTIMATION OF RESONANT DE-ICING SYSTEMS | ICAS2026_0660 |
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| Candon, M. | TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT | ICAS2026_0183 |
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| Carrese, R. | GEOMETRY PARAMETERISATION VIA A STRUCTURAL MODAL BASIS FOR AERODYNAMIC SHAPE OPTIMISATION | ICAS2026_0155 |
| Casalino, D. | CHALLENGES IN ADVANCED AIR MOBILITY NOISE PREDICTION - FROM SOURCE TO PERCEPTION | ICAS2026_0345 |
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| Castellanos, R. | GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION | ICAS2026_1011 |
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| Cavallaro, R. | HIERARCHICAL HIGH-ORDER BEAM MODELS FOR OPTIMISATION-ORIENTED ANALYSIS OF COMPOSITE WING-LIKE STRUCTURES | ICAS2026_0930 |
| Cecrdle, J. | WIND TUNNEL TESTING OF WHIRL FLUTTER AEROELASTIC DEMONSTRATOR | ICAS2026_0014 |
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| Cesnik, C.E.S. | RESIDUAL LEARNING FRAMEWORK FOR NONLINEAR AEROELASTIC–FLIGHT-DYNAMICS CONTROL-ORIENTED MODELING OF VERY FLEXIBLE AIRCRAFT | ICAS2026_0664 |
| Cestino, E. | MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELING | ICAS2026_0634 |
| Chakraborty, I. | A WORKFLOW FOR RAPID DESIGN, SIMULATION, FABRICATION, AND SUBSCALE FLIGHT-TESTING OF NOVEL AIRCRAFT CONCEPTS | ICAS2026_0845 |
| Chakraborty, I. | SIMULATION MODEL CALIBRATION USING SYSTEM IDENTIFICATION FOR A VECTORED-THRUST MULTI-TILT-ROTOR CONFIGURATION | ICAS2026_0929 |
| Chalupczynski, R. | MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS | ICAS2026_0143 |
| Chamitoff, G. | GUST ERROR METHOD (GEM): PARAMETER IDENTIFICATION FOR AIRCRAFT SUBJECT TO VON KÁRMÁN PROCESS NOISE | ICAS2026_0633 |
| Chan, J. | FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION | ICAS2026_0888 |
| Chan, J.L.C | PERFORMANCE COMPARISON BETWEEN PASSENGER AIRCRAFT WITH NOVEL PROPULSION SYSTEMS AT CONCEPTUAL DESIGN LEVEL | ICAS2026_0447 |
| Chan, J.L.C. | COMPARING DIFFERENT SEMI-EMPIRICAL AERODYNAMIC TOOLS FOR ANALYSING NOVEL AIRCRAFT CONFIGURATIONS | ICAS2026_0445 |
| Chance, A. | ATTITUDE CONTROL TECHNIQUES FOR A MICRO-SCALE FLAP-BASED AERODYNAMIC DECELERATOR SYSTEM | ICAS2026_0361 |
| Chandrasekar, V. | ON THE FEASIBILITY OF MACHINE LEARNING-BASED DETECTION OF AIRCRAFT LIGHTNING STRIKE RISK AREAS | ICAS2026_0803 |
| Chang, B.S. | HIGH-PRECISION EDDY-CURRENT TIP CLEARANCE SENSOR WITHEXCEPTIONALHEAT RESISTANCE | ICAS2026_0483 |
| Chang, C.Y. | AUTOMATIC GENERATION OF PHYSICAL SYSTEM MODELS FOR AIRCRAFT SYSTEMS BASED ON LLMS | ICAS2026_0479 |
| Chang, J. | MODELING OF AIRCRAFT COMPONENT PLACEMENTS WITH BIN PACKING | ICAS2026_0460 |
| Chao, M. | COMPARATIVE DESIGN OF SBW AIRCRAFT WITH AERODYNAMIC SHAPE OPTIMIZATION FOR THREE DIFFERENT PROPULSION LAYOUTS | ICAS2026_0078 |
| Chappell, A. | SUBSCALE FLIGHT TRAINING EFFECTS ON PILOT WORKLOAD AND PERFORMANCE DURING VTOL HQTES | ICAS2026_0685 |
| Chaudhary, N.K. | MAGNETOPLASMAIONIC (MPI) ENGINE | ICAS2026_0739 |
| Chen, C. | A DISTRIBUTED MULTI-SOURCE SENSOR FUSION METHOD FOR COLLABORATIVE TARGET TRACKING | ICAS2026_0590 |
| Chen, F. | ACTIVE FLOW CONTROL AND THERMAL PROTECTION FOR A WING-BODY CONFIGURATION BASED ON LATERAL JET | ICAS2026_0255 |
| Chen, G. | NUMERICAL SIMULATION OF STRESS-OXIDATION DAMAGE IN C/SIC COMPOSITES AT HIGH TEMPERATURES | ICAS2026_0276 |
| Chen, M.X. | MULTI-BODY DYNAMIC MODELING OF A BIRD-LIKE FLAPPING-WING VEHICLE: ANALYSIS OF FLAPPING-AERODYNAMIC COUPLING EFFECTS | ICAS2026_0191 |
| Chen, Q. | DEEP LEARNING-BASED INVERSION OF NEAR-FIELD OVERPRESSURE SIGNATURES FOR LOW-BOOM SUPERSONIC TRANSPORT | ICAS2026_0278 |
| Chen, Q. | AIRFRAME-INLET INTEGRATION DESIGN FOR AN OVER-WING-MOUNTED SUPERSONIC TRANSPORT CONFIGURATION | ICAS2026_0501 |
| Chen, Q. | LOW BOOM DESIGN AND ANALYSIS OF A BLENDED-WING-BODY CONFIGURATION FOR LARGE-SIZED SUPERSONIC TRANSPORT | ICAS2026_0552 |
| Chen, S. | CST PARAMETRIC MODELING AND MULTI-OBJECTIVE OPTIMIZATION RECONFIGURATION STUDY OF A BLENDED-WING-BODY AIRCRAFT | ICAS2026_0455 |
| Chen, S. | MODELING, SIMULATION AND EVALUATION OF LARGE FOREST FIRE EXTINGUISHING AND RESCUE BASED ON AVIATION MATERIEL | ICAS2026_0910 |
| Chen, S. | NONLINEAR FRICTION MODELING OF HELIX SWING HYDRAULIC CYLINDERS FOR MORPHING AIRCRAFT USING PHYSICS-INFORMED NEURAL NETWORKS (PITCH SESSION) | ICAS2026_1097 |
| Chen, S.Y. | PREDICTION OF MINIMUM STARTING PRESSURE FOR HYDROSTATIC HELICAL ROTARY ACTUATOR USING PHYSICS-INFORMED NEURAL NETWORKS | ICAS2026_0593 |
| Chen, T. | NUMERICAL INVESTIGATION OF GUST LOAD ALLEVIATION FOR WINGS WITH PASSIVELY RELEASED FFWT | ICAS2026_0785 |
| Chen, T. | COMPARATIVE ANALYSIS OF DIFFERENT NUMERICAL SIMULATION METHODS FOR PROPELLER SLIPSTREAM | ICAS2026_0795 |
| Chen, T. | AILERON EFFICIENCY ANALYSIS OF FLEXIBLE HIGH-ASPECT-RATIO WING | ICAS2026_0796 |
| Chen, X.M. | COMPRESSIVE PERFORMANCE OF VARIABLE-STIFFNESS COMPOSITE HYPERBOLIC STIFFENED PANELS BASED ON GEOMETRIC PATH MAPPING | ICAS2026_0082 |
| Chen, X.W. | AFTERBODY CURVATURE EFFECTS ON FLOW LOSS CHARACTERISTICS BASED ON ENTROPY PRODUCTION | ICAS2026_0781 |
| Chen, Y. | MODEL PREDICTIVE CONTROL OF HYDROGEN–ELECTRIC AIRPORT ENERGY SYSTEMS FOR SUSTAINABLE GROUND OPERATIONS | ICAS2026_0016 |
| Chen, Y.S. | A NOVEL DUAL-PHASE BAYESIAN ESTIMATION AND MULTI-TASK LEARNING METHOD FOR PROCESS OPTIMIZATION FOR REDUCING LACK-OF-FUSION DEFECTS DURING LASER POWDER BED FUSION | ICAS2026_0270 |
| Chen, Y.Z. | ROBUST FAULT DIAGNOSIS FOR AERO-ENGINE NETWORKED CONTROL SYSTEMS UNDER TRANSMISSION UNCERTAINTIES | ICAS2026_0149 |
| Chen, Z. | FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES | ICAS2026_0171 |
| Chen, Z. | A COMPARATIVE STUDY OF THE AERODYNAMIC CHARACTERISTICS OF FOUR CONFIGURATIONS | ICAS2026_0280 |
| Chen, Z. | UNIFIED SEPARATION ASSURANCE FOR MULTI-UAV OPERATIONS: RISK-CALIBRATED BASELINES AND FAULT-AWARE ADAPTIVE RESOLUTION | ICAS2026_0554 |
| Chen, Z. | MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY | ICAS2026_0566 |
| Chen, Z. | PASSIVE FLOW CONTROL OF A TURBULENT BOUNDARY LAYER AT THE VERGE OF SEPARATION USING SURFACE ROUGHNESS | ICAS2026_1085 |
| Chen, Z.L. | EXERGY-BASED AERODYNAMIC CHARACTERISTICS ANALYSIS OF THE NASA COMMON RESEARCH MODEL AND BWB CONFIGURATION CIVIL AIRCRAFT | ICAS2026_0373 |
| Chen, Z.L. | 2D AND 3D TRAJECTORY PLANNING FOR UAVS FORMATION SYSTEM USING DYNAMIC WINDOW APPROACH | ICAS2026_0735 |
| Chen, Z.L. | INLET OPTIMIZATION DESIGN OF A BOUNDARY LAYER INGESTION PROPULSION SYSTEM | ICAS2026_0906 |
| Cheng, J.B. | A DISTRIBUTED MULTI-SOURCE SENSOR FUSION METHOD FOR COLLABORATIVE TARGET TRACKING | ICAS2026_0590 |
| Cheng, W. | QUANTIFYING LAND AERIAL RESCUE DEMAND INTENSITY: A DATA-DRIVEN MODELING APPROACH FOR DEFINING THE AIR-GROUND OPERATIONAL BOUNDARY | ICAS2026_0298 |
| Cheng, W. | SYSTEM EFFECTIVENESS EVALUATION OF CHINA'S AVIATION EMERGENCY COMMUNICATION SYSTEM | ICAS2026_0322 |
| Cheng, W. | MODELING, SIMULATION AND EVALUATION OF LARGE FOREST FIRE EXTINGUISHING AND RESCUE BASED ON AVIATION MATERIEL | ICAS2026_0910 |
| Chipper, M. | A FULL-SCALE DEMONSTRATOR FOR RAPID TESTING OF HELICOPTER AIRFRAMES USING ADVANCED CONTROL SYSTEM METHODOLOGIES | ICAS2026_0157 |
| Chisholm, H. | HYBRID ROCKET HOT-GAS DRIVER FOR DIRECT-CONNECT SCRAMJET THERMO-STRUCTURAL SCREENING | ICAS2026_0508 |
| Cho, B. | THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A WING–ROTOR CONFIGURATION FOR A FOLDING WING UAV | ICAS2026_0873 |
| Cho, J. | EXPERIMENTAL INVESTIGATION OF BLOWING RATIO EFFECT ON FLOW REGIMES OF TRANSPIRATION COOLING IN LATTICE POROUS MEDIA | ICAS2026_0776 |
| Cho, S. | CONVEX OPTIMIZATION-BASED EMERGENCY LANDING TRAJECTORY GENERATION FOR UAM VEHICLES | ICAS2026_0532 |
| Cho, Y. | UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS | ICAS2026_0521 |
| Choi, H | FEASIBILITY OF ELECTROPULSING-INDUCED FATIGUE CRACK CLOSURE IN AEROSPACE METALLIC MATERIALS | ICAS2026_0365 |
| Choi, H. | THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A WING–ROTOR CONFIGURATION FOR A FOLDING WING UAV | ICAS2026_0873 |
| Choi, H.S. | HYPERSONIC VEHICLE FLIGHT SIMULATION AND FLIGHT CONTROL | ICAS2026_0174 |
| Choi, S. | THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A WING–ROTOR CONFIGURATION FOR A FOLDING WING UAV | ICAS2026_0873 |
| Choi, W.I. | DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+ | ICAS2026_0130 |
| Chow, L. | FACTORS AFFECTING COMMUNICATION IN AVIATION | ICAS2026_0059 |
| Christen , C. | VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS | ICAS2026_0336 |
| Christensen, J.M. | ON THE APPLICABILITY OF SAFETY NETS: A SAFETY-BY-DESIGN SOLUTION FOR CERTIFYING NEURAL NETWORKS | ICAS2026_0210 |
| Christensen, J.M. | COVERAGE-DRIVEN VERIFICATION FOR SAFETY-BY-DESIGN IN AI-BASED COLLISION AVOIDANCE SYSTEMS | ICAS2026_0536 |
| Christiansen, F.H. | LINKING PRODUCT FAMILY ARCHITECTURE ANALYSIS AND COMPONENT-LEVEL OPTIMISATION USING SYSTEM MODELS | ICAS2026_0305 |
| Christiansen, F.H. | ASSESSING THE POTENTIAL OF MULTI-MODEL TOPOLOGY OPTIMIZATION FOR MODULAR LIGHTWEIGHT DESIGN OF AIRCRAFT CABIN STRUCTURES | ICAS2026_0406 |
| Christie, R. | NOVEL METHODS FOR THE CHARACTERISATION OF INTAKE FLOW DISTORTION | ICAS2026_0110 |
| Chu, D.L. | A HYBRID 0D–2D WHOLE-ENGINE MATCHING FRAMEWORK FOR TURBOJET ENGINE PERFORMANCE SIMULATION | ICAS2026_0687 |
| Chu, L.D. | PARAMETRIC DESIGN AND MULTI-OBJECTIVE OPTIMIZATION OF EXHAUST NOZZLE FOR GAS TURBINE ENGINES | ICAS2026_0579 |
| Chudnovsky, D. | SIMULATION-BASED ANALYSIS OF REDUNDANT UAV NAVIGATION UNDER GNSS OUTAGES | ICAS2026_0079 |
| Ci, K. | PREDICTION OF MINIMUM STARTING PRESSURE FOR HYDROSTATIC HELICAL ROTARY ACTUATOR USING PHYSICS-INFORMED NEURAL NETWORKS | ICAS2026_0593 |
| Ciliberti, D. | MIXED-FIDELITY, NONLINEAR AIRCRAFT MISSION MODELING FOR HYBRID REGIONAL AIRCRAFT DESIGN VERIFICATION | ICAS2026_0836 |
| Cinar, G. | A MULTI-SCALE COMPUTATIONAL FRAMEWORK FOR EVALUATING TECHNOLOGY IMPACTS ON FUTURE AIRCRAFT FLEETS | ICAS2026_0416 |
| Cini, A. | AN INCREMENTAL MODULAR MDO FRAMEWORK FOR HYDROGEN-ELECTRIC POWERTRAIN SIZING AND INTEGRATION IN GENERAL AVIATION AIRCRAFT | ICAS2026_0876 |
| Cini, A. | HIERARCHICAL HIGH-ORDER BEAM MODELS FOR OPTIMISATION-ORIENTED ANALYSIS OF COMPOSITE WING-LIKE STRUCTURES | ICAS2026_0930 |
| Cini, A. | AN AUTOMATED PARAMETRIC FRAMEWORK FOR EARLY-STAGE STRUCTURAL DESIGN AND OPTIMIZATION OF COMPOSITE AIRFRAMES | ICAS2026_0948 |
| Ciottoli, P.P. | MULTI-OBJECTIVE SHAPE OPTIMIZATION OF A LAUNCH VEHICLE FAIRING ACROSS MULTIPLE FLOW REGIMES | ICAS2026_0284 |
| Citron, T. | APPLICATION OF AI IN AEROSPACE AND IMPLICATIONS FOR AEROSPACE ENGINEERS | ICAS2026_0990 |
| Civera, M. | AIRFRAME HEALTH MONITORING ON THE BAE SYSTEMS HAWK T1A JET TRAINER | ICAS2026_0706 |
| Clarendon, J. | ATTITUDE CONTROL TECHNIQUES FOR A MICRO-SCALE FLAP-BASED AERODYNAMIC DECELERATOR SYSTEM | ICAS2026_0361 |
| Clark, L. | LOWERING THE BARRIER TO AEROACOUSTIC PREDICTION: GPU-COMPUTED SBES FOR FAR-FIELD LANDING GEAR NOISE PREDICTION | ICAS2026_1105 |
| Clark, P. | FIVE DEACADES OF T-38 WING TEARDOWNS: DATA, INSIGHT, AND IMPACT | ICAS2026_0830 |
| Clococeanu, M. | FLIGHT MISSION MODELING WITH VARYING BASELINE DATA: APPLICAITON IN BUSINESS AVIATION | ICAS2026_0315 |
| Clococeanu, M. | GLOBAL EMISSION MONITOR FOR 2023 | ICAS2026_0666 |
| Coder, J. | CFD VISION 2030 LOOKING FORWARD: PANEL DISCUSSION WITH J.CODER, J.P.SLOTNICK, N.J.WYMAN, C.WINKLER | ICAS2026_0999 |
| Coder, J.G. | EVALUATING THE LAMINAR FLOW ON A SLOTTED, NATURAL-LAMINAR-FLOW WING IN THE NASA AMES 11-FOOT TRANSONIC WIND TUNNEL | ICAS2026_0472 |
| Coder, J.G. | MULTIPOINT INVERSE DESIGN FOR TRANSONIC, SLOTTED, NATURAL-LAMINAR-FLOW WINGS | ICAS2026_0934 |
| Coder, J.G. | OVERVIEW OF VERIFICATION AND VALIDATION EFFORTS FOR PDE-BASED LAMINAR-TURBULENT TRANSITION MODELS | ICAS2026_0936 |
| Coertze, R. | CONCEPT OF OPERATIONS FOR A HYDROGEN-ELECTRIC POWERED MODIFIED DASH 8-300 REGIONAL AIRCRAFT: PERFORMANCE, OPERATIONAL, AND REGULATORY IMPACTS | ICAS2026_0307 |
| Cognolato, N. | DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY | ICAS2026_0827 |
| Coiro, D. | MULTIDISCIPLINARY APPROACH FOR THE AERODYNAMIC CHARACTERIZATION OF AN INFLATABLE CLOSED-WING HYBRID HIGH-ALTITUDE PSEUDO-SATELLITE | ICAS2026_0371 |
| Collins, J. | GEOMETRY PARAMETERISATION VIA A STRUCTURAL MODAL BASIS FOR AERODYNAMIC SHAPE OPTIMISATION | ICAS2026_0155 |
| Comer, A. | SUBSCALE FLIGHT TRAINING EFFECTS ON PILOT WORKLOAD AND PERFORMANCE DURING VTOL HQTES | ICAS2026_0685 |
| Comer, A. | EXPERIMENTAL CHARACTERIZATION OF PROPELLER-WING INTERACTIONS FOR A SUBSCALE LIFT + CRUISE VTOL UAV | ICAS2026_0689 |
| Comer, A.M. | OPTIMIZATION OF INTERCONNECTED 3D-PRINTED STRUCTURES FOR UAVS | ICAS2026_0943 |
| Condé Rocha Murça, M. | A SEMI-AUTONOMOUS DECISION SUPPORT TOOL FOR ATC IN EN-ROUTE REROUTING OPERATIONS | ICAS2026_0947 |
| Condomines, J.-P. | A STALL EXTENSION TO LIFTING-LINE THEORY: IMPLEMENTATION AND VALIDATION IN ASWING | ICAS2026_0720 |
| Connolly, J. | MODERNISING AT SCALE: DELIVERING AUSTRALIA’S NEXT-GENERATION AIR TRAFFIC SYSTEM | ICAS2026_1089 |
| Cooper, J. | ENABLING FORWARD SWEPT WING DESIGNS | ICAS2026_0381 |
| Coppotelli, G. | GROUND VIBRATION TEST ANALYSIS OF A PC-9 AIRCRAFT USING DELAY-EMBEDDED DYNAMIC MODE DECOMPOSITION WITH CONTROL | ICAS2026_0153 |
| Corcione, S. | COST-DRIVER MULTIDISCIPLINARY FRAMEWORK FOR WINGLET DESIGN: A REGIONAL AIRCRAFT CASE STUDY | ICAS2026_0783 |
| Corsi, M. | ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT | ICAS2026_0897 |
| Cox, J. | GUST ERROR METHOD (GEM): PARAMETER IDENTIFICATION FOR AIRCRAFT SUBJECT TO VON KÁRMÁN PROCESS NOISE | ICAS2026_0633 |
| Crase, S. | FLIGHT TRIALS OF DRONES CONTROLLED BY AI LARGE LANGUAGE MODELS | ICAS2026_0156 |
| Crase, S. | IMPLEMENTATION OF DISTRIBUTED SWARM GUIDANCE ALGORITHMS ON LOW-COST UAVS | ICAS2026_0771 |
| Cristea, G.C. | ARCHITECTED LATTICE SANDWICH STRUCTURES FOR LIGHTWEIGHT IMPACT AND ENERGY ABSORPTION APPLICATIONS | ICAS2026_0053 |
| Crossley, W.A. | SCHEDULING AND ROUTING FOR TIMETABLE-BOUND URBAN AIR MOBILITY OPERATIONS | ICAS2026_0103 |
| Cuco, A.P.C. | A QUALITATIVE FRAMEWORK FOR AIRCRAFT WING MANUFACTURING AND DECISION MAKING | ICAS2026_0766 |
| Cummings, M. | ENTRY INTO SERVICE REQUIRES CERTIFICATION FOR NOVEL TECHNOLOGY | ICAS2026_0398 |
| Cunha, J.A. | OFFLINE MULTIMODAL LARGE LANGUAGE MODELS FOR DECISION SUPPORT IN AIR OPERATIONS | ICAS2026_0450 |
| D'Aniello, F.A. | LARGE EDDY SIMULATIONS OF LOW-REYNOLDS NUMBER FLOWS IN THE COMPRESSIBLE REGIME | ICAS2026_0267 |
| Dabrowski, I. | MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS | ICAS2026_0143 |
| Dadashi, A. | DATA-DRIVEN TECHNOLOGY INTELLIGENCE: AN APPLICATION TO AIRCRAFT ENGINE MAINTENANCE | ICAS2026_1034 |
| Dai, W. | UNIFIED SEPARATION ASSURANCE FOR MULTI-UAV OPERATIONS: RISK-CALIBRATED BASELINES AND FAULT-AWARE ADAPTIVE RESOLUTION | ICAS2026_0554 |
| Dai, Y.T. | FLUTTER ANALYSIS OF A DYNAMIC VARIABLE-SWEEP WING | ICAS2026_0179 |
| Dalbies, E. | PERSPECTIVES & PROGRESS ON NEXTGEN PROPULSION FOR FUTURE AIRLINERS FROM SAFRAN’S STANDPOINT | ICAS2026_1099 |
| Daley, A. | RE-THINKING END OF LIFE AIRCRAFT INTERIORS THROUGH CO-DESIGN AND REPURPOSING | ICAS2026_0840 |
| Dalinajara Abreu Smith Borges, G. | PHYSICS-INFORMED NEURAL OPERATORS FOR DISTURBANCE FIELD PREDICTION IN NONPARALLEL BOUNDARY-LAYER STABILITY ANALYSIS | ICAS2026_0051 |
| Daniels, S. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Dantas, J.P.A. | OFFLINE MULTIMODAL LARGE LANGUAGE MODELS FOR DECISION SUPPORT IN AIR OPERATIONS | ICAS2026_0450 |
| Daoud, F. | NOVEL MULTIDISCIPLINARY MISSION-OPTIMISED AIRCRAFT DEVELOPMENT METHODOLOGY IN CONSIDERATION OF PASSIVE/ACTIVE CONTROL | ICAS2026_0230 |
| Daoud, F. | AN INDIVIDUALISED, SCALABLE PROJECT-BASED LEARNING FRAMEWORK FOR STRUCTURE DESIGN COURSES ESTABLISHED IN A LARGE AEROSPACE STUDY PROGRAMME | ICAS2026_0718 |
| Daria, V. | BEYOND THE HARDWARE: REGULATION AND CERTIFICATION AS THE CRITICAL PATH TO ADF AUTONOMOUS CAPABILITY | ICAS2026_0252 |
| Das, A. | GROUND VIBRATION TEST ANALYSIS OF A PC-9 AIRCRAFT USING DELAY-EMBEDDED DYNAMIC MODE DECOMPOSITION WITH CONTROL | ICAS2026_0153 |
| Das, A. | TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT | ICAS2026_0183 |
| Das, A. | NON-LINEAR PARAMETRIC MODEL FOR THE 3DOF MOTION OF A BOX IN WAVES USING SPARSE REGRESSION | ICAS2026_0228 |
| Das, M. | RE-THINKING END OF LIFE AIRCRAFT INTERIORS THROUGH CO-DESIGN AND REPURPOSING | ICAS2026_0840 |
| Das, R. | DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS | ICAS2026_0250 |
| Dautel, C.A. | VLSEC: A CONCEPT FOR SECURING VIRTUAL LINKS IN AVIONICS NETWORKS THROUGH CENTRALIZED GROUP KEY MANAGEMENT | ICAS2026_0701 |
| Davids, M. | LASER SCANNING STRATEGIES TO INVESTIGATE THE EFFECTS OF OXIDATION IN PURE TANTALUM | ICAS2026_0507 |
| Daw, Z. | ONTOLOGY-BASED SENSOR HEALTH MONITORING: A DYNAMIC ONTOLOGY-BASED FAULT DETECTION AND CLASSIFICATION FOR TIMESERIES DATA | ICAS2026_0716 |
| de Castro da Silva, A.F. | ASSESSING VORTEX BREAKDOWN AND COUPLING IN DELTA WING PLANFORMS THROUGH HIGH-FIDELITY DDES SIMULATIONS | ICAS2026_0939 |
| de Kock, M.R. | EFFECTS OF LIFT DISTRIBUTION AND WING POSTURE ON THE STABILITY AND CONTROL OF TAILLESS AIRCRAFT | ICAS2026_0924 |
| de Kruijk, J. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| De Marco, A. | MIXED-FIDELITY, NONLINEAR AIRCRAFT MISSION MODELING FOR HYBRID REGIONAL AIRCRAFT DESIGN VERIFICATION | ICAS2026_0836 |
| De Masellis, R. | APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS | ICAS2026_0359 |
| De Masellis, R. | AI IN THE COCKPIT: THE JARVIS STORY | ICAS2026_0547 |
| de Rosa Jacinto, M. | AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS | ICAS2026_0195 |
| de Rosa Jacinto, M. | PREDICTION OF PROPELLER NOISE IN LOW REYNOLDS NUMBER OPERATION USING MACHINE LEARNING MODELS | ICAS2026_0196 |
| de Rosa Jacinto, M. | INTEGRATION OF ACOUSTIC LINERS AND INTERNAL BYPASS CHANNELS INTO AAM PROPELLERS FOR NOISE REDUCTION | ICAS2026_0197 |
| de Smit, M. | ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS | ICAS2026_1005 |
| de Souza Rehder, I. | AUTOMATING SYSTEM MODELING USING LARGE LANGUAGE MODELS | ICAS2026_0809 |
| DeBlois, A. | A BENCHMARK FOR UNCERTAINTY QUANTIFICATION AND OPTIMIZATION UNDER UNCERTAINTY IN CONCEPTUAL AIRCRAFT DESIGN: THE F25-OUU CHALLENGE PROBLEM | ICAS2026_0320 |
| Defoort, S. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Defoort, S. | FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION | ICAS2026_0888 |
| Degenhardt, R. | INTERNATIONAL AND EUROPEAN RESEARCH AND TECHNOLOGY INFRASTRUCTURE DATA BASES IN AVIATION | ICAS2026_0181 |
| Degenhardt, R. | ADVANCES IN NON-DESTRUCTIVE BUCKLING PREDICTION OF THIN-WALLED STRUCTURES BY VIBRATIONS | ICAS2026_0313 |
| Degroote, J. | INFLUENCE OF ZIGZAG TAPE–INDUCED TRANSITION ON THE DU89-134 AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBER | ICAS2026_0221 |
| Deiler, C. | DYN-MARS: A NEW CONCEPT ENABLING THE BEST APPROACH FLIGHT PROFILE | ICAS2026_0265 |
| DeLaurentis, D.A. | SCHEDULING AND ROUTING FOR TIMETABLE-BOUND URBAN AIR MOBILITY OPERATIONS | ICAS2026_0103 |
| Delbecq, S. | ENDURANCE EVALUATION OF DIFFERENT UAV CONFIGURATIONS AND POWERTRAIN ARCHITECTURES | ICAS2026_0636 |
| Delgado, A. | ACCURACY AND EFFICIENCY OF TRANSITION–TURBULENCE MODELS IN PREDICTING HIGH AND LOW REYNOLDS NUMBER PROPELLER PERFORMANCE | ICAS2026_0226 |
| Delgado González, Y. | CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING | ICAS2026_1004 |
| Dell'Amico, A. | MODELLING COUPLED ON-BOARD SYSTEMS IN AIRCRAFT DESIGN | ICAS2026_0201 |
| Dell'Edera, A. | VALIDATION OF A LOW-COST DATA ACQUISITION SYSTEM FOR AIRCRAFT VIBRATION TESTING | ICAS2026_0724 |
| Delon, X. | AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC | ICAS2026_0347 |
| Delot, A.-L. | INTERNATIONAL AND EUROPEAN RESEARCH AND TECHNOLOGY INFRASTRUCTURE DATA BASES IN AVIATION | ICAS2026_0181 |
| Demant, N. | DEVELOPMENT OF CONTROL LAWS FOR ENHANCED PERFORMANCE AND AEROELASTIC STABILITY OF EVTOL AIRCRAFT | ICAS2026_0452 |
| Demel, B. | COMPOSITE FUSELAGE TECHNOLOGIES FOR NEXT GENERATION COMMERCIAL AIRCRAFT | ICAS2026_0115 |
| Depuru-Mohan, K. | FLOW SOLUTIONS AROUND VON KÁRMÁN OGIVES AT SUPERSONIC SPEEDS USING PHYSICS-INFORMED NEURAL NETWORKS AND PSP | ICAS2026_0632 |
| Dessena, G. | AIRFRAME HEALTH MONITORING ON THE BAE SYSTEMS HAWK T1A JET TRAINER | ICAS2026_0706 |
| Dessena, G. | VALIDATION OF A LOW-COST DATA ACQUISITION SYSTEM FOR AIRCRAFT VIBRATION TESTING | ICAS2026_0724 |
| Dessio Junior, G. | A MACHINE-LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION FRAMEWORK USING FREE-FORM DEFORMATION AND DEEP NEURAL NETWORKS | ICAS2026_0061 |
| Di Cicca, G.M. | MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELING | ICAS2026_0634 |
| Di Fede, F. | EXPERIMENTAL VALIDATION OF A FUEL CELL SYSTEM DIGITAL TWIN FOR A FULL-ELECTRIC AIRCRAFT POWERTRAIN | ICAS2026_0303 |
| Di Fiore, F. | MULTIDISCIPLINARY DESIGN OF COMPLIANT DEFORMABLE WINGS FOR IMPROVED AIRCRAFT EFFICIENCY: INTRODUCING AN ARCHITECTURE-AWARE OPTIMIZATION STRATEGY | ICAS2026_0610 |
| di Nucci, V | EMBRAER'S PERSPECTIVES & PROGRESS TOWARDS NEXTGEN AIRLINERS | ICAS2026_1026 |
| Di Pasquale, D. | NUMERICAL BOUNDARY LAYER VALIDATION TECHNIQUE USING RAE M2155 SWEPT WING | ICAS2026_0283 |
| Di Pasquale, D. | PROPOSAL FOR DISTINGUISHING USABLE DATA UNDER HIGH WIND TUNNEL BLOCKAGE USING AN RAE2822 TEST CASE | ICAS2026_0592 |
| Di Pasquale, D. | MODELLING SENSITIVITIES IN THREE-DIMENSIONAL FZRA-SPECTRUM ICE-SHAPE PREDICTION FOR THE CRM-HL STOWED CONFIGURATION | ICAS2026_0896 |
| Di Pasquale, D. | IMPLEMENTATION OF PROPELLER-WING INTERFERENCE MODEL AND HORIZONTAL TAIL ANALYSIS INTO A VISCOUS FULL POTENTIAL FLOW SOLVER FRAMEWORK FOR AIRCRAFT DESIGN | ICAS2026_0915 |
| Di Pasquale, D. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Di Rito, G. | A MODEL PREDICTIVE CONTROL STRATEGY FOR THE ENERGY MANAGEMENT OF HYBRID ELECTRIC PROPULSION SYSTEMS IN FIXED-WING UAVS | ICAS2026_0613 |
| Di Rito, G. | POWER-HIL TESTING OF LI-PO BATTERY PACKS FOR LIGHTWEIGHT EVTOL UAVS | ICAS2026_0619 |
| Di Stasio, M. | MULTIDISCIPLINARY DESIGN EXPLORATION OF HYBRID-ELECTRIC REGIONAL AIRCRAFT | ICAS2026_0360 |
| Di Stasio, M. | TOP-LEVEL AIRCRAFT REQUIREMENT TRADE STUDIES FOR HYDROGEN FUEL CELL REGIONAL AIRCRAFT | ICAS2026_0703 |
| Di Stasio, M. | OVERVIEW OF CRITICAL ISSUES AND OPPORTUNITIES FOR NEW A/C WITH HYBRID AND FULL-ELECTRIC POWERTRAIN | ICAS2026_0984 |
| Dias, G.R. | PREDICTION OF STRUCTURAL VIBRATIONS INDUCED BY MASS-UNBALANCED ELECTRIC PROPULSION SYSTEMS | ICAS2026_0901 |
| Dickinson, A. | FLIGHT PLANNING, THE FORGOTTEN ASSET | ICAS2026_1003 |
| Diecke, S. | ANALYSIS OF SOFTWARE DEVELOPMENT METHODS FOR A RECONFIGURABLE BATTERY SYSTEM FOR USE IN AN ELECTRIC AIRCRAFT | ICAS2026_0957 |
| Dietmüller, S. | JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION | ICAS2026_0212 |
| Dietz, G. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Dietzsch, G. | OFFLINE MULTIMODAL LARGE LANGUAGE MODELS FOR DECISION SUPPORT IN AIR OPERATIONS | ICAS2026_0450 |
| Dincer, U. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Ding, Y. | TEMPORAL INJECTION FOR REAL-TIME FLYING-BIRD DETECTION WITH RT-DETR | ICAS2026_0457 |
| Ding, Y. | RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING | ICAS2026_0782 |
| Dinh, T.Q. | PARAMETRIC DESIGN AND MULTI-OBJECTIVE OPTIMIZATION OF EXHAUST NOZZLE FOR GAS TURBINE ENGINES | ICAS2026_0579 |
| Discussion, P. | PANEL DISCUSSION WITH H. SCHLICKENMAIER (MODERATOR), D. PETERSON, M. CUMMINGS, C. BACZYNSKI, J. MARIS AND M. TRASKOS (DURATION TIL END OF THE BLOCK) | ICAS2026_1063 |
| Dixon, B. | ACCELERATED EXPERIMENTAL INVESTIGATION OF ENVIRONMENTALLY ASSISTED CRACKING IN AA7085 | ICAS2026_0244 |
| Djartov, B. | EXPLAINABILITY AT ALL LEVELS OF SYSTEM DEVELOPMENT: INSIGHTS FROM THE DESIGN OF INTELLIGENT SYSTEMS IN AVIATION | ICAS2026_0177 |
| Doan, N.A.K. | INVERSE AIRFOIL DESIGN USING AERODYNAMICALLY CONDITIONED VARIATIONAL AUTOENCODERS | ICAS2026_0894 |
| Dokter, G. | KEY STAKEHOLDERS IN AEROSPACE FOR A SUSTAINABLE AND CIRCULAR PRODUCT DEVELOPMENT - A SYSTEMATIC APPROACH | ICAS2026_0222 |
| Doll, C. | AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC | ICAS2026_0347 |
| Doll, C. | CONTROL ALLOCATION AND SIZING FOR OVER-ACTUATED AIRCRAFT | ICAS2026_0725 |
| Domínguez, D. | ACCURACY AND EFFICIENCY OF TRANSITION–TURBULENCE MODELS IN PREDICTING HIGH AND LOW REYNOLDS NUMBER PROPELLER PERFORMANCE | ICAS2026_0226 |
| Domínguez, D. | EXPERIMENTAL INVESTIGATION OF WISHBONE VORTEX GENERATOR EFFECTS ON THE NACA 4412 AIRFOIL AT LOW REYNOLDS NUMBERS | ICAS2026_0232 |
| Donaldson, B. | EXPLORING DETROIT METROPOLITAN WAYNE COUNTY AIRPORT AS A TESTBED FOR RESOLVING INTEGRATION CHALLENGES FOR AIR TAXI OPERATIONS | ICAS2026_0682 |
| Donelli, G. | VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS | ICAS2026_0336 |
| Donelli, G. | AIRCRAFT AND INDUSTRIAL SYSTEMS CO-ARCHITECTING BASED ON VALUE-DRIVEN MBPLE APPROACH | ICAS2026_0337 |
| Dong, M. | RECEPTIVITY OF NON-MODAL STREAKS IN HYPERSONIC BLUNT BOUNDARY LAYERS: FROM NUMERICS TO ASYMPTOTICS | ICAS2026_0070 |
| Dong, M. | ORIGIN OF TRANSIENT TURBULENT SPOTS IN HYPERSONIC SWEPT BOUNDARY LAYERS WITH MORPHING SWEEP ANGLES | ICAS2026_0094 |
| Dong, W. | NUMERICAL SIMULATION OF SUPERCOOLED LARGE DROPLET IMPINGEMENT ON ROTATING FAN BLADES | ICAS2026_0242 |
| Dong, W. | JET-INDUCED SWIRLING FLOW AND WALL HEAT TRANSFER FOR AERO-ENGINE NACELLE SWIRL ANTI-ICING SYSTEM | ICAS2026_0339 |
| Dong, Z. | NUMERICAL SIMULATION OF SUPERCOOLED LARGE DROPLET IMPINGEMENT ON ROTATING FAN BLADES | ICAS2026_0242 |
| Dong, Z.Y. | JET-INDUCED SWIRLING FLOW AND WALL HEAT TRANSFER FOR AERO-ENGINE NACELLE SWIRL ANTI-ICING SYSTEM | ICAS2026_0339 |
| Donovan, William Dean | PRACTICAL INNOVATION IN AEROSPACE | ICAS2026_1013 |
| Doolan, C. | EXPERIMENTAL INVESTIGATION ON THE INNER DUCT SURFACE UNSTEADY PRESSURE OF A DUCTED PROPELLER | ICAS2026_0033 |
| Dowell, E. H. | TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT | ICAS2026_0183 |
| Dragomirescu, A. | ARCHITECTED LATTICE SANDWICH STRUCTURES FOR LIGHTWEIGHT IMPACT AND ENERGY ABSORPTION APPLICATIONS | ICAS2026_0053 |
| Drake, M. | BOEING PRODUCT DEVELOPMENT - CHALLENGES AND OPPORTUNITIES IN SUSTAINABILITY | ICAS2026_0987 |
| Drawin, S. | ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS | ICAS2026_1005 |
| Du, Y.Q. | INVERSE AEROELASTIC SIZING FOR STRUT-BRACED WINGS VIA PHYSICS-GUIDED GENERATIVE MODELING | ICAS2026_0100 |
| Duarte da Silva, C.C. | A SIMULATION METHODOLOGY FOR MULTIROTOR-ASSISTED UAV LAUNCH | ICAS2026_0937 |
| Duda, H. | FLIGHT OPERATIONS AND TESTING OF A 450 KG EXPERIMENTAL GYROPLANE UAV | ICAS2026_0331 |
| Duda, H. | IMPACT OF SYSTEM LATENCIES ON PILOT INTERACTION AND HANDLING OF AN ELECTRICALLY POWERED GYROPLANE UAV WITH FPV-BASED REMOTE CONTROL | ICAS2026_0335 |
| Duensing, J. | A COMPARATIVE WMLES STUDY OF THE CRM-HL IN FREE-AIR AND IN THE NTF FACILITY | ICAS2026_0793 |
| Duggleby, A. | FROM FIRST ROTATING DETONATION ROCKET ENGINE (RDRE) FLIGHT TO HYPERSONIC RDRE FLIGHT | ICAS2026_1073 |
| Duplaa, S. | EXERGY AND INTEGRAL BOUNDARY LAYER PARAMETERS CHARACTERISTIC CURVES FOR AERODYNAMIC DESIGN AND OPTIMIZATION | ICAS2026_0378 |
| Duplaa, S. | EPSILON V4: AN OPEN-SOURCE TOOL FOR EXTENDED AERODYNAMICS EXERGY ANALYSIS | ICAS2026_0654 |
| Döll, C. | AI IN AVIATION CYBERSECURITY RISK ASSESSMENT: OPPORTUNITIES AND CHALLENGES | ICAS2026_1009 |
| Edgington-Mitchell, D. | MECHANISMS OF SCREECH MODE STAGING IN UNDEREXPANDED SUPERSONIC JETS | ICAS2026_1082 |
| Edmonds, B. | LOWERING THE BARRIER TO AEROACOUSTIC PREDICTION: GPU-COMPUTED SBES FOR FAR-FIELD LANDING GEAR NOISE PREDICTION | ICAS2026_1105 |
| Edsel, A. | SCHEDULING AND ROUTING FOR TIMETABLE-BOUND URBAN AIR MOBILITY OPERATIONS | ICAS2026_0103 |
| Ehlers, T. | JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION | ICAS2026_0212 |
| Eisenhut, D. | DATA-DRIVEN FAST NOISE PREDICTION OF AN UNCONVENTIONAL AIRCRAFT USING HIGH-FIDELITY SIMULATION DATA | ICAS2026_0273 |
| El Akoury, R. | AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC | ICAS2026_0347 |
| El-Soueidan, M. | HEAT EXCHANGER MODELING METHODS FOR HYDROGEN POWERED AERO ENGINES DURING THERMODYNAMIC CYCLE DESIGN | ICAS2026_0574 |
| Elia, R. | AI IN AVIATION CYBERSECURITY RISK ASSESSMENT: OPPORTUNITIES AND CHALLENGES | ICAS2026_1009 |
| Elliott, A. | PHYSICS-INFORMED MACHINE LEARNING FOR FLIGHT DYNAMICS IDENTIFICATION OF THE SAAB 340B USING FLIGHT TEST DATA | ICAS2026_0686 |
| Enea, G. | RUNWAY-AWARE CAPACITY ENVELOPES FOR LONG-RANGE ARRIVAL METERING UNDER OPERATING-DIRECTION CHANGES AT SINGAPORE CHANGI | ICAS2026_0408 |
| Enea, G. | A COMPARISON OF TRAJECTORY-BASED OPERATIONS IN THE UNITED STATES AND EUROPE IN SUPPORT OF GLOBAL HARMONIZATION | ICAS2026_0412 |
| Enghardt, L. | IMPACT ASSESSMENT OF COMPONENT FAILURES IN A PEM-FUEL CELL BASED PROPULSION SYSTEM FOR AIRCRAFT APPLICATIONS FOCUSING ON WATER MANAGEMENT | ICAS2026_0139 |
| Epps, N.A. | DYN-MARS: A NEW CONCEPT ENABLING THE BEST APPROACH FLIGHT PROFILE | ICAS2026_0265 |
| Erartsin, O. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Ericksen, M.J. | NUMERICAL CHARACTERISATION OF SHIP-AIRWAKE EFFECTS ON MEDIUM-WEIGHT UAV APPROACH AND GO-AROUND OPERATIONS TO CANBERRA-CLASS LHDS | ICAS2026_0759 |
| Escudero, M.A. | FLOW SOLUTIONS AROUND VON KÁRMÁN OGIVES AT SUPERSONIC SPEEDS USING PHYSICS-INFORMED NEURAL NETWORKS AND PSP | ICAS2026_0632 |
| Espinosa Juarez, E. | LOSS OF RELIABILITY OF NEW GENERATION ENGINES: THE CASE STUDY OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION AS A SYSTEM OF SYSTEMS | ICAS2026_0822 |
| Espinosa-Juárez, E. | MODELLING COUPLED ON-BOARD SYSTEMS IN AIRCRAFT DESIGN | ICAS2026_0201 |
| Espinosa-Juarez, E. | TOWARDS AN ECOSYSTEM FOR AERONAUTICAL RESEARCH IN MEXICO | ICAS2026_0639 |
| Espinosa-Juárez, E. | TOWARDS A SYSTEM-OF-SYSTEMS ENGINEERING ROADMAP FOR INTEGRATING SUSTAINABLE AVIATION FUEL INTO MEXICO’S AIRPORT FUEL INFRASTRUCTURE | ICAS2026_0722 |
| Esposito, A. | HRV BASED PILOTS WORKLOAD PREDICTION FOR AN INTELLIGENT COCKPIT WARNING SYSTEM | ICAS2026_0422 |
| Estival, D. | FACTORS AFFECTING COMMUNICATION IN AVIATION | ICAS2026_0059 |
| Eun, Y.J. | WEATHER-DRIVEN DEEP LEARNING FOR AIRPORT RUNWAY DIRECTION FORECASTING | ICAS2026_0838 |
| Evans, B. | A FULL-SCALE DEMONSTRATOR FOR RAPID TESTING OF HELICOPTER AIRFRAMES USING ADVANCED CONTROL SYSTEM METHODOLOGIES | ICAS2026_0157 |
| F. Azevedo, J.L. | PHYSICS-INFORMED NEURAL OPERATORS FOR DISTURBANCE FIELD PREDICTION IN NONPARALLEL BOUNDARY-LAYER STABILITY ANALYSIS | ICAS2026_0051 |
| F. Azevedo, J.L. | HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION OF WIND TURBINES USING A DISCRETE ADJOINT APPROACH | ICAS2026_0052 |
| F. Azevedo, J.L. | A MACHINE-LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION FRAMEWORK USING FREE-FORM DEFORMATION AND DEEP NEURAL NETWORKS | ICAS2026_0061 |
| Fabozzi, F.D. | DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY | ICAS2026_0827 |
| Fadda, T. | AUGMENTED REALITY SAFETY NETS FOR INCREASED AIRPORT SAFETY | ICAS2026_0811 |
| Fadda, T. | DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY | ICAS2026_0827 |
| Fadda, T. | AURAL DIGITAL TWIN FOR AIRCRAFT CABIN DESIGN | ICAS2026_0899 |
| Fadda, T. | VR FOR CABIN DESIGN AND CERTIFYING DIGITAL MRO MEASURES | ICAS2026_1109 |
| Faezeh, P. | AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES (PITCH SESSION) | ICAS2026_1095 |
| Falcone, L. | COST-DRIVER MULTIDISCIPLINARY FRAMEWORK FOR WINGLET DESIGN: A REGIONAL AIRCRAFT CASE STUDY | ICAS2026_0783 |
| Fallast, A. | MODELING OF CRITICAL WEATHER FLIGHT PERFORMANCE OF MULTICOPTER UAVS FOR RESILIENT CONTROLLER DESIGN. | ICAS2026_0695 |
| Faltum, L. | AGENTIC AI FOR AIRCRAFT PRELIMINARY DESIGN: PROOF OF CONCEPT | ICAS2026_0575 |
| Fan, Y. | EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN | ICAS2026_0490 |
| Fan, Y. | NUMERICAL STUDY OF UNSTEADY DISTORTION IN AN S-DUCT INTAKE SUBJECTED TO BLAST SHOCK WAVES | ICAS2026_0510 |
| Fang, J. | PREDEFINED-TIME AFFINE FORMATION FAULT-TOLERANT CONTROL FOR FIXED-WING UAVS WITH INPUT SATURATION | ICAS2026_0098 |
| Farcy, D. | STATIC AND DYNAMIC WIND-TUNNEL TESTING OF A TRANSPORT AIRCRAFT MODEL IN-STALL AND POST-STALL FLIGHT REGIMES | ICAS2026_0203 |
| Fard, M. | GROUND VIBRATION TEST ANALYSIS OF A PC-9 AIRCRAFT USING DELAY-EMBEDDED DYNAMIC MODE DECOMPOSITION WITH CONTROL | ICAS2026_0153 |
| Feng, H.J. | QUASI-STEADY AERODYNAMIC AND MBD COUPLED FLIGHT SIMULATION OF FOLDING MORPHING UAV | ICAS2026_0237 |
| Feng, R.-S. | STUDY ON THE INJECTOR JETTING CHARACTERISTICS FOR VENTILATION EFFICIENCY OPTIMIZATION IN AIRCRAFT ENGINE LUBRICATION SYSTEMS | ICAS2026_0849 |
| Feng, Y. | A THERMO-MECHANICAL PHASE FIELD MODEL CONSIDERING SOLID-LIQUID TRANSITION: APPLICATION TO ELECTROTHERMAL DE-ICING | ICAS2026_0025 |
| Fenthum, D. | INVESTIGATING A STABLE LIFTING FUSELAGE FOR A TWO SEAT SAILPLANE OF THE GULL WING CONFIGURATION | ICAS2026_0931 |
| Feretto, D. | SUPPORTING THE REGULATORY COMMUNITY SHAPING THE FUTURE OF SUSTAINABLE HIGH-SPEED CIVIL AVIATION: THE ESATTO FRAMEWORK | ICAS2026_0926 |
| Fernandes, J.E.M. | FIXED-WING AIRCRAFT PORT-HAMILTONIAN DYNAMICS AND CONTROL | ICAS2026_0425 |
| Fernandes, J.E.M. | AUTOPILOT DESIGN OF AN UNSTABLE FIGHTER USING MODEL PREDICTIVE CONTROL | ICAS2026_0791 |
| Fernandes Lourenço, G. | TRIM PERFORMANCE EXPLORATION FOR AN AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION AND A TAIL THRUST UNIT | ICAS2026_0377 |
| Fernandes Viana, R. | A SEMI-AUTONOMOUS DECISION SUPPORT TOOL FOR ATC IN EN-ROUTE REROUTING OPERATIONS | ICAS2026_0947 |
| Fernández, J. | WIND TUNNEL INVESTIGATION OF HELICOPTER LOADS DURING URBAN OPERATIONS ON A BUILDING WITH COLUMNAR VORTEX GENERATORS | ICAS2026_0049 |
| Fernández, J. | CFD ANALYSIS OF MMRTG THERMAL PLUME ON THE EXTERNAL AERODYNAMICS OF A MARS ROVER | ICAS2026_0054 |
| Fernández, J. | DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE. | ICAS2026_0427 |
| Ferrand, V. | THIN AEROFOILS OSCILLATING IN A CONFINED INVISCID FLOW | ICAS2026_0637 |
| Ferrara, G. | EXPERIMENTAL VALIDATION OF A FUEL CELL SYSTEM DIGITAL TWIN FOR A FULL-ELECTRIC AIRCRAFT POWERTRAIN | ICAS2026_0303 |
| Ferraz, A.T. | VIRTUAL COMMISSIONING APPLIED TO ROS AIRCRAFT ROBOTIC CELL | ICAS2026_0198 |
| Ferreira, G.V. | A SIMULATION METHODOLOGY FOR MULTIROTOR-ASSISTED UAV LAUNCH | ICAS2026_0937 |
| Ferreira, M.S. | STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR IMPACT RESPONSE FOR LIGHTWEIGHT FIXED-WING UAVS | ICAS2026_0833 |
| Ferrigno, F. | INTERNATIONAL AND EUROPEAN RESEARCH AND TECHNOLOGY INFRASTRUCTURE DATA BASES IN AVIATION | ICAS2026_0181 |
| Field, I. | NEW INSIGHTS INTO AA7085 ENVIRONMENTALLY ASSISTED CRACKING THROUGH HIGH RESOLUTION FRACTOGRAPHY | ICAS2026_0234 |
| Field, I. | ACCELERATED EXPERIMENTAL INVESTIGATION OF ENVIRONMENTALLY ASSISTED CRACKING IN AA7085 | ICAS2026_0244 |
| Fields, T. | ATTITUDE CONTROL TECHNIQUES FOR A MICRO-SCALE FLAP-BASED AERODYNAMIC DECELERATOR SYSTEM | ICAS2026_0361 |
| Filho, A.A. | OSCILLATORY FAILURE DETECTION IN AIRCRAFT ACTUATION SYSTEMS USING WAVELET TRANSFORM | ICAS2026_0683 |
| Filippatos, A. | TOWARDS INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES: INSPECTABILITY ASSESSMENT OF HAT-STIFFENED PANELS | ICAS2026_0914 |
| Filippatos, A. | AI-ASSISTED DESIGN OF HOLISTICALLY SUSTAINABLE AEROSTRUCTURES | ICAS2026_0975 |
| Finck, T. | FLIGHT CENTRIC ATC – HOW TO SOLVE CONFLICTS WITHOUT COMMUNICATION AND COORDINATION OVERLOADS? | ICAS2026_0178 |
| Finck, T. | A COMPARISON OF TRAJECTORY-BASED OPERATIONS IN THE UNITED STATES AND EUROPE IN SUPPORT OF GLOBAL HARMONIZATION | ICAS2026_0412 |
| Finke, M. | VALIDATION OF TRADITIONAL COMPETENCY-BASED ASSESSMENT AND EXPERIENCE-BASED AUTHORISATION FOR AIR TRAFFIC CONTROLLERS | ICAS2026_0568 |
| Fiore, M. | EPSILON V4: AN OPEN-SOURCE TOOL FOR EXTENDED AERODYNAMICS EXERGY ANALYSIS | ICAS2026_0654 |
| Fischer, M. | NASA RESEARCH FOR AIRLINERS OF 2050 AND BEYOND / DLR\'S PERSPECTIVES & PROGRESS ON AIRLINERS FOR 2050+ ENERGY LANDSCAPES | ICAS2026_0983 |
| Footer, C. | CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING | ICAS2026_1004 |
| Forlingieri, M. | AIRCRAFT AND INDUSTRIAL SYSTEMS CO-ARCHITECTING BASED ON VALUE-DRIVEN MBPLE APPROACH | ICAS2026_0337 |
| Fornaciari, E. | ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT | ICAS2026_0897 |
| Foster, W. | DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS | ICAS2026_0250 |
| Francoeur, D. | DESIGN AND OPERATION OF LOW-COST MULTI-SCALE TEST BEDS FOR BATTERY THERMAL RUNAWAY INITIATION AND PROPAGATION | ICAS2026_0030 |
| Frank, J. | MODULAR JET AND PROPELLER ENGINE – PART I: INITIAL STUDIES | ICAS2026_0813 |
| Frank, J. | MODULAR JET AND PROPELLER ENGINE – PART II: INTEGRATED DESIGN PROCESS AND DESIGN SPACE ASSESSMENT | ICAS2026_0829 |
| Franke, D. | KEY PARAMETER IDENTIFICATION IN AIRCRAFT STRAIN PREDICTION MODELS | ICAS2026_0032 |
| Franzoni, F. | ADVANCES IN NON-DESTRUCTIVE BUCKLING PREDICTION OF THIN-WALLED STRUCTURES BY VIBRATIONS | ICAS2026_0313 |
| Frascareli Ali, I. | EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY | ICAS2026_1116 |
| Frediani, A. | LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY | ICAS2026_0643 |
| Freer, R. | EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION | ICAS2026_0673 |
| Frei, L. | AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS | ICAS2026_0195 |
| Frey, Y. | NOVEL METHODS FOR THE CHARACTERISATION OF INTAKE FLOW DISTORTION | ICAS2026_0110 |
| Frey, Y. | EFFECT OF INTAKE AERODYNAMICS AND FLOW DISTORTION ON FAN STALL INCEPTION | ICAS2026_0111 |
| Friedrich, M. | EXPLAINABILITY AT ALL LEVELS OF SYSTEM DEVELOPMENT: INSIGHTS FROM THE DESIGN OF INTELLIGENT SYSTEMS IN AVIATION | ICAS2026_0177 |
| Frulla, G. | MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELING | ICAS2026_0634 |
| Fröhler, B. | RUBBER ENGINE INTEGRATED OPTIMIZATION STRATEGY FOR OVERALL AIRCRAFT DESIGN | ICAS2026_0612 |
| Fu, J. | A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS | ICAS2026_0538 |
| Fu, J. | PREDICTION OF MINIMUM STARTING PRESSURE FOR HYDROSTATIC HELICAL ROTARY ACTUATOR USING PHYSICS-INFORMED NEURAL NETWORKS | ICAS2026_0593 |
| Fu, J. | AN EMBEDDED PHYSICS-INFORMED NEURAL NETWORK (PINN) FRAMEWORK FOR HIGH-FIDELITY REAL-TIME SIMULATION OF A FLIGHT CONTROL SURFACE ACTUATION SYSTEM | ICAS2026_0715 |
| Fu, J. | PERFORMANCE DEGRADATION ANALYSIS OF RESOLVER FAULTS IN ELECTRO-MECHANICAL ACTUATOR | ICAS2026_0784 |
| Fu, J. | MECHANISM-DATA FUSION MODELING METHOD FOR AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEMS | ICAS2026_0961 |
| Fu, J.C. | ROBUST ATTITUDE RECOVERY CONTROL FOR AIR-LAUNCHED FOLDING-WING UAVS VIA DISTURBANCE-COMPENSATED SUPER-TWISTING SLIDING MODE | ICAS2026_0506 |
| Fu, Q. | MULTI-BODY DYNAMIC MODELING OF A BIRD-LIKE FLAPPING-WING VEHICLE: ANALYSIS OF FLAPPING-AERODYNAMIC COUPLING EFFECTS | ICAS2026_0191 |
| Fu, S. | PILOT WORKLOAD PROFILES UNDER CONTINUOUS MULTI-TASKING AND SPARSE EVENTS VIGILANCE | ICAS2026_0091 |
| Fu, S. | HYPERSONIC RECEPTIVITY TO FREESTREAM DISTURBANCES OVER A BLUNT WEDGE: A LINEARIZED NAVIER-STOKES APPROACH | ICAS2026_0653 |
| Fuchs, A. | APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS | ICAS2026_0359 |
| Fuchs, A. | AI IN THE COCKPIT: THE JARVIS STORY | ICAS2026_0547 |
| Fuchs, M. | AUTOMATED KNOWLEDGE-BASED CABIN DESIGN AND EVALUATION WITHIN A PRELIMINARY AIRCRAFT DESIGN LOOP | ICAS2026_0214 |
| Fuchsgruber, S. | SENSITIVITY-BASED REFERENCE TRAJECTORY UPDATES FOR AIRCRAFT PATH-FOLLOWING MODEL PREDICTIVE CONTROL | ICAS2026_0821 |
| Fujio, C. | PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN | ICAS2026_0370 |
| Fujio, C. | MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) | ICAS2026_1074 |
| Fureby, C. | PHYSICAL AND NUMERICAL MODELING OF SUPERSONIC COMBUSTION FOR HYPERSONIC FLIGHT | ICAS2026_1075 |
| Fusaro, R. | SUPPORTING THE REGULATORY COMMUNITY SHAPING THE FUTURE OF SUSTAINABLE HIGH-SPEED CIVIL AVIATION: THE ESATTO FRAMEWORK | ICAS2026_0926 |
| Fürst, J. | MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELING | ICAS2026_0634 |
| Galffy, A. | ANALYSIS OF A DUAL AIR DATA AND MULTI-HOLE PRESSURE PROBE BOOM | ICAS2026_0775 |
| Galinski, C. | STABILITY ANALYSIS OF A LIGHT UAV WITH SOLAR PROPULSION | ICAS2026_0219 |
| Gallagher, C. | INVESTIGATION OF DECARBONISATION PATHWAYS FOR SHORT HAUL AVIATION USING A DISCRETE OPTIMISATION DECISION-MAKING ALGORITHM | ICAS2026_0396 |
| Gampe, A. | APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS | ICAS2026_0359 |
| Gan, K. | EFFECTS OF FLYING WING CONFIGURATION PARAMETERS ON AERODYNAMICS AND STABILITY | ICAS2026_0263 |
| Gan, K. | RESEARCH ON AERODYNAMIC-STEALTH INTEGRATED DESIGN METHODOLOGY BASED ON MPPO ALGORITHM | ICAS2026_0462 |
| Gan, Y. | SUPERVISED DIMENSIONALITY-REDUCED MULTI-FIDELITY SURROGATE MODEL ASSISTED HIGH-DIMENSIONAL NATURAL LAMINAR FLOW OPTIMIZATION | ICAS2026_0502 |
| Gao, H. | TEMPORAL INJECTION FOR REAL-TIME FLYING-BIRD DETECTION WITH RT-DETR | ICAS2026_0457 |
| Gao, H. | RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING | ICAS2026_0782 |
| Gao, J. | TEMPORAL INJECTION FOR REAL-TIME FLYING-BIRD DETECTION WITH RT-DETR | ICAS2026_0457 |
| Gao, J. | RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING | ICAS2026_0782 |
| Gao, X.H. | AUTOMATIC GENERATION OF PHYSICAL SYSTEM MODELS FOR AIRCRAFT SYSTEMS BASED ON LLMS | ICAS2026_0479 |
| Gao, Y. | OPTIMIZATION OF MORPHOLOGICAL AND KINEMATIC PARAMETER FOR FLAPPING WING IN FORWARD FLIGHT | ICAS2026_0089 |
| Gao, Y. | PILOT WORKLOAD PROFILES UNDER CONTINUOUS MULTI-TASKING AND SPARSE EVENTS VIGILANCE | ICAS2026_0091 |
| Gao, Y. | EFFECTS OF FLYING WING CONFIGURATION PARAMETERS ON AERODYNAMICS AND STABILITY | ICAS2026_0263 |
| Gao, Y.N. | BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL | ICAS2026_0647 |
| Gao, Z. | FLIGHT-TEST DATA-DRIVEN HIGH-ANGLE-OF-ATTACK DYNAMICS MODELING VIA LSTM-POLYNOMIAL HYBRID APPROACH | ICAS2026_0269 |
| Gao, Z. | LOW-NOISE VERTIPORT PROCEDURE PLANNING USING DEEP REINFORCEMENT LEARNING | ICAS2026_0580 |
| Gao, Z. | RECIPROCITY-GUIDED JOINT BASE STATION PLACEMENT AND FLIGHT CORRIDOR PLANNING FOR URBAN AIR MOBILITY | ICAS2026_0587 |
| Gao, Z. | GEOMETRY-DRIVEN AIR TRAFFIC CONFLICT RESOLUTION VIA CAUCHY-STOKES RANDERS METRIC | ICAS2026_0605 |
| Garbarino, L. | REAL-TIME EMULATION TESTBENCH FOR FUEL-CELL/BATTERY HYBRIDIZATION IN HYDROGEN-ELECTRIC AVIATION | ICAS2026_0338 |
| Garcia, A. | A MULTI-SCALE COMPUTATIONAL FRAMEWORK FOR EVALUATING TECHNOLOGY IMPACTS ON FUTURE AIRCRAFT FLEETS | ICAS2026_0416 |
| García-Gutiérrez, A. | EXPERIMENTAL INVESTIGATION OF WISHBONE VORTEX GENERATOR EFFECTS ON THE NACA 4412 AIRFOIL AT LOW REYNOLDS NUMBERS | ICAS2026_0232 |
| Garcia-Martinez, J. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Garofano, A. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Garth, James | DISCRIMINATORY AUTONOMY: OPERATING FASTER, SMARTER, AND WITH PURPOSE | ICAS2026_1012 |
| Gates, S. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Gauvrit-Ledogar, J. | FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION | ICAS2026_0888 |
| Gavrilovic, N. | COMPARATIVE ATMOSPHERIC MEASUREMENTS USING UAV-MOUNTED ULTRASONIC ANEMOMETER AND DOPPLER LIDAR | ICAS2026_0133 |
| Gavrilovic, N. | CHALLENGES AND SOLUTIONS FOR LIQUID HYDROGEN-POWERED UAVS: REGULATIONS AND CASE STUDY INSIGHTS | ICAS2026_0213 |
| Ge, Y. | SEMI-SUPERVISED MULTI-TASK CONSISTENCY LEARNING FOR DEFECT DETECTION AND DEPTH ESTIMATION | ICAS2026_0072 |
| Ge, Z.H. | PERFORMANCE DEGRADATION ANALYSIS OF RESOLVER FAULTS IN ELECTRO-MECHANICAL ACTUATOR | ICAS2026_0784 |
| Gearhart, S. | A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. | ICAS2026_0041 |
| Gee-Landman, N. | AIRBRAKES CONTROL SYSTEM FOR PRECISE APOGEE CONTROL OF A SOUNDING ROCKET | ICAS2026_0843 |
| Geisbauer, S. | TOWARDS CERTIFICATION BY ANALYSIS: A MILITARY AIRWORTHINESS PERSPECTIVE | ICAS2026_1051 |
| Gendron, M. | DESIGN AND OPERATION OF LOW-COST MULTI-SCALE TEST BEDS FOR BATTERY THERMAL RUNAWAY INITIATION AND PROPAGATION | ICAS2026_0030 |
| Geraghty, D. | DYNAMIC RECONFIGURABLE PATH PLANNING FOR FIRE-FIGHTING UAVS | ICAS2026_0217 |
| Gerber, M. | NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT | ICAS2026_0216 |
| Gerber, M. | DYN-MARS: A NEW CONCEPT ENABLING THE BEST APPROACH FLIGHT PROFILE | ICAS2026_0265 |
| Gerdts, M. | SENSITIVITY-BASED REFERENCE TRAJECTORY UPDATES FOR AIRCRAFT PATH-FOLLOWING MODEL PREDICTIVE CONTROL | ICAS2026_0821 |
| Germain, J. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Gerner, T. | TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT | ICAS2026_0183 |
| Gerner, T. | DECOUPLED DEEP REINFORCEMENT LEARNING FOR AUTONOMOUS LANDING OF UAVS ON SHIPS | ICAS2026_0867 |
| Giannouloudis, A. | MIDAS: A MODULAR SOFTWARE FOR INTAKE FLOW DISTORTION ANALYSIS | ICAS2026_0705 |
| Gibbs, J. | CONCEPTUAL DESIGN OF A MIDDLE-OF-THE-MARKET AIRCRAFT FOR EDUCATIONAL PURPOSES | ICAS2026_0420 |
| Gliszczynski, A. | INTERNATIONAL AND EUROPEAN RESEARCH AND TECHNOLOGY INFRASTRUCTURE DATA BASES IN AVIATION | ICAS2026_0181 |
| Gliszczynski, A. | ADVANCES IN NON-DESTRUCTIVE BUCKLING PREDICTION OF THIN-WALLED STRUCTURES BY VIBRATIONS | ICAS2026_0313 |
| Goeppel, S.B. | REDUCING AIR TRAFFIC COMPLEXITY IN JAPANESE AIRSPACE THROUGH MINOR LATERAL TRAJECTORY ADJUSTMENTS | ICAS2026_0048 |
| Goerttler, A. | A GRAPH NEURAL NETWORK SIMULATOR FOR TRANSONIC VORTEX-DOMINATED FLOWS ON THE DLR-F23 CONFIGURATION | ICAS2026_0358 |
| Goerttler, A. | REYNOLDS NUMBER SCALING EFFECTS IN TRANSONIC CAVITY AERODYNAMICS: A HIGH-FIDELITY EXPERIMENTAL AND NUMERICAL FRAMEWORK | ICAS2026_0362 |
| Goetzendorf-Grabowski, T. | STABILITY ANALYSIS OF A LIGHT UAV WITH SOLAR PROPULSION | ICAS2026_0219 |
| Gojon, R. | STUDY OF THE FEASIBILITY OF ACOUSTIC LINERS INSIDE THE BEAM THAT INTERACTS WITH A UAV DRONE ROTOR | ICAS2026_0743 |
| Gollnick, V. | INTERFACING MISSION SIMULATION WITH INTELLIGENT AGENTIC SYSTEMS FOR OPERATIONAL AND ETHICAL EVALUATION | ICAS2026_0675 |
| Gollnick, V. | DATA-DRIVEN SYNTHESIS OF AIRCRAFT FEEDBACK CONTROL LAWS FOR NEW COMMERCIAL FLIGHT SCENARIOS | ICAS2026_0891 |
| Gollnick, V. | STANDARDIZED TAKE-OFF AND LANDING PROCEDURES FOR AIR TAXIS: URBAN AIR MOBILITY | ICAS2026_0946 |
| Gomes, L.F.S. | COST-EFFECTIVE CFD REPRODUCTION OF DPW-7 CASE 2A FOR CRM TRANSONIC PITCHING-MOMENT PREDICTION AND ADAPTIVE-REFINEMENT ASSESSMENT | ICAS2026_0953 |
| Gómez Falcón, L. | TOWARDS A SYSTEM-OF-SYSTEMS ENGINEERING ROADMAP FOR INTEGRATING SUSTAINABLE AVIATION FUEL INTO MEXICO’S AIRPORT FUEL INFRASTRUCTURE | ICAS2026_0722 |
| Gong, R.X. | ANOMALY B-VALUE DETECTION AND EXCLUSION OF GBAS BASED ON WAVELET MULTI-RESOLUTION ANALYSIS | ICAS2026_0028 |
| Gong, Z. | RESEARCH ON GENERALIZED REPRESENTATION OF FLYING-WING CONFIGURATIONS BASED ON DEEP LEARNING | ICAS2026_0458 |
| Gonzales-DeGreiff, P. | IGNIT3: AN INTEGRATED COMPUTATIONAL FRAMEWORK FOR NON-IDEAL THERMODYNAMIC ANALYSIS AND OPTIMIZATION OF TURBOJET AND TURBOFAN ENGINES | ICAS2026_0426 |
| González Cabeza, J.I. | ASSESSING AN ALTERNATE AIRPORT ASSISTANT | ICAS2026_0192 |
| Gonzalez-Mitte, J. | IGNIT3: AN INTEGRATED COMPUTATIONAL FRAMEWORK FOR NON-IDEAL THERMODYNAMIC ANALYSIS AND OPTIMIZATION OF TURBOJET AND TURBOFAN ENGINES | ICAS2026_0426 |
| Gonzalo, J. | ACCURACY AND EFFICIENCY OF TRANSITION–TURBULENCE MODELS IN PREDICTING HIGH AND LOW REYNOLDS NUMBER PROPELLER PERFORMANCE | ICAS2026_0226 |
| Gostar, A.K. | DECOUPLED DEEP REINFORCEMENT LEARNING FOR AUTONOMOUS LANDING OF UAVS ON SHIPS | ICAS2026_0867 |
| Gou, L. | FLIGHT-DATA-DRIVEN PHYSICS-INFORMED COMPONENT MAP DERIVATION WITH STRUCTURAL COMPLIANCE | ICAS2026_0690 |
| Gou, L.F. | ADAPTIVE PREDICTION HORIZON-BASED MODEL PREDICTIVE CONTROL FOR AERO ENGINE | ICAS2026_0148 |
| Gou, L.F. | ROBUST FAULT DIAGNOSIS FOR AERO-ENGINE NETWORKED CONTROL SYSTEMS UNDER TRANSMISSION UNCERTAINTIES | ICAS2026_0149 |
| Gou, L.F. | INTELLIGENT FULL-ENVELOPE OPTIMIZATION OF TRANSIENT CONTROL LAWS FOR ADAPTIVE CYCLE ENGINES VIA TRANSFER LEARNING-ENHANCED DEEP REINFORCEMENT LEARNING | ICAS2026_0584 |
| Gowree, E. | THIN AEROFOILS OSCILLATING IN A CONFINED INVISCID FLOW | ICAS2026_0637 |
| Grandhi, R.V. | EVALUATION OF PERCEIVED X-15 FLYING QUALITIES BASED ON RAPID AERODYNAMIC PREDICTIONS | ICAS2026_0817 |
| Granzoto, R.M. | COST-EFFECTIVE CFD REPRODUCTION OF DPW-7 CASE 2A FOR CRM TRANSONIC PITCHING-MOMENT PREDICTION AND ADAPTIVE-REFINEMENT ASSESSMENT | ICAS2026_0953 |
| Greco, C.S. | AIRFOIL DESIGN OPTIMIZATION FOR HIGH-LIFT AND HIGH-EFFICIENCY APPLICATIONS USING DEEP REINFORCEMENT LEARNING | ICAS2026_0546 |
| Greco, C.S. | PASSIVE FLOW CONTROL OF A TURBULENT BOUNDARY LAYER AT THE VERGE OF SEPARATION USING SURFACE ROUGHNESS | ICAS2026_1085 |
| Groot, K.J. | EVALUATING THE LAMINAR FLOW ON A SLOTTED, NATURAL-LAMINAR-FLOW WING IN THE NASA AMES 11-FOOT TRANSONIC WIND TUNNEL | ICAS2026_0472 |
| Grothe, I. | FIVE DEACADES OF T-38 WING TEARDOWNS: DATA, INSIGHT, AND IMPACT | ICAS2026_0830 |
| Grube, R.W. | GAP OPTIMIZATION ADAPTIVE TOOL FOR LARGE SCALE FLEXIBLE STRUCTURE ASSEMBLY | ICAS2026_0058 |
| Grönstedt, T. | CURRENT AND ALTERNATIVE PROPULSION SYSTEMS IN EUROPE | ICAS2026_0981 |
| Gu, D.-D. | MATERIAL-STRUCTURE INTEGRATED LASER ADDITIVE MANUFACTURING OF HIGH-PERFORMANCE PARTS FOR AERONAUTICAL APPLICATIONS | ICAS2026_0260 |
| Gu, D.D. | BALANCING STRENGTH AND THERMAL CONDUCTIVITY IN LPBF-PROCESSED ALUMINUM-BASED MATERIALS | ICAS2026_0124 |
| Gu, D.D. | PROCESS OPTIMIZATION, MANUFACTURING QUALITY AND MECHANICAL PROPERTIES OF HIGH-VOLUME-FRACTION TIB2 REINFORCED AL-BASED COMPOSITES PREPARED BY SELECTIVE LASER MELTING | ICAS2026_0126 |
| Gu, D.D. | A NOVEL DUAL-PHASE BAYESIAN ESTIMATION AND MULTI-TASK LEARNING METHOD FOR PROCESS OPTIMIZATION FOR REDUCING LACK-OF-FUSION DEFECTS DURING LASER POWDER BED FUSION | ICAS2026_0270 |
| Gu, Y.S. | GEOMETRICALLY EXACT MODEL OF CANTILEVER BEAM UNDERGOING LARGE DEFLECTION AND LINEARIZED DYNAMICS CHARACTERIZATION | ICAS2026_0071 |
| Gu, Y.S. | AEROSERVOELASTIC MODELING AND ANALYSIS OF THRUST VECTORING LAUNCH VEHICLE CONSIDERING RIGID-ELASTIC INTERACTION | ICAS2026_0262 |
| Guan, H. | RESONANT ELASTIC SHAFT THRUST VECTORING: IMPLICATIONS FOR UAV DESIGNS | ICAS2026_0484 |
| Guan, S. | PERFORMANCE DEGRADATION ANALYSIS OF RESOLVER FAULTS IN ELECTRO-MECHANICAL ACTUATOR | ICAS2026_0784 |
| Guan, S. | MECHANISM-DATA FUSION MODELING METHOD FOR AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEMS | ICAS2026_0961 |
| Gueyffier, D. | HYBRID AI-SIMULATION FOR AERODYNAMICS APPLICATIONS | ICAS2026_1018 |
| Gunasekaran, S. | NUMERICAL INVESTIGATION OF SHOCKWAVE TURBULENT BOUNDARY LAYER INTERACTION AT MACH 2.5 OVER A COMPRESSION RAMP | ICAS2026_0550 |
| Gungen, B. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Guo, J. | UNCONTROLLED TAILLESS GLIDING: PAPER AEROPLANES GEOMETRY, AERODYNAMICS AND FLIGHT DURATION ANALYSIS | ICAS2026_0392 |
| Guo, J. | LOW-NOISE VERTIPORT PROCEDURE PLANNING USING DEEP REINFORCEMENT LEARNING | ICAS2026_0580 |
| Guo, J. | RECIPROCITY-GUIDED JOINT BASE STATION PLACEMENT AND FLIGHT CORRIDOR PLANNING FOR URBAN AIR MOBILITY | ICAS2026_0587 |
| Guo, J. | GEOMETRY-DRIVEN AIR TRAFFIC CONFLICT RESOLUTION VIA CAUCHY-STOKES RANDERS METRIC | ICAS2026_0605 |
| Guo, X. | PERFORMANCE DEGRADATION ASSESSMENT METHOD FOR AERO-ENGINES ACROSS THE FULL-LIFE-CYCLE BASED ON DIGITAL TWIN | ICAS2026_0856 |
| Guo, Y. | ADAPTIVE PRACTICAL PRESCRIBED-TIME FAULT-TOLERANT CONTROL FOR SMALL TANDEM-ROTOR UAV FORMATIONS | ICAS2026_0037 |
| Guo, Y. | PREDEFINED-TIME AFFINE FORMATION FAULT-TOLERANT CONTROL FOR FIXED-WING UAVS WITH INPUT SATURATION | ICAS2026_0098 |
| Guo, Y. | AN AEROELASTIC DYNAMICS MODELING METHOD FOR INSECT-INSPIRED FLEXIBLE FLAPPING-WING UAV | ICAS2026_0141 |
| Guo, Y. | AERODYNAMIC PERFORMANCE ANALYSIS OF A NOVEL LIFT-THRUST INTEGRATED ROTARY FLAPPING AERIAL VEHICLE | ICAS2026_0184 |
| Guo, Z.Q. | AUTOMATIC GENERATION OF PHYSICAL SYSTEM MODELS FOR AIRCRAFT SYSTEMS BASED ON LLMS | ICAS2026_0479 |
| Gupta, P. | SOME OBSERVATIONS ON DEEP STALL LANDING, WITH APPLICATION TO SMALL UNMANNED AIRCRAFT | ICAS2026_1091 |
| Göppel, S. | PROVIDING SENSOR INFORMATION FOR BOARDING TIME PREDICTION | ICAS2026_0611 |
| Görtz, A. | EVALUATION OF LIQUID HYDROGEN CONDITIONING CONCEPTS FOR AIRCRAFT ENGINES EMPLOYING EXHAUST GAS WASTE HEAT RECOVERY | ICAS2026_0551 |
| Görtz, A. | HEAT EXCHANGER MODELING METHODS FOR HYDROGEN POWERED AERO ENGINES DURING THERMODYNAMIC CYCLE DESIGN | ICAS2026_0574 |
| Habibi Husain, A. | MBSE AS A KEY ENABLER IN AEROSPACE DIGITAL ENGINEERING | ICAS2026_1087 |
| Hagedorn-Hansen, D. | LASER SCANNING STRATEGIES TO INVESTIGATE THE EFFECTS OF OXIDATION IN PURE TANTALUM | ICAS2026_0507 |
| Hagl, M. | VALIDATION OF TRADITIONAL COMPETENCY-BASED ASSESSMENT AND EXPERIENCE-BASED AUTHORISATION FOR AIR TRAFFIC CONTROLLERS | ICAS2026_0568 |
| Hallerbach, S. | ON THE APPLICABILITY OF SAFETY NETS: A SAFETY-BY-DESIGN SOLUTION FOR CERTIFYING NEURAL NETWORKS | ICAS2026_0210 |
| Hallerbach, S. | COVERAGE-DRIVEN VERIFICATION FOR SAFETY-BY-DESIGN IN AI-BASED COLLISION AVOIDANCE SYSTEMS | ICAS2026_0536 |
| Hallstedt, S.I. | KEY STAKEHOLDERS IN AEROSPACE FOR A SUSTAINABLE AND CIRCULAR PRODUCT DEVELOPMENT - A SYSTEMATIC APPROACH | ICAS2026_0222 |
| Hallstedt, S.I. | CURRENT AND ALTERNATIVE PROPULSION SYSTEMS IN EUROPE | ICAS2026_0981 |
| Hallwright, T. | DESIGN ASSESSMENT OF A HELICOPTER BLADE | ICAS2026_0225 |
| Hamada, Y. | ON THE FEASIBILITY OF MACHINE LEARNING-BASED DETECTION OF AIRCRAFT LIGHTNING STRIKE RISK AREAS | ICAS2026_0803 |
| Hamann, A. | APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS | ICAS2026_0359 |
| Hammad, A. | IMPACT OF DIFFERENT PROPELLER CONFIGURATIONS ON THE FLIGHT DYNAMICS AND STABILITY OF A SMALL REGIONAL ELECTRIC AIRCRAFT | ICAS2026_0837 |
| Hammer, B. | GARTEUR: FRAMEWORK, ORGANIZATION AND COLLABORATIVE RESEARCH | ICAS2026_1101 |
| Han, C. | A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY | ICAS2026_0627 |
| Han, J. | PHYSICS-INFORMED LEARNING-BASED RECOVERY TRAJECTORY PREDICTION FOR AUTOMATIC GROUND COLLISION AVOIDANCE | ICAS2026_0865 |
| Han, J.-H. | EXPERIMENTAL INVESTIGATION OF BLOWING RATIO EFFECT ON FLOW REGIMES OF TRANSPIRATION COOLING IN LATTICE POROUS MEDIA | ICAS2026_0776 |
| Han, J.-H. | AERO-MECHANICAL ANALYSIS OF A BIRD-INSPIRED ORNITHOPTER USING AN INTEGRATED SIMULATION FRAMEWORK | ICAS2026_0777 |
| Han, L. | FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES | ICAS2026_0171 |
| Han, S.W. | ROBUST ATTITUDE RECOVERY CONTROL FOR AIR-LAUNCHED FOLDING-WING UAVS VIA DISTURBANCE-COMPENSATED SUPER-TWISTING SLIDING MODE | ICAS2026_0506 |
| Han, Z. | MULTIDISCIPLINARY PHYSICS-CONSTRAINED GENERATIVE DESIGN OF DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2026_0088 |
| Han, Z. | PROPULSIVE EFFICIENCY AND ENERGY ANALYSIS OF AIRCRAFT CONCEPTS WITH AFT-FUSELAGE BOUNDARY-LAYER-INGESTION | ICAS2026_1112 |
| Han, Z.-H. | DEEP LEARNING-BASED INVERSION OF NEAR-FIELD OVERPRESSURE SIGNATURES FOR LOW-BOOM SUPERSONIC TRANSPORT | ICAS2026_0278 |
| Han, Z.-H. | AIRFRAME-INLET INTEGRATION DESIGN FOR AN OVER-WING-MOUNTED SUPERSONIC TRANSPORT CONFIGURATION | ICAS2026_0501 |
| Han, Z.-H. | POINT-CLOUD-BASED INTELLIGENT DESIGN OF FLYING-WING CONFIGURATIONS WITH CONDITIONAL GENERATION AND PRESSURE PREDICTION | ICAS2026_0528 |
| Han, Z.H | ADAPTIVE-PREFERENCE MULTI-OBJECTIVE REINFORCEMENT LEARNING FOR WIDE-SPEED-REGIME AIRFOIL OPTIMIZATION | ICAS2026_0393 |
| Han, Z.H. | INVERSE AEROELASTIC SIZING FOR STRUT-BRACED WINGS VIA PHYSICS-GUIDED GENERATIVE MODELING | ICAS2026_0100 |
| Han, Z.H. | LOW BOOM DESIGN AND ANALYSIS OF A BLENDED-WING-BODY CONFIGURATION FOR LARGE-SIZED SUPERSONIC TRANSPORT | ICAS2026_0552 |
| Hanan, J.C. | OPTIMIZATION OF INTERCONNECTED 3D-PRINTED STRUCTURES FOR UAVS | ICAS2026_0943 |
| Handford, D. | CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS | ICAS2026_0749 |
| Hanis, T. | LATERAL-DIRECTIONAL HANDLING AND FLYING QUALITIES ASSESSMENT OF A BLENDED WING BODY (BWB) ACFA 2020 CONFIGURATION | ICAS2026_0630 |
| Hao, W. | MISSION-PROFILE-BASED HYBRID POWER SYSTEM DESIGN AND OPTIMIZATION FOR VTOL AIRCRAFT IN REGIONAL AIR MOBILITY | ICAS2026_0696 |
| Harada, A. | SENSITIVITY STUDY OF DEPARTURE TIME ACCURACY FOR AIRPORT COLLABORATIVE DECISION MAKING USING FAST-TIME SIMULATION | ICAS2026_0860 |
| Hardt, M. | ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT | ICAS2026_0897 |
| Hariansyah, M.A. | A BILEVEL STRATEGY FOR ON-DESIGN EVTOL SIZING AND OFF-DESIGN STRUCTURAL WEIGHT OPTIMIZATION | ICAS2026_0209 |
| Hariansyah, M.A. | OPTIMAL CONCEPTUAL DESIGN AND UPGRADE STRATEGIES FOR EVTOL AIRCRAFT UNDER EVOLVING TECHNOLOGIES | ICAS2026_0631 |
| Hartley, D. | HYBRID ROCKET HOT-GAS DRIVER FOR DIRECT-CONNECT SCRAMJET THERMO-STRUCTURAL SCREENING | ICAS2026_0508 |
| Hasan, M.J. | IMPLICATIONS OF AAM OPERATIONS FOR FUTURE SHARED AIRSPACE IN VICTORIA, AUSTRALIA | ICAS2026_1083 |
| Hasan, Y.J. | ASSESSMENT OF THE LANDING CAPABILITIES OF A FLEXIBLE HIGH-ALTITUDE PLATFORM AT LONGITUDINAL AND LATERAL-DIRECTIONAL WIND DISTURBANCES | ICAS2026_0208 |
| Hasan, Y.J. | NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT | ICAS2026_0216 |
| Haselbach, F. | AIRBUS\' PERSPECTIVES & PROGRESS ON AIRLINERS FOR 2050+ ENERGY LANDSCAPES | ICAS2026_1024 |
| Hashioka, T. | NEW TEST RESULTS OF THE 3.23% FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2026_0328 |
| Haug, J.P. | TOWARDS AN ONTOLOGY-BASED APPROACH FOR DISCIPLINE-SPECIFIC ENGINEERING VIEWS IN ENGINE DESIGN | ICAS2026_0353 |
| Hazyuk, I. | A MODEL PREDICTIVE CONTROL STRATEGY FOR THE ENERGY MANAGEMENT OF HYBRID ELECTRIC PROPULSION SYSTEMS IN FIXED-WING UAVS | ICAS2026_0613 |
| Hazyuk, I. | POWER-HIL TESTING OF LI-PO BATTERY PACKS FOR LIGHTWEIGHT EVTOL UAVS | ICAS2026_0619 |
| He, H.-X. | EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT ENHANCEMENT OF A HIGH-LIFT CONFIGURATION | ICAS2026_0516 |
| He, J. | FLIGHT-TEST DATA-DRIVEN HIGH-ANGLE-OF-ATTACK DYNAMICS MODELING VIA LSTM-POLYNOMIAL HYBRID APPROACH | ICAS2026_0269 |
| He, J. | NUMERICAL INVESTIGATION OF GUST LOAD ALLEVIATION FOR WINGS WITH PASSIVELY RELEASED FFWT | ICAS2026_0785 |
| He, J. | COMPARATIVE ANALYSIS OF DIFFERENT NUMERICAL SIMULATION METHODS FOR PROPELLER SLIPSTREAM | ICAS2026_0795 |
| He, J. | AILERON EFFICIENCY ANALYSIS OF FLEXIBLE HIGH-ASPECT-RATIO WING | ICAS2026_0796 |
| He, J.W. | A UNIFIED PARAMETRIC MODELING METHOD FOR CONVENTIONAL, SEMI-BURIED, AND EMBEDDED INLETS | ICAS2026_0515 |
| He, J.Y. | MULTI-FIDELITY BAYESIAN NEURAL NETWORKS FOR STEALTH/AERODYNAMIC DATA FUSION METHOD | ICAS2026_0485 |
| He, K. | INTEGRATED CONTROL STRATEGY BASED ON PHYSICS-INFORMED MODEL-BASED REINFORCEMENT LEARNING FOR AIRBORNE HIGH-ENERGY SYSTEMS | ICAS2026_0621 |
| He, L. | ACTIVE FLOW CONTROL AND THERMAL PROTECTION FOR A WING-BODY CONFIGURATION BASED ON LATERAL JET | ICAS2026_0255 |
| He, M.S. | AFTERBODY CURVATURE EFFECTS ON FLOW LOSS CHARACTERISTICS BASED ON ENTROPY PRODUCTION | ICAS2026_0781 |
| He, P. | A DISTRIBUTED MULTI-SOURCE SENSOR FUSION METHOD FOR COLLABORATIVE TARGET TRACKING | ICAS2026_0590 |
| He, S. | TIME-VARYING AEROELASTIC MODELING AND FLUTTER ANALYSIS OF TELESCOPIC WINGS | ICAS2026_0620 |
| He, X. | A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY | ICAS2026_0627 |
| He, Y. | LOW-NOISE VERTIPORT PROCEDURE PLANNING USING DEEP REINFORCEMENT LEARNING | ICAS2026_0580 |
| He, Y. | RECIPROCITY-GUIDED JOINT BASE STATION PLACEMENT AND FLIGHT CORRIDOR PLANNING FOR URBAN AIR MOBILITY | ICAS2026_0587 |
| He, Y. | GEOMETRY-DRIVEN AIR TRAFFIC CONFLICT RESOLUTION VIA CAUCHY-STOKES RANDERS METRIC | ICAS2026_0605 |
| He, Y.L. | WIND FIELD PERCEPTION AND FEATURE PREDICTION FOR LOW-ALTITUDE SMALL FIXED-WING UAVS TOWARDS ENERGY HARVESTING | ICAS2026_0742 |
| He, Z.Z. | DATA-DRIVEN TURBULENCE MODELING FOR MULTI-MECHANISM SEPARATED FLOWS OVER ICED AIRFOILS | ICAS2026_0112 |
| Healy, F. | ENABLING FORWARD SWEPT WING DESIGNS | ICAS2026_0381 |
| Heath, N. | CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS | ICAS2026_0749 |
| Hebbar, A. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Heck, A.G. | PREDICTION OF STRUCTURAL VIBRATIONS INDUCED BY MASS-UNBALANCED ELECTRIC PROPULSION SYSTEMS | ICAS2026_0901 |
| Heesbeen, B. | NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT | ICAS2026_0216 |
| Hein, L. | FLIGHT PERFORMANCE ANALYSIS OF ELECTRIC AIRCRAFT UNDER MOTOR FAILURE CONDITIONS USING REDUCED-ORDER MODELING | ICAS2026_0539 |
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| Heo, J. | EXPERIMENTAL INVESTIGATION OF BLOWING RATIO EFFECT ON FLOW REGIMES OF TRANSPIRATION COOLING IN LATTICE POROUS MEDIA | ICAS2026_0776 |
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| Jang, Y.J. | FLIGHT TEST VALIDATION OF A VISION-GUIDED MULTIROTOR TERMINAL INTERCEPTION SYSTEM | ICAS2026_0737 |
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| Janszen, G. | IMPACT TOLERANCE OF DRILLED THICK C/SIC CERAMIC MATRIX COMPOSITES | ICAS2026_0357 |
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| Jin, S.Z. | FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING | ICAS2026_0172 |
| Jinks, E. | PHYSICS-INFORMED MACHINE LEARNING FOR FLIGHT DYNAMICS IDENTIFICATION OF THE SAAB 340B USING FLIGHT TEST DATA | ICAS2026_0686 |
| Joern, P. | COMPOSITE FUSELAGE TECHNOLOGIES FOR NEXT GENERATION COMMERCIAL AIRCRAFT | ICAS2026_0115 |
| Joiner, K. | BEYOND THE HARDWARE: REGULATION AND CERTIFICATION AS THE CRITICAL PATH TO ADF AUTONOMOUS CAPABILITY | ICAS2026_0252 |
| Joiner, K.F. | FEASIBILITY OF ELECTRIC DUCTED FANS TO REPLACE OPEN PROPELLERS ON AN ELECTRIFIED TRAINING AIRCRAFT | ICAS2026_0084 |
| Jones, C.J. | METROLOGY METHODS FOR ISOLATING PROFILE FORM, WAVINESS, STEPS, AND TWIST FROM SCANS OF SMALL-SCALE LAMINAR FLOW WIND TUNNEL MODELS | ICAS2026_0428 |
| Jones, M. | INTERMITTENT LOW FREQUENCY EXPERIMENTAL CAVITY DYNAMICS | ICAS2026_0748 |
| Jones, M. | CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS | ICAS2026_0749 |
| Jones, M. | FORCE RECONSTRUCTION TECHNIQUES FOR DYNAMIC LOAD ESTIMATION ON GENERIC GEOMETRIES IN LOW-SPEED WIND TUNNEL TESTING | ICAS2026_0790 |
| Joshin, S. | HPC-BASED PARAMETER SPACE EXPLORATION FOR DENSE PICOSAT FORMATION FLYING TOWARD DIRECT-TO-DEVICE COMMUNICATIONS | ICAS2026_0869 |
| Jouannet, C. | ONTOLOGY-BASED EXPLORATION OF SYSTEM-OF-SYSTEMS ARCHITECTURES USING A FEDERATED STRUCTURE | ICAS2026_0046 |
| Jouannet, C. | THE CONFERENCE LOCATIONS: A QUANTITATIVE APPROACH TO REDUCING IMPACT GLOBAL TRAVEL | ICAS2026_0607 |
| Jouannet, C. | DIGITAL ENGINEERING IN THE AGE OF AI AS BASIS FOR SYSTEM OF SYSTEMS ENGINEERING | ICAS2026_1108 |
| Joyce, K. | BEYOND THE HARDWARE: REGULATION AND CERTIFICATION AS THE CRITICAL PATH TO ADF AUTONOMOUS CAPABILITY | ICAS2026_0252 |
| Julien, C. | AEROELASTIC DESIGN OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT IN AN MDO FRAMEWORK | ICAS2026_0342 |
| Julien, C. | COMBINED TOPOLOGY AND COMPOSITE LAMINATE OPTIMIZATION OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT | ICAS2026_0355 |
| Julien, C. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Jung, C. | UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS | ICAS2026_0521 |
| Jung, D. | THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A WING–ROTOR CONFIGURATION FOR A FOLDING WING UAV | ICAS2026_0873 |
| Jung, K.-W. | OPTIMAL ZEM-BASED MIDCOURSE GUIDANCE FOR INTERCEPTORS USING TRAJECTORY PREDICTION | ICAS2026_0563 |
| Jung, M. | PHYSICS-INFORMED LEARNING-BASED RECOVERY TRAJECTORY PREDICTION FOR AUTOMATIC GROUND COLLISION AVOIDANCE | ICAS2026_0865 |
| Jung, Y. | CONVEX OPTIMIZATION-BASED EMERGENCY LANDING TRAJECTORY GENERATION FOR UAM VEHICLES | ICAS2026_0532 |
| Jux, C. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Jürisson, A. | REDUCED-ORDER MODELLING OF MINI-TAB SPOILER DYNAMICS FOR GUST LOAD ALLEVIATION | ICAS2026_0374 |
| Ka, J.Y. | COOPERATIVE TRACKING ALGORITHM OF MULTIPLE UAVS USING PSO FOR AERIAL SURVEILLANCE | ICAS2026_0709 |
| Kachel, S. | WATER TUNNEL EXPERIMENTS AND CFD ANALYSES OF A COMBAT AIRCRAFT WITH LEADING-EDGE VORTEX CONTROLLERS | ICAS2026_0763 |
| Kachel, S. | EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY | ICAS2026_0789 |
| Kajikawa, R. | FEASIBILITY STUDY ON IMPROVING ARRIVAL-SEPARATION STABILITY THROUGH ARRIVAL TRAJECTORY ANALYSIS AT CONGESTED AIRPORTS | ICAS2026_0329 |
| Kalampoukas, T. | TOWARDS INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES: INSPECTABILITY ASSESSMENT OF HAT-STIFFENED PANELS | ICAS2026_0914 |
| Kaleagasi, O. | DESIGN ASSESSMENT OF A HELICOPTER BLADE | ICAS2026_0225 |
| Kamat, A. | EXPLORING DETROIT METROPOLITAN WAYNE COUNTY AIRPORT AS A TESTBED FOR RESOLVING INTEGRATION CHALLENGES FOR AIR TAXI OPERATIONS | ICAS2026_0682 |
| Kanayama, M. | THE NUMERICAL SIMULATIONS OF THE ACOUSTIC SHIELDING EFFECTS ON THE BLADE-VORTEX INTERACTION NOISE OF THE HART-II MODEL | ICAS2026_0488 |
| Kang, C. | REINFORCEMENT LEARNING-BASED ADAPTIVE WEIGHTING OF SWARM GUIDANCE LAWS FOR SMALL FIXED-WING UAVS | ICAS2026_0765 |
| Kang, S. | UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS | ICAS2026_0521 |
| Kang, Y.-E. | DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+ | ICAS2026_0130 |
| Kania, K. | STUDY ON THE IMPACT OF TRIM CONDITION ON LATERAL AND DIRECTIONAL STABILITY FOR A TAILLESS AIRCRAFT | ICAS2026_0330 |
| Kania, K. | A NEW APPROACH TO MODELLING THE FLIGHT DYNAMICS OF A TAILLESS AIRCRAFT | ICAS2026_0658 |
| Kanitz, R. | FLIGHT MISSION MODELING WITH VARYING BASELINE DATA: APPLICAITON IN BUSINESS AVIATION | ICAS2026_0315 |
| Kantzidis, P. | DEVELOPMENT OF CONTROL LAWS FOR ENHANCED PERFORMANCE AND AEROELASTIC STABILITY OF EVTOL AIRCRAFT | ICAS2026_0452 |
| Kantzidis, P. | GROUND-EFFECT ANALYSIS OF SMALL DUCTED PROPELLERS: A NUMERICAL–EXPERIMENTAL STUDY | ICAS2026_0456 |
| Kapoor, P.P. | DESIGN AND TESTING OF A BUOYANT UAV FOR AGRICULTURAL SURVEILLANCE | ICAS2026_0594 |
| Karabasov, Sergey A. | HIGH-FIDELITY NUMERICAL INVESTIGATION OF ROTOR-WING INTERACTIONS IN A MULTI-ROTOR DISTRIBUTED ELECTRIC PROPULSION CONFIGURATION | ICAS2026_0678 |
| Karunathilake, S. | SUBSCALE FLIGHT TRAINING EFFECTS ON PILOT WORKLOAD AND PERFORMANCE DURING VTOL HQTES | ICAS2026_0685 |
| Kaster Marini, V. | A CASE STUDY OF CONTEXT OPERATIONS WITH LARGE LANGUAGE MODELS FOR THE SYSTEMS ARCHITECTURE DESIGN OF A HEAVY SAR UAV | ICAS2026_1049 |
| Kato, H. | PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN | ICAS2026_0370 |
| Kawagoe, Y. | EVALUATING IMPACT OF INTERNATIONAL DEPARTURE TIME CONTROL ON DOMESTIC ARRIVAL DELAYS IN JAPAN USING MULTI-OBJECTIVE SIMULATION-BASED OPTIMIZATION | ICAS2026_0779 |
| Kawamoto, Y. | UNSTEADY AERODYNAMIC OPTIMIZATION OF A THIN ANGULAR AIRFOIL USING CARTESIAN MESH CFD WITH THE LEVEL SET METHOD | ICAS2026_0767 |
| Kawamura, T. | NEW TEST RESULTS OF THE 3.23% FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2026_0328 |
| Kazula, S. | IMPACT ASSESSMENT OF COMPONENT FAILURES IN A PEM-FUEL CELL BASED PROPULSION SYSTEM FOR AIRCRAFT APPLICATIONS FOCUSING ON WATER MANAGEMENT | ICAS2026_0139 |
| Kazula, S. | NUMERICAL AND EXPERIMENTAL EVALUATION OF COMPACT TPMS AND OFFSET-STRIP-FIN HEAT EXCHANGERS FOR FUEL CELL SYSTEM COOLING IN AN ELECTRIC AIRCRAFT | ICAS2026_0652 |
| Kazula, S. | THERMAL–HYDRAULIC OPTIMIZATION OF AXIALLY GRADED OFFSET STRIP-FIN HEAT EXCHANGERS FOR MEGAWATT-CLASS FUEL CELL ELECTRIC AIRCRAFT | ICAS2026_0826 |
| Keillor, J. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Kekoc, V. | EXPLAINABLE NATURAL LANGUAGE PROCESSING FOR AIRCRAFT STRUCTURAL INTEGRITY DEFECT CLASSIFICATION | ICAS2026_0738 |
| Kekus-Kumor, P. | RECENT ADVANCES IN AEROACOUSTIC DESIGN OF ADVANCED AIR MOBILITY VEHICLES | ICAS2026_0964 |
| Keller, D. | INTEGRATION OF A SOLID OXIDE FUEL CELL PROPULSION SYSTEM: A TECHNOLOGY DEVELOPMENT GOAL FOR REGIONAL AIRCRAFT | ICAS2026_0319 |
| Kibler, K.S. | X-59 EXTERNAL VISION SYSTEM FLIGHT TESTING | ICAS2026_0769 |
| Kim, D. | LEARNING-BASED CONTROL ALLOCATION FOR OVER-ACTUATED VTOL AIRCRAFT WITH NONLINEAR DYNAMICS | ICAS2026_0567 |
| Kim, E.J. | SYSTEM IDENTIFICATION OF SMALL-SCALE HELICOPTER VIA EKF WITH DATA-DRIVEN NOISE COVARIANCE DETERMINATION | ICAS2026_0176 |
| Kim, H. | DUAL BEZIER SPACE-TIME OPTIMIZATION UNDER HARD OBSERVATION-WINDOW CONSTRAINTS: A FEASIBILITY-ORIENTED JERK-CAP COMPARISON | ICAS2026_0805 |
| Kim, H.-G. | OFFLINE REINFORCEMENT LEARNING FOR INFRARED IMAGE-BASED MISSILE GUIDANCE AND CONTROL | ICAS2026_0858 |
| Kim, H.-S. | PHYSICS-INFORMED LEARNING-BASED RECOVERY TRAJECTORY PREDICTION FOR AUTOMATIC GROUND COLLISION AVOIDANCE | ICAS2026_0865 |
| Kim, H.J. | NEURAL NETWORK BASED SLIDING MODE CONTROL FOR HYPERSONIC LONGITUDINAL CONTROL | ICAS2026_0872 |
| Kim, H.W. | WEATHER-DRIVEN DEEP LEARNING FOR AIRPORT RUNWAY DIRECTION FORECASTING | ICAS2026_0838 |
| Kim, J. | UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS | ICAS2026_0521 |
| Kim, J.-H. | COMBINED IMPACT OF JET STREAM AND TURBULENCE ON LONG-TERM TRANS-OCEANIC FLIGHT ROUTES | ICAS2026_0994 |
| Kim, M. | AI-BASED MAINTENANCE CODE CORRECTION FOR RELIABLE MTBF ANALYSIS | ICAS2026_0770 |
| Kim, S. | OPTIMAL ZEM-BASED MIDCOURSE GUIDANCE FOR INTERCEPTORS USING TRAJECTORY PREDICTION | ICAS2026_0563 |
| Kim, S. | OFFLINE REINFORCEMENT LEARNING FOR INFRARED IMAGE-BASED MISSILE GUIDANCE AND CONTROL | ICAS2026_0858 |
| Kim, S. | PHYSICS-INFORMED LEARNING-BASED RECOVERY TRAJECTORY PREDICTION FOR AUTOMATIC GROUND COLLISION AVOIDANCE | ICAS2026_0865 |
| Kim, S.J. | TRAJECTORY OPTIMIZATION FOR TAKEOFF/LANDING BASED ON FLAP-AND-GLIDE FOR FLAPPING-WING UNMANNED AERIAL VEHICLE | ICAS2026_0164 |
| Kim, S.K. | TRAJECTORY OPTIMIZATION FOR TAKEOFF/LANDING BASED ON FLAP-AND-GLIDE FOR FLAPPING-WING UNMANNED AERIAL VEHICLE | ICAS2026_0164 |
| Kim, S.K. | DISTURBANCE OBSERVER-BASED ADAPTIVE NONSINGULAR TERMINAL SLIDING MODE CONTROL FOR FAULT-TOLERANT CONTROL OF QUAD-TILTROTOR EVTOL | ICAS2026_0166 |
| Kim, S.K. | SOFTWARE-IN-THE-LOOP SIMULATION OF DISTRIBUTED 3D INTEGRATED SWARM GUIDANCE FOR FIXED-WING UAVS | ICAS2026_0167 |
| Kim, S.K. | SYSTEM IDENTIFICATION OF SMALL-SCALE HELICOPTER VIA EKF WITH DATA-DRIVEN NOISE COVARIANCE DETERMINATION | ICAS2026_0176 |
| Kim, S.W. | DISTURBANCE OBSERVER-BASED ADAPTIVE NONSINGULAR TERMINAL SLIDING MODE CONTROL FOR FAULT-TOLERANT CONTROL OF QUAD-TILTROTOR EVTOL | ICAS2026_0166 |
| Kim, Y. | DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+ | ICAS2026_0130 |
| Kim, Y. | UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS | ICAS2026_0521 |
| Kim, Y. | LEARNING-BASED CONTROL ALLOCATION FOR OVER-ACTUATED VTOL AIRCRAFT WITH NONLINEAR DYNAMICS | ICAS2026_0567 |
| Kim, Y. | THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A WING–ROTOR CONFIGURATION FOR A FOLDING WING UAV | ICAS2026_0873 |
| Kim, Y.R. | FLIGHT TEST VALIDATION OF A VISION-GUIDED MULTIROTOR TERMINAL INTERCEPTION SYSTEM | ICAS2026_0737 |
| King, C. | FIVE DEACADES OF T-38 WING TEARDOWNS: DATA, INSIGHT, AND IMPACT | ICAS2026_0830 |
| Kipouros, T. | CURRENT AND ALTERNATIVE PROPULSION SYSTEMS IN EUROPE | ICAS2026_0981 |
| Kirkness, J. | EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER CONTROLLED CAVITY FLOW FOR PIEZOELECTRIC ENERGY HARVESTING APPLICATIONS | ICAS2026_1080 |
| Kirschnek, P. | AN INTEGRATED SYSTEM-LEVEL AND MULTIPHYSICS APPROACH FOR AIRCRAFT LH2 FUEL SYSTEM DESIGN | ICAS2026_0316 |
| Kirschnek, P. | AERODYNAMIC AND STABILITY-DRIVEN PRE-DESIGN OF A FUEL-CELL POWERED FLYING WING AIRCRAFT | ICAS2026_0318 |
| Kirschnek, P. | EVALUATION OF LIQUID HYDROGEN CONDITIONING CONCEPTS FOR AIRCRAFT ENGINES EMPLOYING EXHAUST GAS WASTE HEAT RECOVERY | ICAS2026_0551 |
| Kirste, A. | AGENTIC AI FOR AIRCRAFT PRELIMINARY DESIGN: PROOF OF CONCEPT | ICAS2026_0575 |
| Kishimoto, N. | EFFECT OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS | ICAS2026_0517 |
| Kishimoto, N. | EFFECT OF MORPHOLOGICAL CHANGES ON THE AERODYNAMIC CHARACTERISTICS OF THE WING AND TAIL FEATHERS OF A TAXIDERMY BLACK-TAILED GULL | ICAS2026_0852 |
| Kiszkowiak, L. | WATER TUNNEL EXPERIMENTS AND CFD ANALYSES OF A COMBAT AIRCRAFT WITH LEADING-EDGE VORTEX CONTROLLERS | ICAS2026_0763 |
| Kiszkowiak, L. | EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY | ICAS2026_0789 |
| Klaas, T. | ICE DETECTION: CORRELATION OF ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES TESTED IN ICING WIND TUNNEL | ICAS2026_0186 |
| Klein, C. | ONTOLOGY-BASED SENSOR HEALTH MONITORING: A DYNAMIC ONTOLOGY-BASED FAULT DETECTION AND CLASSIFICATION FOR TIMESERIES DATA | ICAS2026_0716 |
| Klein, M. | LAMINAR SEPARATION ON AN AIRFOIL WITH PERTURBATION OF OUTER AND INNER BOUNDARY CONDITIONS | ICAS2026_0368 |
| Klimczyk, W. | PRACTICAL ASPECTS OF ROTOR AERODYNAMIC AND AEROACOUSTIC DESIGN OPTIMIZATION | ICAS2026_0923 |
| Klimczyk, W. | RECENT ADVANCES IN AEROACOUSTIC DESIGN OF ADVANCED AIR MOBILITY VEHICLES | ICAS2026_0964 |
| Knöös Franzén, L. | ONTOLOGY-BASED EXPLORATION OF SYSTEM-OF-SYSTEMS ARCHITECTURES USING A FEDERATED STRUCTURE | ICAS2026_0046 |
| Knöös Franzén, L. | LOSS OF RELIABILITY OF NEW GENERATION ENGINES: THE CASE STUDY OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION AS A SYSTEM OF SYSTEMS | ICAS2026_0822 |
| Ko, H.-S. | AERO-MECHANICAL ANALYSIS OF A BIRD-INSPIRED ORNITHOPTER USING AN INTEGRATED SIMULATION FRAMEWORK | ICAS2026_0777 |
| Kober, M. | NUMERICAL AND EXPERIMENTAL EVALUATION OF COMPACT TPMS AND OFFSET-STRIP-FIN HEAT EXCHANGERS FOR FUEL CELL SYSTEM COOLING IN AN ELECTRIC AIRCRAFT | ICAS2026_0652 |
| Kober, M. | THERMAL–HYDRAULIC OPTIMIZATION OF AXIALLY GRADED OFFSET STRIP-FIN HEAT EXCHANGERS FOR MEGAWATT-CLASS FUEL CELL ELECTRIC AIRCRAFT | ICAS2026_0826 |
| Koch, S. | REYNOLDS NUMBER SCALING EFFECTS IN TRANSONIC CAVITY AERODYNAMICS: A HIGH-FIDELITY EXPERIMENTAL AND NUMERICAL FRAMEWORK | ICAS2026_0362 |
| Koester, F. | COVERAGE-DRIVEN VERIFICATION FOR SAFETY-BY-DESIGN IN AI-BASED COLLISION AVOIDANCE SYSTEMS | ICAS2026_0536 |
| Koga, M. | PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN | ICAS2026_0370 |
| Koga, M. | AN OVERVIEW OF JAXA’S HIGH-SPEED FLIGHT R&D: FROM SUPERSONIC FLIGHT TO HYPERSONIC TRANSPORTATION | ICAS2026_1067 |
| Koga, M. | SDF-BASED GEOMETRY BLENDING OF HYPERSONIC VEHICLE CONCEPTS | ICAS2026_1070 |
| Kohzai, M. | AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMI-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT THE JAXA 6.5M X 5.5M LOW SPEED WIND TUNNEL | ICAS2026_0256 |
| Kohzai, M. | AEROACOUSTIC WIND TUNNEL TESTING AND CFD STUDY USING JAXA 8% SEMISPAN HIGH-LIFT COMMON RESEARCH MODEL IN JAXA FQUROH-2 PROJECT | ICAS2026_0756 |
| Kok, J. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Kokkolaras, M. | MODELING OF AIRCRAFT COMPONENT PLACEMENTS WITH BIN PACKING | ICAS2026_0460 |
| Kolb, M.G. | DESIGN AND INVESTIGATION OF A SHORT-TO-MEDIUM-RANGE AIRCRAFT WITH LIQUID HYDROGEN AND SAF MULTI-FUEL PROPULSION | ICAS2026_0073 |
| Konowalski, J. | MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS | ICAS2026_0143 |
| Kontani, S. | APPROPRIATE ATC GO-AROUND INSTRUCTION TIMING TO PREVENT RUNWAY COLLISIONS | ICAS2026_0863 |
| Koo, T.-R.T. | CLIMATE HAZARD TIMING AND FLIGHT DEMAND COOCCURRENCE: A DEMAND-WEIGHTED EXPOSURE FRAMEWORK | ICAS2026_0870 |
| Koolhof, I.S. | A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. | ICAS2026_0041 |
| Koopman, C. | SUPPORTING PILOT SITUATIONAL AWARENESS BY EXTRACTING INSIGHTS FROM AN AI EXPERT | ICAS2026_0648 |
| Kopardekar, P.H. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Korn, B. | FLIGHT CENTRIC ATC – HOW TO SOLVE CONFLICTS WITHOUT COMMUNICATION AND COORDINATION OVERLOADS? | ICAS2026_0178 |
| Korn, B. | A COMPARISON OF TRAJECTORY-BASED OPERATIONS IN THE UNITED STATES AND EUROPE IN SUPPORT OF GLOBAL HARMONIZATION | ICAS2026_0412 |
| Kos, J. | FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION | ICAS2026_0888 |
| Koschlik, A.K. | VR FOR CABIN DESIGN AND CERTIFYING DIGITAL MRO MEASURES | ICAS2026_1109 |
| Kotzem, M. | ADVANCED MODELING AND ANALYSIS OF A LIQUID HYDROGEN SHORT-MEDIUM RANGE AIRCRAFT CONCEPT FOR 2035 | ICAS2026_0333 |
| Kouchlef, M. | PARAMETRIC AEROELASTIC STUDY OF WINGLET GEOMETRY USING VORTEX LATTICE METHOD FOR FUTURE PASSIVE MORPHING APPLICATIONS | ICAS2026_0326 |
| Koutsambasis, C. | FLYING BY THE THREAD OF MY PANTS: USING HOUSEHOLD TEXTILES COMPOSITES FOR ACCESSIBLE UAV AIRFRAMES | ICAS2026_0499 |
| Kovar, P. | MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELING | ICAS2026_0634 |
| Kowalski, R. | A MULTIDIMENSIONAL FRAMEWORK FOR DEMONSTRATION AND V&V CAPABILITIES FOR NEXT-GENERATION FLIGHT CONTROL SYSTEMS | ICAS2026_0093 |
| Kozulovic, D. | EXPERIMENTAL VALIDATION OF A COANDA-BASED FLUIDIC THRUST VECTORING NOZZLE USING A HIGH-SPEED WIND TUNNEL | ICAS2026_0151 |
| Kozulovic, D. | INVESTIGATION OF GENERIC SWIRL DISTORTION AND ITS EFFECTS ON COMPRESSOR PERFORMANCE AND FLOW STABILITY | ICAS2026_0334 |
| Kramar, V. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Krasniqi, M. | AERODYNAMIC OPTIMISATION OF BIOINSPIRED CORRUGATED WINGS FOR HIGH-EFFICIENCY MAV GLIDING | ICAS2026_0665 |
| Krause, D. | LINKING PRODUCT FAMILY ARCHITECTURE ANALYSIS AND COMPONENT-LEVEL OPTIMISATION USING SYSTEM MODELS | ICAS2026_0305 |
| Krause, D. | ASSESSING THE POTENTIAL OF MULTI-MODEL TOPOLOGY OPTIMIZATION FOR MODULAR LIGHTWEIGHT DESIGN OF AIRCRAFT CABIN STRUCTURES | ICAS2026_0406 |
| Krein, A | SETTING THE STAGE FOR THE GLOBAL SUSTAINABLE AVIATION TRACK WITH GLOBAL AIRLINES | ICAS2026_1020 |
| Krewinkel, R. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF HYDROGEN FLAMES UNDER COLD INJECTION CONDITIONS | ICAS2026_0299 |
| Kriewall Peters, V. | ADVANCED MODELING AND ANALYSIS OF A LIQUID HYDROGEN SHORT-MEDIUM RANGE AIRCRAFT CONCEPT FOR 2035 | ICAS2026_0333 |
| Krummenauer, M. | INVESTIGATION OF GENERIC SWIRL DISTORTION AND ITS EFFECTS ON COMPRESSOR PERFORMANCE AND FLOW STABILITY | ICAS2026_0334 |
| Krus, P. | SIMULATION-BASED AUTOPILOT TUNING FOR FIXED-WING UAVS | ICAS2026_0435 |
| Krus, P. | TRACING MATERIAL PROPERTIES TO SYSTEM-LEVEL PERFORMANCE: A NORMALISED SENSITIVITY ANALYSIS FOR A BOEING 737-CLASS AIRCRAFT | ICAS2026_0640 |
| Krus, P. | AI-SUPPORTED AIRCRAFT SYSTEM ARCHITECTURE SYNTHESIS | ICAS2026_0668 |
| Krus, P. | AUTOMATING SYSTEM MODELING USING LARGE LANGUAGE MODELS | ICAS2026_0809 |
| Krus, P. | METHODOLOGY AND V1 PROTOTYPE OF AN ADAPTIVE/ADAPTABLE MULTI-UAV GCS HMI IN A FLOOD SAR CO-SIMULATION TESTBED | ICAS2026_0932 |
| Krus, P. | A CASE STUDY OF CONTEXT OPERATIONS WITH LARGE LANGUAGE MODELS FOR THE SYSTEMS ARCHITECTURE DESIGN OF A HEAVY SAR UAV | ICAS2026_1049 |
| Kuci, F. | GROUND-EFFECT ANALYSIS OF SMALL DUCTED PROPELLERS: A NUMERICAL–EXPERIMENTAL STUDY | ICAS2026_0456 |
| Kuenz, A. | JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION | ICAS2026_0212 |
| Kugler, L. | FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION | ICAS2026_0888 |
| Kulhanek, R. | WIND TUNNEL TESTING OF WHIRL FLUTTER AEROELASTIC DEMONSTRATOR | ICAS2026_0014 |
| Kumar, A. | LOW-SPEED EXPERIMENTAL INVESTIGATION OF PODDED ENGINE INTEGRATION OF FLYING V AIRCRAFT | ICAS2026_0218 |
| Kumar, M. | MULTI-SENSOR BASED ADAPTIVE FUSION SCHEME FOR POSITION ESTIMATION OF MULTIROTOR UAV SYSTEMS IN GPS-DENIED ENVIRONMENTS | ICAS2026_1033 |
| Kumar, N. | IMPLICATIONS OF AAM OPERATIONS FOR FUTURE SHARED AIRSPACE IN VICTORIA, AUSTRALIA | ICAS2026_1083 |
| Kumar, S. | IMPLEMENTATION OF PROPELLER-WING INTERFERENCE MODEL AND HORIZONTAL TAIL ANALYSIS INTO A VISCOUS FULL POTENTIAL FLOW SOLVER FRAMEWORK FOR AIRCRAFT DESIGN | ICAS2026_0915 |
| Kumar, S.N. | AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH | ICAS2026_1015 |
| Kunwar, B. | A WORKFLOW FOR RAPID DESIGN, SIMULATION, FABRICATION, AND SUBSCALE FLIGHT-TESTING OF NOVEL AIRCRAFT CONCEPTS | ICAS2026_0845 |
| Kunwar, B. | SIMULATION MODEL CALIBRATION USING SYSTEM IDENTIFICATION FOR A VECTORED-THRUST MULTI-TILT-ROTOR CONFIGURATION | ICAS2026_0929 |
| Kurka, P. | WHO SHOULD SIT AT THE EXIT ROW? A HUMAN FACTORS APPROACH TO EMERGENCY EVACUATION PASSENGER SELECTION IN COMMERCIAL AVIATION | ICAS2026_0154 |
| Kurka, P.B. | FROM DATA TO DEBRIEF: A FRAMEWORK FOR PILOT PERFORMANCE ASSESSMENT | ICAS2026_0692 |
| Kurtulus, D.F. | INTERACTION OF COUNTER-PLUNGING BIPLANE AIRFOILS WITH A FLAT PLATE BOUNDARY LAYER AND WAKE | ICAS2026_0655 |
| Kurtulus, D.F. | THREE-DIMENSIONAL FLOW STRUCTURES OVER A LOW-ASPECT-RATIO PLUNGING WING | ICAS2026_0916 |
| Kurz, J. | NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT | ICAS2026_0216 |
| Kwiek, A. | A NEW APPROACH TO MODELLING THE FLIGHT DYNAMICS OF A TAILLESS AIRCRAFT | ICAS2026_0658 |
| Kwon, Y | FEASIBILITY OF ELECTROPULSING-INDUCED FATIGUE CRACK CLOSURE IN AEROSPACE METALLIC MATERIALS | ICAS2026_0365 |
| Künstler, E.M. | EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT | ICAS2026_0274 |
| Kyprianidis, K. | COMPARATIVE ASSESSMENT OF PROPULSION SYSTEM ARCHITECTURES TAILORED FOR SUPERSONIC APPLICATIONS | ICAS2026_0207 |
| Kyriazis, T. | AI-ASSISTED DESIGN OF HOLISTICALLY SUSTAINABLE AEROSTRUCTURES | ICAS2026_0975 |
| Köster, F. | ON THE APPLICABILITY OF SAFETY NETS: A SAFETY-BY-DESIGN SOLUTION FOR CERTIFYING NEURAL NETWORKS | ICAS2026_0210 |
| Lampl, D.E. | PROPULSION SYSTEM MODELING AND OPTIMIZATION FOR CONCEPTUAL DESIGN OF HYBRID-ELECTRIC VTOL AIRCRAFT | ICAS2026_0401 |
| Lannoo, A. | AIRCRAFT MASS EVALUATION MODEL: FROM TUBE-AND-WING TO BLENDED WING BODY USING WHALE. | ICAS2026_0211 |
| Lannoo, A. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Lanot, D. | COMPARATIVE ATMOSPHERIC MEASUREMENTS USING UAV-MOUNTED ULTRASONIC ANEMOMETER AND DOPPLER LIDAR | ICAS2026_0133 |
| Larsson, R | SYSTEM IDENTIFICATION USING FLIGHT TEST DATA AND MACHINE LEARNING | ICAS2026_0622 |
| Larsson, R. | A 3D-PRINTED TESTBED FOR FLIGHT CONTROL SYSTEM RESEARCH. | ICAS2026_0713 |
| Lasne, D. | FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING | ICAS2026_0172 |
| Lau, A. | JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION | ICAS2026_0212 |
| Lau, A. | THREE-DIMENSIONAL ADAPTIVE TRAJECTORY OPTIMIZATION FOR RPAS-BASED ATMOSPHERIC MEASUREMENTS | ICAS2026_0292 |
| Lau, A. | FLIGHT MISSION MODELING WITH VARYING BASELINE DATA: APPLICAITON IN BUSINESS AVIATION | ICAS2026_0315 |
| Laubner, M. | FLIGHT OPERATIONS AND TESTING OF A 450 KG EXPERIMENTAL GYROPLANE UAV | ICAS2026_0331 |
| Laubner, M. | IMPACT OF SYSTEM LATENCIES ON PILOT INTERACTION AND HANDLING OF AN ELECTRICALLY POWERED GYROPLANE UAV WITH FPV-BASED REMOTE CONTROL | ICAS2026_0335 |
| Laurin, F. | CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING | ICAS2026_1004 |
| Lawson, C. | FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION | ICAS2026_0888 |
| Lawson, N.J. | NUMERICAL CHARACTERISATION OF SHIP-AIRWAKE EFFECTS ON MEDIUM-WEIGHT UAV APPROACH AND GO-AROUND OPERATIONS TO CANBERRA-CLASS LHDS | ICAS2026_0759 |
| Lawson, N.J. | ANALYSIS OF A DUAL AIR DATA AND MULTI-HOLE PRESSURE PROBE BOOM | ICAS2026_0775 |
| Lawson, N.J. | EXPERIMENTAL STUDY OF GROUND EFFECT ON A HEAVING NACA0012 AEROFOIL | ICAS2026_0970 |
| Lawson, N.J. | EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER CONTROLLED CAVITY FLOW FOR PIEZOELECTRIC ENERGY HARVESTING APPLICATIONS | ICAS2026_1080 |
| Lazzaro, G. | DEVELOPMENT OF CONTROL LAWS FOR ENHANCED PERFORMANCE AND AEROELASTIC STABILITY OF EVTOL AIRCRAFT | ICAS2026_0452 |
| Lebbin, P. | A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. | ICAS2026_0041 |
| Lee, B.J. | HYPERSONIC RESEARCH AND DEVELOPMENT IN THE REPUBLIC OF KOREA: FROM FUNDAMENTAL AEROTHERMODYNAMICS TO FLIGHT DEMONSTRATION | ICAS2026_1066 |
| Lee, C.-H. | HYPERSONIC VEHICLE FLIGHT SIMULATION AND FLIGHT CONTROL | ICAS2026_0174 |
| Lee, C.-H. | OPTIMAL GUIDANCE ALGORITHM FOR BOOST-BACK OF REUSABLE LAUNCH VEHICLES | ICAS2026_0505 |
| Lee, C.-H. | TRAJECTORY OPTIMIZATION OF HIT-TO-KILL INTERCEPTORS VIA SEQUENTIAL CONVEX PROGRAMMING APPROACH | ICAS2026_0534 |
| Lee, C.-H. | OPTIMAL ZEM-BASED MIDCOURSE GUIDANCE FOR INTERCEPTORS USING TRAJECTORY PREDICTION | ICAS2026_0563 |
| Lee, D | FEASIBILITY OF ELECTROPULSING-INDUCED FATIGUE CRACK CLOSURE IN AEROSPACE METALLIC MATERIALS | ICAS2026_0365 |
| Lee, D. | DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+ | ICAS2026_0130 |
| Lee, D. | A SINGLE-LOOP BAYESIAN OPTIMIZATION FRAMEWORK FOR MULTIDISCIPLINARY DESIGN OPTIMIZATION UNDER UNCERTAINTY | ICAS2026_0524 |
| Lee, D.J. | COOPERATIVE TRACKING ALGORITHM OF MULTIPLE UAVS USING PSO FOR AERIAL SURVEILLANCE | ICAS2026_0709 |
| Lee, E.-H. | AERO-MECHANICAL ANALYSIS OF A BIRD-INSPIRED ORNITHOPTER USING AN INTEGRATED SIMULATION FRAMEWORK | ICAS2026_0777 |
| Lee, G. | A SINGLE-LOOP BAYESIAN OPTIMIZATION FRAMEWORK FOR MULTIDISCIPLINARY DESIGN OPTIMIZATION UNDER UNCERTAINTY | ICAS2026_0524 |
| Lee, H. | LEARNING-BASED CONTROL ALLOCATION FOR OVER-ACTUATED VTOL AIRCRAFT WITH NONLINEAR DYNAMICS | ICAS2026_0567 |
| Lee, H.M. | HYPERSONIC VEHICLE FLIGHT SIMULATION AND FLIGHT CONTROL | ICAS2026_0174 |
| Lee, I. | AI-BASED MAINTENANCE CODE CORRECTION FOR RELIABLE MTBF ANALYSIS | ICAS2026_0770 |
| Lee, I.H. | AFFINE-INVARIANT ELLIPTICAL STATE ESTIMATION FOR ROBUST EXTENDED OBJECT TRACKING | ICAS2026_0344 |
| Lee, J. | UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS | ICAS2026_0521 |
| Lee, J. | EXPERIMENTAL INVESTIGATION OF BLOWING RATIO EFFECT ON FLOW REGIMES OF TRANSPIRATION COOLING IN LATTICE POROUS MEDIA | ICAS2026_0776 |
| Lee, J.D. | LEARNING-BASED CONTROL ALLOCATION FOR OVER-ACTUATED VTOL AIRCRAFT WITH NONLINEAR DYNAMICS | ICAS2026_0567 |
| Lee, J.S. | ESTIMATION AND ANALYSIS OF RNP REQUIREMENTS FOR HETEROGENEOUS UAM CONFIGURATIONS: INSIGHTS FROM OPPAV DEMONSTRATION | ICAS2026_0802 |
| Lee, K. | AIRCRAFT CLIMB PROFILE PREDICTION VIA MACHINE LEARNING-BASED FRAMEWORK | ICAS2026_0893 |
| Lee, M. | INFORMATIVE PATH PLANNING BASED ON REDUCED-RANK GAUSSIAN PROCESS FOR HAZARDOUS SUBSTANCE MONITORING | ICAS2026_0513 |
| Lee, S. | DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+ | ICAS2026_0130 |
| Lee, S. | DUAL BEZIER SPACE-TIME OPTIMIZATION UNDER HARD OBSERVATION-WINDOW CONSTRAINTS: A FEASIBILITY-ORIENTED JERK-CAP COMPARISON | ICAS2026_0805 |
| Lee, S.-G. | AERO-MECHANICAL ANALYSIS OF A BIRD-INSPIRED ORNITHOPTER USING AN INTEGRATED SIMULATION FRAMEWORK | ICAS2026_0777 |
| Lee, W.S. | TRAJECTORY OPTIMIZATION FOR TAKEOFF/LANDING BASED ON FLAP-AND-GLIDE FOR FLAPPING-WING UNMANNED AERIAL VEHICLE | ICAS2026_0164 |
| Lee, Y. | THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A WING–ROTOR CONFIGURATION FOR A FOLDING WING UAV | ICAS2026_0873 |
| Legovich, M.A. | EXPERIMENTAL STUDY OF GROUND EFFECT ON A HEAVING NACA0012 AEROFOIL | ICAS2026_0970 |
| Legrand, B. | CHALLENGES AND SOLUTIONS FOR LIQUID HYDROGEN-POWERED UAVS: REGULATIONS AND CASE STUDY INSIGHTS | ICAS2026_0213 |
| Legriffon, I. | CHALLENGES IN ADVANCED AIR MOBILITY NOISE PREDICTION - FROM SOURCE TO PERCEPTION | ICAS2026_0345 |
| Lehmann, M. | VLSEC: A CONCEPT FOR SECURING VIRTUAL LINKS IN AVIONICS NETWORKS THROUGH CENTRALIZED GROUP KEY MANAGEMENT | ICAS2026_0701 |
| Lei, W.L. | AEROSERVOELASTIC MODELING AND ANALYSIS OF THRUST VECTORING LAUNCH VEHICLE CONSIDERING RIGID-ELASTIC INTERACTION | ICAS2026_0262 |
| Lemetti, A. | UNCERTAINTY ANALYSIS AND EYE-TRACKING-BASED CLUSTERING IN AIR TRAFFIC CONTROLLER WORKLOAD PREDICTION | ICAS2026_0118 |
| Lemetti, A. | AIRSPACE CAPACITY IMPLICATIONS OF CONTRAIL-AWARE TRAJECTORY OPTIMIZATION | ICAS2026_0224 |
| Léonard, P.L.Y. | KEY STAKEHOLDERS IN AEROSPACE FOR A SUSTAINABLE AND CIRCULAR PRODUCT DEVELOPMENT - A SYSTEMATIC APPROACH | ICAS2026_0222 |
| Lesak, S. | AERODYNAMIC AND STABILITY-DRIVEN PRE-DESIGN OF A FUEL-CELL POWERED FLYING WING AIRCRAFT | ICAS2026_0318 |
| Lesak, S. | MODELING OF CRITICAL WEATHER FLIGHT PERFORMANCE OF MULTICOPTER UAVS FOR RESILIENT CONTROLLER DESIGN. | ICAS2026_0695 |
| Lessa, C. | WHO SHOULD SIT AT THE EXIT ROW? A HUMAN FACTORS APPROACH TO EMERGENCY EVACUATION PASSENGER SELECTION IN COMMERCIAL AVIATION | ICAS2026_0154 |
| Li, A. | PREDEFINED-TIME AFFINE FORMATION FAULT-TOLERANT CONTROL FOR FIXED-WING UAVS WITH INPUT SATURATION | ICAS2026_0098 |
| Li, A.J. | ADAPTIVE PRACTICAL PRESCRIBED-TIME FAULT-TOLERANT CONTROL FOR SMALL TANDEM-ROTOR UAV FORMATIONS | ICAS2026_0037 |
| Li, B. | NUMERICAL SIMULATION OF STRESS-OXIDATION DAMAGE IN C/SIC COMPOSITES AT HIGH TEMPERATURES | ICAS2026_0276 |
| Li, B. | DATA-DRIVEN AERODYNAMIC MODEL OF THE DISTRIBUTED PROPULSION WING | ICAS2026_0297 |
| Li, B. | RESEARCH ON OVERALL AERODYNAMIC DESIGN OF GRID-DUCT INTEGRATED VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING AIRCRAFT | ICAS2026_0482 |
| Li, C.-Y. | TIME-VARYING AEROELASTIC MODELING AND FLUTTER ANALYSIS OF TELESCOPIC WINGS | ICAS2026_0620 |
| Li, D. | PHYSICAL DESIGN CONCEPTS OF VORTEX GENERATOR ARRAYS FOR AIRCRAFT AFT-BODIES DRIVEN BY DISTINCT DRAG REDUCTION MECHANISMS | ICAS2026_0185 |
| Li, D. | CST PARAMETRIC MODELING AND MULTI-OBJECTIVE OPTIMIZATION RECONFIGURATION STUDY OF A BLENDED-WING-BODY AIRCRAFT | ICAS2026_0455 |
| Li, F. | COMPARATIVE DESIGN OF SBW AIRCRAFT WITH AERODYNAMIC SHAPE OPTIMIZATION FOR THREE DIFFERENT PROPULSION LAYOUTS | ICAS2026_0078 |
| Li, G.L. | HIGH-ALTITUDE PERFORMANCE AND ONE-DIMENSIONAL MODELING OF A DUAL-ROTOR GEROTOR PUMP FOR AEROENGINE LUBRICATION SYSTEMS | ICAS2026_0352 |
| Li, G.L. | STUDY ON OIL CAVITATION AND PUMPING CHARACTERISTICS OF SURFACE MICROTOPOGRAPHY GRAPHITE SEALS | ICAS2026_0461 |
| Li, H.X. | RESEARCH ON EFFECTIVENESS-DRIVEN INTELLIGENT OPTIMIZATION METHOD FOR CONCEPTUAL LAYOUT OF AIRCRAFT | ICAS2026_0596 |
| Li, J. | EXPERIMENTAL INVESTIGATION ON THE INNER DUCT SURFACE UNSTEADY PRESSURE OF A DUCTED PROPELLER | ICAS2026_0033 |
| Li, J. | A DISTRIBUTED MULTI-SOURCE SENSOR FUSION METHOD FOR COLLABORATIVE TARGET TRACKING | ICAS2026_0590 |
| Li, J.C. | DATA-DRIVEN SHAPE PARAMETERIZATION FOR EFFECTIVE AERODYNAMIC DESIGN OPTIMIZATION OF PROPELLERS | ICAS2026_0476 |
| Li, J.X. | BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL | ICAS2026_0647 |
| Li, L. | COMPARATIVE DESIGN OF SBW AIRCRAFT WITH AERODYNAMIC SHAPE OPTIMIZATION FOR THREE DIFFERENT PROPULSION LAYOUTS | ICAS2026_0078 |
| Li, L. | QUASI-STEADY AERODYNAMIC AND MBD COUPLED FLIGHT SIMULATION OF FOLDING MORPHING UAV | ICAS2026_0237 |
| Li, M. | AERODYNAMIC OPTIMIZATION DESIGN OF FULL-WING SOLAR-POWERED UAV FOR FLOW SEPARATION CONTROL | ICAS2026_0122 |
| Li, M. | EFFECT OF LIP/NOZZLE DEFLECTION ANGLE ON THE AERODYNAMIC AND PROPULSIVE CHARACTERISTICS OF PROPULSIVE WING UNIT | ICAS2026_0200 |
| Li, M. | DATA-DRIVEN AERODYNAMIC MODEL OF THE DISTRIBUTED PROPULSION WING | ICAS2026_0297 |
| Li, M. | TOROIDAL RECIRCULATION, SADDLE-POINT TOPOLOGY, AND WALL-JET OUTWASH IN A TWIN-ROTOR SYSTEM IN GROUND EFFECT | ICAS2026_0804 |
| Li, M. | EXPERIMENTAL STUDY OF GROUND EFFECT ON A HEAVING NACA0012 AEROFOIL | ICAS2026_0970 |
| Li, M.Z. | EXPLORING DETROIT METROPOLITAN WAYNE COUNTY AIRPORT AS A TESTBED FOR RESOLVING INTEGRATION CHALLENGES FOR AIR TAXI OPERATIONS | ICAS2026_0682 |
| Li, P.F. | RESEARCH ON EFFECTIVENESS-DRIVEN INTELLIGENT OPTIMIZATION METHOD FOR CONCEPTUAL LAYOUT OF AIRCRAFT | ICAS2026_0596 |
| Li, P.F. | COARSE–FINE COUPLED MBSE FOR SURVIVABILITY PARAMETER DESIGN OF STEALTH CARRIER-BASED TANKER | ICAS2026_0671 |
| Li, S. | STRUCTURAL DESIGN AND PERFORMANCE STUDY OF A TWO-STAGE DYNAMIC PRESSURE OIL-AIR SEPARATOR | ICAS2026_0341 |
| Li, S. | STUDY ON OIL CAVITATION AND PUMPING CHARACTERISTICS OF SURFACE MICROTOPOGRAPHY GRAPHITE SEALS | ICAS2026_0461 |
| Li, S. | EFFICIENT ROTOR AERODYNAMIC SHAPE DESIGN USING A MULTI-FIDELITY NEURAL NETWORK-BASED GLOBAL OPTIMIZATION METHOD | ICAS2026_0492 |
| Li, S. | MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK | ICAS2026_0493 |
| Li, S. | MULTI-OBJECTIVE OPTIMIZATION OF AERO-ENGINE BEARING CHAMBER SCAVENGE STRUCTURE BASED ON NSGA-II | ICAS2026_0623 |
| Li, S. | CURVATURE-CONTROLLED MORPHING OF FOLDING WINGTIPS USING HONEYCOMB PLATES | ICAS2026_0853 |
| Li, S. | VANE-LESS 3D WIND ESTIMATION FOR FIXED-WING UAVS: A PHYSICS-AUGMENTED TEMPORAL RESIDUAL NETWORK APPROACH | ICAS2026_0859 |
| Li, S.-K. | INVESTIGATION OF DISTRIBUTED PROPELLER PROPULSIVE CHARACTERISTICS UNDER NON-AXIAL INFLOW | ICAS2026_0108 |
| Li, S.K. | AUTONOMOUS FLIGHT AND INTELLIGENT TARGET LOCALIZATION FOR JUNGLE RECONNAISSANCE UAVS | ICAS2026_0649 |
| Li, X. | LEAKAGE PREDICTION AND GEOMETRIC PARAMETER OPTIMIZATION OF STEPPED LABYRINTH SEALS BASED ON DATA-DRIVEN SURROGATE MODELS | ICAS2026_0862 |
| Li, X.L. | ADAPTIVE PRACTICAL PRESCRIBED-TIME FAULT-TOLERANT CONTROL FOR SMALL TANDEM-ROTOR UAV FORMATIONS | ICAS2026_0037 |
| Li, Y. | POWER FLOW DYNAMICS AND COUPLING MECHANISMS IN POWER-BY-WIRE ACTUATION: A COMPREHENSIVE MODELING AND ANALYSIS APPROACH | ICAS2026_0561 |
| Li, Y. | INTEGRATED CONTROL STRATEGY BASED ON PHYSICS-INFORMED MODEL-BASED REINFORCEMENT LEARNING FOR AIRBORNE HIGH-ENERGY SYSTEMS | ICAS2026_0621 |
| Li, Y.P. | STRUCTURAL DESIGN AND PERFORMANCE STUDY OF A TWO-STAGE DYNAMIC PRESSURE OIL-AIR SEPARATOR | ICAS2026_0341 |
| Li, Y.P. | STUDY ON OIL CAVITATION AND PUMPING CHARACTERISTICS OF SURFACE MICROTOPOGRAPHY GRAPHITE SEALS | ICAS2026_0461 |
| Li, Z. | AN AEROELASTIC DYNAMICS MODELING METHOD FOR INSECT-INSPIRED FLEXIBLE FLAPPING-WING UAV | ICAS2026_0141 |
| Li, Z. | EFFECTS OF FLAPPING–PITCHING PHASE DIFFERENCE ON THE AERODYNAMIC PERFORMANCE OF HOVERING DRAGONFLY WINGS | ICAS2026_0193 |
| Li, Z. | MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK | ICAS2026_0493 |
| Li, Z. | POWER FLOW DYNAMICS AND COUPLING MECHANISMS IN POWER-BY-WIRE ACTUATION: A COMPREHENSIVE MODELING AND ANALYSIS APPROACH | ICAS2026_0561 |
| Li, Z. | INTEGRATED CONTROL STRATEGY BASED ON PHYSICS-INFORMED MODEL-BASED REINFORCEMENT LEARNING FOR AIRBORNE HIGH-ENERGY SYSTEMS | ICAS2026_0621 |
| Li, Z.L. | PREDICTION OF MINIMUM STARTING PRESSURE FOR HYDROSTATIC HELICAL ROTARY ACTUATOR USING PHYSICS-INFORMED NEURAL NETWORKS | ICAS2026_0593 |
| Li, Z.X | ADAPTIVE-PREFERENCE MULTI-OBJECTIVE REINFORCEMENT LEARNING FOR WIDE-SPEED-REGIME AIRFOIL OPTIMIZATION | ICAS2026_0393 |
| Liang, G.A. | ADAPTIVE PREDICTION HORIZON-BASED MODEL PREDICTIVE CONTROL FOR AERO ENGINE | ICAS2026_0148 |
| Liang, G.A. | ROBUST FAULT DIAGNOSIS FOR AERO-ENGINE NETWORKED CONTROL SYSTEMS UNDER TRANSMISSION UNCERTAINTIES | ICAS2026_0149 |
| Liang, S.Y. | IMPACT LOAD IDENTIFICATION METHOD FOR AIRCRAFT RUDDER PLANES BASED ON NARX NEURAL NETWORK | ICAS2026_0379 |
| Liang, Z. | MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY | ICAS2026_0566 |
| Liem, R.P. | A BILEVEL STRATEGY FOR ON-DESIGN EVTOL SIZING AND OFF-DESIGN STRUCTURAL WEIGHT OPTIMIZATION | ICAS2026_0209 |
| Liem, R.P. | OPTIMAL CONCEPTUAL DESIGN AND UPGRADE STRATEGIES FOR EVTOL AIRCRAFT UNDER EVOLVING TECHNOLOGIES | ICAS2026_0631 |
| Lin, R.X. | COARSE–FINE COUPLED MBSE FOR SURVIVABILITY PARAMETER DESIGN OF STEALTH CARRIER-BASED TANKER | ICAS2026_0671 |
| Lin, T. | NUMERICAL STUDY ON DYNAMIC STALL OF FIGHTER AIRCRAFT AT HIGH ANGLE OF ATTACK USING DYNAMIC IMPROVED DELAYED DETACHED EDDY SIMULATION | ICAS2026_0480 |
| Lin, T.-Y. | AN ADAPTIVE AND PARAMETER-FREE SLOPE LIMITER FOR UNSTRUCTURED COMPRESSIBLE FLOW SOLVER | ICAS2026_0241 |
| Lin, W. | DATA-DRIVEN SHAPE PARAMETERIZATION FOR EFFECTIVE AERODYNAMIC DESIGN OPTIMIZATION OF PROPELLERS | ICAS2026_0476 |
| Lin, Y. | LOW BOOM DESIGN AND ANALYSIS OF A BLENDED-WING-BODY CONFIGURATION FOR LARGE-SIZED SUPERSONIC TRANSPORT | ICAS2026_0552 |
| Lin, Z. | DYNAMIC RECONFIGURABLE PATH PLANNING FOR FIRE-FIGHTING UAVS | ICAS2026_0217 |
| Ling, R.X. | RESEARCH ON EFFECTIVENESS-DRIVEN INTELLIGENT OPTIMIZATION METHOD FOR CONCEPTUAL LAYOUT OF AIRCRAFT | ICAS2026_0596 |
| Linguerri, L. | DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY | ICAS2026_0827 |
| Link, A. | INTEGRATION OF A SOLID OXIDE FUEL CELL PROPULSION SYSTEM: A TECHNOLOGY DEVELOPMENT GOAL FOR REGIONAL AIRCRAFT | ICAS2026_0319 |
| Liscouët, J. | ENDURANCE EVALUATION OF DIFFERENT UAV CONFIGURATIONS AND POWERTRAIN ARCHITECTURES | ICAS2026_0636 |
| Liscouët-Hanke, S. | INTEGRATING SYSTEM ARCHITECTURE OPTIMIZATION INTO MODEL-BASED SYSTEMS ENGINEERING METHODS | ICAS2026_0229 |
| Liscouët-Hanke, S. | A FRAMEWORK FOR AUTOMATED SYSTEM COMPONENT PLACEMENT IN AIRCRAFT CONCEPTUAL DESIGN | ICAS2026_0348 |
| Liscouët-Hanke, S. | EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION | ICAS2026_0673 |
| Liu, C. | AN EFFICIENT TRANSITION PREDICTION METHOD USING NEURAL NETWORK SURROGATE MODELS | ICAS2026_0254 |
| Liu, F. | MULTI-OBJECTIVE OPTIMIZATION OF AERO-ENGINE BEARING CHAMBER SCAVENGE STRUCTURE BASED ON NSGA-II | ICAS2026_0623 |
| Liu, F.L. | HIGH-PRECISION EDDY-CURRENT TIP CLEARANCE SENSOR WITHEXCEPTIONALHEAT RESISTANCE | ICAS2026_0483 |
| Liu, H. | PHYSICAL DESIGN CONCEPTS OF VORTEX GENERATOR ARRAYS FOR AIRCRAFT AFT-BODIES DRIVEN BY DISTINCT DRAG REDUCTION MECHANISMS | ICAS2026_0185 |
| Liu, H. | AFTERBODY CURVATURE EFFECTS ON FLOW LOSS CHARACTERISTICS BASED ON ENTROPY PRODUCTION | ICAS2026_0781 |
| Liu, H.L. | PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA | ICAS2026_0624 |
| Liu, H.L. | BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL | ICAS2026_0647 |
| Liu, J. | AN AEROELASTIC DYNAMICS MODELING METHOD FOR INSECT-INSPIRED FLEXIBLE FLAPPING-WING UAV | ICAS2026_0141 |
| Liu, J. | AERODYNAMIC PERFORMANCE ANALYSIS OF A NOVEL LIFT-THRUST INTEGRATED ROTARY FLAPPING AERIAL VEHICLE | ICAS2026_0184 |
| Liu, J. | A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY | ICAS2026_0627 |
| Liu, J.N | RESEARCH ON OFFENSIVE AUTONOMOUS VEHICLE TRAJECTORY PREDICTION METHOD BASED ON IMPROVED INVERSE REINFORCEMENT LEARNING IN AIRCRAFT ACTIVE DEFENSE MODE | ICAS2026_0531 |
| Liu, J.T. | PARAMETER INVERSION ALGORITHM FOR AERO-ENGINE γ-PHOTON FLOW FIELD IMAGES BASED ON UNET-GAN ARCHITECTURE | ICAS2026_0264 |
| Liu, L. | A BILEVEL STRATEGY FOR ON-DESIGN EVTOL SIZING AND OFF-DESIGN STRUCTURAL WEIGHT OPTIMIZATION | ICAS2026_0209 |
| Liu, P. | STATIC GROUND EFFECT OF HIGH-ASPECT-RATIO WINGS | ICAS2026_0295 |
| Liu, P.Q. | SUPERSONIC GROUND EFFECT AERODYNAMICS OF A SLENDER BODY | ICAS2026_0598 |
| Liu, T. | PHYSICAL DESIGN CONCEPTS OF VORTEX GENERATOR ARRAYS FOR AIRCRAFT AFT-BODIES DRIVEN BY DISTINCT DRAG REDUCTION MECHANISMS | ICAS2026_0185 |
| Liu, W.Z. | RESEARCH ON EFFECTIVENESS-DRIVEN INTELLIGENT OPTIMIZATION METHOD FOR CONCEPTUAL LAYOUT OF AIRCRAFT | ICAS2026_0596 |
| Liu, W.Z. | COARSE–FINE COUPLED MBSE FOR SURVIVABILITY PARAMETER DESIGN OF STEALTH CARRIER-BASED TANKER | ICAS2026_0671 |
| Liu, X. | FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING | ICAS2026_0172 |
| Liu, X. | STUDY ON INDUCED DRAG CALCULATION FOR BIRD-LIKE WINGTIP SLOTS USING WAKE-PLANE INTEGRATION | ICAS2026_0466 |
| Liu, X. | MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK | ICAS2026_0493 |
| Liu, Y. | AERODYNAMIC REQUIREMENTS ASSESSMENT OF CIVIL AIRCRAFT BASED ON AIRWORTHINESS PERFORMANCE | ICAS2026_0106 |
| Liu, Y. | STUDY ON DAMAGE SEVERITY ASSESSMENT METHODS FOR ASYMMETRICALLY DAMAGED LOITERING MUNITIONS | ICAS2026_0306 |
| Liu, Y. | FLIGHT-DATA-DRIVEN PHYSICS-INFORMED COMPONENT MAP DERIVATION WITH STRUCTURAL COMPLIANCE | ICAS2026_0690 |
| Liu, Y.C. | MULTI-BODY DYNAMIC MODELING OF A BIRD-LIKE FLAPPING-WING VEHICLE: ANALYSIS OF FLAPPING-AERODYNAMIC COUPLING EFFECTS | ICAS2026_0191 |
| Liu, Y.C. | AERODYNAMIC EFFECT OF PITCHING MOTION FOR FLAPPING AIRFOIL ACROSS DIFFERENT SWEEPING TRAJECTORIES | ICAS2026_0542 |
| Liu, Z. | MULTI-OBJECTIVE OPTIMIZATION OF AERO-ENGINE BEARING CHAMBER SCAVENGE STRUCTURE BASED ON NSGA-II | ICAS2026_0623 |
| Liu, Z.-K. | AN ADAPTIVE AND PARAMETER-FREE SLOPE LIMITER FOR UNSTRUCTURED COMPRESSIBLE FLOW SOLVER | ICAS2026_0241 |
| Liu, Z.X. | HIGH-PRECISION EDDY-CURRENT TIP CLEARANCE SENSOR WITHEXCEPTIONALHEAT RESISTANCE | ICAS2026_0483 |
| Lloyd, A. | ENERGY DISSIPATION OF THIN-WALLED RIBBED SPHERES FOR CARGO AIRDROP | ICAS2026_0290 |
| Lloyd, S. | EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION | ICAS2026_0673 |
| Lodares Gomez, D. | ADAPTIVE FLIGHT CONTROL LAWS APPLIED TO AIR REFUELING WITH RECEIVERS EQUIPPED WITH RECEPTACLE OUT OF THE PLANE OF SYMMETRY | ICAS2026_0011 |
| López, D. | EXPERIMENTAL INVESTIGATION OF WISHBONE VORTEX GENERATOR EFFECTS ON THE NACA 4412 AIRFOIL AT LOW REYNOLDS NUMBERS | ICAS2026_0232 |
| Lorenz, S. | FLIGHT OPERATIONS AND TESTING OF A 450 KG EXPERIMENTAL GYROPLANE UAV | ICAS2026_0331 |
| Lorenz, S. | IMPACT OF SYSTEM LATENCIES ON PILOT INTERACTION AND HANDLING OF AN ELECTRICALLY POWERED GYROPLANE UAV WITH FPV-BASED REMOTE CONTROL | ICAS2026_0335 |
| Losada Costoso, D. | AERODYNAMIC TRANSONIC DESIGN OF A STRUT-BRACED WING | ICAS2026_0223 |
| Losada Costoso, D. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Lott, M. | AN MBSE-ORIENTED FRAMEWORK FOR AEROSPACE SYSTEMS EDUCATION: THE CEA-UFMG LIGHT-AIRCRAFT DESIGN-BUILD-TEST TRADITION | ICAS2026_0933 |
| Low, K.H. | UNIFIED SEPARATION ASSURANCE FOR MULTI-UAV OPERATIONS: RISK-CALIBRATED BASELINES AND FAULT-AWARE ADAPTIVE RESOLUTION | ICAS2026_0554 |
| Lowenberg, M. | EVALUATION OF STALL BEHAVIOUR OF T-TAIL AIRCRAFT: MODELLING AND FLIGHT TEST | ICAS2026_0518 |
| Loxton, B. | BUILDING A TECHNOLOGY PLATFORM FOR THE ELECTRIC AGE | ICAS2026_1102 |
| Lu, L.J. | ADAPTIVE PREDICTION HORIZON-BASED MODEL PREDICTIVE CONTROL FOR AERO ENGINE | ICAS2026_0148 |
| Lu, L.J. | ROBUST FAULT DIAGNOSIS FOR AERO-ENGINE NETWORKED CONTROL SYSTEMS UNDER TRANSMISSION UNCERTAINTIES | ICAS2026_0149 |
| Lu, X. | CST PARAMETRIC MODELING AND MULTI-OBJECTIVE OPTIMIZATION RECONFIGURATION STUDY OF A BLENDED-WING-BODY AIRCRAFT | ICAS2026_0455 |
| Lu, Y. | MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY | ICAS2026_0566 |
| Lu, Y.Y. | PILOT WORKLOAD PROFILES UNDER CONTINUOUS MULTI-TASKING AND SPARSE EVENTS VIGILANCE | ICAS2026_0091 |
| Lua, J. | HIGH-FIDELITY ANALYSIS OF AIRCRAFT TAIL BUFFETING UNDER DYNAMIC MANEUVERING | ICAS2026_0927 |
| Lua, J. | A PROCESS-STRUCTURE-PROPERTY-PERFORMANCE FRAMEWORK FOR DIGITAL ENGINEERING-ENABLED REPAIR OF ALUMINUM PARTS | ICAS2026_0940 |
| Lugrin, M. | UNDERSTANDING HYPERSONIC BOUNDARY LAYER LAMINAR TO TURBULENT TRANSITION IN WIND TUNNEL ENVIRONMENT | ICAS2026_1002 |
| Lundström, D. | SIMULATION-BASED AUTOPILOT TUNING FOR FIXED-WING UAVS | ICAS2026_0435 |
| Lundström, D. | A 3D-PRINTED TESTBED FOR FLIGHT CONTROL SYSTEM RESEARCH. | ICAS2026_0713 |
| Luo, J. | AIRCRAFT BUFFET QUANTIFICATION | ICAS2026_0206 |
| LUO, Zhengdong | A RAPID AERODYNAMIC ASSESSMENT METHOD FOR BATTLE-DAMAGED CRUISE MISSILES | ICAS2026_0578 |
| Lusher, D. | AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMI-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT THE JAXA 6.5M X 5.5M LOW SPEED WIND TUNNEL | ICAS2026_0256 |
| Lübbe, S. | MODEL-BASED FUNCTIONAL HAZARD ASSESSMENT BASED ON ARP4761A USING SYSML V1 AND SYSML V2 | ICAS2026_0674 |
| Lübbe, S.M. | PROPAGATING SAFETY ASSESSMENT RESULTS FOR SYSTEM ARCHITECTURE CANDIDATES IN MBSE | ICAS2026_0399 |
| Lyu, D.C. | PREDICTION OF MINIMUM STARTING PRESSURE FOR HYDROSTATIC HELICAL ROTARY ACTUATOR USING PHYSICS-INFORMED NEURAL NETWORKS | ICAS2026_0593 |
| Lyu, D.C. | AN EMBEDDED PHYSICS-INFORMED NEURAL NETWORK (PINN) FRAMEWORK FOR HIGH-FIDELITY REAL-TIME SIMULATION OF A FLIGHT CONTROL SURFACE ACTUATION SYSTEM | ICAS2026_0715 |
| Lyu, S. | COMPARING DIFFERENT SEMI-EMPIRICAL AERODYNAMIC TOOLS FOR ANALYSING NOVEL AIRCRAFT CONFIGURATIONS | ICAS2026_0445 |
| Lyu, Y. | MULTI-OBJECTIVE OPTIMIZATION OF AERO-ENGINE BEARING CHAMBER SCAVENGE STRUCTURE BASED ON NSGA-II | ICAS2026_0623 |
| Lyu, Y.G. | HIGH-ALTITUDE PERFORMANCE AND ONE-DIMENSIONAL MODELING OF A DUAL-ROTOR GEROTOR PUMP FOR AEROENGINE LUBRICATION SYSTEMS | ICAS2026_0352 |
| Lyu, Y.G. | HIGH-PRECISION EDDY-CURRENT TIP CLEARANCE SENSOR WITHEXCEPTIONALHEAT RESISTANCE | ICAS2026_0483 |
| Ma, L. | MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK | ICAS2026_0493 |
| Ma, R.B. | COMPRESSIVE PERFORMANCE OF VARIABLE-STIFFNESS COMPOSITE HYPERBOLIC STIFFENED PANELS BASED ON GEOMETRIC PATH MAPPING | ICAS2026_0082 |
| Ma, T. | A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS | ICAS2026_0538 |
| Ma, T.L. | ROBUST ATTITUDE RECOVERY CONTROL FOR AIR-LAUNCHED FOLDING-WING UAVS VIA DISTURBANCE-COMPENSATED SUPER-TWISTING SLIDING MODE | ICAS2026_0506 |
| Ma, X.K. | EXERGY-BASED AERODYNAMIC CHARACTERISTICS ANALYSIS OF THE NASA COMMON RESEARCH MODEL AND BWB CONFIGURATION CIVIL AIRCRAFT | ICAS2026_0373 |
| Ma, X.K. | 2D AND 3D TRAJECTORY PLANNING FOR UAVS FORMATION SYSTEM USING DYNAMIC WINDOW APPROACH | ICAS2026_0735 |
| Ma, X.K. | INLET OPTIMIZATION DESIGN OF A BOUNDARY LAYER INGESTION PROPULSION SYSTEM | ICAS2026_0906 |
| Ma, Y. | MULTIDISCIPLINARY PHYSICS-CONSTRAINED GENERATIVE DESIGN OF DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2026_0088 |
| Ma, Y. | PROPULSIVE EFFICIENCY AND ENERGY ANALYSIS OF AIRCRAFT CONCEPTS WITH AFT-FUSELAGE BOUNDARY-LAYER-INGESTION | ICAS2026_1112 |
| Ma, Y.Y. | INVERSE AEROELASTIC SIZING FOR STRUT-BRACED WINGS VIA PHYSICS-GUIDED GENERATIVE MODELING | ICAS2026_0100 |
| Maatz, I. | FORCE RECONSTRUCTION TECHNIQUES FOR DYNAMIC LOAD ESTIMATION ON GENERIC GEOMETRIES IN LOW-SPEED WIND TUNNEL TESTING | ICAS2026_0790 |
| Machado, L.H.J. | STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR IMPACT RESPONSE FOR LIGHTWEIGHT FIXED-WING UAVS | ICAS2026_0833 |
| Machado, L.H.J. | MODEL-BASED INTEGRATION OF FLIGHT-TEST EVIDENCE AND SEMI-EMPIRICAL PERFORMANCE MODELS: THE ACS-100 SORA LIGHT AIRCRAFT CASE STUDY | ICAS2026_0917 |
| Machado, L.H.J. | AN MBSE-ORIENTED FRAMEWORK FOR AEROSPACE SYSTEMS EDUCATION: THE CEA-UFMG LIGHT-AIRCRAFT DESIGN-BUILD-TEST TRADITION | ICAS2026_0933 |
| Machado Cardoso Júnior , M. | WHO SHOULD SIT AT THE EXIT ROW? A HUMAN FACTORS APPROACH TO EMERGENCY EVACUATION PASSENGER SELECTION IN COMMERCIAL AVIATION | ICAS2026_0154 |
| MacManus, D. | NOVEL METHODS FOR THE CHARACTERISATION OF INTAKE FLOW DISTORTION | ICAS2026_0110 |
| MacManus, D. | EFFECT OF INTAKE AERODYNAMICS AND FLOW DISTORTION ON FAN STALL INCEPTION | ICAS2026_0111 |
| MacManus, D. | MIDAS: A MODULAR SOFTWARE FOR INTAKE FLOW DISTORTION ANALYSIS | ICAS2026_0705 |
| MacManus, D. | MODELLING SENSITIVITIES IN THREE-DIMENSIONAL FZRA-SPECTRUM ICE-SHAPE PREDICTION FOR THE CRM-HL STOWED CONFIGURATION | ICAS2026_0896 |
| MacManus, D. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Mad, H. | AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS | ICAS2026_0195 |
| Madavan, N. | NASA RESEARCH FOR AIRLINERS OF 2050 AND BEYOND / DLR\'S PERSPECTIVES & PROGRESS ON AIRLINERS FOR 2050+ ENERGY LANDSCAPES | ICAS2026_0983 |
| Madhuranath, G. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Maeda, Y. | ASSESSMENT OF ENGINE-OUT ATMOSPHERIC EMISSIONS FROM COCONUT-OIL-DERIVED BIOJET FUEL | ICAS2026_0487 |
| Mahr, T. | RE-THINKING END OF LIFE AIRCRAFT INTERIORS THROUGH CO-DESIGN AND REPURPOSING | ICAS2026_0840 |
| Maia Nunes Celestino, F. | HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION OF WIND TURBINES USING A DISCRETE ADJOINT APPROACH | ICAS2026_0052 |
| Maier, M. | HIGH-FIDELITY DATASET-BASED SHAPE AND STRUCTURE OPTIMIZATION FOR AIRCRAFT DESIGN | ICAS2026_0042 |
| Mainini, L. | DYNAMIC RECONFIGURABLE PATH PLANNING FOR FIRE-FIGHTING UAVS | ICAS2026_0217 |
| Mainini, L. | MULTIDISCIPLINARY DESIGN OF COMPLIANT DEFORMABLE WINGS FOR IMPROVED AIRCRAFT EFFICIENCY: INTRODUCING AN ARCHITECTURE-AWARE OPTIMIZATION STRATEGY | ICAS2026_0610 |
| Mainini, L. | COMPUTATIONAL AVENUES TO ADVANCE DIGITAL CAPABILITIES AND EMPOWER SYNERGIES FOR THE BLUE SKIES | ICAS2026_1081 |
| Makino, Y. | AN OVERVIEW OF JAXA’S HIGH-SPEED FLIGHT R&D: FROM SUPERSONIC FLIGHT TO HYPERSONIC TRANSPORTATION | ICAS2026_1067 |
| Malaponte, G. | REAL-TIME EMULATION TESTBENCH FOR FUEL-CELL/BATTERY HYBRIDIZATION IN HYDROGEN-ELECTRIC AVIATION | ICAS2026_0338 |
| Malicki, L. | WATER TUNNEL EXPERIMENTS AND CFD ANALYSES OF A COMBAT AIRCRAFT WITH LEADING-EDGE VORTEX CONTROLLERS | ICAS2026_0763 |
| Malicki, L. | EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY | ICAS2026_0789 |
| Malinek, P. | WIND TUNNEL TESTING OF WHIRL FLUTTER AEROELASTIC DEMONSTRATOR | ICAS2026_0014 |
| Malka, S. | DIGITAL TWIN FOR AIR DEFENSE: LIVE-VIRTUAL-CONSTRUCTIVE INTEGRATION AND DECISION SUPPORT | ICAS2026_0076 |
| Malka, S. | SIMULATION-BASED ANALYSIS OF REDUNDANT UAV NAVIGATION UNDER GNSS OUTAGES | ICAS2026_0079 |
| Mamou, M. | WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH | ICAS2026_0438 |
| Man Fung, D.S. | INNOVATION & TRANSFORMATION AT SINGAPORE CHANGI AIRPORT AND A CASE STUDY ON AI-ENABLED LINE MAINTENANCE OPERATIONS | ICAS2026_0995 |
| Mangas Pita, A. | ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT | ICAS2026_0897 |
| Mangiacrapa, L. | ICE DETECTION: CORRELATION OF ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES TESTED IN ICING WIND TUNNEL | ICAS2026_0186 |
| Manindrakumar, D.M. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Manning, A. | A FULL-SCALE DEMONSTRATOR FOR RAPID TESTING OF HELICOPTER AIRFRAMES USING ADVANCED CONTROL SYSTEM METHODOLOGIES | ICAS2026_0157 |
| Manovski, P. | CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS | ICAS2026_0749 |
| Marciniuk, M. | WATER TUNNEL EXPERIMENTS AND CFD ANALYSES OF A COMBAT AIRCRAFT WITH LEADING-EDGE VORTEX CONTROLLERS | ICAS2026_0763 |
| Marciniuk, M. | EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY | ICAS2026_0789 |
| Marinaro, G. | REAL-TIME EMULATION TESTBENCH FOR FUEL-CELL/BATTERY HYBRIDIZATION IN HYDROGEN-ELECTRIC AVIATION | ICAS2026_0338 |
| Marino, M. | VORTEX TOPOLOGY AND CORE-UNWINDING MECHANISM IN SPIROID WINGTIP DEVICES USING LAGRANGIAN PARTICLE TRACKING | ICAS2026_0162 |
| Marino, M. | FLYING BY THE THREAD OF MY PANTS: USING HOUSEHOLD TEXTILES COMPOSITES FOR ACCESSIBLE UAV AIRFRAMES | ICAS2026_0499 |
| Marinus, B.G. | CONTINUOUS UNSTEADY ADJOINT VARIATIONAL MULTISCALE METHOD FOR AIRFOILS SHAPE OPTIMIZATION | ICAS2026_0105 |
| Marinus, B.G. | INFLUENCE OF ZIGZAG TAPE–INDUCED TRANSITION ON THE DU89-134 AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBER | ICAS2026_0221 |
| Marinus, B.G. | FLOW SOLUTIONS AROUND VON KÁRMÁN OGIVES AT SUPERSONIC SPEEDS USING PHYSICS-INFORMED NEURAL NETWORKS AND PSP | ICAS2026_0632 |
| Maris, J, | ENTRY INTO SERVICE REQUIRES CERTIFICATION FOR NOVEL TECHNOLOGY | ICAS2026_0398 |
| Mark, M. | EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION | ICAS2026_0673 |
| Markatos, D. | TOWARDS INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES: INSPECTABILITY ASSESSMENT OF HAT-STIFFENED PANELS | ICAS2026_0914 |
| Markatos, D. | AI-ASSISTED DESIGN OF HOLISTICALLY SUSTAINABLE AEROSTRUCTURES | ICAS2026_0975 |
| Markmiller, J. | OPTIMIZATION APPROACHES FOR THE SHEAR-POSTBUCKLING DESIGN OF THERMOPLASTIC THIN-PLY COMPOSITE SHELLS IN HELICOPTERS | ICAS2026_0614 |
| Marouf, A. | AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC | ICAS2026_0347 |
| Marshall, C. | INTERMITTENT LOW FREQUENCY EXPERIMENTAL CAVITY DYNAMICS | ICAS2026_0748 |
| Marshall, C. | CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS | ICAS2026_0749 |
| Marshall, C. | FORCE RECONSTRUCTION TECHNIQUES FOR DYNAMIC LOAD ESTIMATION ON GENERIC GEOMETRIES IN LOW-SPEED WIND TUNNEL TESTING | ICAS2026_0790 |
| Martinez Jimenez, V. | ADAPTIVE FLIGHT CONTROL LAWS APPLIED TO AIR REFUELING WITH RECEIVERS EQUIPPED WITH RECEPTACLE OUT OF THE PLANE OF SYMMETRY | ICAS2026_0011 |
| Martinez Teres, I. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Martini, M. | LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY | ICAS2026_0643 |
| Martins, J.R.R.A. | A MIXED-FIDELITY VISCOUS-INVISCID INTERACTION APPROACH FOR WING AERODYNAMIC DESIGN OPTIMIZATION | ICAS2026_0469 |
| Martins, R.S. | WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH | ICAS2026_0438 |
| Martins, Y.A.D. | A QUALITATIVE FRAMEWORK FOR AIRCRAFT WING MANUFACTURING AND DECISION MAKING | ICAS2026_0766 |
| Marzocca, P. | GROUND VIBRATION TEST ANALYSIS OF A PC-9 AIRCRAFT USING DELAY-EMBEDDED DYNAMIC MODE DECOMPOSITION WITH CONTROL | ICAS2026_0153 |
| Marzocca, P. | GEOMETRY PARAMETERISATION VIA A STRUCTURAL MODAL BASIS FOR AERODYNAMIC SHAPE OPTIMISATION | ICAS2026_0155 |
| Marzocca, P. | TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT | ICAS2026_0183 |
| Marzocca, P. | NON-LINEAR PARAMETRIC MODEL FOR THE 3DOF MOTION OF A BOX IN WAVES USING SPARSE REGRESSION | ICAS2026_0228 |
| Marzocca, P. | GROUND-EFFECT ANALYSIS OF SMALL DUCTED PROPELLERS: A NUMERICAL–EXPERIMENTAL STUDY | ICAS2026_0456 |
| Marzocca, P. | EXPLAINABLE NATURAL LANGUAGE PROCESSING FOR AIRCRAFT STRUCTURAL INTEGRITY DEFECT CLASSIFICATION | ICAS2026_0738 |
| Marzocca, P. | DECOUPLED DEEP REINFORCEMENT LEARNING FOR AUTONOMOUS LANDING OF UAVS ON SHIPS | ICAS2026_0867 |
| Mason, E. | JET ZERO: ATJ SAF PROJECT DEVELOPER | ICAS2026_0985 |
| Matesanz-Garcia, J. | NOVEL METHODS FOR THE CHARACTERISATION OF INTAKE FLOW DISTORTION | ICAS2026_0110 |
| Matias, J.C. | WIND TUNNEL INVESTIGATION OF HELICOPTER LOADS DURING URBAN OPERATIONS ON A BUILDING WITH COLUMNAR VORTEX GENERATORS | ICAS2026_0049 |
| Matías, J.C. | CFD ANALYSIS OF MMRTG THERMAL PLUME ON THE EXTERNAL AERODYNAMICS OF A MARS ROVER | ICAS2026_0054 |
| Matías, J.C. | DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE. | ICAS2026_0427 |
| Matida, E. | WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH | ICAS2026_0438 |
| Matsuda, H. | IMPACT OF DYNAMIC METERING OPERATIONS UNDER ADVERSE WEATHER AND MITIGATION THROUGH OPTIMAL SEQUENCING | ICAS2026_0591 |
| Matsui, K. | INITIAL GEOMETRIC UNCERTAINTY ASSESSMENT IN COMPRESSOR AIRFOILS USING PHYSICS-BASED DIRECT MANIPULATED FFD | ICAS2026_0768 |
| Matsuno, Y. | IMPACT OF DYNAMIC METERING OPERATIONS UNDER ADVERSE WEATHER AND MITIGATION THROUGH OPTIMAL SEQUENCING | ICAS2026_0591 |
| Matsuo, A. | MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) | ICAS2026_1074 |
| Matthes, S. | JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION | ICAS2026_0212 |
| Matuschek, T. | MODULAR JET AND PROPELLER ENGINE – PART I: INITIAL STUDIES | ICAS2026_0813 |
| Matuschek, T. | MODULAR JET AND PROPELLER ENGINE – PART II: INTEGRATED DESIGN PROCESS AND DESIGN SPACE ASSESSMENT | ICAS2026_0829 |
| Mauersberger, M. | OPTIMIZATION APPROACHES FOR THE SHEAR-POSTBUCKLING DESIGN OF THERMOPLASTIC THIN-PLY COMPOSITE SHELLS IN HELICOPTERS | ICAS2026_0614 |
| Mavris, D. | MODELING & PRELIMINARY ANALYSIS OF AN ECOFRIENDLY AIRBORNE GLOBAL LUXURY EKRANOPLAN | ICAS2026_0055 |
| Mavris, D.N. | TOWARDS AN ECOSYSTEM FOR AERONAUTICAL RESEARCH IN MEXICO | ICAS2026_0639 |
| Mavris, D.N. | FEATURE MODEL CREATION THROUGH MISSION ANALYSIS IN THE CONTEXT OF VEHICLE FAMILIES | ICAS2026_0918 |
| May, M. | KNOW YOUR LIMITS: ESTIMATING THE TILT-WING TRANSITION CORRIDOR UNDER FAILURE CONDITIONS | ICAS2026_0152 |
| May, M. | TETHERED HOVER FLIGHT TESTS OF BASELINE CONTROL LAWS FOR A TANDEM TILT-WING SUB-SCALE DEMONSTRATOR | ICAS2026_0404 |
| Mayer, F. | REYNOLDS NUMBER SCALING EFFECTS IN TRANSONIC CAVITY AERODYNAMICS: A HIGH-FIDELITY EXPERIMENTAL AND NUMERICAL FRAMEWORK | ICAS2026_0362 |
| Mayima, A. | APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS | ICAS2026_0359 |
| Mayima, A. | AI IN THE COCKPIT: THE JARVIS STORY | ICAS2026_0547 |
| Maynard, N. | AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC | ICAS2026_0347 |
| Mazharmanesh, S. | MECHANISMS OF SCREECH MODE STAGING IN UNDEREXPANDED SUPERSONIC JETS | ICAS2026_1082 |
| McCarthy, J. | INTERMITTENT LOW FREQUENCY EXPERIMENTAL CAVITY DYNAMICS | ICAS2026_0748 |
| McCarthy, J. | FORCE RECONSTRUCTION TECHNIQUES FOR DYNAMIC LOAD ESTIMATION ON GENERIC GEOMETRIES IN LOW-SPEED WIND TUNNEL TESTING | ICAS2026_0790 |
| McCormick, C. | A WORKFLOW FOR RAPID DESIGN, SIMULATION, FABRICATION, AND SUBSCALE FLIGHT-TESTING OF NOVEL AIRCRAFT CONCEPTS | ICAS2026_0845 |
| McCormick, C. | SIMULATION MODEL CALIBRATION USING SYSTEM IDENTIFICATION FOR A VECTORED-THRUST MULTI-TILT-ROTOR CONFIGURATION | ICAS2026_0929 |
| McGuire, J. | IMPLEMENTATION OF DISTRIBUTED SWARM GUIDANCE ALGORITHMS ON LOW-COST UAVS | ICAS2026_0771 |
| McIvor, B. | IMPLEMENTATION OF DISTRIBUTED SWARM GUIDANCE ALGORITHMS ON LOW-COST UAVS | ICAS2026_0771 |
| McKee, S. | NEUROMORPHIC ASCENT: REVOLUTIONISING AIRCRAFT STORES COMPATIBILITY AND INTELLIGENT & AUTONOMOUS SYSTEMS | ICAS2026_0831 |
| McNamee Freire, S. | ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT | ICAS2026_0897 |
| Meglio, C. | PASSIVE FLOW CONTROL OF A TURBULENT BOUNDARY LAYER AT THE VERGE OF SEPARATION USING SURFACE ROUGHNESS | ICAS2026_1085 |
| Meheut, M. | AERODYNAMIC TRANSONIC DESIGN OF A STRUT-BRACED WING | ICAS2026_0223 |
| Méheut, M. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Mei, Y.H. | EARLY WARNING FOR POTENTIAL BIRD STRIKES: STRATEGIC OPTIMIZATION OF PAN-TILT-ZOOM SENSOR NETWORKS FOR BIRD HAZARD DECREASE IN AIRPORT ENVIRONMENT | ICAS2026_0439 |
| Meier, J. | VALIDATION OF TRADITIONAL COMPETENCY-BASED ASSESSMENT AND EXPERIENCE-BASED AUTHORISATION FOR AIR TRAFFIC CONTROLLERS | ICAS2026_0568 |
| Meirelles, L.J.F. | COST-EFFECTIVE CFD REPRODUCTION OF DPW-7 CASE 2A FOR CRM TRANSONIC PITCHING-MOMENT PREDICTION AND ADAPTIVE-REFINEMENT ASSESSMENT | ICAS2026_0953 |
| Melkert, J. | BLI/PROPULSION STUDIES AT TU DELFT (PART I) | ICAS2026_1061 |
| Melkert, J. | BLI/PROPULSION STUDIES AT TU DELFT (PART II) | ICAS2026_1062 |
| Mello, J.M. | EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY | ICAS2026_0080 |
| Mello, J.M.G. | VIRTUAL COMMISSIONING APPLIED TO ROS AIRCRAFT ROBOTIC CELL | ICAS2026_0198 |
| Mello, J.M.G. | A QUALITATIVE FRAMEWORK FOR AIRCRAFT WING MANUFACTURING AND DECISION MAKING | ICAS2026_0766 |
| Melone, G. | MULTIDISCIPLINARY DESIGN EXPLORATION OF HYBRID-ELECTRIC REGIONAL AIRCRAFT | ICAS2026_0360 |
| Mendiguchia Meuser, M. | JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION | ICAS2026_0212 |
| Meng, Y. | NUMERICAL INVESTIGATION OF GEOMETRIC EFFECTS ON INFRARED CHARACTERISTICS OF MULTI-STREAM SERPENTINE NOZZLES | ICAS2026_0788 |
| Merrifield, J. | THE TREATMENT OF NON-IDEAL SURFACE TOPOLOGIES RELATED TO HIGH-SPEED VEHICLE DESIGN | ICAS2026_1071 |
| Mertens, C. | ON THE GROUND AND IN FLIGHT: AERODYNAMIC AND AEROELASTIC TESTING SUPPORTING INNOVATION IN AERONAUTICS | ICAS2026_1001 |
| Messias Magalhães Júnior, J. | PHYSICS-INFORMED NEURAL OPERATORS FOR DISTURBANCE FIELD PREDICTION IN NONPARALLEL BOUNDARY-LAYER STABILITY ANALYSIS | ICAS2026_0051 |
| Messias Magalhães Júnior, J. | A MACHINE-LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION FRAMEWORK USING FREE-FORM DEFORMATION AND DEEP NEURAL NETWORKS | ICAS2026_0061 |
| Meyer, H. | ONTOLOGY-BASED SENSOR HEALTH MONITORING: A DYNAMIC ONTOLOGY-BASED FAULT DETECTION AND CLASSIFICATION FOR TIMESERIES DATA | ICAS2026_0716 |
| Meyer, L. | UNCERTAINTY ANALYSIS AND EYE-TRACKING-BASED CLUSTERING IN AIR TRAFFIC CONTROLLER WORKLOAD PREDICTION | ICAS2026_0118 |
| Mi, B. | RESEARCH ON OVERALL AERODYNAMIC DESIGN OF GRID-DUCT INTEGRATED VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING AIRCRAFT | ICAS2026_0482 |
| Mi, B. | EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN | ICAS2026_0490 |
| Mi, B.G. | STUDY ON DAMAGE SEVERITY ASSESSMENT METHODS FOR ASYMMETRICALLY DAMAGED LOITERING MUNITIONS | ICAS2026_0306 |
| Mi, B.G. | MODELING AND ANALYSIS OF ACTIVE FLUTTER SUPPRESSION OF THE PREPOSITIVE ELLIPTICAL WING-MAIN WING COMPOSITE CONFIGURATION | ICAS2026_0494 |
| Mi, B.G. | NUMERICAL STUDY OF UNSTEADY DISTORTION IN AN S-DUCT INTAKE SUBJECTED TO BLAST SHOCK WAVES | ICAS2026_0510 |
| Mi, B.G. | A UNIFIED PARAMETRIC MODELING METHOD FOR CONVENTIONAL, SEMI-BURIED, AND EMBEDDED INLETS | ICAS2026_0515 |
| Mi, B.G. | RESEARCH ON AERODYNAMIC-STRUCTURAL RAPID EVALUATION AND OPTIMIZATION METHODS FOR JOINED-WING CONFIGURATIONS | ICAS2026_0577 |
| MI, Baigang | A RAPID AERODYNAMIC ASSESSMENT METHOD FOR BATTLE-DAMAGED CRUISE MISSILES | ICAS2026_0578 |
| Miao, S. | SEMI-SUPERVISED MULTI-TASK CONSISTENCY LEARNING FOR DEFECT DETECTION AND DEPTH ESTIMATION | ICAS2026_0072 |
| Migliorini, M. | MIDAS: A MODULAR SOFTWARE FOR INTAKE FLOW DISTORTION ANALYSIS | ICAS2026_0705 |
| Miki, H. | SPILLAGE DRAG REDUCTION IN DIVERTERLESS SUPERSONIC INLET | ICAS2026_0418 |
| Milani, Z. | WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH | ICAS2026_0438 |
| Milz, D. | KNOW YOUR LIMITS: ESTIMATING THE TILT-WING TRANSITION CORRIDOR UNDER FAILURE CONDITIONS | ICAS2026_0152 |
| Milz, D. | TETHERED HOVER FLIGHT TESTS OF BASELINE CONTROL LAWS FOR A TANDEM TILT-WING SUB-SCALE DEMONSTRATOR | ICAS2026_0404 |
| Min, S. | MODELLING SENSITIVITIES IN THREE-DIMENSIONAL FZRA-SPECTRUM ICE-SHAPE PREDICTION FOR THE CRM-HL STOWED CONFIGURATION | ICAS2026_0896 |
| Mingione, G. | ICE DETECTION: CORRELATION OF ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES TESTED IN ICING WIND TUNNEL | ICAS2026_0186 |
| Miris, G. | HIGH-RATE AUTOMATED STAMP FORMING OF CF/LM-PAEK COMPOSITES FOR NEXT-GENERATION UAV AEROSTRUCTURES | ICAS2026_0286 |
| Mishra, C. | RESEARCH PLATFORM AIRSHIP: DESIGN AND FLIGHT CHARACTERISTICS FOR URBAN OPERATIONS | ICAS2026_0576 |
| Misol, M. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Missato, T.A. | ASSESSING VORTEX BREAKDOWN AND COUPLING IN DELTA WING PLANFORMS THROUGH HIGH-FIDELITY DDES SIMULATIONS | ICAS2026_0939 |
| Mitrotta, F.M.A. | VALIDATION OF A LOW-COST DATA ACQUISITION SYSTEM FOR AIRCRAFT VIBRATION TESTING | ICAS2026_0724 |
| Mittenecker, B. | AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS | ICAS2026_0195 |
| Moëns, F. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Moerland, E. | THE CONFERENCE LOCATIONS: A QUANTITATIVE APPROACH TO REDUCING IMPACT GLOBAL TRAVEL | ICAS2026_0607 |
| Mohd-Nasir, D. | DESIGN AND TESTING OF A BUOYANT UAV FOR AGRICULTURAL SURVEILLANCE | ICAS2026_0594 |
| Mohsin, H. | NUMERICAL BOUNDARY LAYER VALIDATION TECHNIQUE USING RAE M2155 SWEPT WING | ICAS2026_0283 |
| Mohsin, H. | PROPOSAL FOR DISTINGUISHING USABLE DATA UNDER HIGH WIND TUNNEL BLOCKAGE USING AN RAE2822 TEST CASE | ICAS2026_0592 |
| Molesworth, B. | FACTORS AFFECTING COMMUNICATION IN AVIATION | ICAS2026_0059 |
| Molesworth, B.R.C. | QUANTIFYING THE EFFECT OF IN-CABIN NOISE ON COGNITION | ICAS2026_0056 |
| Molesworth, B.R.C. | A HUMAN-CENTRIC APPROACH TO UNDERSTANDING THE CONTRIBUTING FACTORS OF PILOT-RELATED RUNWAY INCURSIONS | ICAS2026_0086 |
| Mollet, C. | AEROELASTIC DESIGN OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT IN AN MDO FRAMEWORK | ICAS2026_0342 |
| Mollet, C. | COMBINED TOPOLOGY AND COMPOSITE LAMINATE OPTIMIZATION OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT | ICAS2026_0355 |
| Mollet, C. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Mollwitz, V. | A COMPARISON OF TRAJECTORY-BASED OPERATIONS IN THE UNITED STATES AND EUROPE IN SUPPORT OF GLOBAL HARMONIZATION | ICAS2026_0412 |
| Montagner, S. | PROPELLER AERODYNAMICS UNDER NON-UNIFORM INFLOWS | ICAS2026_0444 |
| Monteleone, F. | VERTIPORT FINAL APPROACH AND TAKEOFF AREA ORIENTATION IDENTIFICATION USING COUPLED MICROSCALE WIND AND FLIGHT DYNAMICS ANALYSIS | ICAS2026_0150 |
| Montella, N. | NUMERICAL REBUILDING OF AERODYNAMIC WIND TUNNEL ANALYSES OF A CREW RETURN VEHICLE | ICAS2026_0572 |
| Montero-Sistiaga, M.L. | ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS | ICAS2026_1005 |
| Montiel Viruel, V. | TOWARDS A SYSTEM-OF-SYSTEMS ENGINEERING ROADMAP FOR INTEGRATING SUSTAINABLE AVIATION FUEL INTO MEXICO’S AIRPORT FUEL INFRASTRUCTURE | ICAS2026_0722 |
| Montoya-Ospina, S. | STUDY OF THE FEASIBILITY OF ACOUSTIC LINERS INSIDE THE BEAM THAT INTERACTS WITH A UAV DRONE ROTOR | ICAS2026_0743 |
| Moon, J.H. | FLIGHT TEST VALIDATION OF A VISION-GUIDED MULTIROTOR TERMINAL INTERCEPTION SYSTEM | ICAS2026_0737 |
| Mooney, S. | CLIMATE HAZARD TIMING AND FLIGHT DEMAND COOCCURRENCE: A DEMAND-WEIGHTED EXPOSURE FRAMEWORK | ICAS2026_0870 |
| Mooney, W. | DESIGN AND OPERATION OF LOW-COST MULTI-SCALE TEST BEDS FOR BATTERY THERMAL RUNAWAY INITIATION AND PROPAGATION | ICAS2026_0030 |
| Morales, M.A.V. | FIXED-WING AIRCRAFT PORT-HAMILTONIAN DYNAMICS AND CONTROL | ICAS2026_0425 |
| Morales, M.A.V. | AUTOPILOT DESIGN OF AN UNSTABLE FIGHTER USING MODEL PREDICTIVE CONTROL | ICAS2026_0791 |
| Morales, M.T. | AUTOPILOT DESIGN OF AN UNSTABLE FIGHTER USING MODEL PREDICTIVE CONTROL | ICAS2026_0791 |
| Moran, T. | FIVE DEACADES OF T-38 WING TEARDOWNS: DATA, INSIGHT, AND IMPACT | ICAS2026_0830 |
| Moreau, D. | EXPERIMENTAL INVESTIGATION ON THE INNER DUCT SURFACE UNSTEADY PRESSURE OF A DUCTED PROPELLER | ICAS2026_0033 |
| Moreau, D. | LOW MACH NUMBER AEROACOUSTICS R&D AT UNSW SYDNEY | ICAS2026_1044 |
| Moreira, F.C. | A STUDY ON THE CELL REYNOLDS NUMBER AS A PARAMETER FOR MESH QUALITY ON HYPERSONIC FLOWS | ICAS2026_0065 |
| Morel, A. | ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS | ICAS2026_1005 |
| Moreno-Escolastico, P. | AN INCREMENTAL MODULAR MDO FRAMEWORK FOR HYDROGEN-ELECTRIC POWERTRAIN SIZING AND INTEGRATION IN GENERAL AVIATION AIRCRAFT | ICAS2026_0876 |
| Mori, K. | ASSESSMENT OF ENGINE-OUT ATMOSPHERIC EMISSIONS FROM COCONUT-OIL-DERIVED BIOJET FUEL | ICAS2026_0487 |
| Mori, R. | A PEAKS-OVER-THRESHOLD APPROACH TO RUNWAY COLLISION RISK ESTIMATION FOR EFFICIENT ARRIVAL OPERATIONS | ICAS2026_0332 |
| Mori, R. | APPROPRIATE ATC GO-AROUND INSTRUCTION TIMING TO PREVENT RUNWAY COLLISIONS | ICAS2026_0863 |
| Morioka, S. | HPC-BASED PARAMETER SPACE EXPLORATION FOR DENSE PICOSAT FORMATION FLYING TOWARD DIRECT-TO-DEVICE COMMUNICATIONS | ICAS2026_0869 |
| Morioka, S. | MANEUVER- AND DELAY-ROBUST DISTRIBUTED SATELLITE SSA VIA SPATIO-TEMPORAL GRAPH FORECASTING | ICAS2026_0959 |
| Moriot, J. | EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION | ICAS2026_0673 |
| Morita, N. | DYNAMIC ANALYSES AND FLIGHT TESTING FOR THE DESIGN OF FLOATING CANARD AIRCRAFT | ICAS2026_0346 |
| Morita, N. | COMPARISON OF FLEXIBLE AIRCRAFT CONFIGURATIONS USING AEROELASTIC ANALYSIS | ICAS2026_0609 |
| Moruzzi, M.C. | AURAL DIGITAL TWIN FOR AIRCRAFT CABIN DESIGN | ICAS2026_0899 |
| Moschetta, J.-M. | A STALL EXTENSION TO LIFTING-LINE THEORY: IMPLEMENTATION AND VALIDATION IN ASWING | ICAS2026_0720 |
| Moser, N. | NOVEL MULTIDISCIPLINARY MISSION-OPTIMISED AIRCRAFT DEVELOPMENT METHODOLOGY IN CONSIDERATION OF PASSIVE/ACTIVE CONTROL | ICAS2026_0230 |
| Moser, N. | AN INDIVIDUALISED, SCALABLE PROJECT-BASED LEARNING FRAMEWORK FOR STRUCTURE DESIGN COURSES ESTABLISHED IN A LARGE AEROSPACE STUDY PROGRAMME | ICAS2026_0718 |
| Moses, T. | NOISE-OPTIMIZED HOVER PROPELLER DESIGN FOR VTOL CARGO DRONES IN TRANSIENT FLIGHT CONDITIONS | ICAS2026_0569 |
| Moshin, H. | MODELLING SENSITIVITIES IN THREE-DIMENSIONAL FZRA-SPECTRUM ICE-SHAPE PREDICTION FOR THE CRM-HL STOWED CONFIGURATION | ICAS2026_0896 |
| Mottola, E.P. | AIRFRAME HEALTH MONITORING ON THE BAE SYSTEMS HAWK T1A JET TRAINER | ICAS2026_0706 |
| Mou, Y. | PHYSICAL DESIGN CONCEPTS OF VORTEX GENERATOR ARRAYS FOR AIRCRAFT AFT-BODIES DRIVEN BY DISTINCT DRAG REDUCTION MECHANISMS | ICAS2026_0185 |
| Mourad, J. | THIN AEROFOILS OSCILLATING IN A CONFINED INVISCID FLOW | ICAS2026_0637 |
| Mouritz, A.P. | ENHANCEMENT AND DEGRADATION: THE DUAL ROLE OF GRAPHENE NANOPLATELETS ON THE STRUCTURAL PERFORMANCE OF COMPOSITE T-JOINTS AND MECHANISTIC INSIGHTS | ICAS2026_0868 |
| Mudrik, L. | ROBUST ESTIMATION-AWARE GUIDANCE FOR STOCHASTIC INTERCEPTION WITH PARAMETRIC UNCERTAINTY | ICAS2026_0123 |
| Mueller, V. N. | AN INDIVIDUALISED, SCALABLE PROJECT-BASED LEARNING FRAMEWORK FOR STRUCTURE DESIGN COURSES ESTABLISHED IN A LARGE AEROSPACE STUDY PROGRAMME | ICAS2026_0718 |
| Mueller, V.N. | NOVEL MULTIDISCIPLINARY MISSION-OPTIMISED AIRCRAFT DEVELOPMENT METHODOLOGY IN CONSIDERATION OF PASSIVE/ACTIVE CONTROL | ICAS2026_0230 |
| Mukhopadhaya, J. | AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH | ICAS2026_1015 |
| Munholand, L. | TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT | ICAS2026_0183 |
| Munshi, A.K. | PRELIMINARY SIZING METHODOLOGY FOR HYBRID-ELECTRIC PROPULSION SYSTEM IN CARGO AIRSHIPS | ICAS2026_0688 |
| Murahashi, Y. | NEW TEST RESULTS OF THE 3.23% FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2026_0328 |
| Murata, Y. | AEROACOUSTIC WIND TUNNEL TESTING AND CFD STUDY USING JAXA 8% SEMISPAN HIGH-LIFT COMMON RESEARCH MODEL IN JAXA FQUROH-2 PROJECT | ICAS2026_0756 |
| Murayama, M. | AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMI-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT THE JAXA 6.5M X 5.5M LOW SPEED WIND TUNNEL | ICAS2026_0256 |
| Murayama, M. | AEROACOUSTIC WIND TUNNEL TESTING AND CFD STUDY USING JAXA 8% SEMISPAN HIGH-LIFT COMMON RESEARCH MODEL IN JAXA FQUROH-2 PROJECT | ICAS2026_0756 |
| Murça, M. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Murphy, A. | PRATT & WHITNEY: MEETING THE FUTURE PROPULSION NEEDS OF COMMERCIAL AVIATION | ICAS2026_1008 |
| Murphy, A. | A MULTI-FUEL PROPULSION SYSTEM STRATEGY FOR AVIATION TRANSPORT RESILIENCE | ICAS2026_1016 |
| Murray, G. | A PROCESS-STRUCTURE-PROPERTY-PERFORMANCE FRAMEWORK FOR DIGITAL ENGINEERING-ENABLED REPAIR OF ALUMINUM PARTS | ICAS2026_0940 |
| Muscarello, V. | VERTIPORT FINAL APPROACH AND TAKEOFF AREA ORIENTATION IDENTIFICATION USING COUPLED MICROSCALE WIND AND FLIGHT DYNAMICS ANALYSIS | ICAS2026_0150 |
| Muscarello, V. | DEVELOPMENT OF CONTROL LAWS FOR ENHANCED PERFORMANCE AND AEROELASTIC STABILITY OF EVTOL AIRCRAFT | ICAS2026_0452 |
| Muscarello, V. | GROUND-EFFECT ANALYSIS OF SMALL DUCTED PROPELLERS: A NUMERICAL–EXPERIMENTAL STUDY | ICAS2026_0456 |
| Mwasandube, M.A. | VORTEX TOPOLOGY AND CORE-UNWINDING MECHANISM IN SPIROID WINGTIP DEVICES USING LAGRANGIAN PARTICLE TRACKING | ICAS2026_0162 |
| Myschik, S. | GAIN OPTIMIZATION FOR CASCADED INDI CONTROL WITH INTEGRATED PERFORMANCE AND ROBUSTNESS REQUIREMENTS | ICAS2026_0372 |
| Myschik, S. | FLIGHT PERFORMANCE ANALYSIS OF ELECTRIC AIRCRAFT UNDER MOTOR FAILURE CONDITIONS USING REDUCED-ORDER MODELING | ICAS2026_0539 |
| Myschik, S. | HARDWARE-IN-THE-LOOP VERIFICATION OF A SAFETY-CRITICAL RECONFIGURABLE BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIRCRAFT | ICAS2026_0557 |
| Naeem, F. | STANDARDIZED TAKE-OFF AND LANDING PROCEDURES FOR AIR TAXIS: URBAN AIR MOBILITY | ICAS2026_0946 |
| Nagai, H. | UNSTEADY AERODYNAMIC OPTIMIZATION OF A THIN ANGULAR AIRFOIL USING CARTESIAN MESH CFD WITH THE LEVEL SET METHOD | ICAS2026_0767 |
| Nagarajan, P. | ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES | ICAS2026_0289 |
| Nagarajan, P. | AN AUTONOMY ARCHITECTURE FOR COLLABORATIVE UAV SWARMS - A BOTTOM-UP PERSPECTIVE | ICAS2026_0670 |
| Nagata, T. | SDF-BASED GEOMETRY BLENDING OF HYPERSONIC VEHICLE CONCEPTS | ICAS2026_1070 |
| Nagel, B. | AUTOMATED KNOWLEDGE-BASED CABIN DESIGN AND EVALUATION WITHIN A PRELIMINARY AIRCRAFT DESIGN LOOP | ICAS2026_0214 |
| Nagel, B. | VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS | ICAS2026_0336 |
| Nagel, B. | NUMERICAL PREDICTION OF CABIN NOISE FOR FUTURE SHORT-HAUL AIRCRAFT IN EARLY AIRCRAFT DESIGN | ICAS2026_0364 |
| Nagel, B. | PIONEERING THE EXCHANGE OF KNOWLEDGE IN AIRCRAFT DESIGN | ICAS2026_1107 |
| Nagl, J. | AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS | ICAS2026_0195 |
| Nakamura, H. | ASSESSING AIRLINE PURCHASE MOTIVATION FOR HYDROGEN AIRCRAFT UNDER FUTURE CORSIA | ICAS2026_0031 |
| Nakaya, S. | MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) | ICAS2026_1074 |
| Nava Gaxiola, C. | ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT | ICAS2026_0897 |
| Navarro, A. | PHYSICS-INFORMED MACHINE LEARNING FOR FLIGHT DYNAMICS IDENTIFICATION OF THE SAAB 340B USING FLIGHT TEST DATA | ICAS2026_0686 |
| Neely, A. | CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS | ICAS2026_0749 |
| Neely, A. | EXPERIMENTAL DEVELOPMENT OF HIGH-SPEED AEROSPACE SYSTEMS: CHALLENGES & OPPORTUNITIES | ICAS2026_1050 |
| Neely, A. | RECENT DEVELOPMENTS IN HYPERSONIC INNOVATION, SCIENCE & TECHNOLOGY IN AUSTRALIA | ICAS2026_1064 |
| Neely, A. | PREDICTING THE RESPONSE OF HIGH-TEMPERATURE STRUCTURE FOR HIGH-SPEED VEHICLES THROUGH SIMULATION AND MEASUREMENT | ICAS2026_1093 |
| Newby, T | RR PERSPECTIVES & PROGRESS ON NEXTGEN PROPULSION FOR FUTURE AIRLINERS | ICAS2026_1037 |
| Ng, C.S.X. | AN AUGMENTED AIRPORT MODEL FOR GROUND OPERATIONS ANALYSIS: A CASE STUDY OF NARITA INTERNATIONAL AIRPORT | ICAS2026_0272 |
| Nguyen, H.H. | A HYBRID 0D–2D WHOLE-ENGINE MATCHING FRAMEWORK FOR TURBOJET ENGINE PERFORMANCE SIMULATION | ICAS2026_0687 |
| Nguyen, H.P.U. | ASSESSMENT OF ENGINE-OUT ATMOSPHERIC EMISSIONS FROM COCONUT-OIL-DERIVED BIOJET FUEL | ICAS2026_0487 |
| Nguyen, J. | ATTITUDE CONTROL TECHNIQUES FOR A MICRO-SCALE FLAP-BASED AERODYNAMIC DECELERATOR SYSTEM | ICAS2026_0361 |
| Nguyen, N.-V. | A RELIABLE AND COST-EFFICIENT DATA ACQUISITION SYSTEM FOR MIL-HDBK-1763-COMPLIANT STATIC EJECTION TESTING OF AIRCRAFT EXTERNAL STORES | ICAS2026_0170 |
| Nguyen, P.-M. | A RELIABLE AND COST-EFFICIENT DATA ACQUISITION SYSTEM FOR MIL-HDBK-1763-COMPLIANT STATIC EJECTION TESTING OF AIRCRAFT EXTERNAL STORES | ICAS2026_0170 |
| Nguyen, T.-.B. | A RELIABLE AND COST-EFFICIENT DATA ACQUISITION SYSTEM FOR MIL-HDBK-1763-COMPLIANT STATIC EJECTION TESTING OF AIRCRAFT EXTERNAL STORES | ICAS2026_0170 |
| Nguyen, V.-T. | A RELIABLE AND COST-EFFICIENT DATA ACQUISITION SYSTEM FOR MIL-HDBK-1763-COMPLIANT STATIC EJECTION TESTING OF AIRCRAFT EXTERNAL STORES | ICAS2026_0170 |
| Nguyen Van, E. | AERODYNAMIC TRANSONIC DESIGN OF A STRUT-BRACED WING | ICAS2026_0223 |
| Nguyen Van, E. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Nguyen-Van, E. | FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION | ICAS2026_0888 |
| Niakate, B. | FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING | ICAS2026_0172 |
| Nian, C.C. | DATA-DRIVEN SHAPE PARAMETERIZATION FOR EFFECTIVE AERODYNAMIC DESIGN OPTIMIZATION OF PROPELLERS | ICAS2026_0476 |
| Nichman, L. | WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH | ICAS2026_0438 |
| Nicolosi, F. | MULTIDISCIPLINARY DESIGN EXPLORATION OF HYBRID-ELECTRIC REGIONAL AIRCRAFT | ICAS2026_0360 |
| Nicolosi, F. | TOP-LEVEL AIRCRAFT REQUIREMENT TRADE STUDIES FOR HYDROGEN FUEL CELL REGIONAL AIRCRAFT | ICAS2026_0703 |
| Nicolosi, F. | COST-DRIVER MULTIDISCIPLINARY FRAMEWORK FOR WINGLET DESIGN: A REGIONAL AIRCRAFT CASE STUDY | ICAS2026_0783 |
| Nicolosi, F. | MIXED-FIDELITY, NONLINEAR AIRCRAFT MISSION MODELING FOR HYBRID REGIONAL AIRCRAFT DESIGN VERIFICATION | ICAS2026_0836 |
| Nicolosi, F. | OVERVIEW OF CRITICAL ISSUES AND OPPORTUNITIES FOR NEW A/C WITH HYBRID AND FULL-ELECTRIC POWERTRAIN | ICAS2026_0984 |
| Nie, H. | AN EFFICIENT TRANSITION PREDICTION METHOD USING NEURAL NETWORK SURROGATE MODELS | ICAS2026_0254 |
| Niedermeier, D. | ASSESSING AN ALTERNATE AIRPORT ASSISTANT | ICAS2026_0192 |
| Niemann, H. | VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS | ICAS2026_0336 |
| Niessen, K. | KEY PARAMETER IDENTIFICATION IN AIRCRAFT STRAIN PREDICTION MODELS | ICAS2026_0032 |
| Nieto-Centenero, J. | GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION | ICAS2026_1011 |
| Nikodem, F. | FLIGHT TESTING OF A HIGH-ALTITUDE UNCREWED AND SOLAR POWERED PLATFORM HEAVIER THAN AIR | ICAS2026_0296 |
| Nimura, R. | SPILLAGE DRAG REDUCTION IN DIVERTERLESS SUPERSONIC INLET | ICAS2026_0418 |
| Nishida, H. | EXPERIMENTAL STUDY OF LOAD ALLEVIATION WITH PASSIVE ADAPTIVE CAMBER AIRFOILS | ICAS2026_0730 |
| Nishizuka, S. | EFFECT OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS | ICAS2026_0517 |
| Nithya, D.S. | VERTIPORT FINAL APPROACH AND TAKEOFF AREA ORIENTATION IDENTIFICATION USING COUPLED MICROSCALE WIND AND FLIGHT DYNAMICS ANALYSIS | ICAS2026_0150 |
| Niu, Y.L. | BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL | ICAS2026_0647 |
| Nogueira, P.A.S. | MECHANISMS OF SCREECH MODE STAGING IN UNDEREXPANDED SUPERSONIC JETS | ICAS2026_1082 |
| Noll, R. | GAP OPTIMIZATION ADAPTIVE TOOL FOR LARGE SCALE FLEXIBLE STRUCTURE ASSEMBLY | ICAS2026_0058 |
| Noordman, B. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Notman, D. | IMPLICATIONS OF AAM OPERATIONS FOR FUTURE SHARED AIRSPACE IN VICTORIA, AUSTRALIA | ICAS2026_1083 |
| Nugnes, V. | A MULTI-RANGE HYBRID-ELECTRIC OPEN-ROTOR AIRCRAFT CONCEPT FOR THE WIDE-BODY PASSENGER CLASS | ICAS2026_0625 |
| Nunley, A. | OPTIMIZATION OF INTERCONNECTED 3D-PRINTED STRUCTURES FOR UAVS | ICAS2026_0943 |
| Nöhren, L. | EVALUATING HUMAN-MACHINE-TEAMING CONCEPTS FOR A HIGHLY AUTOMATED GROUND CONTROLLER WORKING POSITION | ICAS2026_0302 |
| Oberthür, L. | INVESTIGATION OF GENERIC SWIRL DISTORTION AND ITS EFFECTS ON COMPRESSOR PERFORMANCE AND FLOW STABILITY | ICAS2026_0334 |
| Ogawa, S. | ASSESSMENT OF ENGINE-OUT ATMOSPHERIC EMISSIONS FROM COCONUT-OIL-DERIVED BIOJET FUEL | ICAS2026_0487 |
| Ogawa, T. | DYNAMIC ANALYSES AND FLIGHT TESTING FOR THE DESIGN OF FLOATING CANARD AIRCRAFT | ICAS2026_0346 |
| Oh, K.R. | ESTIMATION AND ANALYSIS OF RNP REQUIREMENTS FOR HETEROGENEOUS UAM CONFIGURATIONS: INSIGHTS FROM OPPAV DEMONSTRATION | ICAS2026_0802 |
| Ohneiser, O. | VALIDATION OF TRADITIONAL COMPETENCY-BASED ASSESSMENT AND EXPERIENCE-BASED AUTHORISATION FOR AIR TRAFFIC CONTROLLERS | ICAS2026_0568 |
| Okabayashi, R. | ROBUST MOTION ESTIMATION FOR INDOOR MAVS USING WIDE-FIELD-INTEGRATION OF OPTIC FLOW | ICAS2026_0163 |
| Okamoto, K. | A SYSTEMATIC, TUNING-FREE ATTITUDE CONTROL METHOD FOR VTOL UAVS | ICAS2026_0096 |
| Okamoto, M. | UNSTEADY AERODYNAMIC OPTIMIZATION OF A THIN ANGULAR AIRFOIL USING CARTESIAN MESH CFD WITH THE LEVEL SET METHOD | ICAS2026_0767 |
| Okubo, N. | DYNAMIC ANALYSES AND FLIGHT TESTING FOR THE DESIGN OF FLOATING CANARD AIRCRAFT | ICAS2026_0346 |
| Okubo, N. | COMPARISON OF FLEXIBLE AIRCRAFT CONFIGURATIONS USING AEROELASTIC ANALYSIS | ICAS2026_0609 |
| Olichevis Halila, G.L. | PHYSICS-INFORMED NEURAL OPERATORS FOR DISTURBANCE FIELD PREDICTION IN NONPARALLEL BOUNDARY-LAYER STABILITY ANALYSIS | ICAS2026_0051 |
| Olichevis Halila, G.L. | HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION OF WIND TURBINES USING A DISCRETE ADJOINT APPROACH | ICAS2026_0052 |
| Olichevis Halila, G.L. | A MACHINE-LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION FRAMEWORK USING FREE-FORM DEFORMATION AND DEEP NEURAL NETWORKS | ICAS2026_0061 |
| Oliveira, A.A.J. | STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR IMPACT RESPONSE FOR LIGHTWEIGHT FIXED-WING UAVS | ICAS2026_0833 |
| Oliveira, J.V.N. | STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR IMPACT RESPONSE FOR LIGHTWEIGHT FIXED-WING UAVS | ICAS2026_0833 |
| Oliveira, W. | EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY | ICAS2026_0080 |
| Omoto, K. | INITIAL GEOMETRIC UNCERTAINTY ASSESSMENT IN COMPRESSOR AIRFOILS USING PHYSICS-BASED DIRECT MANIPULATED FFD | ICAS2026_0768 |
| Orchard, D. | WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH | ICAS2026_0438 |
| Orgiu, A. | ENDURANCE EVALUATION OF DIFFERENT UAV CONFIGURATIONS AND POWERTRAIN ARCHITECTURES | ICAS2026_0636 |
| Orlando, C. | HRV BASED PILOTS WORKLOAD PREDICTION FOR AN INTELLIGENT COCKPIT WARNING SYSTEM | ICAS2026_0422 |
| Ortiz, R. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Oshman, Y. | ROBUST ESTIMATION-AWARE GUIDANCE FOR STOCHASTIC INTERCEPTION WITH PARAMETRIC UNCERTAINTY | ICAS2026_0123 |
| Otomo, S. | EXPERIMENTAL STUDY OF LOAD ALLEVIATION WITH PASSIVE ADAPTIVE CAMBER AIRFOILS | ICAS2026_0730 |
| Ott, L. | TETHERED HOVER FLIGHT TESTS OF BASELINE CONTROL LAWS FOR A TANDEM TILT-WING SUB-SCALE DEMONSTRATOR | ICAS2026_0404 |
| Otten, T. | MODULAR JET AND PROPELLER ENGINE – PART I: INITIAL STUDIES | ICAS2026_0813 |
| Otten, T. | MODULAR JET AND PROPELLER ENGINE – PART II: INTEGRATED DESIGN PROCESS AND DESIGN SPACE ASSESSMENT | ICAS2026_0829 |
| Oyama, A. | SUPERIOR CRUISE EFFICIENCY OF A NOVEL EVTOL CONFIGURATION FEATURING INCLINED PROPELLERS AND A PARASOL WING | ICAS2026_0238 |
| Ozcakir, O.M. | A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. | ICAS2026_0041 |
| Ozoroski, T.A. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Pacaux-Lemoine, M.-P. | MULTI-STATE FLIGHT DECK DISPLAY LAYOUT OPTIMIZATION UNDER FAILURE AND REVERSION CONDITIONS | ICAS2026_0604 |
| Pagano, A. | REAL-TIME EMULATION TESTBENCH FOR FUEL-CELL/BATTERY HYBRIDIZATION IN HYDROGEN-ELECTRIC AVIATION | ICAS2026_0338 |
| Pagwiwoko, C. | DESIGN ASSESSMENT OF A HELICOPTER BLADE | ICAS2026_0225 |
| Paillard, C. | EPSILON V4: AN OPEN-SOURCE TOOL FOR EXTENDED AERODYNAMICS EXERGY ANALYSIS | ICAS2026_0654 |
| Pak, F. | AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES | ICAS2026_0954 |
| Palaia, G. | ASSESSMENT OF LIQUID HYDROGEN-POWERED AIRCRAFT RANGE: A NOVEL BREGUET FORMULATION | ICAS2026_0285 |
| Palaia, G. | AN INTEGRATED CONCEPTUAL DESIGN WORKFLOW FOR LIQUID HYDROGEN-POWERED BOX-WING AIRCRAFT | ICAS2026_0400 |
| Palaia, G. | IGNIT3: AN INTEGRATED COMPUTATIONAL FRAMEWORK FOR NON-IDEAL THERMODYNAMIC ANALYSIS AND OPTIMIZATION OF TURBOJET AND TURBOFAN ENGINES | ICAS2026_0426 |
| Palaia, G. | LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY | ICAS2026_0643 |
| Palar, P.S. | OPTIMAL CONCEPTUAL DESIGN AND UPGRADE STRATEGIES FOR EVTOL AIRCRAFT UNDER EVOLVING TECHNOLOGIES | ICAS2026_0631 |
| Palm, F. | ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS | ICAS2026_1005 |
| Palma, D. | UNCERTAINTY QUANTIFICATION AND CROSS-CORRELATION EFFECTS IN AERODYNAMIC COEFFICIENTS DERIVED QUANTITIES | ICAS2026_0281 |
| Palma, D. | BUFFETING SCALE EFFECTS ON A LAUNCH VEHICLE: HYBRID RANS-LES ANALYSIS | ICAS2026_0282 |
| Palma, D. | MULTI-OBJECTIVE SHAPE OPTIMIZATION OF A LAUNCH VEHICLE FAIRING ACROSS MULTIPLE FLOW REGIMES | ICAS2026_0284 |
| Palmer, J.L. | VORTEX TOPOLOGY AND CORE-UNWINDING MECHANISM IN SPIROID WINGTIP DEVICES USING LAGRANGIAN PARTICLE TRACKING | ICAS2026_0162 |
| Palmer, J.L. | AIRBRAKES CONTROL SYSTEM FOR PRECISE APOGEE CONTROL OF A SOUNDING ROCKET | ICAS2026_0843 |
| Palmer, J.L. | IMPLICATIONS OF AAM OPERATIONS FOR FUTURE SHARED AIRSPACE IN VICTORIA, AUSTRALIA | ICAS2026_1083 |
| Palop, H. | APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS | ICAS2026_0359 |
| Palop, H. | AI IN THE COCKPIT: THE JARVIS STORY | ICAS2026_0547 |
| Pan, J. | MECHANISM-DATA FUSION MODELING METHOD FOR AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEMS | ICAS2026_0961 |
| Pan, Y. | CRITICAL LOAD-CASE AND CONSTRAINT IDENTIFICATION FOR PRELIMINARY COMPOSITE WING SIZING USING RAPID DESIGN TOOLS | ICAS2026_0628 |
| Panchal, P. | HARDWARE-IN-THE-LOOP VERIFICATION OF A SAFETY-CRITICAL RECONFIGURABLE BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIRCRAFT | ICAS2026_0557 |
| Panchal, P. | RECONFIGURABLE MULTILEVEL BATTERY ARCHITECTURE FOR SMALL UAV PROPULSION SYSTEMS | ICAS2026_0684 |
| Panchal, P. | ANALYSIS OF SOFTWARE DEVELOPMENT METHODS FOR A RECONFIGURABLE BATTERY SYSTEM FOR USE IN AN ELECTRIC AIRCRAFT | ICAS2026_0957 |
| Panel, 1 | PANEL DISCUSSION | ICAS2026_1038 |
| Panel, P | PANEL DISCUSSION Q&A WITH THE AIRLINES | ICAS2026_1028 |
| Panel, P | PANEL DISCUSSION Q&A WITH THE AIRCRAFT OEMS | ICAS2026_1029 |
| Panel, P | PANEL DISCUSSION Q&A WITH THE SPEAKERS | ICAS2026_1031 |
| Panel, P | PANEL DISCUSSION Q&A WITH THE SPEAKERS | ICAS2026_1032 |
| Panel, P. | PANEL DISCUSSION (TIL END OF THE BLOCK) | ICAS2026_1077 |
| Panel, P.D. | PANEL DISCUSSION | ICAS2026_1104 |
| Pant, R.S. | DESIGN AND TESTING OF A BUOYANT UAV FOR AGRICULTURAL SURVEILLANCE | ICAS2026_0594 |
| Pant, R.S. | PRELIMINARY SIZING METHODOLOGY FOR HYBRID-ELECTRIC PROPULSION SYSTEM IN CARGO AIRSHIPS | ICAS2026_0688 |
| Pant, R.S. | SIZING OF LINEAR ACTUATORS FOR SPAN EXTENSION OF HALE UAV | ICAS2026_0807 |
| Pant, R.S. | LIMITED HORIZON AIRLINE SCHEDULING USING GREY THEORY AND GRASP FRAMEWORK | ICAS2026_0816 |
| Pant, R.S. | OPTIMISATION OF OPERATING RADII FOR DRONE WAREHOUSES | ICAS2026_0900 |
| Panta, J. | FEMTOSECOND LASER PAINT STRIPPING ON AIRCRAFT COATINGS: EXPERIMENTAL AND NUMERICAL ASSESSMENT | ICAS2026_0159 |
| Pantelakis, S. | TOWARDS INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES: INSPECTABILITY ASSESSMENT OF HAT-STIFFENED PANELS | ICAS2026_0914 |
| Pantelakis, S. | AI-ASSISTED DESIGN OF HOLISTICALLY SUSTAINABLE AEROSTRUCTURES | ICAS2026_0975 |
| Pantelas, P. | VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS | ICAS2026_0336 |
| Paolillo, G. | AIRFOIL DESIGN OPTIMIZATION FOR HIGH-LIFT AND HIGH-EFFICIENCY APPLICATIONS USING DEEP REINFORCEMENT LEARNING | ICAS2026_0546 |
| Papenfuss, A. | EXPLAINABILITY AT ALL LEVELS OF SYSTEM DEVELOPMENT: INSIGHTS FROM THE DESIGN OF INTELLIGENT SYSTEMS IN AVIATION | ICAS2026_0177 |
| Papenfuß, A. | ASSESSING AN ALTERNATE AIRPORT ASSISTANT | ICAS2026_0192 |
| Parello, R. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Parisot-Dupuis, H. | STUDY OF THE FEASIBILITY OF ACOUSTIC LINERS INSIDE THE BEAM THAT INTERACTS WITH A UAV DRONE ROTOR | ICAS2026_0743 |
| Park, H | FEASIBILITY OF ELECTROPULSING-INDUCED FATIGUE CRACK CLOSURE IN AEROSPACE METALLIC MATERIALS | ICAS2026_0365 |
| Park, H.U. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Park, M. | INFORMATIVE PATH PLANNING BASED ON REDUCED-RANK GAUSSIAN PROCESS FOR HAZARDOUS SUBSTANCE MONITORING | ICAS2026_0513 |
| Park, S. | DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+ | ICAS2026_0130 |
| Parra, F. | ACCURACY AND EFFICIENCY OF TRANSITION–TURBULENCE MODELS IN PREDICTING HIGH AND LOW REYNOLDS NUMBER PROPELLER PERFORMANCE | ICAS2026_0226 |
| Parra, F. | EXPERIMENTAL INVESTIGATION OF WISHBONE VORTEX GENERATOR EFFECTS ON THE NACA 4412 AIRFOIL AT LOW REYNOLDS NUMBERS | ICAS2026_0232 |
| Pascarella, D. | AI IN AVIATION CYBERSECURITY RISK ASSESSMENT: OPPORTUNITIES AND CHALLENGES | ICAS2026_1009 |
| Pasquale, D. | COMPARING DIFFERENT SEMI-EMPIRICAL AERODYNAMIC TOOLS FOR ANALYSING NOVEL AIRCRAFT CONFIGURATIONS | ICAS2026_0445 |
| Passoni, R. | IMPACT TOLERANCE OF DRILLED THICK C/SIC CERAMIC MATRIX COMPOSITES | ICAS2026_0357 |
| Pastor Muro, A. | ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS | ICAS2026_1005 |
| Pate, S. | DESIGN AND DEVELOPMENT OF A BLENDED WING BODY CONCEPT USING AUGMENTED INTELLIGENCE FOR SYSTEMS ENGINEERING | ICAS2026_1042 |
| Paul, T.S. | TOWARDS THE INTEGRATION OF NEUROPHYSIOLOGICAL SIGNALS AND HUMAN BODY DYNAMICS FOR ADAPTIVE CONTROL ALLOCATION | ICAS2026_0363 |
| Pei, Y. | SEMI-SUPERVISED MULTI-TASK CONSISTENCY LEARNING FOR DEFECT DETECTION AND DEPTH ESTIMATION | ICAS2026_0072 |
| Peleshok, I. | PHASE-SPECIFIC SEMI-EMPIRICAL AEROACOUSTIC NOISE MODELING OF A CARGO EVTOL UAV WITH CONSIDERATION OF A SIMPLIFIED URBAN FLYOVER CASE | ICAS2026_0828 |
| Pelosi, M. | DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS | ICAS2026_0250 |
| Peng, Y.-H. | DEEP LEARNING-BASED INVERSION OF NEAR-FIELD OVERPRESSURE SIGNATURES FOR LOW-BOOM SUPERSONIC TRANSPORT | ICAS2026_0278 |
| Pennino, R. | EXPERIMENTAL VALIDATION OF A FUEL CELL SYSTEM DIGITAL TWIN FOR A FULL-ELECTRIC AIRCRAFT POWERTRAIN | ICAS2026_0303 |
| Pepper, C.A. | A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. | ICAS2026_0041 |
| Perez, R. | THE CONFERENCE LOCATIONS: A QUANTITATIVE APPROACH TO REDUCING IMPACT GLOBAL TRAVEL | ICAS2026_0607 |
| Perez Fuentes, F. | TOWARDS AN ECOSYSTEM FOR AERONAUTICAL RESEARCH IN MEXICO | ICAS2026_0639 |
| Perra, U. | AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES | ICAS2026_0954 |
| Persechino, G. | MULTIDISCIPLINARY APPROACH FOR THE AERODYNAMIC CHARACTERIZATION OF AN INFLATABLE CLOSED-WING HYBRID HIGH-ALTITUDE PSEUDO-SATELLITE | ICAS2026_0371 |
| Perz, R. | MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS | ICAS2026_0143 |
| Peter, J. | GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION | ICAS2026_1011 |
| Petersen, S. | ASSESSING AN ALTERNATE AIRPORT ASSISTANT | ICAS2026_0192 |
| Peterson, D. | EXPERIENCES CERTIFYING INNOVATIVE VEHICLES IN AUSTRALIA | ICAS2026_1106 |
| Petersson, Ö. | HIGH-FIDELITY DATASET-BASED SHAPE AND STRUCTURE OPTIMIZATION FOR AIRCRAFT DESIGN | ICAS2026_0042 |
| Petrillo, A. | MULTI-OBJECTIVE SHAPE OPTIMIZATION OF A LAUNCH VEHICLE FAIRING ACROSS MULTIPLE FLOW REGIMES | ICAS2026_0284 |
| Peukert, M. | UNCERTAINTY ANALYSIS AND EYE-TRACKING-BASED CLUSTERING IN AIR TRAFFIC CONTROLLER WORKLOAD PREDICTION | ICAS2026_0118 |
| Pezzella, G. | NUMERICAL REBUILDING OF AERODYNAMIC WIND TUNNEL ANALYSES OF A CREW RETURN VEHICLE | ICAS2026_0572 |
| Pfeifer, S. | AN INTEGRATED SYSTEM-LEVEL AND MULTIPHYSICS APPROACH FOR AIRCRAFT LH2 FUEL SYSTEM DESIGN | ICAS2026_0316 |
| Pfeifer, S. | MODAL-BASED FUEL LEVEL ESTIMATION OF CRYOGENIC PROPELLANT TANKS | ICAS2026_0663 |
| Pflueger Tejero, P. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Pham, A.C. | PARAMETRIC DESIGN AND MULTI-OBJECTIVE OPTIMIZATION OF EXHAUST NOZZLE FOR GAS TURBINE ENGINES | ICAS2026_0579 |
| Pham, C.A. | A HYBRID 0D–2D WHOLE-ENGINE MATCHING FRAMEWORK FOR TURBOJET ENGINE PERFORMANCE SIMULATION | ICAS2026_0687 |
| Pham, Q.-V. | A RELIABLE AND COST-EFFICIENT DATA ACQUISITION SYSTEM FOR MIL-HDBK-1763-COMPLIANT STATIC EJECTION TESTING OF AIRCRAFT EXTERNAL STORES | ICAS2026_0170 |
| Pham, T.A. | A HYBRID 0D–2D WHOLE-ENGINE MATCHING FRAMEWORK FOR TURBOJET ENGINE PERFORMANCE SIMULATION | ICAS2026_0687 |
| Phan, N. | HIGH-FIDELITY ANALYSIS OF AIRCRAFT TAIL BUFFETING UNDER DYNAMIC MANEUVERING | ICAS2026_0927 |
| Phan, N. | A PROCESS-STRUCTURE-PROPERTY-PERFORMANCE FRAMEWORK FOR DIGITAL ENGINEERING-ENABLED REPAIR OF ALUMINUM PARTS | ICAS2026_0940 |
| Phillips, B.D. | A BENCHMARK FOR UNCERTAINTY QUANTIFICATION AND OPTIMIZATION UNDER UNCERTAINTY IN CONCEPTUAL AIRCRAFT DESIGN: THE F25-OUU CHALLENGE PROBLEM | ICAS2026_0320 |
| Picanço, P.H.C. | STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR IMPACT RESPONSE FOR LIGHTWEIGHT FIXED-WING UAVS | ICAS2026_0833 |
| Pinjala, L. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Pinon-Fischer, O. | BEYOND AI HYPE: TRUST, EVALUATION, AND HUMAN JUDGEMENT IN AEROSPACE ENGINEERING | ICAS2026_1043 |
| Pinon-Fischer, O. | DIGITAL ENGINEERING FOR TRANSFORMATIVE AEROSPACE | ICAS2026_1088 |
| Piovesan, T. | MIDAS: A MODULAR SOFTWARE FOR INTAKE FLOW DISTORTION ANALYSIS | ICAS2026_0705 |
| Pirillo, L. | UNCERTAINTY QUANTIFICATION AND CROSS-CORRELATION EFFECTS IN AERODYNAMIC COEFFICIENTS DERIVED QUANTITIES | ICAS2026_0281 |
| Pirillo, L. | BUFFETING SCALE EFFECTS ON A LAUNCH VEHICLE: HYBRID RANS-LES ANALYSIS | ICAS2026_0282 |
| Pirillo, L. | MULTI-OBJECTIVE SHAPE OPTIMIZATION OF A LAUNCH VEHICLE FAIRING ACROSS MULTIPLE FLOW REGIMES | ICAS2026_0284 |
| Piscopo, G. | MULTIDISCIPLINARY DESIGN EXPLORATION OF HYBRID-ELECTRIC REGIONAL AIRCRAFT | ICAS2026_0360 |
| Piskur, P. | WATER TUNNEL EXPERIMENTS AND CFD ANALYSES OF A COMBAT AIRCRAFT WITH LEADING-EDGE VORTEX CONTROLLERS | ICAS2026_0763 |
| Piskur, P. | EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY | ICAS2026_0789 |
| Pitarque, R. | NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT | ICAS2026_0216 |
| Platzer, M.F. | INTERACTION OF COUNTER-PLUNGING BIPLANE AIRFOILS WITH A FLAT PLATE BOUNDARY LAYER AND WAKE | ICAS2026_0655 |
| Platzer, M.F. | THREE-DIMENSIONAL FLOW STRUCTURES OVER A LOW-ASPECT-RATIO PLUNGING WING | ICAS2026_0916 |
| Polishchuk, T. | UNCERTAINTY ANALYSIS AND EYE-TRACKING-BASED CLUSTERING IN AIR TRAFFIC CONTROLLER WORKLOAD PREDICTION | ICAS2026_0118 |
| Polishchuk, T. | AIRSPACE CAPACITY IMPLICATIONS OF CONTRAIL-AWARE TRAJECTORY OPTIMIZATION | ICAS2026_0224 |
| Poltronieri, G.M. | A STUDY ON THE CELL REYNOLDS NUMBER AS A PARAMETER FOR MESH QUALITY ON HYPERSONIC FLOWS | ICAS2026_0065 |
| Pommier-Budinger, V. | A MPC–MHE STRATEGY FOR FREQUENCY TRACKING AND PARAMETERS ESTIMATION OF RESONANT DE-ICING SYSTEMS | ICAS2026_0660 |
| Pop, M. | ARCHITECTED LATTICE SANDWICH STRUCTURES FOR LIGHTWEIGHT IMPACT AND ENERGY ABSORPTION APPLICATIONS | ICAS2026_0053 |
| Porfido, N.J. | EVALUATING THE LAMINAR FLOW ON A SLOTTED, NATURAL-LAMINAR-FLOW WING IN THE NASA AMES 11-FOOT TRANSONIC WIND TUNNEL | ICAS2026_0472 |
| Porter, J. | THE ROLE OF COMMUNITY ENGAGEMENT IN INTRODUCING UNMANNED AERIAL VEHICLE TECHNOLOGY: A RAPID SCOPING REVIEW | ICAS2026_1017 |
| Pothin, J. | A MPC–MHE STRATEGY FOR FREQUENCY TRACKING AND PARAMETERS ESTIMATION OF RESONANT DE-ICING SYSTEMS | ICAS2026_0660 |
| Pradyumna, N. | TOROIDAL RECIRCULATION, SADDLE-POINT TOPOLOGY, AND WALL-JET OUTWASH IN A TWIN-ROTOR SYSTEM IN GROUND EFFECT | ICAS2026_0804 |
| Prakash, T. | SIZING OF LINEAR ACTUATORS FOR SPAN EXTENSION OF HALE UAV | ICAS2026_0807 |
| Prakasha, P. | DIGITAL ENGINEERING IN THE AGE OF AI AS BASIS FOR SYSTEM OF SYSTEMS ENGINEERING | ICAS2026_1108 |
| Priasso, V. | AIRCRAFT MASS EVALUATION MODEL: FROM TUBE-AND-WING TO BLENDED WING BODY USING WHALE. | ICAS2026_0211 |
| Priasso, V. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Prince, S. | STATIC AND DYNAMIC WIND-TUNNEL TESTING OF A TRANSPORT AIRCRAFT MODEL IN-STALL AND POST-STALL FLIGHT REGIMES | ICAS2026_0203 |
| Prince, S. | NUMERICAL INVESTIGATION OF SHOCKWAVE TURBULENT BOUNDARY LAYER INTERACTION AT MACH 2.5 OVER A COMPRESSION RAMP | ICAS2026_0550 |
| Prince, S. | MODELLING SENSITIVITIES IN THREE-DIMENSIONAL FZRA-SPECTRUM ICE-SHAPE PREDICTION FOR THE CRM-HL STOWED CONFIGURATION | ICAS2026_0896 |
| Prince, S. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Prince, S.A. | NUMERICAL BOUNDARY LAYER VALIDATION TECHNIQUE USING RAE M2155 SWEPT WING | ICAS2026_0283 |
| Prince, S.A. | PROPOSAL FOR DISTINGUISHING USABLE DATA UNDER HIGH WIND TUNNEL BLOCKAGE USING AN RAE2822 TEST CASE | ICAS2026_0592 |
| Proenca, A. | STATIC AND DYNAMIC WIND-TUNNEL TESTING OF A TRANSPORT AIRCRAFT MODEL IN-STALL AND POST-STALL FLIGHT REGIMES | ICAS2026_0203 |
| Proskurov, S. | NUMERICAL PREDICTION OF CABIN NOISE FOR FUTURE SHORT-HAUL AIRCRAFT IN EARLY AIRCRAFT DESIGN | ICAS2026_0364 |
| Prpic, J. | RE-THINKING END OF LIFE AIRCRAFT INTERIORS THROUGH CO-DESIGN AND REPURPOSING | ICAS2026_0840 |
| Pruter, I. | FLIGHT OPERATIONS AND TESTING OF A 450 KG EXPERIMENTAL GYROPLANE UAV | ICAS2026_0331 |
| Pruter, I. | IMPACT OF SYSTEM LATENCIES ON PILOT INTERACTION AND HANDLING OF AN ELECTRICALLY POWERED GYROPLANE UAV WITH FPV-BASED REMOTE CONTROL | ICAS2026_0335 |
| Pusztai, D. | EVALUATION OF STALL BEHAVIOUR OF T-TAIL AIRCRAFT: MODELLING AND FLIGHT TEST | ICAS2026_0518 |
| Putra, S. | A WORKFLOW FOR RAPID DESIGN, SIMULATION, FABRICATION, AND SUBSCALE FLIGHT-TESTING OF NOVEL AIRCRAFT CONCEPTS | ICAS2026_0845 |
| Putra, S. | SIMULATION MODEL CALIBRATION USING SYSTEM IDENTIFICATION FOR A VECTORED-THRUST MULTI-TILT-ROTOR CONFIGURATION | ICAS2026_0929 |
| Pywell, S. | FLIGHT TRIALS OF DRONES CONTROLLED BY AI LARGE LANGUAGE MODELS | ICAS2026_0156 |
| Q, &A | PANEL DISCUSSION AND Q&A | ICAS2026_1048 |
| Q, 1 | PANEL DISCUSSION AND Q&A | ICAS2026_1047 |
| Qian, W. | MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY | ICAS2026_0566 |
| Qian, W. | A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY | ICAS2026_0627 |
| Qiao, K. | FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES | ICAS2026_0171 |
| Qiao, L. | QUASI-STEADY AERODYNAMIC AND MBD COUPLED FLIGHT SIMULATION OF FOLDING MORPHING UAV | ICAS2026_0237 |
| Qiao, M. | INTELLIGENT FULL-ENVELOPE OPTIMIZATION OF TRANSIENT CONTROL LAWS FOR ADAPTIVE CYCLE ENGINES VIA TRANSFER LEARNING-ENHANCED DEEP REINFORCEMENT LEARNING | ICAS2026_0584 |
| Qin, Y. | FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES | ICAS2026_0171 |
| Qu, H.L. | MECHANISM-DATA FUSION MODELING METHOD FOR AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEMS | ICAS2026_0961 |
| Qu, Q. | STATIC GROUND EFFECT OF HIGH-ASPECT-RATIO WINGS | ICAS2026_0295 |
| Qu, Q.L. | SUPERSONIC GROUND EFFECT AERODYNAMICS OF A SLENDER BODY | ICAS2026_0598 |
| Qu, Y. | PHYSICS-INFORMED NEURAL NETWORK BASED MODELING OF DYNAMIC BEHAVIOR OF AERIAL REFUELING HOSE | ICAS2026_0109 |
| Quagliarella, D. | NUMERICAL REBUILDING OF AERODYNAMIC WIND TUNNEL ANALYSES OF A CREW RETURN VEHICLE | ICAS2026_0572 |
| Quagliarella, D. | GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION | ICAS2026_1011 |
| Quaranta, G. | VERTIPORT FINAL APPROACH AND TAKEOFF AREA ORIENTATION IDENTIFICATION USING COUPLED MICROSCALE WIND AND FLIGHT DYNAMICS ANALYSIS | ICAS2026_0150 |
| Quarta, A.A. | ASSESSMENT OF LIQUID HYDROGEN-POWERED AIRCRAFT RANGE: A NOVEL BREGUET FORMULATION | ICAS2026_0285 |
| Quarta, A.A. | AN INTEGRATED CONCEPTUAL DESIGN WORKFLOW FOR LIQUID HYDROGEN-POWERED BOX-WING AIRCRAFT | ICAS2026_0400 |
| Queiroz, S. | VLSEC: A CONCEPT FOR SECURING VIRTUAL LINKS IN AVIONICS NETWORKS THROUGH CENTRALIZED GROUP KEY MANAGEMENT | ICAS2026_0701 |
| Quix, H. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| R. de Oliveira, W. | A FORMALLY VERIFIED, EVENT-DRIVEN ROS SCADA SUPERVISORY SYSTEM ARCHITECTURE FOR SAFETY-CRITICAL ROBOTIC CELLS IN AEROSPACE MANUFACTURING | ICAS2026_0945 |
| R. O. A. Maximo, M. | A SEMI-AUTONOMOUS DECISION SUPPORT TOOL FOR ATC IN EN-ROUTE REROUTING OPERATIONS | ICAS2026_0947 |
| Rabiega, M. | ENABLING HIGH RATE COMPOSITE MANUFACTURING THROUGH A ROBUST MANUFACTURING DIGITAL ECOSYSTEM | ICAS2026_0966 |
| Raddatz, F. | PHYSICS-INFORMED NEURAL NETWORKS FOR ULTRASONIC LAMB WAVE RECONSTRUCTION IN NON-DESTRUCTIVE TESTING | ICAS2026_0573 |
| Raddatz, F. | ONTOLOGY-BASED SENSOR HEALTH MONITORING: A DYNAMIC ONTOLOGY-BASED FAULT DETECTION AND CLASSIFICATION FOR TIMESERIES DATA | ICAS2026_0716 |
| Rade, D. | A SIMULATION METHODOLOGY FOR MULTIROTOR-ASSISTED UAV LAUNCH | ICAS2026_0937 |
| Rade, D.A. | A QUALITATIVE FRAMEWORK FOR AIRCRAFT WING MANUFACTURING AND DECISION MAKING | ICAS2026_0766 |
| Rade, D.A. | PREDICTION OF STRUCTURAL VIBRATIONS INDUCED BY MASS-UNBALANCED ELECTRIC PROPULSION SYSTEMS | ICAS2026_0901 |
| Railean, N. | GROUND-EFFECT ANALYSIS OF SMALL DUCTED PROPELLERS: A NUMERICAL–EXPERIMENTAL STUDY | ICAS2026_0456 |
| Raiola, M. | AN INCREMENTAL MODULAR MDO FRAMEWORK FOR HYDROGEN-ELECTRIC POWERTRAIN SIZING AND INTEGRATION IN GENERAL AVIATION AIRCRAFT | ICAS2026_0876 |
| Raj, P. | PREPARING AERONAUTICAL ENGINEERING UNDERGRADUATES FOR WORKING IN GLOBAL TEAMS | ICAS2026_0453 |
| Rajanna, M.R. | HIGH-FIDELITY ANALYSIS OF AIRCRAFT TAIL BUFFETING UNDER DYNAMIC MANEUVERING | ICAS2026_0927 |
| Rajanna, M.R. | A PROCESS-STRUCTURE-PROPERTY-PERFORMANCE FRAMEWORK FOR DIGITAL ENGINEERING-ENABLED REPAIR OF ALUMINUM PARTS | ICAS2026_0940 |
| Rajeepan, D.T. | ANALYSIS OF A DUAL AIR DATA AND MULTI-HOLE PRESSURE PROBE BOOM | ICAS2026_0775 |
| Rajek, M. | RECENT ADVANCES IN AEROACOUSTIC DESIGN OF ADVANCED AIR MOBILITY VEHICLES | ICAS2026_0964 |
| Rak, M. | AI IN AVIATION CYBERSECURITY RISK ASSESSMENT: OPPORTUNITIES AND CHALLENGES | ICAS2026_1009 |
| Ramotsabi, K. | REFLECTIONS ON THE AEROSPACE ENGINEERING DEVELOPMENT PROGRAMME AT THE CSIR | ICAS2026_0549 |
| Ramprakash, T.A. | IMPLEMENTATION OF PROPELLER-WING INTERFERENCE MODEL AND HORIZONTAL TAIL ANALYSIS INTO A VISCOUS FULL POTENTIAL FLOW SOLVER FRAMEWORK FOR AIRCRAFT DESIGN | ICAS2026_0915 |
| Ran, X. | A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY | ICAS2026_0627 |
| Rana, Z.A. | NUMERICAL INVESTIGATION OF SHOCKWAVE TURBULENT BOUNDARY LAYER INTERACTION AT MACH 2.5 OVER A COMPRESSION RAMP | ICAS2026_0550 |
| Rancourt, D. | DESIGN AND OPERATION OF LOW-COST MULTI-SCALE TEST BEDS FOR BATTERY THERMAL RUNAWAY INITIATION AND PROPAGATION | ICAS2026_0030 |
| Rancourt, D. | EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION | ICAS2026_0673 |
| Rao, G. | BLI/PROPULSION STUDIES AT TU DELFT (PART I) | ICAS2026_1061 |
| Rao, G. | BLI/PROPULSION STUDIES AT TU DELFT (PART II) | ICAS2026_1062 |
| Rao, S. | TOWARDS MULTI-DISCIPLINARY OPTIMIZATION OF A GENERIC HYPERSONIC VEHICLE – AN OVERVIEW OF RESEARCH AT LHSR, IISC | ICAS2026_1068 |
| RAPISARDA, Andrea | HIGH-FIDELITY NUMERICAL INVESTIGATION OF ROTOR-WING INTERACTIONS IN A MULTI-ROTOR DISTRIBUTED ELECTRIC PROPULSION CONFIGURATION | ICAS2026_0678 |
| Raptis, N. | TOWARDS INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES: INSPECTABILITY ASSESSMENT OF HAT-STIFFENED PANELS | ICAS2026_0914 |
| Rashidi, T.H. | CLIMATE HAZARD TIMING AND FLIGHT DEMAND COOCCURRENCE: A DEMAND-WEIGHTED EXPOSURE FRAMEWORK | ICAS2026_0870 |
| Rasines Mazo, J. | COMMON RESEARCH MODELS FOR SMALL UNCREWED AERIAL VEHICLES | ICAS2026_0801 |
| Ravandi, M. | HIGH-RATE AUTOMATED STAMP FORMING OF CF/LM-PAEK COMPOSITES FOR NEXT-GENERATION UAV AEROSTRUCTURES | ICAS2026_0286 |
| Ravikanti, B. | LOSS OF RELIABILITY OF NEW GENERATION ENGINES: THE CASE STUDY OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION AS A SYSTEM OF SYSTEMS | ICAS2026_0822 |
| Ravikumar, K. | A COMPARATIVE WMLES STUDY OF THE CRM-HL IN FREE-AIR AND IN THE NTF FACILITY | ICAS2026_0793 |
| Redondo Torrico, N. | ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS | ICAS2026_1005 |
| Reed, H.L. | EVALUATING THE LAMINAR FLOW ON A SLOTTED, NATURAL-LAMINAR-FLOW WING IN THE NASA AMES 11-FOOT TRANSONIC WIND TUNNEL | ICAS2026_0472 |
| Reh, S. | CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING | ICAS2026_1004 |
| Rehfeld, N. | ICE DETECTION: CORRELATION OF ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES TESTED IN ICING WIND TUNNEL | ICAS2026_0186 |
| Rehfeldt, J. | OPTIMIZATION APPROACHES FOR THE SHEAR-POSTBUCKLING DESIGN OF THERMOPLASTIC THIN-PLY COMPOSITE SHELLS IN HELICOPTERS | ICAS2026_0614 |
| Rehman, T. | IMPACT RESISTANCE ENHANCEMENT IN FIBER-REINFORCED COMPOSITES USING CARBON/BASALT HYBRIDIZATION APPROACHES | ICAS2026_0885 |
| Reindle, H. | RESEARCH PLATFORM AIRSHIP: DESIGN AND FLIGHT CHARACTERISTICS FOR URBAN OPERATIONS | ICAS2026_0576 |
| Reiner, J. | EFFICIENT SIMULATION AND UNCERTAINTY QUANTIFICATION OF PROGRESSIVE CRUSHING IN COMPOSITE LAMINATES | ICAS2026_0160 |
| Reis, A. | WHO SHOULD SIT AT THE EXIT ROW? A HUMAN FACTORS APPROACH TO EMERGENCY EVACUATION PASSENGER SELECTION IN COMMERCIAL AVIATION | ICAS2026_0154 |
| Reis, J.L.C. | MODEL-BASED INTEGRATION OF FLIGHT-TEST EVIDENCE AND SEMI-EMPIRICAL PERFORMANCE MODELS: THE ACS-100 SORA LIGHT AIRCRAFT CASE STUDY | ICAS2026_0917 |
| Reis, J.L.C. | AN MBSE-ORIENTED FRAMEWORK FOR AEROSPACE SYSTEMS EDUCATION: THE CEA-UFMG LIGHT-AIRCRAFT DESIGN-BUILD-TEST TRADITION | ICAS2026_0933 |
| Reisier, A. | ACCELERATING THE LEARNING CURVE: GENERATIVE AI FOR WORKED EXAMPLES IN HUMAN FACTORS ANALYSIS | ICAS2026_0038 |
| Reitmann, S. | PROVIDING SENSOR INFORMATION FOR BOARDING TIME PREDICTION | ICAS2026_0611 |
| Rempel, M.A. | AUTOPILOT DESIGN OF AN UNSTABLE FIGHTER USING MODEL PREDICTIVE CONTROL | ICAS2026_0791 |
| Ren, Y.L. | AUTOMATIC GENERATION OF PHYSICAL SYSTEM MODELS FOR AIRCRAFT SYSTEMS BASED ON LLMS | ICAS2026_0479 |
| Renault, J. | LATERAL-DIRECTIONAL HANDLING AND FLYING QUALITIES ASSESSMENT OF A BLENDED WING BODY (BWB) ACFA 2020 CONFIGURATION | ICAS2026_0630 |
| Reyner, C. | OPTIMAL CONCEPTUAL DESIGN AND UPGRADE STRATEGIES FOR EVTOL AIRCRAFT UNDER EVOLVING TECHNOLOGIES | ICAS2026_0631 |
| Reynolds, A.-A. | EXPERIMENTAL INVESTIGATION OF BLOWING RATIO EFFECT ON FLOW REGIMES OF TRANSPIRATION COOLING IN LATTICE POROUS MEDIA | ICAS2026_0776 |
| Reynolds, C. | ENABLING HIGH RATE COMPOSITE MANUFACTURING THROUGH A ROBUST MANUFACTURING DIGITAL ECOSYSTEM | ICAS2026_0966 |
| Reynolds, T. | A COMPARISON OF TRAJECTORY-BASED OPERATIONS IN THE UNITED STATES AND EUROPE IN SUPPORT OF GLOBAL HARMONIZATION | ICAS2026_0412 |
| Reysset, A. | A MODEL PREDICTIVE CONTROL STRATEGY FOR THE ENERGY MANAGEMENT OF HYBRID ELECTRIC PROPULSION SYSTEMS IN FIXED-WING UAVS | ICAS2026_0613 |
| Reysset, A. | POWER-HIL TESTING OF LI-PO BATTERY PACKS FOR LIGHTWEIGHT EVTOL UAVS | ICAS2026_0619 |
| Reysset, A. | A MPC–MHE STRATEGY FOR FREQUENCY TRACKING AND PARAMETERS ESTIMATION OF RESONANT DE-ICING SYSTEMS | ICAS2026_0660 |
| Rezgui, D. | ENABLING FORWARD SWEPT WING DESIGNS | ICAS2026_0381 |
| Rhode, D. | AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH | ICAS2026_1015 |
| Ribolla, G.C. | COST-EFFECTIVE CFD REPRODUCTION OF DPW-7 CASE 2A FOR CRM TRANSONIC PITCHING-MOMENT PREDICTION AND ADAPTIVE-REFINEMENT ASSESSMENT | ICAS2026_0953 |
| Riccardi, G. | ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT | ICAS2026_0897 |
| Riccio, A. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Riccio, E. | MULTIDISCIPLINARY APPROACH FOR THE AERODYNAMIC CHARACTERIZATION OF AN INFLATABLE CLOSED-WING HYBRID HIGH-ALTITUDE PSEUDO-SATELLITE | ICAS2026_0371 |
| Rieger, C. | IN-FLIGHT LOW-COST THRUST MEASUREMENT SYSTEM FOR SMALL UNMANNED AERIAL VEHICLES | ICAS2026_0597 |
| Rietdijk, B. | CONCEPT OF OPERATIONS FOR A HYDROGEN-ELECTRIC POWERED MODIFIED DASH 8-300 REGIONAL AIRCRAFT: PERFORMANCE, OPERATIONAL, AND REGULATORY IMPACTS | ICAS2026_0307 |
| Riethausen, S. | A 3D-PRINTED TESTBED FOR FLIGHT CONTROL SYSTEM RESEARCH. | ICAS2026_0713 |
| Rispin, J. | COMPARING DIFFERENT SEMI-EMPIRICAL AERODYNAMIC TOOLS FOR ANALYSING NOVEL AIRCRAFT CONFIGURATIONS | ICAS2026_0445 |
| Rivers, M. | CROSS-TEST COMPARISONS AND REYNOLDS NUMBER EFFECTS IN THE CRM-HL ECOSYSTEM | ICAS2026_0844 |
| Rivers, M. | ECOSYSTEM UPDATES AND PLANS | ICAS2026_1046 |
| Rivers, M.B. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Rizk, H. | MANEUVER- AND DELAY-ROBUST DISTRIBUTED SATELLITE SSA VIA SPATIO-TEMPORAL GRAPH FORECASTING | ICAS2026_0959 |
| Rizzo, E. | LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY | ICAS2026_0643 |
| Roca, V | AIRBUS PRODUCT DEVELOPMENT - CHALLENGES AND OPPORTUNITIES IN SUSTAINABILITY | ICAS2026_1023 |
| Roco, A. | HYBRID ROCKET HOT-GAS DRIVER FOR DIRECT-CONNECT SCRAMJET THERMO-STRUCTURAL SCREENING | ICAS2026_0508 |
| Rodrigues, J. | DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS | ICAS2026_0250 |
| Rodrigues, J. | DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS (PITCH SESSION) | ICAS2026_1094 |
| Rodrigues Arnaud, L. | HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION OF WIND TURBINES USING A DISCRETE ADJOINT APPROACH | ICAS2026_0052 |
| Rodríguez Sevillano, A.A. | DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE. | ICAS2026_0427 |
| Rodríguez-Sevillano, A.A. | CFD ANALYSIS OF MMRTG THERMAL PLUME ON THE EXTERNAL AERODYNAMICS OF A MARS ROVER | ICAS2026_0054 |
| Roesing, J. | LIFE CYCLE ANALYSIS OF EMISSIONS IN AVIATION: IDENTIFIYING AND ADJUSTING FACTORS TO REDUCE CARBON EMISSIONS | ICAS2026_0451 |
| Rogers, H.B. | EVALUATION OF PERCEIVED X-15 FLYING QUALITIES BASED ON RAPID AERODYNAMIC PREDICTIONS | ICAS2026_0817 |
| Rogers, J. | NEW INSIGHTS INTO AA7085 ENVIRONMENTALLY ASSISTED CRACKING THROUGH HIGH RESOLUTION FRACTOGRAPHY | ICAS2026_0234 |
| Rogers, J. | ACCELERATED EXPERIMENTAL INVESTIGATION OF ENVIRONMENTALLY ASSISTED CRACKING IN AA7085 | ICAS2026_0244 |
| Rogers, J. | LABORATORY METHOD FOR REPLICATING FASTENER HOLE CORROSION IN AA7085 | ICAS2026_0253 |
| Romesh, A. | LOWERING THE BARRIER TO AEROACOUSTIC PREDICTION: GPU-COMPUTED SBES FOR FAR-FIELD LANDING GEAR NOISE PREDICTION | ICAS2026_1105 |
| Romo Martinez, I. | ADAPTIVE FLIGHT CONTROL LAWS APPLIED TO AIR REFUELING WITH RECEIVERS EQUIPPED WITH RECEPTACLE OUT OF THE PLANE OF SYMMETRY | ICAS2026_0011 |
| Roscher, S. | EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT | ICAS2026_0274 |
| Rosser, K. | FLIGHT TRIALS OF DRONES CONTROLLED BY AI LARGE LANGUAGE MODELS | ICAS2026_0156 |
| Roth, Y.C. | COMPOSITE FUSELAGE TECHNOLOGIES FOR NEXT GENERATION COMMERCIAL AIRCRAFT | ICAS2026_0115 |
| Rouchon, J.-F. | AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC | ICAS2026_0347 |
| Roudolff, F. | CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING | ICAS2026_1004 |
| Roudolff, F. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Rowedder, C. | COMPOSITE FUSELAGE TECHNOLOGIES FOR NEXT GENERATION COMMERCIAL AIRCRAFT | ICAS2026_0115 |
| Ruberte Bailo, J. | A LAMINAR TAILORED WING WITH CATNLF AND HLFC FOR EXTRA LONG RANGE | ICAS2026_0187 |
| Ruscio, J.P. | EXERGY AND INTEGRAL BOUNDARY LAYER PARAMETERS CHARACTERISTIC CURVES FOR AERODYNAMIC DESIGN AND OPTIMIZATION | ICAS2026_0378 |
| Russo, A. | CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING | ICAS2026_1004 |
| Rutherford, D. | AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH | ICAS2026_1015 |
| Rutili de Lima, C. | A SEMI-AUTONOMOUS DECISION SUPPORT TOOL FOR ATC IN EN-ROUTE REROUTING OPERATIONS | ICAS2026_0947 |
| Rüter, J. | DEEP LEARNING VS. TRADITIONAL COMPUTER VISION FOR UAV LANDING SITE DETECTION IN ADVERSE WEATHER | ICAS2026_0288 |
| S. Braga, F. | A FORMALLY VERIFIED, EVENT-DRIVEN ROS SCADA SUPERVISORY SYSTEM ARCHITECTURE FOR SAFETY-CRITICAL ROBOTIC CELLS IN AEROSPACE MANUFACTURING | ICAS2026_0945 |
| Saachi, F. | ENABLING FORWARD SWEPT WING DESIGNS | ICAS2026_0381 |
| Saadeh, N. | SWEEP ANGLE STUDY OF A STRUT-BRACED-WING REGIONAL JET WITH NATURAL LAMINAR FLOW | ICAS2026_0066 |
| Sadelfeld, A. | COMPOSITE FUSELAGE TECHNOLOGIES FOR NEXT GENERATION COMMERCIAL AIRCRAFT | ICAS2026_0115 |
| Sáez, R. | NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT | ICAS2026_0216 |
| Sain, C. | THERMAL–HYDRAULIC OPTIMIZATION OF AXIALLY GRADED OFFSET STRIP-FIN HEAT EXCHANGERS FOR MEGAWATT-CLASS FUEL CELL ELECTRIC AIRCRAFT | ICAS2026_0826 |
| Sain, C.K. | NUMERICAL AND EXPERIMENTAL EVALUATION OF COMPACT TPMS AND OFFSET-STRIP-FIN HEAT EXCHANGERS FOR FUEL CELL SYSTEM COOLING IN AN ELECTRIC AIRCRAFT | ICAS2026_0652 |
| Sajid, Z. | IMPACT RESISTANCE ENHANCEMENT IN FIBER-REINFORCED COMPOSITES USING CARBON/BASALT HYBRIDIZATION APPROACHES | ICAS2026_0885 |
| Sakai, F. | EFFECT OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS | ICAS2026_0517 |
| Sakata, R. | EFFECT OF MORPHOLOGICAL CHANGES ON THE AERODYNAMIC CHARACTERISTICS OF THE WING AND TAIL FEATHERS OF A TAXIDERMY BLACK-TAILED GULL | ICAS2026_0852 |
| Sakurai, T. | FLIGHT DYNAMICS AND GUIDANCE CONTROL FOR AIRCRAFT IN TYPHOON ENVIRONMENTS FOR DELIVERY OF TYPHOON CONTROL SUBSTANCE | ICAS2026_0246 |
| Sakurai, T. | DESIGN AND FEASIBILITY ASSESSMENT OF TRANSPORT OPERATIONS FOR DELIVERING TYPHOON CONTROL SUBSTANCES | ICAS2026_0247 |
| Salagaras, M. | ACCELERATED EXPERIMENTAL INVESTIGATION OF ENVIRONMENTALLY ASSISTED CRACKING IN AA7085 | ICAS2026_0244 |
| Salagaras, M. | LABORATORY METHOD FOR REPLICATING FASTENER HOLE CORROSION IN AA7085 | ICAS2026_0253 |
| Salazar, M. | AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES | ICAS2026_0954 |
| Salem, K. | IGNIT3: AN INTEGRATED COMPUTATIONAL FRAMEWORK FOR NON-IDEAL THERMODYNAMIC ANALYSIS AND OPTIMIZATION OF TURBOJET AND TURBOFAN ENGINES | ICAS2026_0426 |
| San Millán, F.J. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Sanchez Mata, A. | LOSS OF RELIABILITY OF NEW GENERATION ENGINES: THE CASE STUDY OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION AS A SYSTEM OF SYSTEMS | ICAS2026_0822 |
| Sanghi, D. | RESIDUAL LEARNING FRAMEWORK FOR NONLINEAR AEROELASTIC–FLIGHT-DYNAMICS CONTROL-ORIENTED MODELING OF VERY FLEXIBLE AIRCRAFT | ICAS2026_0664 |
| Sangkarat, P. | DEVELOPMENT OF CONDUCTIVE COMPOSITE MATERIALS FOR HIGH VOLTAGE APPLICATIONS | ICAS2026_0036 |
| Sankrithi, M. | MODELING & PRELIMINARY ANALYSIS OF AN ECOFRIENDLY AIRBORNE GLOBAL LUXURY EKRANOPLAN | ICAS2026_0055 |
| Sansica, A. | AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMI-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT THE JAXA 6.5M X 5.5M LOW SPEED WIND TUNNEL | ICAS2026_0256 |
| Santer, M. | AERO-THERMO-STRUCTURAL OPTIMIZATION OF INTEGRATED THERMAL PROTECTION SYSTEMS | ICAS2026_1069 |
| Santos, E.J.T. | STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR IMPACT RESPONSE FOR LIGHTWEIGHT FIXED-WING UAVS | ICAS2026_0833 |
| Santos Alencar, R. | WHO SHOULD SIT AT THE EXIT ROW? A HUMAN FACTORS APPROACH TO EMERGENCY EVACUATION PASSENGER SELECTION IN COMMERCIAL AVIATION | ICAS2026_0154 |
| Sanz De Blas, A. | ADAPTIVE FLIGHT CONTROL LAWS APPLIED TO AIR REFUELING WITH RECEIVERS EQUIPPED WITH RECEPTACLE OUT OF THE PLANE OF SYMMETRY | ICAS2026_0011 |
| Saravanan, P. | SUBSCALE FLIGHT TRAINING EFFECTS ON PILOT WORKLOAD AND PERFORMANCE DURING VTOL HQTES | ICAS2026_0685 |
| Sarmento, A.G.P. | METHODOLOGY AND V1 PROTOTYPE OF AN ADAPTIVE/ADAPTABLE MULTI-UAV GCS HMI IN A FLOOD SAR CO-SIMULATION TESTBED | ICAS2026_0932 |
| Sarmento, A.G.P. | A SIMULATION METHODOLOGY FOR MULTIROTOR-ASSISTED UAV LAUNCH | ICAS2026_0937 |
| Sasaki, D. | PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN | ICAS2026_0370 |
| Sasaki, D. | UNSTEADY AERODYNAMIC OPTIMIZATION OF A THIN ANGULAR AIRFOIL USING CARTESIAN MESH CFD WITH THE LEVEL SET METHOD | ICAS2026_0767 |
| Sasaki, D. | INITIAL GEOMETRIC UNCERTAINTY ASSESSMENT IN COMPRESSOR AIRFOILS USING PHYSICS-BASED DIRECT MANIPULATED FFD | ICAS2026_0768 |
| Sasaki, Y. | DYNAMIC ANALYSES AND FLIGHT TESTING FOR THE DESIGN OF FLOATING CANARD AIRCRAFT | ICAS2026_0346 |
| Saska, M. | DECOUPLED DEEP REINFORCEMENT LEARNING FOR AUTONOMOUS LANDING OF UAVS ON SHIPS | ICAS2026_0867 |
| Sathya Kumar, P. | SIMULATION-BASED EVALUATION OF SIGNALISED INTERSECTIONS FOR EMERGENCY SAFETY LANDINGS IN URBAN AIR MOBILITY | ICAS2026_0325 |
| Sato, M. | SUPERIOR CRUISE EFFICIENCY OF A NOVEL EVTOL CONFIGURATION FEATURING INCLINED PROPELLERS AND A PARASOL WING | ICAS2026_0238 |
| Sato, T. | MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) | ICAS2026_1074 |
| Sawaki, Y. | NEW TEST RESULTS OF THE 3.23% FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2026_0328 |
| Sawalhi, N. | CYCLOSTATIONARY ANALYSIS AND UNSUPERVISED CLUSTERING FOR DETECTING CRACKS IN HELICOPTER GEARBOX CASING | ICAS2026_1111 |
| Scardigli, A. | GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION | ICAS2026_1011 |
| Scavella, P. | AIRFOIL DESIGN OPTIMIZATION FOR HIGH-LIFT AND HIGH-EFFICIENCY APPLICATIONS USING DEEP REINFORCEMENT LEARNING | ICAS2026_0546 |
| Schaefer, J.A. | A BENCHMARK FOR UNCERTAINTY QUANTIFICATION AND OPTIMIZATION UNDER UNCERTAINTY IN CONCEPTUAL AIRCRAFT DESIGN: THE F25-OUU CHALLENGE PROBLEM | ICAS2026_0320 |
| Schaefer, J.A. | PROGRESS TOWARDS AIRCRAFT CERTIFICATION BY ANALYSIS WITHIN THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTIC | ICAS2026_1053 |
| Schaper, M. | EVALUATING HUMAN-MACHINE-TEAMING CONCEPTS FOR A HIGHLY AUTOMATED GROUND CONTROLLER WORKING POSITION | ICAS2026_0302 |
| Schatrow, P. | ADVANCED MODELING AND ANALYSIS OF A LIQUID HYDROGEN SHORT-MEDIUM RANGE AIRCRAFT CONCEPT FOR 2035 | ICAS2026_0333 |
| Schlautmann, N. | RESEARCH PLATFORM AIRSHIP: DESIGN AND FLIGHT CHARACTERISTICS FOR URBAN OPERATIONS | ICAS2026_0576 |
| Schlickenmaier, H. | ENTRY INTO SERVICE REQUIRES CERTIFICATION FOR NOVEL TECHNOLOGY | ICAS2026_0398 |
| Schmeink, J. | RUBBER ENGINE INTEGRATED OPTIMIZATION STRATEGY FOR OVERALL AIRCRAFT DESIGN | ICAS2026_0612 |
| Schmelcher, M. | EVALUATION OF LIQUID HYDROGEN CONDITIONING CONCEPTS FOR AIRCRAFT ENGINES EMPLOYING EXHAUST GAS WASTE HEAT RECOVERY | ICAS2026_0551 |
| Schmidt, C. | UNCERTAINTY ANALYSIS AND EYE-TRACKING-BASED CLUSTERING IN AIR TRAFFIC CONTROLLER WORKLOAD PREDICTION | ICAS2026_0118 |
| Schmidt, R. | DEEP LEARNING VS. TRADITIONAL COMPUTER VISION FOR UAV LANDING SITE DETECTION IN ADVERSE WEATHER | ICAS2026_0288 |
| Schmitz, G. | FLIGHT OPERATIONS AND TESTING OF A 450 KG EXPERIMENTAL GYROPLANE UAV | ICAS2026_0331 |
| Schmitz, G. | IMPACT OF SYSTEM LATENCIES ON PILOT INTERACTION AND HANDLING OF AN ELECTRICALLY POWERED GYROPLANE UAV WITH FPV-BASED REMOTE CONTROL | ICAS2026_0335 |
| Schmollgruber, P. | FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION | ICAS2026_0888 |
| Schmollgruber, P. | PIONEERING THE EXCHANGE OF KNOWLEDGE IN AIRCRAFT DESIGN | ICAS2026_1107 |
| Schneider, C. | METROLOGY METHODS FOR ISOLATING PROFILE FORM, WAVINESS, STEPS, AND TWIST FROM SCANS OF SMALL-SCALE LAMINAR FLOW WIND TUNNEL MODELS | ICAS2026_0428 |
| Schneiders, N. | INTEGRATION OF A SOLID OXIDE FUEL CELL PROPULSION SYSTEM: A TECHNOLOGY DEVELOPMENT GOAL FOR REGIONAL AIRCRAFT | ICAS2026_0319 |
| Schnell, R. | CONCEPTUAL PERFORMANCE AND MASS ASSESSMENT OF AN OPEN FAN ENGINE FOR THE DLR-F25 AIRCRAFT | ICAS2026_0261 |
| Schoemaker, D. | DESIGN ASSESSMENT OF A HELICOPTER BLADE | ICAS2026_0225 |
| Schog, S. | EXPLAINABILITY AT ALL LEVELS OF SYSTEM DEVELOPMENT: INSIGHTS FROM THE DESIGN OF INTELLIGENT SYSTEMS IN AVIATION | ICAS2026_0177 |
| Schopferer, S. | ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES | ICAS2026_0289 |
| Schopferer, S. | AN AUTONOMY ARCHITECTURE FOR COLLABORATIVE UAV SWARMS - A BOTTOM-UP PERSPECTIVE | ICAS2026_0670 |
| Schubert, M. | PHYSICS-INFORMED NEURAL NETWORKS FOR ULTRASONIC LAMB WAVE RECONSTRUCTION IN NON-DESTRUCTIVE TESTING | ICAS2026_0573 |
| Schuchardt, B. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Schuchardt, B. | IFAR 2025 PERSPECTIVES ON NOISE REDUCTION FOR EMERGING AND CONVENTIONAL AIR TRANSPORT | ICAS2026_0912 |
| Schuchardt, B.I. | CHALLENGES IN ADVANCED AIR MOBILITY NOISE PREDICTION - FROM SOURCE TO PERCEPTION | ICAS2026_0345 |
| Schuff, M. | TOWARDS AN ONTOLOGY-BASED APPROACH FOR DISCIPLINE-SPECIFIC ENGINEERING VIEWS IN ENGINE DESIGN | ICAS2026_0353 |
| Schultz, M. | REDUCING AIR TRAFFIC COMPLEXITY IN JAPANESE AIRSPACE THROUGH MINOR LATERAL TRAJECTORY ADJUSTMENTS | ICAS2026_0048 |
| Schultz, M. | AN AUGMENTED AIRPORT MODEL FOR GROUND OPERATIONS ANALYSIS: A CASE STUDY OF NARITA INTERNATIONAL AIRPORT | ICAS2026_0272 |
| Schultz, M. | SIMULATION-BASED EVALUATION OF SIGNALISED INTERSECTIONS FOR EMERGENCY SAFETY LANDINGS IN URBAN AIR MOBILITY | ICAS2026_0325 |
| Schultz, M. | RUNWAY-AWARE CAPACITY ENVELOPES FOR LONG-RANGE ARRIVAL METERING UNDER OPERATING-DIRECTION CHANGES AT SINGAPORE CHANGI | ICAS2026_0408 |
| Schultz, M. | PROVIDING SENSOR INFORMATION FOR BOARDING TIME PREDICTION | ICAS2026_0611 |
| Schultz, V. | ENTRY INTO SERVICE REQUIRES CERTIFICATION FOR NOVEL TECHNOLOGY | ICAS2026_0398 |
| Schulz, M. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Schumann, H. | A MULTIDIMENSIONAL FRAMEWORK FOR DEMONSTRATION AND V&V CAPABILITIES FOR NEXT-GENERATION FLIGHT CONTROL SYSTEMS | ICAS2026_0093 |
| Schwagerus, N. | EXPERIMENTAL VALIDATION OF A COANDA-BASED FLUIDIC THRUST VECTORING NOZZLE USING A HIGH-SPEED WIND TUNNEL | ICAS2026_0151 |
| Schweiger, K. | ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT | ICAS2026_0897 |
| Schwengler, J. | FLIGHT MISSION MODELING WITH VARYING BASELINE DATA: APPLICAITON IN BUSINESS AVIATION | ICAS2026_0315 |
| Schwerzmann, F. | DYN-MARS: A NEW CONCEPT ENABLING THE BEST APPROACH FLIGHT PROFILE | ICAS2026_0265 |
| Schüppstuhl, T. | ASSESSING THE POTENTIAL OF MULTI-MODEL TOPOLOGY OPTIMIZATION FOR MODULAR LIGHTWEIGHT DESIGN OF AIRCRAFT CABIN STRUCTURES | ICAS2026_0406 |
| Schäfer, M. | PROPAGATING SAFETY ASSESSMENT RESULTS FOR SYSTEM ARCHITECTURE CANDIDATES IN MBSE | ICAS2026_0399 |
| Schäfer, M. | MODEL-BASED FUNCTIONAL HAZARD ASSESSMENT BASED ON ARP4761A USING SYSML V1 AND SYSML V2 | ICAS2026_0674 |
| Scott, C.D. | OPTIMIZATION OF INTERCONNECTED 3D-PRINTED STRUCTURES FOR UAVS | ICAS2026_0943 |
| Scott, M. | EXPLAINABLE NATURAL LANGUAGE PROCESSING FOR AIRCRAFT STRUCTURAL INTEGRITY DEFECT CLASSIFICATION | ICAS2026_0738 |
| Scott, M. | VR FOR CABIN DESIGN AND CERTIFYING DIGITAL MRO MEASURES | ICAS2026_1109 |
| Scott, M.J. | A MIXED REALITY FRAMEWORK FOR EVALUATING AIRCRAFT PRE-FLIGHT WALK-AROUND TRAINING | ICAS2026_0464 |
| Sebastiani, B. | DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY | ICAS2026_0827 |
| Seefried, A. | A SIMULATION STUDY ON THE EFFECT OF EXTENDED ROTATIONAL KINEMATICS IN HEXAPOD MOTION SIMULATORS | ICAS2026_0662 |
| Seitz, A. | A LAMINAR TAILORED WING WITH CATNLF AND HLFC FOR EXTRA LONG RANGE | ICAS2026_0187 |
| Sekine, K. | EVALUATING IMPACT OF INTERNATIONAL DEPARTURE TIME CONTROL ON DOMESTIC ARRIVAL DELAYS IN JAPAN USING MULTI-OBJECTIVE SIMULATION-BASED OPTIMIZATION | ICAS2026_0779 |
| Sekyra, N. | RESEARCH PLATFORM AIRSHIP: DESIGN AND FLIGHT CHARACTERISTICS FOR URBAN OPERATIONS | ICAS2026_0576 |
| Seo, B. | SYSTEM IDENTIFICATION OF SMALL-SCALE HELICOPTER VIA EKF WITH DATA-DRIVEN NOISE COVARIANCE DETERMINATION | ICAS2026_0176 |
| Seo, D.H. | DISTURBANCE OBSERVER-BASED ADAPTIVE NONSINGULAR TERMINAL SLIDING MODE CONTROL FOR FAULT-TOLERANT CONTROL OF QUAD-TILTROTOR EVTOL | ICAS2026_0166 |
| Seok, M | FEASIBILITY OF ELECTROPULSING-INDUCED FATIGUE CRACK CLOSURE IN AEROSPACE METALLIC MATERIALS | ICAS2026_0365 |
| Seon, H. | AIRCRAFT CLIMB PROFILE PREDICTION VIA MACHINE LEARNING-BASED FRAMEWORK | ICAS2026_0893 |
| Serpico, C. | REAL-TIME EMULATION TESTBENCH FOR FUEL-CELL/BATTERY HYBRIDIZATION IN HYDROGEN-ELECTRIC AVIATION | ICAS2026_0338 |
| Serpieri, J. | PROPELLER AERODYNAMICS UNDER NON-UNIFORM INFLOWS | ICAS2026_0444 |
| Sha, Z. | DEVELOPMENT OF CONDUCTIVE COMPOSITE MATERIALS FOR HIGH VOLTAGE APPLICATIONS | ICAS2026_0036 |
| Shahjahan, S. | SIMULATION OF FIFTH-GENERATION HIGH-PERFORMANCE AIRCRAFT USING VISCOUS SURFACE-VORTICITY PANEL METHOD | ICAS2026_0119 |
| Shahjahan, S. | SIMULATION OF AERODYNAMIC GROUND EFFECT FOR TILTED PROPELLERS USING VISCOUS SURFACE-VORTICITY PANEL METHOD | ICAS2026_0120 |
| Shang, B.L. | RESEARCH ON EFFECTIVENESS-DRIVEN INTELLIGENT OPTIMIZATION METHOD FOR CONCEPTUAL LAYOUT OF AIRCRAFT | ICAS2026_0596 |
| Shang, B.L. | COARSE–FINE COUPLED MBSE FOR SURVIVABILITY PARAMETER DESIGN OF STEALTH CARRIER-BASED TANKER | ICAS2026_0671 |
| Shang, Y. | POWER FLOW DYNAMICS AND COUPLING MECHANISMS IN POWER-BY-WIRE ACTUATION: A COMPREHENSIVE MODELING AND ANALYSIS APPROACH | ICAS2026_0561 |
| Sharma, A. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Sharp, R. | MODERNISING AT SCALE: DELIVERING AUSTRALIA’S NEXT-GENERATION AIR TRAFFIC SYSTEM | ICAS2026_1089 |
| Shaw, S. | TOWARDS CERTIFICATION BY ANALYSIS: A MILITARY AIRWORTHINESS PERSPECTIVE | ICAS2026_1051 |
| Sheaf, C. | NOVEL METHODS FOR THE CHARACTERISATION OF INTAKE FLOW DISTORTION | ICAS2026_0110 |
| Shen, G. | MISSION-PROFILE-BASED HYBRID POWER SYSTEM DESIGN AND OPTIMIZATION FOR VTOL AIRCRAFT IN REGIONAL AIR MOBILITY | ICAS2026_0696 |
| Shen, H.R. | EFFECTS OF SLOT LOCATION ON FLOW AND HEAT TRANSFER IN A LATTICEWORK COOLING CHANNEL: AN MRV EXPERIMENT AND NUMERICAL STUDY | ICAS2026_0545 |
| Shen, Z.Q. | EFFICIENT ROTOR AERODYNAMIC SHAPE DESIGN USING A MULTI-FIDELITY NEURAL NETWORK-BASED GLOBAL OPTIMIZATION METHOD | ICAS2026_0492 |
| Shetty, S. | VALIDATION OF TRADITIONAL COMPETENCY-BASED ASSESSMENT AND EXPERIENCE-BASED AUTHORISATION FOR AIR TRAFFIC CONTROLLERS | ICAS2026_0568 |
| Shi, H. | INVESTIGATION OF PLUME NON-EQUILIBRIUM INFRARED RADIATION CHARACTERISTICS AT DIFFERENT MACH NUMBERS | ICAS2026_0043 |
| Shi, H. | NUMERICAL SIMULATION OF HYPERSONIC PLASMA FLOW BASED ON NONLINEAR COUPLED CONSTITUTIVE RELATIONS | ICAS2026_0311 |
| Shi, H. | PD-STGNN: A PHYSICS-INFORMED DYNAMIC SPATIO-TEMPORAL GRAPH NEURAL NETWORK FOR AERO-ENGINE THRUST PREDICTION | ICAS2026_0314 |
| Shi, J. | INVESTIGATION OF PLUME NON-EQUILIBRIUM INFRARED RADIATION CHARACTERISTICS AT DIFFERENT MACH NUMBERS | ICAS2026_0043 |
| Shi, J. | NUMERICAL INVESTIGATION OF GEOMETRIC EFFECTS ON INFRARED CHARACTERISTICS OF MULTI-STREAM SERPENTINE NOZZLES | ICAS2026_0788 |
| Shi, L.L. | NUMERICAL STUDY OF UNSTEADY DISTORTION IN AN S-DUCT INTAKE SUBJECTED TO BLAST SHOCK WAVES | ICAS2026_0510 |
| Shi, Y.-J. | EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT ENHANCEMENT OF A HIGH-LIFT CONFIGURATION | ICAS2026_0516 |
| Shim, B. | AI-BASED MAINTENANCE CODE CORRECTION FOR RELIABLE MTBF ANALYSIS | ICAS2026_0770 |
| Shim, J. | OPTIMAL GUIDANCE ALGORITHM FOR BOOST-BACK OF REUSABLE LAUNCH VEHICLES | ICAS2026_0505 |
| Shima, E. | SUPERIOR CRUISE EFFICIENCY OF A NOVEL EVTOL CONFIGURATION FEATURING INCLINED PROPELLERS AND A PARASOL WING | ICAS2026_0238 |
| Shin, J. | OFFLINE REINFORCEMENT LEARNING FOR INFRARED IMAGE-BASED MISSILE GUIDANCE AND CONTROL | ICAS2026_0858 |
| Shin, J.H. | NEURAL NETWORK BASED SLIDING MODE CONTROL FOR HYPERSONIC LONGITUDINAL CONTROL | ICAS2026_0872 |
| Shin, S. | HYPERSONIC VEHICLE FLIGHT SIMULATION AND FLIGHT CONTROL | ICAS2026_0174 |
| Shiva Prakasha, P. | LOSS OF RELIABILITY OF NEW GENERATION ENGINES: THE CASE STUDY OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION AS A SYSTEM OF SYSTEMS | ICAS2026_0822 |
| Sibilski, K. | EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY | ICAS2026_0789 |
| Siemer, T. | NOVEL MULTIDISCIPLINARY MISSION-OPTIMISED AIRCRAFT DEVELOPMENT METHODOLOGY IN CONSIDERATION OF PASSIVE/ACTIVE CONTROL | ICAS2026_0230 |
| Siemer, T. | AN INDIVIDUALISED, SCALABLE PROJECT-BASED LEARNING FRAMEWORK FOR STRUCTURE DESIGN COURSES ESTABLISHED IN A LARGE AEROSPACE STUDY PROGRAMME | ICAS2026_0718 |
| Sieradzki, A. | RECENT ADVANCES IN AEROACOUSTIC DESIGN OF ADVANCED AIR MOBILITY VEHICLES | ICAS2026_0964 |
| Silberhorn, D. | A MULTI-RANGE HYBRID-ELECTRIC OPEN-ROTOR AIRCRAFT CONCEPT FOR THE WIDE-BODY PASSENGER CLASS | ICAS2026_0625 |
| Silla, M. | DESIGN ASSESSMENT OF A HELICOPTER BLADE | ICAS2026_0225 |
| Silva, A.V.S. | A QUALITATIVE FRAMEWORK FOR AIRCRAFT WING MANUFACTURING AND DECISION MAKING | ICAS2026_0766 |
| Silva, C. | EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY | ICAS2026_0080 |
| Silva, C.C.D. | VIRTUAL COMMISSIONING APPLIED TO ROS AIRCRAFT ROBOTIC CELL | ICAS2026_0198 |
| Silva, C.C.D. | A QUALITATIVE FRAMEWORK FOR AIRCRAFT WING MANUFACTURING AND DECISION MAKING | ICAS2026_0766 |
| Silva, D.V.R. | PREDICTION OF STRUCTURAL VIBRATIONS INDUCED BY MASS-UNBALANCED ELECTRIC PROPULSION SYSTEMS | ICAS2026_0901 |
| Silva Figueredo, V. | PHYSICS-INFORMED NEURAL OPERATORS FOR DISTURBANCE FIELD PREDICTION IN NONPARALLEL BOUNDARY-LAYER STABILITY ANALYSIS | ICAS2026_0051 |
| Simon, A. | EVALUATING HUMAN-MACHINE-TEAMING CONCEPTS FOR A HIGHLY AUTOMATED GROUND CONTROLLER WORKING POSITION | ICAS2026_0302 |
| Simon, F. | STUDY OF THE FEASIBILITY OF ACOUSTIC LINERS INSIDE THE BEAM THAT INTERACTS WITH A UAV DRONE ROTOR | ICAS2026_0743 |
| Simon, F. | IFAR 2025 PERSPECTIVES ON NOISE REDUCTION FOR EMERGING AND CONVENTIONAL AIR TRANSPORT | ICAS2026_0912 |
| Singer, N. | NOVEL MULTIDISCIPLINARY MISSION-OPTIMISED AIRCRAFT DEVELOPMENT METHODOLOGY IN CONSIDERATION OF PASSIVE/ACTIVE CONTROL | ICAS2026_0230 |
| Singer, N. | AN INDIVIDUALISED, SCALABLE PROJECT-BASED LEARNING FRAMEWORK FOR STRUCTURE DESIGN COURSES ESTABLISHED IN A LARGE AEROSPACE STUDY PROGRAMME | ICAS2026_0718 |
| Singh, J, | A BENCHMARK FOR UNCERTAINTY QUANTIFICATION AND OPTIMIZATION UNDER UNCERTAINTY IN CONCEPTUAL AIRCRAFT DESIGN: THE F25-OUU CHALLENGE PROBLEM | ICAS2026_0320 |
| Singh, P. | LIMITED HORIZON AIRLINE SCHEDULING USING GREY THEORY AND GRASP FRAMEWORK | ICAS2026_0816 |
| Sirak, E. | SIMULATION OF FIFTH-GENERATION HIGH-PERFORMANCE AIRCRAFT USING VISCOUS SURFACE-VORTICITY PANEL METHOD | ICAS2026_0119 |
| Sirois, F. | EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION | ICAS2026_0673 |
| Sitompul, D. | AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH | ICAS2026_1015 |
| Sittel, V. | RESEARCH PLATFORM AIRSHIP: DESIGN AND FLIGHT CHARACTERISTICS FOR URBAN OPERATIONS | ICAS2026_0576 |
| Skrna, D. | AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS | ICAS2026_0195 |
| Skrna, D. | PREDICTION OF PROPELLER NOISE IN LOW REYNOLDS NUMBER OPERATION USING MACHINE LEARNING MODELS | ICAS2026_0196 |
| Skrna, D. | INTEGRATION OF ACOUSTIC LINERS AND INTERNAL BYPASS CHANNELS INTO AAM PROPELLERS FOR NOISE REDUCTION | ICAS2026_0197 |
| Skusa, I.O. | OSCILLATORY FAILURE DETECTION IN AIRCRAFT ACTUATION SYSTEMS USING WAVELET TRANSFORM | ICAS2026_0683 |
| Slotnick, J. | CFD VISION 2030 PROGRESS AND NEXT STEPS | ICAS2026_0998 |
| Slotnick, J. | PANEL DISCUSSION WITH J. SLOTNICK, B.APONSO, D.PETERSON, T.ISHIDA, H.SCKLICKENMAIER (DURATION 100 MINUTES) | ICAS2026_1055 |
| Smart, M. | THE DART HYPERSONIC VEHICLE: FROM CONCEPT TO LAUNCH | ICAS2026_1072 |
| Smetanova, L. | AIRSPACE CAPACITY IMPLICATIONS OF CONTRAIL-AWARE TRAJECTORY OPTIMIZATION | ICAS2026_0224 |
| Smith, H | PERFORMANCE COMPARISON BETWEEN PASSENGER AIRCRAFT WITH NOVEL PROPULSION SYSTEMS AT CONCEPTUAL DESIGN LEVEL | ICAS2026_0447 |
| Smith, H. | COMPARING DIFFERENT SEMI-EMPIRICAL AERODYNAMIC TOOLS FOR ANALYSING NOVEL AIRCRAFT CONFIGURATIONS | ICAS2026_0445 |
| Smith, J. | CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS | ICAS2026_0749 |
| Smith, P. | A HOLISTIC APPROACH TO ENABLE ADVANCED AIR MOBILITY FOR REGIONAL, RURAL AND REMOTE AUSTRALIA | ICAS2026_0988 |
| Soemarwoto, B.I. | AERODYNAMIC FEASIBILITY OF A NOVEL SWIVEL ROTOR ARCHITECTURE | ICAS2026_0866 |
| SOLNTSEV, Igor | HIGH-FIDELITY NUMERICAL INVESTIGATION OF ROTOR-WING INTERACTIONS IN A MULTI-ROTOR DISTRIBUTED ELECTRIC PROPULSION CONFIGURATION | ICAS2026_0678 |
| Soltz, L.G.M. | MODEL-BASED INTEGRATION OF FLIGHT-TEST EVIDENCE AND SEMI-EMPIRICAL PERFORMANCE MODELS: THE ACS-100 SORA LIGHT AIRCRAFT CASE STUDY | ICAS2026_0917 |
| Somers, D.M. | EVALUATING THE LAMINAR FLOW ON A SLOTTED, NATURAL-LAMINAR-FLOW WING IN THE NASA AMES 11-FOOT TRANSONIC WIND TUNNEL | ICAS2026_0472 |
| Somerville, A. | FEASIBILITY OF ELECTRIC DUCTED FANS TO REPLACE OPEN PROPELLERS ON AN ELECTRIFIED TRAINING AIRCRAFT | ICAS2026_0084 |
| Song, B. | OPTIMIZATION OF MORPHOLOGICAL AND KINEMATIC PARAMETER FOR FLAPPING WING IN FORWARD FLIGHT | ICAS2026_0089 |
| Song, B. | STUDY ON INDUCED DRAG CALCULATION FOR BIRD-LIKE WINGTIP SLOTS USING WAKE-PLANE INTEGRATION | ICAS2026_0466 |
| Song, B. | AERODYNAMIC EFFECT OF PITCHING MOTION FOR FLAPPING AIRFOIL ACROSS DIFFERENT SWEEPING TRAJECTORIES | ICAS2026_0542 |
| Song, B.F. | MULTI-BODY DYNAMIC MODELING OF A BIRD-LIKE FLAPPING-WING VEHICLE: ANALYSIS OF FLAPPING-AERODYNAMIC COUPLING EFFECTS | ICAS2026_0191 |
| Song, B.F. | RESEARCH ON AN AERODYNAMIC LOAD METHODOLOGY FOR FLAPPING WINGS BASED ON EXPERIMENTALLY ACQUIRED DEFORMATION | ICAS2026_0747 |
| Song, C. | NUMERICAL SIMULATION OF HYPERSONIC PLASMA FLOW BASED ON NONLINEAR COUPLED CONSTITUTIVE RELATIONS | ICAS2026_0311 |
| Song, C. | PD-STGNN: A PHYSICS-INFORMED DYNAMIC SPATIO-TEMPORAL GRAPH NEURAL NETWORK FOR AERO-ENGINE THRUST PREDICTION | ICAS2026_0314 |
| Song, C. | PERFORMANCE DEGRADATION ASSESSMENT METHOD FOR AERO-ENGINES ACROSS THE FULL-LIFE-CYCLE BASED ON DIGITAL TWIN | ICAS2026_0856 |
| Song, H.Z. | PREDICTION OF MINIMUM STARTING PRESSURE FOR HYDROSTATIC HELICAL ROTARY ACTUATOR USING PHYSICS-INFORMED NEURAL NETWORKS | ICAS2026_0593 |
| Song, J. | DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+ | ICAS2026_0130 |
| Song, K. | ADAPTIVE-PREFERENCE MULTI-OBJECTIVE REINFORCEMENT LEARNING FOR WIDE-SPEED-REGIME AIRFOIL OPTIMIZATION | ICAS2026_0393 |
| Song, K. | AIRFRAME-INLET INTEGRATION DESIGN FOR AN OVER-WING-MOUNTED SUPERSONIC TRANSPORT CONFIGURATION | ICAS2026_0501 |
| Song, S. | CASCADE ADRC FOR TRAJECTORY TRACKING OF A FLYING-WING SOLAR AIRCRAFT UNDER WIND DISTURBANCES | ICAS2026_0128 |
| Song, S. | WIND FIELD PERCEPTION AND FEATURE PREDICTION FOR LOW-ALTITUDE SMALL FIXED-WING UAVS TOWARDS ENERGY HARVESTING | ICAS2026_0742 |
| Song, W. | OPTIMIZATION OF MORPHOLOGICAL AND KINEMATIC PARAMETER FOR FLAPPING WING IN FORWARD FLIGHT | ICAS2026_0089 |
| Song, W. | AN EFFICIENT TRANSITION PREDICTION METHOD USING NEURAL NETWORK SURROGATE MODELS | ICAS2026_0254 |
| Song, W.-P. | EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT ENHANCEMENT OF A HIGH-LIFT CONFIGURATION | ICAS2026_0516 |
| Song, W.-P. | POINT-CLOUD-BASED INTELLIGENT DESIGN OF FLYING-WING CONFIGURATIONS WITH CONDITIONAL GENERATION AND PRESSURE PREDICTION | ICAS2026_0528 |
| Song, W.P. | A ROTOR TRANSITION PREDICTION METHOD BASED ON GALILEAN INVARIANCE AND THE C1 CROSSFLOW TRANSITION CRITERION | ICAS2026_0463 |
| Song, W.P. | EFFICIENT ROTOR AERODYNAMIC SHAPE DESIGN USING A MULTI-FIDELITY NEURAL NETWORK-BASED GLOBAL OPTIMIZATION METHOD | ICAS2026_0492 |
| Song, Y.L. | PARAMETER INVERSION ALGORITHM FOR AERO-ENGINE γ-PHOTON FLOW FIELD IMAGES BASED ON UNET-GAN ARCHITECTURE | ICAS2026_0264 |
| Soria, J. | PASSIVE FLOW CONTROL OF A TURBULENT BOUNDARY LAYER AT THE VERGE OF SEPARATION USING SURFACE ROUGHNESS | ICAS2026_1085 |
| Sorokina, N. | HARDWARE-IN-THE-LOOP VERIFICATION OF A SAFETY-CRITICAL RECONFIGURABLE BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIRCRAFT | ICAS2026_0557 |
| Sorokina, N. | RECONFIGURABLE MULTILEVEL BATTERY ARCHITECTURE FOR SMALL UAV PROPULSION SYSTEMS | ICAS2026_0684 |
| Sorokina, N. | ANALYSIS OF SOFTWARE DEVELOPMENT METHODS FOR A RECONFIGURABLE BATTERY SYSTEM FOR USE IN AN ELECTRIC AIRCRAFT | ICAS2026_0957 |
| Sousa, V.C.B. | A COMPARATIVE WMLES STUDY OF THE CRM-HL IN FREE-AIR AND IN THE NTF FACILITY | ICAS2026_0793 |
| Souza, J.P.B. | STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR IMPACT RESPONSE FOR LIGHTWEIGHT FIXED-WING UAVS | ICAS2026_0833 |
| Sozer, E. | A COMPARATIVE WMLES STUDY OF THE CRM-HL IN FREE-AIR AND IN THE NTF FACILITY | ICAS2026_0793 |
| Spratling, H.R. | ULTRASONIC NON-DESTRUCTIVE TESTING: SYSTEM SELECTION FOR CHARACTERISATION AND DETECTION OF DEFECTS IN REPAIRED COMPOSITE MATERIALS | ICAS2026_0861 |
| Stamoulis, K. | TOWARDS INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES: INSPECTABILITY ASSESSMENT OF HAT-STIFFENED PANELS | ICAS2026_0914 |
| Stamoulis, K.P. | FROM DATA TO DECISIONS: A CONCEPTUAL FRAMEWORK FOR DATA-DRIVEN AIRLINE OPERATIONS AND SUSTAINMENT | ICAS2026_0710 |
| Starck, G. | AERODYNAMIC TRANSONIC DESIGN OF A STRUT-BRACED WING | ICAS2026_0223 |
| Stefan, A. | ARCHITECTED LATTICE SANDWICH STRUCTURES FOR LIGHTWEIGHT IMPACT AND ENERGY ABSORPTION APPLICATIONS | ICAS2026_0053 |
| Stefanetti, M. | DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY | ICAS2026_0827 |
| Stefani, T. | ON THE APPLICABILITY OF SAFETY NETS: A SAFETY-BY-DESIGN SOLUTION FOR CERTIFYING NEURAL NETWORKS | ICAS2026_0210 |
| Stefani, T. | COVERAGE-DRIVEN VERIFICATION FOR SAFETY-BY-DESIGN IN AI-BASED COLLISION AVOIDANCE SYSTEMS | ICAS2026_0536 |
| Stekovic, S. | TRACING MATERIAL PROPERTIES TO SYSTEM-LEVEL PERFORMANCE: A NORMALISED SENSITIVITY ANALYSIS FOR A BOEING 737-CLASS AIRCRAFT | ICAS2026_0640 |
| Stella, F. | UNCERTAINTY QUANTIFICATION AND CROSS-CORRELATION EFFECTS IN AERODYNAMIC COEFFICIENTS DERIVED QUANTITIES | ICAS2026_0281 |
| Stella, F. | BUFFETING SCALE EFFECTS ON A LAUNCH VEHICLE: HYBRID RANS-LES ANALYSIS | ICAS2026_0282 |
| Stella, F. | MULTI-OBJECTIVE SHAPE OPTIMIZATION OF A LAUNCH VEHICLE FAIRING ACROSS MULTIPLE FLOW REGIMES | ICAS2026_0284 |
| Stephens, J. | OVERVIEW OF PROPULSION-AIRFRAME INTEGRATION RESEARCH AT NASA (PART II) | ICAS2026_1060 |
| Stergiou, M.B. | COST-EFFECTIVE CFD REPRODUCTION OF DPW-7 CASE 2A FOR CRM TRANSONIC PITCHING-MOMENT PREDICTION AND ADAPTIVE-REFINEMENT ASSESSMENT | ICAS2026_0953 |
| Stevens, J. | OVERVIEW OF PROPULSION-AIRFRAME INTEGRATION RESEARCH AT NASA (PART I) | ICAS2026_1059 |
| Stevens, K. | OPTIMISING THE HUMAN FACTORS IN ADVANCED AIR MOBILITY | ICAS2026_1084 |
| Stoufflet, B. | THE COLLABORATIVE NATURE OF AVIATION INDUSTRY | ICAS2026_1092 |
| Stragiotti, E. | AERODYNAMIC TRANSONIC DESIGN OF A STRUT-BRACED WING | ICAS2026_0223 |
| Stragiotti, E. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Strauss, J. | LASER SCANNING STRATEGIES TO INVESTIGATE THE EFFECTS OF OXIDATION IN PURE TANTALUM | ICAS2026_0507 |
| Streit, T. | A LAMINAR TAILORED WING WITH CATNLF AND HLFC FOR EXTRA LONG RANGE | ICAS2026_0187 |
| Strohmayer, A. | DATA-DRIVEN FAST NOISE PREDICTION OF AN UNCONVENTIONAL AIRCRAFT USING HIGH-FIDELITY SIMULATION DATA | ICAS2026_0273 |
| Strohmayer, A. | EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT | ICAS2026_0274 |
| Strydom, L. | REFLECTIONS ON THE AEROSPACE ENGINEERING DEVELOPMENT PROGRAMME AT THE CSIR | ICAS2026_0549 |
| Stuart, C. | INVESTIGATION OF DECARBONISATION PATHWAYS FOR SHORT HAUL AVIATION USING A DISCRETE OPTIMISATION DECISION-MAKING ALGORITHM | ICAS2026_0396 |
| Stuermer, A. | SURROGATE-BASED OPTIMIZATION OF AIRCRAFT PROPELLER PERFORMANCE USING A HIGH-FIDELITY AND EFFICIENT RANS FRAMEWORK | ICAS2026_0712 |
| Stumpf, E. | AGENTIC AI FOR AIRCRAFT PRELIMINARY DESIGN: PROOF OF CONCEPT | ICAS2026_0575 |
| Stößel, M. | EXPERIMENTAL VALIDATION OF A COANDA-BASED FLUIDIC THRUST VECTORING NOZZLE USING A HIGH-SPEED WIND TUNNEL | ICAS2026_0151 |
| Stößel, M. | INVESTIGATION OF GENERIC SWIRL DISTORTION AND ITS EFFECTS ON COMPRESSOR PERFORMANCE AND FLOW STABILITY | ICAS2026_0334 |
| Su, Z.C. | HIGH-ALTITUDE PERFORMANCE AND ONE-DIMENSIONAL MODELING OF A DUAL-ROTOR GEROTOR PUMP FOR AEROENGINE LUBRICATION SYSTEMS | ICAS2026_0352 |
| Suizu, H. | A PRELIMINARY STUDY ON DYNAMIC AIRSPACE CONFIGURATION USING FLEXIBLE VERTICAL BOUNDARIES IN DOUBLE-LAYER AIRSPACE | ICAS2026_0697 |
| Suk, J.Y. | DISTURBANCE OBSERVER-BASED ADAPTIVE NONSINGULAR TERMINAL SLIDING MODE CONTROL FOR FAULT-TOLERANT CONTROL OF QUAD-TILTROTOR EVTOL | ICAS2026_0166 |
| Suk, J.Y. | SOFTWARE-IN-THE-LOOP SIMULATION OF DISTRIBUTED 3D INTEGRATED SWARM GUIDANCE FOR FIXED-WING UAVS | ICAS2026_0167 |
| Suk, J.Y. | SYSTEM IDENTIFICATION OF SMALL-SCALE HELICOPTER VIA EKF WITH DATA-DRIVEN NOISE COVARIANCE DETERMINATION | ICAS2026_0176 |
| Sulejmanovic, B. | CONCEPT OF OPERATIONS FOR A HYDROGEN-ELECTRIC POWERED MODIFIED DASH 8-300 REGIONAL AIRCRAFT: PERFORMANCE, OPERATIONAL, AND REGULATORY IMPACTS | ICAS2026_0307 |
| Sumaja, K. | CLIMATE HAZARD TIMING AND FLIGHT DEMAND COOCCURRENCE: A DEMAND-WEIGHTED EXPOSURE FRAMEWORK | ICAS2026_0870 |
| Sumi, A. | EXPERIMENTAL STUDY OF LOAD ALLEVIATION WITH PASSIVE ADAPTIVE CAMBER AIRFOILS | ICAS2026_0730 |
| Sun, B. | PASSIVE FLOW CONTROL OF A TURBULENT BOUNDARY LAYER AT THE VERGE OF SEPARATION USING SURFACE ROUGHNESS | ICAS2026_1085 |
| Sun , S. | CURVATURE-CONTROLLED MORPHING OF FOLDING WINGTIPS USING HONEYCOMB PLATES | ICAS2026_0853 |
| Sun, S.G. | ANOMALY B-VALUE DETECTION AND EXCLUSION OF GBAS BASED ON WAVELET MULTI-RESOLUTION ANALYSIS | ICAS2026_0028 |
| Sun, S.Y. | 3D ANALYSIS AND PREDICTION FOR ASSEMBLY STEP DEVIATIONS OF FOUR-BAR LINKAGE BAY DOORS | ICAS2026_0140 |
| Sun, Y. | UNCONTROLLED TAILLESS GLIDING: PAPER AEROPLANES GEOMETRY, AERODYNAMICS AND FLIGHT DURATION ANALYSIS | ICAS2026_0392 |
| Sun, Y. | EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN | ICAS2026_0490 |
| Sundar, R. | MODELING & PRELIMINARY ANALYSIS OF AN ECOFRIENDLY AIRBORNE GLOBAL LUXURY EKRANOPLAN | ICAS2026_0055 |
| Sunil, E. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Surmann, D. | GAIN OPTIMIZATION FOR CASCADED INDI CONTROL WITH INTEGRATED PERFORMANCE AND ROBUSTNESS REQUIREMENTS | ICAS2026_0372 |
| Suti, A. | A MODEL PREDICTIVE CONTROL STRATEGY FOR THE ENERGY MANAGEMENT OF HYBRID ELECTRIC PROPULSION SYSTEMS IN FIXED-WING UAVS | ICAS2026_0613 |
| Suti, A. | POWER-HIL TESTING OF LI-PO BATTERY PACKS FOR LIGHTWEIGHT EVTOL UAVS | ICAS2026_0619 |
| Suti, A. | A MPC–MHE STRATEGY FOR FREQUENCY TRACKING AND PARAMETERS ESTIMATION OF RESONANT DE-ICING SYSTEMS | ICAS2026_0660 |
| Suzuki, M. | JAL’ CHALLENGE TO THE NET-ZERO GH GAS EMISSION | ICAS2026_0986 |
| Suzuki, S. | NEW TEST RESULTS OF THE 3.23% FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2026_0328 |
| Suzuki, W. | NEW TEST RESULTS OF THE 3.23% FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL | ICAS2026_0328 |
| Swaid, M. | IMPACT OF BOOKING LEAD TIME ON FLEET AND INFRASTRUCTURE IN URBAN AIR MOBILITY | ICAS2026_0672 |
| Swannet, K. | INVERSE AIRFOIL DESIGN USING AERODYNAMICALLY CONDITIONED VARIATIONAL AUTOENCODERS | ICAS2026_0894 |
| Swanton, G. | A FULL-SCALE DEMONSTRATOR FOR RAPID TESTING OF HELICOPTER AIRFRAMES USING ADVANCED CONTROL SYSTEM METHODOLOGIES | ICAS2026_0157 |
| Swierk, J. | MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS | ICAS2026_0143 |
| Szczerba, Z. | EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY | ICAS2026_0789 |
| Szumski, M. | EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY | ICAS2026_0789 |
| Szymanski, M. | DATA-DRIVEN SYNTHESIS OF AIRCRAFT FEEDBACK CONTROL LAWS FOR NEW COMMERCIAL FLIGHT SCENARIOS | ICAS2026_0891 |
| Szöke-Erös, H. | LOSS OF RELIABILITY OF NEW GENERATION ENGINES: THE CASE STUDY OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION AS A SYSTEM OF SYSTEMS | ICAS2026_0822 |
| Sørensen-Libik, K. | HIGH-FIDELITY DATASET-BASED SHAPE AND STRUCTURE OPTIMIZATION FOR AIRCRAFT DESIGN | ICAS2026_0042 |
| Taddei, T. | GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION | ICAS2026_1011 |
| Taguchi, H. | MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) | ICAS2026_1074 |
| Tai, S. | PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA | ICAS2026_0624 |
| Tai, S. | BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL | ICAS2026_0647 |
| Takahashi, H. | MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) | ICAS2026_1074 |
| Takahashi, S. | PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN | ICAS2026_0370 |
| Takahashi, S. | AN OVERVIEW OF JAXA’S HIGH-SPEED FLIGHT R&D: FROM SUPERSONIC FLIGHT TO HYPERSONIC TRANSPORTATION | ICAS2026_1067 |
| Takahashi, S. | SDF-BASED GEOMETRY BLENDING OF HYPERSONIC VEHICLE CONCEPTS | ICAS2026_1070 |
| Takahashi, T.T. | EVALUATION OF PERCEIVED X-15 FLYING QUALITIES BASED ON RAPID AERODYNAMIC PREDICTIONS | ICAS2026_0817 |
| Takaishi, T. | AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMI-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT THE JAXA 6.5M X 5.5M LOW SPEED WIND TUNNEL | ICAS2026_0256 |
| Takaishi, T. | AEROACOUSTIC WIND TUNNEL TESTING AND CFD STUDY USING JAXA 8% SEMISPAN HIGH-LIFT COMMON RESEARCH MODEL IN JAXA FQUROH-2 PROJECT | ICAS2026_0756 |
| Takamoto, M. | ROBUST MOTION ESTIMATION FOR INDOOR MAVS USING WIDE-FIELD-INTEGRATION OF OPTIC FLOW | ICAS2026_0163 |
| Takegoshi, M. | PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN | ICAS2026_0370 |
| Takegoshi, M. | AN OVERVIEW OF JAXA’S HIGH-SPEED FLIGHT R&D: FROM SUPERSONIC FLIGHT TO HYPERSONIC TRANSPORTATION | ICAS2026_1067 |
| Takegoshi, M. | SDF-BASED GEOMETRY BLENDING OF HYPERSONIC VEHICLE CONCEPTS | ICAS2026_1070 |
| Takeichi, N. | FEASIBILITY STUDY ON IMPROVING ARRIVAL-SEPARATION STABILITY THROUGH ARRIVAL TRAJECTORY ANALYSIS AT CONGESTED AIRPORTS | ICAS2026_0329 |
| Takeichi, N. | A PRELIMINARY STUDY ON DYNAMIC AIRSPACE CONFIGURATION USING FLEXIBLE VERTICAL BOUNDARIES IN DOUBLE-LAYER AIRSPACE | ICAS2026_0697 |
| Takizawa, K. | MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) | ICAS2026_1074 |
| Tamayama, M. | EFFECT OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS | ICAS2026_0517 |
| Tamayama, M. | EFFECT OF MORPHOLOGICAL CHANGES ON THE AERODYNAMIC CHARACTERISTICS OF THE WING AND TAIL FEATHERS OF A TAXIDERMY BLACK-TAILED GULL | ICAS2026_0852 |
| Tanahashi, Y. | EFFECT OF MORPHOLOGICAL CHANGES ON THE AERODYNAMIC CHARACTERISTICS OF THE WING AND TAIL FEATHERS OF A TAXIDERMY BLACK-TAILED GULL | ICAS2026_0852 |
| Tanaka, F. | HPC-BASED PARAMETER SPACE EXPLORATION FOR DENSE PICOSAT FORMATION FLYING TOWARD DIRECT-TO-DEVICE COMMUNICATIONS | ICAS2026_0869 |
| Tang, D. | LIGHTWEIGHT AND ROBUST REAL-TIME DETECTION SYSTEM FOR AIRCRAFT SKIN DEFECTS UNDER COMPLEX UAV INSPECTION CONDITIONS | ICAS2026_0134 |
| Tang, E. | LIGHTWEIGHT BIMETALLIC GEARS FOR AEROSPACE TRANSMISSIONS ENABLED BY OPEN-AIR DIFFUSION BONDING | ICAS2026_0991 |
| Tang, H. | FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES | ICAS2026_0171 |
| Tang, X. | RESEARCH ON AERODYNAMIC-STRUCTURAL RAPID EVALUATION AND OPTIMIZATION METHODS FOR JOINED-WING CONFIGURATIONS | ICAS2026_0577 |
| Tangermann, E. | LAMINAR SEPARATION ON AN AIRFOIL WITH PERTURBATION OF OUTER AND INNER BOUNDARY CONDITIONS | ICAS2026_0368 |
| Tanguy, G. | STATIC AND DYNAMIC WIND-TUNNEL TESTING OF A TRANSPORT AIRCRAFT MODEL IN-STALL AND POST-STALL FLIGHT REGIMES | ICAS2026_0203 |
| Tanhashi, Y. | EFFECT OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS | ICAS2026_0517 |
| Tasca, A. | IMPACT TOLERANCE OF DRILLED THICK C/SIC CERAMIC MATRIX COMPOSITES | ICAS2026_0357 |
| Tatar, M. | GAP OPTIMIZATION ADAPTIVE TOOL FOR LARGE SCALE FLEXIBLE STRUCTURE ASSEMBLY | ICAS2026_0058 |
| Tatsukawa, T. | EVALUATING IMPACT OF INTERNATIONAL DEPARTURE TIME CONTROL ON DOMESTIC ARRIVAL DELAYS IN JAPAN USING MULTI-OBJECTIVE SIMULATION-BASED OPTIMIZATION | ICAS2026_0779 |
| Taylor, I.J. | CONCEPTUAL DESIGN OF A MIDDLE-OF-THE-MARKET AIRCRAFT FOR EDUCATIONAL PURPOSES | ICAS2026_0420 |
| Teck, T.L. | INNOVATION & TRANSFORMATION AT SINGAPORE CHANGI AIRPORT AND A CASE STUDY ON AI-ENABLED LINE MAINTENANCE OPERATIONS | ICAS2026_0995 |
| Tejero, F. | EFFECT OF INTAKE AERODYNAMICS AND FLOW DISTORTION ON FAN STALL INCEPTION | ICAS2026_0111 |
| Temme, M.-M. | VALIDATION OF TRADITIONAL COMPETENCY-BASED ASSESSMENT AND EXPERIENCE-BASED AUTHORISATION FOR AIR TRAFFIC CONTROLLERS | ICAS2026_0568 |
| Testera, A. | EXPERIMENTAL VALIDATION OF A FUEL CELL SYSTEM DIGITAL TWIN FOR A FULL-ELECTRIC AIRCRAFT POWERTRAIN | ICAS2026_0303 |
| Teutsch, J. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Teyssier, N. | LIGHTWEIGHT BIMETALLIC GEARS FOR AEROSPACE TRANSMISSIONS ENABLED BY OPEN-AIR DIFFUSION BONDING | ICAS2026_0991 |
| Tezuka, A. | MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) | ICAS2026_1074 |
| Tfaily, A. | EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION | ICAS2026_0673 |
| Thilker, F. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF HYDROGEN FLAMES UNDER COLD INJECTION CONDITIONS | ICAS2026_0299 |
| Thilker, F. | AN INTEGRATED SYSTEM-LEVEL AND MULTIPHYSICS APPROACH FOR AIRCRAFT LH2 FUEL SYSTEM DESIGN | ICAS2026_0316 |
| Thilker, F. | EVALUATION OF LIQUID HYDROGEN CONDITIONING CONCEPTS FOR AIRCRAFT ENGINES EMPLOYING EXHAUST GAS WASTE HEAT RECOVERY | ICAS2026_0551 |
| Thilker, F. | MODAL-BASED FUEL LEVEL ESTIMATION OF CRYOGENIC PROPELLANT TANKS | ICAS2026_0663 |
| Thomas, M. | ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS | ICAS2026_1005 |
| Thomessen, K. | ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES | ICAS2026_0289 |
| Thomessen, K. | AN AUTONOMY ARCHITECTURE FOR COLLABORATIVE UAV SWARMS - A BOTTOM-UP PERSPECTIVE | ICAS2026_0670 |
| Thomessen, K. | ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES (PITCH SESSION) | ICAS2026_1096 |
| Thorne, G. | EFFECT OF INTAKE AERODYNAMICS AND FLOW DISTORTION ON FAN STALL INCEPTION | ICAS2026_0111 |
| Thöne, P. | DYN-MARS: A NEW CONCEPT ENABLING THE BEST APPROACH FLIGHT PROFILE | ICAS2026_0265 |
| Timmons, A. | A PROCESS-STRUCTURE-PROPERTY-PERFORMANCE FRAMEWORK FOR DIGITAL ENGINEERING-ENABLED REPAIR OF ALUMINUM PARTS | ICAS2026_0940 |
| Tiwari, A. | OPTIMISATION OF OPERATING RADII FOR DRONE WAREHOUSES | ICAS2026_0900 |
| Tocci, F. | REYNOLDS NUMBER SCALING EFFECTS IN TRANSONIC CAVITY AERODYNAMICS: A HIGH-FIDELITY EXPERIMENTAL AND NUMERICAL FRAMEWORK | ICAS2026_0362 |
| Tokugawa, N. | DEVELOPMENT OF HYDROPHILIC COATINGS FOR PRACTICAL APPLICATION OF LAMINAR FLOW WINGS | ICAS2026_0841 |
| Tomioka, S. | AN OVERVIEW OF JAXA’S HIGH-SPEED FLIGHT R&D: FROM SUPERSONIC FLIGHT TO HYPERSONIC TRANSPORTATION | ICAS2026_1067 |
| Tomita, N. | EFFECT OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS | ICAS2026_0517 |
| Tomita, N. | EFFECT OF MORPHOLOGICAL CHANGES ON THE AERODYNAMIC CHARACTERISTICS OF THE WING AND TAIL FEATHERS OF A TAXIDERMY BLACK-TAILED GULL | ICAS2026_0852 |
| Tong, X. | NUMERICAL SIMULATION OF STRESS-OXIDATION DAMAGE IN C/SIC COMPOSITES AT HIGH TEMPERATURES | ICAS2026_0276 |
| Torija, A.J. | CHALLENGES IN ADVANCED AIR MOBILITY NOISE PREDICTION - FROM SOURCE TO PERCEPTION | ICAS2026_0345 |
| Tormalm, M. | THE GARTEUR GROUP OF RESPONSABLES IN AERODYNAMICS (GOR AD) AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES | ICAS2026_0989 |
| Tramposch, A. | EXPERIMENTAL AND NUMERICAL INVESTIGATION OF HYDROGEN FLAMES UNDER COLD INJECTION CONDITIONS | ICAS2026_0299 |
| Tramposch, A. | AN INTEGRATED SYSTEM-LEVEL AND MULTIPHYSICS APPROACH FOR AIRCRAFT LH2 FUEL SYSTEM DESIGN | ICAS2026_0316 |
| Tramposch, A. | AERODYNAMIC AND STABILITY-DRIVEN PRE-DESIGN OF A FUEL-CELL POWERED FLYING WING AIRCRAFT | ICAS2026_0318 |
| Tramposch, A. | MODAL-BASED FUEL LEVEL ESTIMATION OF CRYOGENIC PROPELLANT TANKS | ICAS2026_0663 |
| Traskos, M. | ENTRY INTO SERVICE REQUIRES CERTIFICATION FOR NOVEL TECHNOLOGY | ICAS2026_0398 |
| Treichl, T. | TOWARDS THE INTEGRATION OF NEUROPHYSIOLOGICAL SIGNALS AND HUMAN BODY DYNAMICS FOR ADAPTIVE CONTROL ALLOCATION | ICAS2026_0363 |
| Trepiccione, S. | MULTIDISCIPLINARY DESIGN EXPLORATION OF HYBRID-ELECTRIC REGIONAL AIRCRAFT | ICAS2026_0360 |
| Trepiccione, S. | COST-DRIVER MULTIDISCIPLINARY FRAMEWORK FOR WINGLET DESIGN: A REGIONAL AIRCRAFT CASE STUDY | ICAS2026_0783 |
| Trivedi, S. | PRELIMINARY SIZING METHODOLOGY FOR HYBRID-ELECTRIC PROPULSION SYSTEM IN CARGO AIRSHIPS | ICAS2026_0688 |
| Tsuchiya, T. | A SYSTEMATIC, TUNING-FREE ATTITUDE CONTROL METHOD FOR VTOL UAVS | ICAS2026_0096 |
| Tsuchiya, T. | PILOT-IN-THE-LOOP SIMULATION OF OPTIMAL DEEP-STALL RECOVERY FOR T-TAIL AIRLINER | ICAS2026_0125 |
| Tsuchiya, T. | MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) | ICAS2026_1074 |
| Tsue, M. | MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO) | ICAS2026_1074 |
| Tsukuda, K. | PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN | ICAS2026_0370 |
| Tsuru, S. | AIRCRAFT SEQUENCING UNDER UNCERTAINTY: GAME-THEORETIC OPTIMIZATION AND A COMPARATIVE ASSESSMENT OF GLOBAL AND INTRA-AIRLINE COOPERATIVE DECISION FRAMEWORKS | ICAS2026_0446 |
| Tsushima, N. | PARAMETRIC AEROELASTIC STUDY OF WINGLET GEOMETRY USING VORTEX LATTICE METHOD FOR FUTURE PASSIVE MORPHING APPLICATIONS | ICAS2026_0326 |
| Tsushima, N. | AEROELASTIC TAILORING FOR COMPOSITE ADAPTIVE WINGLETS | ICAS2026_0448 |
| Tuchiya, T. | COMPARISON OF FLEXIBLE AIRCRAFT CONFIGURATIONS USING AEROELASTIC ANALYSIS | ICAS2026_0609 |
| Tufano, F. | MULTIDISCIPLINARY APPROACH FOR THE AERODYNAMIC CHARACTERIZATION OF AN INFLATABLE CLOSED-WING HYBRID HIGH-ALTITUDE PSEUDO-SATELLITE | ICAS2026_0371 |
| Tugwell, N. | NEW INSIGHTS INTO AA7085 ENVIRONMENTALLY ASSISTED CRACKING THROUGH HIGH RESOLUTION FRACTOGRAPHY | ICAS2026_0234 |
| Tugwell, N. | ACCELERATED EXPERIMENTAL INVESTIGATION OF ENVIRONMENTALLY ASSISTED CRACKING IN AA7085 | ICAS2026_0244 |
| Tugwell, N. | LABORATORY METHOD FOR REPLICATING FASTENER HOLE CORROSION IN AA7085 | ICAS2026_0253 |
| Tutku Altun, A. | ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT | ICAS2026_0897 |
| Tutty, M.G. | NEUROMORPHIC ASCENT: REVOLUTIONISING AIRCRAFT STORES COMPATIBILITY AND INTELLIGENT & AUTONOMOUS SYSTEMS | ICAS2026_0831 |
| Tvaryanas, A. | A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. | ICAS2026_0041 |
| Türkyilmaz, B. | DESIGN AND INVESTIGATION OF A SHORT-TO-MEDIUM-RANGE AIRCRAFT WITH LIQUID HYDROGEN AND SAF MULTI-FUEL PROPULSION | ICAS2026_0073 |
| Uchiyama, A. | HPC-BASED PARAMETER SPACE EXPLORATION FOR DENSE PICOSAT FORMATION FLYING TOWARD DIRECT-TO-DEVICE COMMUNICATIONS | ICAS2026_0869 |
| Ueno, S. | FLIGHT DYNAMICS AND GUIDANCE CONTROL FOR AIRCRAFT IN TYPHOON ENVIRONMENTS FOR DELIVERY OF TYPHOON CONTROL SUBSTANCE | ICAS2026_0246 |
| Ueno, S. | DESIGN AND FEASIBILITY ASSESSMENT OF TRANSPORT OPERATIONS FOR DELIVERING TYPHOON CONTROL SUBSTANCES | ICAS2026_0247 |
| Ura, H. | AEROACOUSTIC WIND TUNNEL TESTING AND CFD STUDY USING JAXA 8% SEMISPAN HIGH-LIFT COMMON RESEARCH MODEL IN JAXA FQUROH-2 PROJECT | ICAS2026_0756 |
| Ursic, M. | IMPACT TOLERANCE OF DRILLED THICK C/SIC CERAMIC MATRIX COMPOSITES | ICAS2026_0357 |
| Ushio, T. | ON THE FEASIBILITY OF MACHINE LEARNING-BASED DETECTION OF AIRCRAFT LIGHTNING STRIKE RISK AREAS | ICAS2026_0803 |
| Uyhelji, H. | A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. | ICAS2026_0041 |
| Vahaji, S. | NON-LINEAR PARAMETRIC MODEL FOR THE 3DOF MOTION OF A BOX IN WAVES USING SPARSE REGRESSION | ICAS2026_0228 |
| Valencia-Ibáñez, S. | INTEGRATING SYSTEM ARCHITECTURE OPTIMIZATION INTO MODEL-BASED SYSTEMS ENGINEERING METHODS | ICAS2026_0229 |
| van Beeck, J. | INFLUENCE OF ZIGZAG TAPE–INDUCED TRANSITION ON THE DU89-134 AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBER | ICAS2026_0221 |
| van Heerden, A.S.J. | CONCEPTUAL DESIGN OF A MIDDLE-OF-THE-MARKET AIRCRAFT FOR EDUCATIONAL PURPOSES | ICAS2026_0420 |
| van Heerden, Eduard | PROPOSING A STABLE LIFTING FUSELAGE FOR AN AIRLINER OF THE IDEAL AIRCRAFT CONFIGURATION | ICAS2026_0960 |
| van Luijk, N. | VORTEX FLOW CONTROL USING JUNCTURE FILLETS ON A BLUNT-NOSED, CRANKED SWEPT WING | ICAS2026_0047 |
| van Luijk, N. | VORTEX FLOW CONTROL USING JUNCTURE FILLETS ON A BLUNT-NOSED, CRANKED SWEPT WING | ICAS2026_1114 |
| Van Magill, B | TOWARDS A DATABASE OF MICRO-ELECTRIC MOTORS AND ELECTRONIC SPEED CONTROLLERS FOR SMALL UNCREWED AERIAL SYSTEMS | ICAS2026_0882 |
| Van Magill, B. | COMMON RESEARCH MODELS FOR SMALL UNCREWED AERIAL VEHICLES | ICAS2026_0801 |
| van Magill, B. | TOWARDS A DATABASE OF MICRO-ELECTRIC MOTORS AND ELECTRONIC SPEED CONTROLLERS FOR SMALL UNCREWED AERIAL SYSTEMS | ICAS2026_1113 |
| Van Manen, R. | THE MAKING OF LUCHTVAART IN TRANSITIE (LIT) AND THE REMAKING OF A STRONG GLOBALLY CONNECTED NATIONAL AERONAUTICS INDUSTRY | ICAS2026_0651 |
| van Meenen, A. | VORTEX FLOW CONTROL USING JUNCTURE FILLETS ON A BLUNT-NOSED, CRANKED SWEPT WING | ICAS2026_0047 |
| Van Rijswijk, K. | THE MAKING OF LUCHTVAART IN TRANSITIE (LIT) AND THE REMAKING OF A STRONG GLOBALLY CONNECTED NATIONAL AERONAUTICS INDUSTRY | ICAS2026_0651 |
| Van Vaerenbergh, E. | INFLUENCE OF ZIGZAG TAPE–INDUCED TRANSITION ON THE DU89-134 AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBER | ICAS2026_0221 |
| Varriale, C. | TRIM PERFORMANCE EXPLORATION FOR AN AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION AND A TAIL THRUST UNIT | ICAS2026_0377 |
| Varriale, C. | INTERACTIVE NOTEBOOKS TO BRIDGE THE DIDACTIC GAP BETWEEN CALCULUS AND FLIGHT PERFORMANCE OPTIMIZATION | ICAS2026_0380 |
| Varriale, C. | INVERSE AIRFOIL DESIGN USING AERODYNAMICALLY CONDITIONED VARIATIONAL AUTOENCODERS | ICAS2026_0894 |
| Vattathurvalappil, S.H. | ELECTROMAGNETISM FOR SMART MANUFACTURING OF POLYMER COMPOSITES | ICAS2026_0351 |
| Vattathurvalappil, S.H. | ENSEMBLE MACHINE LEARNING FOR UAV PROPELLER PERFORMANCE PREDICTION WITH UNCERTAINTY QUANTIFICATION | ICAS2026_0529 |
| Vauchel, N. | STATIC AND DYNAMIC WIND-TUNNEL TESTING OF A TRANSPORT AIRCRAFT MODEL IN-STALL AND POST-STALL FLIGHT REGIMES | ICAS2026_0203 |
| Vaziri, R. | EFFICIENT SIMULATION AND UNCERTAINTY QUANTIFICATION OF PROGRESSIVE CRUSHING IN COMPOSITE LAMINATES | ICAS2026_0160 |
| Vechtel, D. | NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT | ICAS2026_0216 |
| Veldenz, L. | THE MAKING OF LUCHTVAART IN TRANSITIE (LIT) AND THE REMAKING OF A STRONG GLOBALLY CONNECTED NATIONAL AERONAUTICS INDUSTRY | ICAS2026_0651 |
| Venetsanos, D. | MULTIDISCIPLINARY DESIGN OF COMPLIANT DEFORMABLE WINGS FOR IMPROVED AIRCRAFT EFFICIENCY: INTRODUCING AN ARCHITECTURE-AWARE OPTIMIZATION STRATEGY | ICAS2026_0610 |
| Venning, J. | DECOUPLED DEEP REINFORCEMENT LEARNING FOR AUTONOMOUS LANDING OF UAVS ON SHIPS | ICAS2026_0867 |
| Verhagen, W.J.C. | A MIXED REALITY FRAMEWORK FOR EVALUATING AIRCRAFT PRE-FLIGHT WALK-AROUND TRAINING | ICAS2026_0464 |
| Verhagen, W.J.C. | EXPLAINABLE NATURAL LANGUAGE PROCESSING FOR AIRCRAFT STRUCTURAL INTEGRITY DEFECT CLASSIFICATION | ICAS2026_0738 |
| Verstraete, D | TOWARDS A DATABASE OF MICRO-ELECTRIC MOTORS AND ELECTRONIC SPEED CONTROLLERS FOR SMALL UNCREWED AERIAL SYSTEMS | ICAS2026_0882 |
| Verstraete, D. | COMMON RESEARCH MODELS FOR SMALL UNCREWED AERIAL VEHICLES | ICAS2026_0801 |
| Verstraete, D. | TOROIDAL RECIRCULATION, SADDLE-POINT TOPOLOGY, AND WALL-JET OUTWASH IN A TWIN-ROTOR SYSTEM IN GROUND EFFECT | ICAS2026_0804 |
| Verstraete, D. | EVTOL AND PROPULSION R&D IN THE SYDNEY PROPULSION LAB | ICAS2026_1021 |
| Vertonghen, L. | AEROELASTIC DESIGN OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT IN AN MDO FRAMEWORK | ICAS2026_0342 |
| Vertonghen, L. | COMBINED TOPOLOGY AND COMPOSITE LAMINATE OPTIMIZATION OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT | ICAS2026_0355 |
| Vertonghen, L. | SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT | ICAS2026_0602 |
| Vézina, J. | A FRAMEWORK FOR AUTOMATED SYSTEM COMPONENT PLACEMENT IN AIRCRAFT CONCEPTUAL DESIGN | ICAS2026_0348 |
| Vich, O. | WIND TUNNEL TESTING OF WHIRL FLUTTER AEROELASTIC DEMONSTRATOR | ICAS2026_0014 |
| Villani, E. | EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY | ICAS2026_0080 |
| Villani, E. | VIRTUAL COMMISSIONING APPLIED TO ROS AIRCRAFT ROBOTIC CELL | ICAS2026_0198 |
| Villani, E. | FROM DATA TO DEBRIEF: A FRAMEWORK FOR PILOT PERFORMANCE ASSESSMENT | ICAS2026_0692 |
| Villani, E. | AUTOMATING SYSTEM MODELING USING LARGE LANGUAGE MODELS | ICAS2026_0809 |
| Villani, E. | METHODOLOGY AND V1 PROTOTYPE OF AN ADAPTIVE/ADAPTABLE MULTI-UAV GCS HMI IN A FLOOD SAR CO-SIMULATION TESTBED | ICAS2026_0932 |
| Villani, E. | A SIMULATION METHODOLOGY FOR MULTIROTOR-ASSISTED UAV LAUNCH | ICAS2026_0937 |
| Vincent, A. | MODELLING SENSITIVITIES IN THREE-DIMENSIONAL FZRA-SPECTRUM ICE-SHAPE PREDICTION FOR THE CRM-HL STOWED CONFIGURATION | ICAS2026_0896 |
| Vincent, A. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Vindigni, C.R. | HRV BASED PILOTS WORKLOAD PREDICTION FOR AN INTELLIGENT COCKPIT WARNING SYSTEM | ICAS2026_0422 |
| Vio, G. | EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER CONTROLLED CAVITY FLOW FOR PIEZOELECTRIC ENERGY HARVESTING APPLICATIONS | ICAS2026_1080 |
| Viola, N. | SUPPORTING THE REGULATORY COMMUNITY SHAPING THE FUTURE OF SUSTAINABLE HIGH-SPEED CIVIL AVIATION: THE ESATTO FRAMEWORK | ICAS2026_0926 |
| Viola, N. | EUROPEAN HYPERSONICS OVERVIEW | ICAS2026_1065 |
| Viola, N. | HYPERSONIC TRANSPORT AND WAY FORWARDS WITH THE ICAS DIGITAL PIONEERING INITIATIVE | ICAS2026_1110 |
| Viti, V. | TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT | ICAS2026_0183 |
| Viviani , A. | NUMERICAL REBUILDING OF AERODYNAMIC WIND TUNNEL ANALYSES OF A CREW RETURN VEHICLE | ICAS2026_0572 |
| Vogel, A. | FLIGHT MISSION MODELING WITH VARYING BASELINE DATA: APPLICAITON IN BUSINESS AVIATION | ICAS2026_0315 |
| Vos, R. | VORTEX FLOW CONTROL USING JUNCTURE FILLETS ON A BLUNT-NOSED, CRANKED SWEPT WING | ICAS2026_0047 |
| Vos, R. | LOW-SPEED EXPERIMENTAL INVESTIGATION OF PODDED ENGINE INTEGRATION OF FLYING V AIRCRAFT | ICAS2026_0218 |
| Voth, V. | LLM-ASSISTED GENERATION OF SYSML V2 MODELS FROM STRUCTURED ENGINEERING REPORTS | ICAS2026_0279 |
| Vreeken, J. | ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES | ICAS2026_0871 |
| Vu, H.X. | PARAMETRIC DESIGN AND MULTI-OBJECTIVE OPTIMIZATION OF EXHAUST NOZZLE FOR GAS TURBINE ENGINES | ICAS2026_0579 |
| Vu, X.H. | A HYBRID 0D–2D WHOLE-ENGINE MATCHING FRAMEWORK FOR TURBOJET ENGINE PERFORMANCE SIMULATION | ICAS2026_0687 |
| Wade, J. | LLM-ASSISTED GENERATION OF SYSML V2 MODELS FROM STRUCTURED ENGINEERING REPORTS | ICAS2026_0279 |
| Waghorn, C. | FUTURE SUSTAINABLE AVIATION INFRASTRUCTURE: PROSPECTS & CHALLENGES FROM CHRISTCHURCH AIRPORT\'S PERSPECTIVE | ICAS2026_1027 |
| Wagner, A. | A GRAPH NEURAL NETWORK SIMULATOR FOR TRANSONIC VORTEX-DOMINATED FLOWS ON THE DLR-F23 CONFIGURATION | ICAS2026_0358 |
| Wagner, A. | REYNOLDS NUMBER SCALING EFFECTS IN TRANSONIC CAVITY AERODYNAMICS: A HIGH-FIDELITY EXPERIMENTAL AND NUMERICAL FRAMEWORK | ICAS2026_0362 |
| Wagner, O. | GAP OPTIMIZATION ADAPTIVE TOOL FOR LARGE SCALE FLEXIBLE STRUCTURE ASSEMBLY | ICAS2026_0058 |
| Wahls, R. | GLOBAL SUSTAINABLE AVIATION PANEL DISCUSSION WITH VERONIQUE ROCA, ALAN NEWBY, JIM HILEMAN, CHRISTINE ANDREWS, RICH WAHLS AND CLAIRE WAGHORN (DURATION 100 MINUTES) | ICAS2026_0982 |
| Wainwright, T. | ASSESSING VORTEX BREAKDOWN AND COUPLING IN DELTA WING PLANFORMS THROUGH HIGH-FIDELITY DDES SIMULATIONS | ICAS2026_0939 |
| Waite, L.L. | A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION. | ICAS2026_0041 |
| Wakayama, S. | A BENCHMARK FOR UNCERTAINTY QUANTIFICATION AND OPTIMIZATION UNDER UNCERTAINTY IN CONCEPTUAL AIRCRAFT DESIGN: THE F25-OUU CHALLENGE PROBLEM | ICAS2026_0320 |
| Wan, Z. | TEMPORAL INJECTION FOR REAL-TIME FLYING-BIRD DETECTION WITH RT-DETR | ICAS2026_0457 |
| Wang, A. | GEOMETRY PARAMETERISATION VIA A STRUCTURAL MODAL BASIS FOR AERODYNAMIC SHAPE OPTIMISATION | ICAS2026_0155 |
| Wang, B. | A SINGLE-LOOP BAYESIAN OPTIMIZATION FRAMEWORK FOR MULTIDISCIPLINARY DESIGN OPTIMIZATION UNDER UNCERTAINTY | ICAS2026_0524 |
| Wang, B.X. | A DISTRIBUTED MULTI-SOURCE SENSOR FUSION METHOD FOR COLLABORATIVE TARGET TRACKING | ICAS2026_0590 |
| Wang, C. | PREDEFINED-TIME AFFINE FORMATION FAULT-TOLERANT CONTROL FOR FIXED-WING UAVS WITH INPUT SATURATION | ICAS2026_0098 |
| Wang, C.-H. | DEVELOPMENT OF CONDUCTIVE COMPOSITE MATERIALS FOR HIGH VOLTAGE APPLICATIONS | ICAS2026_0036 |
| Wang, C.Q. | ADAPTIVE PRACTICAL PRESCRIBED-TIME FAULT-TOLERANT CONTROL FOR SMALL TANDEM-ROTOR UAV FORMATIONS | ICAS2026_0037 |
| Wang, C.Y. | COMPRESSIVE PERFORMANCE OF VARIABLE-STIFFNESS COMPOSITE HYPERBOLIC STIFFENED PANELS BASED ON GEOMETRIC PATH MAPPING | ICAS2026_0082 |
| Wang, G. | AN ADAPTIVE AND PARAMETER-FREE SLOPE LIMITER FOR UNSTRUCTURED COMPRESSIBLE FLOW SOLVER | ICAS2026_0241 |
| Wang, G. | QUANTIFYING LAND AERIAL RESCUE DEMAND INTENSITY: A DATA-DRIVEN MODELING APPROACH FOR DEFINING THE AIR-GROUND OPERATIONAL BOUNDARY | ICAS2026_0298 |
| Wang, G. | SYSTEM EFFECTIVENESS EVALUATION OF CHINA'S AVIATION EMERGENCY COMMUNICATION SYSTEM | ICAS2026_0322 |
| Wang, G. | NUMERICAL STUDY ON DYNAMIC STALL OF FIGHTER AIRCRAFT AT HIGH ANGLE OF ATTACK USING DYNAMIC IMPROVED DELAYED DETACHED EDDY SIMULATION | ICAS2026_0480 |
| Wang, G. | MODELING, SIMULATION AND EVALUATION OF LARGE FOREST FIRE EXTINGUISHING AND RESCUE BASED ON AVIATION MATERIEL | ICAS2026_0910 |
| Wang, H. | MULTIPHYSICS COUPLING EFFECT ON INTERFACIAL PROPERTIES OF CNT/GFRP/CFRP COMPOSITES FOR ELECTROTHERMAL ANTI-/DE-ICING APPLICATIONS | ICAS2026_0083 |
| Wang, H. | EFFECTS OF FLAPPING–PITCHING PHASE DIFFERENCE ON THE AERODYNAMIC PERFORMANCE OF HOVERING DRAGONFLY WINGS | ICAS2026_0193 |
| Wang, H. | NUMERICAL STUDY ON DYNAMIC STALL OF FIGHTER AIRCRAFT AT HIGH ANGLE OF ATTACK USING DYNAMIC IMPROVED DELAYED DETACHED EDDY SIMULATION | ICAS2026_0480 |
| Wang, H.-Y. | AN ADAPTIVE AND PARAMETER-FREE SLOPE LIMITER FOR UNSTRUCTURED COMPRESSIBLE FLOW SOLVER | ICAS2026_0241 |
| Wang, J. | AERODYNAMIC EFFECTS OF DISTRIBUTED PROPULSION WING CONFIGURATION PARAMETERS | ICAS2026_0062 |
| Wang, J. | AERODYNAMIC OPTIMIZATION DESIGN OF FULL-WING SOLAR-POWERED UAV FOR FLOW SEPARATION CONTROL | ICAS2026_0122 |
| Wang, J. | EFFECTS OF FLAPPING–PITCHING PHASE DIFFERENCE ON THE AERODYNAMIC PERFORMANCE OF HOVERING DRAGONFLY WINGS | ICAS2026_0193 |
| Wang, J. | STRUCTURAL DESIGN AND PERFORMANCE STUDY OF A TWO-STAGE DYNAMIC PRESSURE OIL-AIR SEPARATOR | ICAS2026_0341 |
| Wang, J.H. | PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA | ICAS2026_0624 |
| Wang, K. | AERODYNAMIC EFFECTS OF DISTRIBUTED PROPULSION WING CONFIGURATION PARAMETERS | ICAS2026_0062 |
| Wang, K. | AERODYNAMIC OPTIMIZATION DESIGN OF FULL-WING SOLAR-POWERED UAV FOR FLOW SEPARATION CONTROL | ICAS2026_0122 |
| Wang, K. | EFFECT OF LIP/NOZZLE DEFLECTION ANGLE ON THE AERODYNAMIC AND PROPULSIVE CHARACTERISTICS OF PROPULSIVE WING UNIT | ICAS2026_0200 |
| Wang, K.-L. | INVESTIGATION OF DISTRIBUTED PROPELLER PROPULSIVE CHARACTERISTICS UNDER NON-AXIAL INFLOW | ICAS2026_0108 |
| Wang, L. | COMPARATIVE DESIGN OF SBW AIRCRAFT WITH AERODYNAMIC SHAPE OPTIMIZATION FOR THREE DIFFERENT PROPULSION LAYOUTS | ICAS2026_0078 |
| Wang, L. | BALANCING STRENGTH AND THERMAL CONDUCTIVITY IN LPBF-PROCESSED ALUMINUM-BASED MATERIALS | ICAS2026_0124 |
| Wang, L. | A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS | ICAS2026_0538 |
| Wang, L.X. | PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA | ICAS2026_0624 |
| Wang, L.X. | BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL | ICAS2026_0647 |
| Wang, L.Z. | ROBUST ATTITUDE RECOVERY CONTROL FOR AIR-LAUNCHED FOLDING-WING UAVS VIA DISTURBANCE-COMPENSATED SUPER-TWISTING SLIDING MODE | ICAS2026_0506 |
| Wang, P.Y. | JET-INDUCED SWIRLING FLOW AND WALL HEAT TRANSFER FOR AERO-ENGINE NACELLE SWIRL ANTI-ICING SYSTEM | ICAS2026_0339 |
| Wang, R. | AERODYNAMIC REQUIREMENTS ASSESSMENT OF CIVIL AIRCRAFT BASED ON AIRWORTHINESS PERFORMANCE | ICAS2026_0106 |
| Wang, R. | DATA-DRIVEN AERODYNAMIC MODEL OF THE DISTRIBUTED PROPULSION WING | ICAS2026_0297 |
| Wang, R. | RESEARCH ON FLIGHT DYNAMICS AND CONTROL CHARACTERISTICS OF MULTI-UAV WINGTIP-LINKED FLIGHT | ICAS2026_0815 |
| Wang, R. | RAPID FLIGHT DYNAMICS EVALUATION OF STRONGLY COUPLED DISTRIBUTED PROPULSION | ICAS2026_0874 |
| Wang, R.Q. | STUDY ON DAMAGE SEVERITY ASSESSMENT METHODS FOR ASYMMETRICALLY DAMAGED LOITERING MUNITIONS | ICAS2026_0306 |
| Wang, S. | RESEARCH ON AERODYNAMIC-STEALTH INTEGRATED DESIGN METHODOLOGY BASED ON MPPO ALGORITHM | ICAS2026_0462 |
| Wang, S. | SUPERVISED DIMENSIONALITY-REDUCED MULTI-FIDELITY SURROGATE MODEL ASSISTED HIGH-DIMENSIONAL NATURAL LAMINAR FLOW OPTIMIZATION | ICAS2026_0502 |
| Wang, S.-K. | MULTI-SCALE LINEAR FEATURE MODULATION DEEP NEURAL OPERATOR FOR RAPID PRESSURE COEFFICIENT PREDICTION | ICAS2026_0473 |
| Wang, S.K. | SPARSE POLYNOMIAL CHAOS-BASED ROBUST OPTIMIZATION DESIGN OF AERODYNAMIC AND SONIC BOOM | ICAS2026_0235 |
| Wang, T. | RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING | ICAS2026_0782 |
| Wang, T.Q. | TEMPORAL INJECTION FOR REAL-TIME FLYING-BIRD DETECTION WITH RT-DETR | ICAS2026_0457 |
| Wang, W. | AFTERBODY CURVATURE EFFECTS ON FLOW LOSS CHARACTERISTICS BASED ON ENTROPY PRODUCTION | ICAS2026_0781 |
| Wang, W. | CYCLOSTATIONARY ANALYSIS AND UNSUPERVISED CLUSTERING FOR DETECTING CRACKS IN HELICOPTER GEARBOX CASING | ICAS2026_1111 |
| Wang, W.Z. | COMPRESSIVE PERFORMANCE OF VARIABLE-STIFFNESS COMPOSITE HYPERBOLIC STIFFENED PANELS BASED ON GEOMETRIC PATH MAPPING | ICAS2026_0082 |
| Wang, X. | CST PARAMETRIC MODELING AND MULTI-OBJECTIVE OPTIMIZATION RECONFIGURATION STUDY OF A BLENDED-WING-BODY AIRCRAFT | ICAS2026_0455 |
| Wang, X. | A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS | ICAS2026_0538 |
| Wang, X. | UNIFIED SEPARATION ASSURANCE FOR MULTI-UAV OPERATIONS: RISK-CALIBRATED BASELINES AND FAULT-AWARE ADAPTIVE RESOLUTION | ICAS2026_0554 |
| Wang, Y. | MULTIPHYSICS COUPLING EFFECT ON INTERFACIAL PROPERTIES OF CNT/GFRP/CFRP COMPOSITES FOR ELECTROTHERMAL ANTI-/DE-ICING APPLICATIONS | ICAS2026_0083 |
| Wang, Y. | MULTIPHYSICS COUPLING EFFECT ON INTERFACIAL PROPERTIES OF CNT/GFRP/CFRP COMPOSITES FOR ELECTROTHERMAL ANTI-/DE-ICING APPLICATIONS | ICAS2026_0083 |
| Wang, Y. | EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN | ICAS2026_0490 |
| Wang, Y. | EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT ENHANCEMENT OF A HIGH-LIFT CONFIGURATION | ICAS2026_0516 |
| Wang, Y. | LOW-NOISE VERTIPORT PROCEDURE PLANNING USING DEEP REINFORCEMENT LEARNING | ICAS2026_0580 |
| Wang, Y. | RECIPROCITY-GUIDED JOINT BASE STATION PLACEMENT AND FLIGHT CORRIDOR PLANNING FOR URBAN AIR MOBILITY | ICAS2026_0587 |
| Wang, Y. | GEOMETRY-DRIVEN AIR TRAFFIC CONFLICT RESOLUTION VIA CAUCHY-STOKES RANDERS METRIC | ICAS2026_0605 |
| Wang, Y.-H. | EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT ENHANCEMENT OF A HIGH-LIFT CONFIGURATION | ICAS2026_0516 |
| Wang, Y.B. | STRUCTURAL DESIGN AND PERFORMANCE STUDY OF A TWO-STAGE DYNAMIC PRESSURE OIL-AIR SEPARATOR | ICAS2026_0341 |
| Wang, Y.Y. | AN EMBEDDED PHYSICS-INFORMED NEURAL NETWORK (PINN) FRAMEWORK FOR HIGH-FIDELITY REAL-TIME SIMULATION OF A FLIGHT CONTROL SURFACE ACTUATION SYSTEM | ICAS2026_0715 |
| Wang, Y.Z. | RESEARCH ON EFFECTIVENESS-DRIVEN INTELLIGENT OPTIMIZATION METHOD FOR CONCEPTUAL LAYOUT OF AIRCRAFT | ICAS2026_0596 |
| Wang, Y.Z. | COARSE–FINE COUPLED MBSE FOR SURVIVABILITY PARAMETER DESIGN OF STEALTH CARRIER-BASED TANKER | ICAS2026_0671 |
| Wang, Z. | INVESTIGATION OF PLUME NON-EQUILIBRIUM INFRARED RADIATION CHARACTERISTICS AT DIFFERENT MACH NUMBERS | ICAS2026_0043 |
| Wang, Z. | PROCESS OPTIMIZATION, MANUFACTURING QUALITY AND MECHANICAL PROPERTIES OF HIGH-VOLUME-FRACTION TIB2 REINFORCED AL-BASED COMPOSITES PREPARED BY SELECTIVE LASER MELTING | ICAS2026_0126 |
| Wang, Z. | MISSION-PROFILE-BASED HYBRID POWER SYSTEM DESIGN AND OPTIMIZATION FOR VTOL AIRCRAFT IN REGIONAL AIR MOBILITY | ICAS2026_0696 |
| Wang, Z. | COOPERATIVE TRACKING ALGORITHM OF MULTIPLE UAVS USING PSO FOR AERIAL SURVEILLANCE | ICAS2026_0709 |
| Wang, Z. | RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING | ICAS2026_0782 |
| Wang, Z. | NUMERICAL INVESTIGATION OF GEOMETRIC EFFECTS ON INFRARED CHARACTERISTICS OF MULTI-STREAM SERPENTINE NOZZLES | ICAS2026_0788 |
| Wang, Z.H. | EARLY WARNING FOR POTENTIAL BIRD STRIKES: STRATEGIC OPTIMIZATION OF PAN-TILT-ZOOM SENSOR NETWORKS FOR BIRD HAZARD DECREASE IN AIRPORT ENVIRONMENT | ICAS2026_0439 |
| Wang, Z.Q. | AUTOMATIC GENERATION OF PHYSICAL SYSTEM MODELS FOR AIRCRAFT SYSTEMS BASED ON LLMS | ICAS2026_0479 |
| Warnakula, K. | DESIGN ASSESSMENT OF A HELICOPTER BLADE | ICAS2026_0225 |
| Wart, A. | THE DART HYPERSONIC VEHICLE: FROM CONCEPT TO LAUNCH | ICAS2026_1072 |
| Watkins, D. | APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS | ICAS2026_0359 |
| Watkins, D. | AI IN THE COCKPIT: THE JARVIS STORY | ICAS2026_0547 |
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| Weber, M. | RESEARCH PLATFORM AIRSHIP: DESIGN AND FLIGHT CHARACTERISTICS FOR URBAN OPERATIONS | ICAS2026_0576 |
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| Wehrel, P. | CONCEPTUAL PERFORMANCE AND MASS ASSESSMENT OF AN OPEN FAN ENGINE FOR THE DLR-F25 AIRCRAFT | ICAS2026_0261 |
| Wehrel, P. | MODULAR JET AND PROPELLER ENGINE – PART II: INTEGRATED DESIGN PROCESS AND DESIGN SPACE ASSESSMENT | ICAS2026_0829 |
| Wehrend, S. | LINKING PRODUCT FAMILY ARCHITECTURE ANALYSIS AND COMPONENT-LEVEL OPTIMISATION USING SYSTEM MODELS | ICAS2026_0305 |
| Wei, D. | EXPERIMENTAL INVESTIGATION OF FRETTING WEAR IN TI-6AL-4V DOVETAIL ASSEMBLIES UNDER RESONANT VIBRATION | ICAS2026_0127 |
| Wei, D. | FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES | ICAS2026_0171 |
| Wei, D. | MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK | ICAS2026_0493 |
| Wei, D.S. | FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING | ICAS2026_0172 |
| Wei, L. | 3D ANALYSIS AND PREDICTION FOR ASSEMBLY STEP DEVIATIONS OF FOUR-BAR LINKAGE BAY DOORS | ICAS2026_0140 |
| Wei, W. | MULTIDISCIPLINARY PHYSICS-CONSTRAINED GENERATIVE DESIGN OF DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2026_0088 |
| Wei, W.Y. | INVERSE AEROELASTIC SIZING FOR STRUT-BRACED WINGS VIA PHYSICS-GUIDED GENERATIVE MODELING | ICAS2026_0100 |
| Wei, X. | COMPARATIVE ANALYSIS OF DIFFERENT NUMERICAL SIMULATION METHODS FOR PROPELLER SLIPSTREAM | ICAS2026_0795 |
| Wei, X. | AILERON EFFICIENCY ANALYSIS OF FLEXIBLE HIGH-ASPECT-RATIO WING | ICAS2026_0796 |
| Wei, Y. | ACTIVE FLOW CONTROL AND THERMAL PROTECTION FOR A WING-BODY CONFIGURATION BASED ON LATERAL JET | ICAS2026_0255 |
| Wei, Y. | LEAKAGE PREDICTION AND GEOMETRIC PARAMETER OPTIMIZATION OF STEPPED LABYRINTH SEALS BASED ON DATA-DRIVEN SURROGATE MODELS | ICAS2026_0862 |
| Weightman, J. | MECHANISMS OF SCREECH MODE STAGING IN UNDEREXPANDED SUPERSONIC JETS | ICAS2026_1082 |
| Weiser, C. | FLIGHT TESTING OF A HIGH-ALTITUDE UNCREWED AND SOLAR POWERED PLATFORM HEAVIER THAN AIR | ICAS2026_0296 |
| Weiser, C. | FLIGHT ENVELOPE PROTECTION FOR HIGH ALTITUDE LONG ENDURANCE AIRCRAFT | ICAS2026_0441 |
| Wende, G. | PHYSICS-INFORMED NEURAL NETWORKS FOR ULTRASONIC LAMB WAVE RECONSTRUCTION IN NON-DESTRUCTIVE TESTING | ICAS2026_0573 |
| Werner, M. | REYNOLDS NUMBER SCALING EFFECTS IN TRANSONIC CAVITY AERODYNAMICS: A HIGH-FIDELITY EXPERIMENTAL AND NUMERICAL FRAMEWORK | ICAS2026_0362 |
| Werthwein, M. | VLSEC: A CONCEPT FOR SECURING VIRTUAL LINKS IN AVIONICS NETWORKS THROUGH CENTRALIZED GROUP KEY MANAGEMENT | ICAS2026_0701 |
| Weyh, T. | RECONFIGURABLE MULTILEVEL BATTERY ARCHITECTURE FOR SMALL UAV PROPULSION SYSTEMS | ICAS2026_0684 |
| Weyh, T. | ANALYSIS OF SOFTWARE DEVELOPMENT METHODS FOR A RECONFIGURABLE BATTERY SYSTEM FOR USE IN AN ELECTRIC AIRCRAFT | ICAS2026_0957 |
| White, P. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Whiteman, L. | RE-THINKING END OF LIFE AIRCRAFT INTERIORS THROUGH CO-DESIGN AND REPURPOSING | ICAS2026_0840 |
| Whittaker, J.J. | PARAMETRIC AERODYNAMIC STUDY OF LEADING-EDGE SERRATIONS ON WING SECTIONS ACROSS REYNOLDS NUMBERS | ICAS2026_0723 |
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| Widjaja, W. | COMPARING DIFFERENT SEMI-EMPIRICAL AERODYNAMIC TOOLS FOR ANALYSING NOVEL AIRCRAFT CONFIGURATIONS | ICAS2026_0445 |
| Wierach, P. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Wies, M. | ASSESSING AN ALTERNATE AIRPORT ASSISTANT | ICAS2026_0192 |
| Willems, F. | AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES | ICAS2026_0954 |
| Williams, S.P. | X-59 EXTERNAL VISION SYSTEM FLIGHT TESTING | ICAS2026_0769 |
| Williams, T. | EFFECT OF INTAKE AERODYNAMICS AND FLOW DISTORTION ON FAN STALL INCEPTION | ICAS2026_0111 |
| Winhard, A. | DYN-MARS: A NEW CONCEPT ENABLING THE BEST APPROACH FLIGHT PROFILE | ICAS2026_0265 |
| Winski, C.S. | CROSS-TEST COMPARISONS AND REYNOLDS NUMBER EFFECTS IN THE CRM-HL ECOSYSTEM | ICAS2026_0844 |
| Winski, C.S. | ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL | ICAS2026_0977 |
| Wits, W.W. | MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS | ICAS2026_1006 |
| Wolde, M. | WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH | ICAS2026_0438 |
| Wong, K.C. | EXPERIMENTAL FLIGHT DYNAMICS AND CONTROL OF AN AGILE FIXED-WING UAV USING HYBRID ONBOARD AND OFFBOARD CONTROL | ICAS2026_0259 |
| Wong, K.C. | ENERGY DISSIPATION OF THIN-WALLED RIBBED SPHERES FOR CARGO AIRDROP | ICAS2026_0290 |
| Wong, K.C. | RESONANT ELASTIC SHAFT THRUST VECTORING: IMPLICATIONS FOR UAV DESIGNS | ICAS2026_0484 |
| Wong, K.C. | GUST ERROR METHOD (GEM): PARAMETER IDENTIFICATION FOR AIRCRAFT SUBJECT TO VON KÁRMÁN PROCESS NOISE | ICAS2026_0633 |
| Wong, K.C. | COOPERATIVE TRACKING ALGORITHM OF MULTIPLE UAVS USING PSO FOR AERIAL SURVEILLANCE | ICAS2026_0709 |
| Wong, K.C. | DRONE TECHNOLOGIES IN AUSTRALIA: FROM AIR-VEHICLE DEVELOPMENT TO AUTONOMOUS FLIGHT SYSTEMS | ICAS2026_1045 |
| Woo, J. | PHYSICS-INFORMED LEARNING-BASED RECOVERY TRAJECTORY PREDICTION FOR AUTOMATIC GROUND COLLISION AVOIDANCE | ICAS2026_0865 |
| Wood, N.G. | INTERFACING MISSION SIMULATION WITH INTELLIGENT AGENTIC SYSTEMS FOR OPERATIONAL AND ETHICAL EVALUATION | ICAS2026_0675 |
| Wozniak, P. | MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS | ICAS2026_0143 |
| Wu, F. | LOW-NOISE VERTIPORT PROCEDURE PLANNING USING DEEP REINFORCEMENT LEARNING | ICAS2026_0580 |
| Wu, F. | RECIPROCITY-GUIDED JOINT BASE STATION PLACEMENT AND FLIGHT CORRIDOR PLANNING FOR URBAN AIR MOBILITY | ICAS2026_0587 |
| Wu, F. | GEOMETRY-DRIVEN AIR TRAFFIC CONFLICT RESOLUTION VIA CAUCHY-STOKES RANDERS METRIC | ICAS2026_0605 |
| Wu, J. | AN EFFICIENT TRANSITION PREDICTION METHOD USING NEURAL NETWORK SURROGATE MODELS | ICAS2026_0254 |
| Wu, J.M. | EFFECTS OF SLOT LOCATION ON FLOW AND HEAT TRANSFER IN A LATTICEWORK COOLING CHANNEL: AN MRV EXPERIMENT AND NUMERICAL STUDY | ICAS2026_0545 |
| Wu, T. | OPTIMIZATION OF MORPHOLOGICAL AND KINEMATIC PARAMETER FOR FLAPPING WING IN FORWARD FLIGHT | ICAS2026_0089 |
| Wu, W. | FLYING BY THE THREAD OF MY PANTS: USING HOUSEHOLD TEXTILES COMPOSITES FOR ACCESSIBLE UAV AIRFRAMES | ICAS2026_0499 |
| Wu, Y. | PHYSICAL DESIGN CONCEPTS OF VORTEX GENERATOR ARRAYS FOR AIRCRAFT AFT-BODIES DRIVEN BY DISTINCT DRAG REDUCTION MECHANISMS | ICAS2026_0185 |
| Wu, Y. | RESPONSE CHARACTERISTICS OF WINGTIP VORTEX INSTABILITY TO EXTERNAL DISTURBANCES | ICAS2026_0194 |
| Wu, Y. | A BILEVEL STRATEGY FOR ON-DESIGN EVTOL SIZING AND OFF-DESIGN STRUCTURAL WEIGHT OPTIMIZATION | ICAS2026_0209 |
| Wu, Y. | QUANTIFYING LAND AERIAL RESCUE DEMAND INTENSITY: A DATA-DRIVEN MODELING APPROACH FOR DEFINING THE AIR-GROUND OPERATIONAL BOUNDARY | ICAS2026_0298 |
| Wu, Y. | NUMERICAL INVESTIGATION OF GEOMETRIC EFFECTS ON INFRARED CHARACTERISTICS OF MULTI-STREAM SERPENTINE NOZZLES | ICAS2026_0788 |
| Wu, Y. | RESEARCH ON FLIGHT DYNAMICS AND CONTROL CHARACTERISTICS OF MULTI-UAV WINGTIP-LINKED FLIGHT | ICAS2026_0815 |
| Wu, Y. | MODELING, SIMULATION AND EVALUATION OF LARGE FOREST FIRE EXTINGUISHING AND RESCUE BASED ON AVIATION MATERIEL | ICAS2026_0910 |
| Wu, Z. | PHYSICS-INFORMED NEURAL NETWORK BASED MODELING OF DYNAMIC BEHAVIOR OF AERIAL REFUELING HOSE | ICAS2026_0109 |
| Wu, Z. | PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA | ICAS2026_0624 |
| Wyman, N. | GEOMETRY AND MESHING ADVANCEMENTS TOWARD CFD VISION 2030 | ICAS2026_1000 |
| Wyman, N.J. | THE ROLE OF NEXT-GENERATION HPC AND MACHINE LEARNING IN ACHIEVING THE 2030 VISION GOALS | ICAS2026_1022 |
| Würfel, J. | EXPLAINABILITY AT ALL LEVELS OF SYSTEM DEVELOPMENT: INSIGHTS FROM THE DESIGN OF INTELLIGENT SYSTEMS IN AVIATION | ICAS2026_0177 |
| Wöhler, S. | CONCEPTUAL PERFORMANCE AND MASS ASSESSMENT OF AN OPEN FAN ENGINE FOR THE DLR-F25 AIRCRAFT | ICAS2026_0261 |
| Wöhler, S. | ADVANCED MODELING AND ANALYSIS OF A LIQUID HYDROGEN SHORT-MEDIUM RANGE AIRCRAFT CONCEPT FOR 2035 | ICAS2026_0333 |
| Xi, L. | PROCESS OPTIMIZATION, MANUFACTURING QUALITY AND MECHANICAL PROPERTIES OF HIGH-VOLUME-FRACTION TIB2 REINFORCED AL-BASED COMPOSITES PREPARED BY SELECTIVE LASER MELTING | ICAS2026_0126 |
| Xi, Y. | HYPERSONIC RECEPTIVITY TO FREESTREAM DISTURBANCES OVER A BLUNT WEDGE: A LINEARIZED NAVIER-STOKES APPROACH | ICAS2026_0653 |
| Xi, Z.Y. | FLUTTER ANALYSIS OF A DYNAMIC VARIABLE-SWEEP WING | ICAS2026_0179 |
| Xiang, Y. | PHYSICAL DESIGN CONCEPTS OF VORTEX GENERATOR ARRAYS FOR AIRCRAFT AFT-BODIES DRIVEN BY DISTINCT DRAG REDUCTION MECHANISMS | ICAS2026_0185 |
| Xiang, Y. | RESPONSE CHARACTERISTICS OF WINGTIP VORTEX INSTABILITY TO EXTERNAL DISTURBANCES | ICAS2026_0194 |
| Xiao, B. | PHYSICS-INFORMED NEURAL NETWORK BASED MODELING OF DYNAMIC BEHAVIOR OF AERIAL REFUELING HOSE | ICAS2026_0109 |
| Xiao, D. | PERFORMANCE DEGRADATION ASSESSMENT METHOD FOR AERO-ENGINES ACROSS THE FULL-LIFE-CYCLE BASED ON DIGITAL TWIN | ICAS2026_0856 |
| Xiao, H. | PARAMETER INVERSION ALGORITHM FOR AERO-ENGINE γ-PHOTON FLOW FIELD IMAGES BASED ON UNET-GAN ARCHITECTURE | ICAS2026_0264 |
| Xiao, H. | NUMERICAL SIMULATION OF HYPERSONIC PLASMA FLOW BASED ON NONLINEAR COUPLED CONSTITUTIVE RELATIONS | ICAS2026_0311 |
| Xiao, H. | PD-STGNN: A PHYSICS-INFORMED DYNAMIC SPATIO-TEMPORAL GRAPH NEURAL NETWORK FOR AERO-ENGINE THRUST PREDICTION | ICAS2026_0314 |
| Xiao, W.D. | PILOT WORKLOAD PROFILES UNDER CONTINUOUS MULTI-TASKING AND SPARSE EVENTS VIGILANCE | ICAS2026_0091 |
| Xiao, Z. | RESPONSE CHARACTERISTICS OF WINGTIP VORTEX INSTABILITY TO EXTERNAL DISTURBANCES | ICAS2026_0194 |
| Xie, T.-S. | STUDY ON THE INJECTOR JETTING CHARACTERISTICS FOR VENTILATION EFFICIENCY OPTIMIZATION IN AIRCRAFT ENGINE LUBRICATION SYSTEMS | ICAS2026_0849 |
| Xie, T.S. | HIGH-ALTITUDE PERFORMANCE AND ONE-DIMENSIONAL MODELING OF A DUAL-ROTOR GEROTOR PUMP FOR AEROENGINE LUBRICATION SYSTEMS | ICAS2026_0352 |
| Xie, Y. | SLIPSTREAM MODELING AND CONTROL ALLOCATION OF A DISTRIBUTED HETEROGENEOUS ELECTRIC PROPULSION TANDEM-WING UAV | ICAS2026_0138 |
| Xie, Y. | IMPLICATIONS OF AAM OPERATIONS FOR FUTURE SHARED AIRSPACE IN VICTORIA, AUSTRALIA | ICAS2026_1083 |
| Xie, Y.H. | RAPID FLIGHT DYNAMICS EVALUATION OF STRONGLY COUPLED DISTRIBUTED PROPULSION | ICAS2026_0874 |
| Xing, K.A. | RESEARCH ON EFFECTIVENESS-DRIVEN INTELLIGENT OPTIMIZATION METHOD FOR CONCEPTUAL LAYOUT OF AIRCRAFT | ICAS2026_0596 |
| Xu, B.-M. | INVESTIGATION OF DISTRIBUTED PROPELLER PROPULSIVE CHARACTERISTICS UNDER NON-AXIAL INFLOW | ICAS2026_0108 |
| Xu, G. | FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES | ICAS2026_0171 |
| Xu, J. | INVESTIGATION OF PLUME NON-EQUILIBRIUM INFRARED RADIATION CHARACTERISTICS AT DIFFERENT MACH NUMBERS | ICAS2026_0043 |
| Xu, J.H. | A ROTOR TRANSITION PREDICTION METHOD BASED ON GALILEAN INVARIANCE AND THE C1 CROSSFLOW TRANSITION CRITERION | ICAS2026_0463 |
| Xu, L. | NUMERICAL STUDY ON DYNAMIC STALL OF FIGHTER AIRCRAFT AT HIGH ANGLE OF ATTACK USING DYNAMIC IMPROVED DELAYED DETACHED EDDY SIMULATION | ICAS2026_0480 |
| Xu, M. | ANOMALY B-VALUE DETECTION AND EXCLUSION OF GBAS BASED ON WAVELET MULTI-RESOLUTION ANALYSIS | ICAS2026_0028 |
| Xu, M. | A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS | ICAS2026_0538 |
| Xu, S.H. | BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL | ICAS2026_0647 |
| Xu, X. | AN AEROELASTIC DYNAMICS MODELING METHOD FOR INSECT-INSPIRED FLEXIBLE FLAPPING-WING UAV | ICAS2026_0141 |
| Xu, X. | STUDY ON AERODYNAMICS OF THE WING WITH FLAP INSPIRED FROM BIRD COVERTS | ICAS2026_0147 |
| Xu, X. | MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY | ICAS2026_0566 |
| Xu, X.L. | INVESTIGATION ON THE HIGH-EFFICIENCY PROPULSION MECHANISMS OF DUCK-WEBBED PADDLING FOR BIOINSPIRED AIRCRAFT APPLICATIONS | ICAS2026_0182 |
| Xu, X.P. | WIND FIELD PERCEPTION AND FEATURE PREDICTION FOR LOW-ALTITUDE SMALL FIXED-WING UAVS TOWARDS ENERGY HARVESTING | ICAS2026_0742 |
| Xu, X.P. | VANE-LESS 3D WIND ESTIMATION FOR FIXED-WING UAVS: A PHYSICS-AUGMENTED TEMPORAL RESIDUAL NETWORK APPROACH | ICAS2026_0859 |
| Xu, Y.F. | PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA | ICAS2026_0624 |
| Xu, Z. | A HYBRID CNN-LSTM AND PSEUDOSPECTRAL METHOD FOR RAPID SPACECRAFT REENTRY OPTIMIZATION | ICAS2026_0099 |
| Xu, Z. | RESEARCH ON OFFENSIVE AUTONOMOUS VEHICLE TRAJECTORY PREDICTION METHOD BASED ON IMPROVED INVERSE REINFORCEMENT LEARNING IN AIRCRAFT ACTIVE DEFENSE MODE | ICAS2026_0531 |
| Xu, Z.C. | LIGHTWEIGHT BIMETALLIC GEARS FOR AEROSPACE TRANSMISSIONS ENABLED BY OPEN-AIR DIFFUSION BONDING | ICAS2026_0991 |
| Xuan, J. | LIGHTWEIGHT AND ROBUST REAL-TIME DETECTION SYSTEM FOR AIRCRAFT SKIN DEFECTS UNDER COMPLEX UAV INSPECTION CONDITIONS | ICAS2026_0134 |
| Xuan, J. | STUDY ON AERODYNAMICS OF THE WING WITH FLAP INSPIRED FROM BIRD COVERTS | ICAS2026_0147 |
| Xue, D. | OPTIMIZATION OF MORPHOLOGICAL AND KINEMATIC PARAMETER FOR FLAPPING WING IN FORWARD FLIGHT | ICAS2026_0089 |
| Xue, D. | STUDY ON INDUCED DRAG CALCULATION FOR BIRD-LIKE WINGTIP SLOTS USING WAKE-PLANE INTEGRATION | ICAS2026_0466 |
| Xue, D. | RESEARCH ON AN AERODYNAMIC LOAD METHODOLOGY FOR FLAPPING WINGS BASED ON EXPERIMENTALLY ACQUIRED DEFORMATION | ICAS2026_0747 |
| Xue, J. | EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN | ICAS2026_0490 |
| Xun, Y.Y. | SUPERSONIC GROUND EFFECT AERODYNAMICS OF A SLENDER BODY | ICAS2026_0598 |
| Yakimenko, O. | DIGITAL TWIN FOR AIR DEFENSE: LIVE-VIRTUAL-CONSTRUCTIVE INTEGRATION AND DECISION SUPPORT | ICAS2026_0076 |
| Yakimenko, O. | SIMULATION-BASED ANALYSIS OF REDUNDANT UAV NAVIGATION UNDER GNSS OUTAGES | ICAS2026_0079 |
| Yakimenko, O. | ATTITUDE CONTROL TECHNIQUES FOR A MICRO-SCALE FLAP-BASED AERODYNAMIC DECELERATOR SYSTEM | ICAS2026_0361 |
| Yamagami, M. | INITIAL GEOMETRIC UNCERTAINTY ASSESSMENT IN COMPRESSOR AIRFOILS USING PHYSICS-BASED DIRECT MANIPULATED FFD | ICAS2026_0768 |
| Yamaguchi, H. | HPC-BASED PARAMETER SPACE EXPLORATION FOR DENSE PICOSAT FORMATION FLYING TOWARD DIRECT-TO-DEVICE COMMUNICATIONS | ICAS2026_0869 |
| Yamaguchi, H. | MANEUVER- AND DELAY-ROBUST DISTRIBUTED SATELLITE SSA VIA SPATIO-TEMPORAL GRAPH FORECASTING | ICAS2026_0959 |
| Yamaguchi, T. | ROBUST MOTION ESTIMATION FOR INDOOR MAVS USING WIDE-FIELD-INTEGRATION OF OPTIC FLOW | ICAS2026_0163 |
| Yamai, Y. | MULTI-STATE FLIGHT DECK DISPLAY LAYOUT OPTIMIZATION UNDER FAILURE AND REVERSION CONDITIONS | ICAS2026_0604 |
| Yamamoto, K. | AEROACOUSTIC WIND TUNNEL TESTING AND CFD STUDY USING JAXA 8% SEMISPAN HIGH-LIFT COMMON RESEARCH MODEL IN JAXA FQUROH-2 PROJECT | ICAS2026_0756 |
| Yan, H. | NUMERICAL SIMULATION OF SUPERCOOLED LARGE DROPLET IMPINGEMENT ON ROTATING FAN BLADES | ICAS2026_0242 |
| Yan, H. | JET-INDUCED SWIRLING FLOW AND WALL HEAT TRANSFER FOR AERO-ENGINE NACELLE SWIRL ANTI-ICING SYSTEM | ICAS2026_0339 |
| Yan, Y. | A HUMAN-CENTRIC APPROACH TO UNDERSTANDING THE CONTRIBUTING FACTORS OF PILOT-RELATED RUNWAY INCURSIONS | ICAS2026_0086 |
| Yan, Z. | FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES | ICAS2026_0171 |
| Yanagisawa, M. | ROBUST MOTION ESTIMATION FOR INDOOR MAVS USING WIDE-FIELD-INTEGRATION OF OPTIC FLOW | ICAS2026_0163 |
| Yang, C. | FLUTTER ANALYSIS OF A DYNAMIC VARIABLE-SWEEP WING | ICAS2026_0179 |
| Yang, C.Y. | GEOMETRICALLY EXACT MODEL OF CANTILEVER BEAM UNDERGOING LARGE DEFLECTION AND LINEARIZED DYNAMICS CHARACTERIZATION | ICAS2026_0071 |
| Yang, H.-H. | AERO-MECHANICAL ANALYSIS OF A BIRD-INSPIRED ORNITHOPTER USING AN INTEGRATED SIMULATION FRAMEWORK | ICAS2026_0777 |
| Yang, H.C. | EXERGY-BASED AERODYNAMIC CHARACTERISTICS ANALYSIS OF THE NASA COMMON RESEARCH MODEL AND BWB CONFIGURATION CIVIL AIRCRAFT | ICAS2026_0373 |
| Yang, H.C. | 2D AND 3D TRAJECTORY PLANNING FOR UAVS FORMATION SYSTEM USING DYNAMIC WINDOW APPROACH | ICAS2026_0735 |
| Yang, H.C. | INLET OPTIMIZATION DESIGN OF A BOUNDARY LAYER INGESTION PROPULSION SYSTEM | ICAS2026_0906 |
| Yang, I. | HYPERSONIC VEHICLE FLIGHT SIMULATION AND FLIGHT CONTROL | ICAS2026_0174 |
| Yang, K.R. | RESEARCH ON AN AERODYNAMIC LOAD METHODOLOGY FOR FLAPPING WINGS BASED ON EXPERIMENTALLY ACQUIRED DEFORMATION | ICAS2026_0747 |
| Yang, L. | LEAKAGE PREDICTION AND GEOMETRIC PARAMETER OPTIMIZATION OF STEPPED LABYRINTH SEALS BASED ON DATA-DRIVEN SURROGATE MODELS | ICAS2026_0862 |
| Yang, L.K. | 3D ANALYSIS AND PREDICTION FOR ASSEMBLY STEP DEVIATIONS OF FOUR-BAR LINKAGE BAY DOORS | ICAS2026_0140 |
| Yang, R. | 3D ANALYSIS AND PREDICTION FOR ASSEMBLY STEP DEVIATIONS OF FOUR-BAR LINKAGE BAY DOORS | ICAS2026_0140 |
| Yang, R. | FEMTOSECOND LASER PAINT STRIPPING ON AIRCRAFT COATINGS: EXPERIMENTAL AND NUMERICAL ASSESSMENT | ICAS2026_0159 |
| Yang, R. | CURVATURE-CONTROLLED MORPHING OF FOLDING WINGTIPS USING HONEYCOMB PLATES | ICAS2026_0853 |
| Yang, S. | PHYSICS-INFORMED NEURAL NETWORK BASED MODELING OF DYNAMIC BEHAVIOR OF AERIAL REFUELING HOSE | ICAS2026_0109 |
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| Yang, Z.C. | GEOMETRICALLY EXACT MODEL OF CANTILEVER BEAM UNDERGOING LARGE DEFLECTION AND LINEARIZED DYNAMICS CHARACTERIZATION | ICAS2026_0071 |
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| Zhang, C. | IMPLICATIONS OF AAM OPERATIONS FOR FUTURE SHARED AIRSPACE IN VICTORIA, AUSTRALIA | ICAS2026_1083 |
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| Zhang, K.-S. | POINT-CLOUD-BASED INTELLIGENT DESIGN OF FLYING-WING CONFIGURATIONS WITH CONDITIONAL GENERATION AND PRESSURE PREDICTION | ICAS2026_0528 |
| Zhang, K.S | ADAPTIVE-PREFERENCE MULTI-OBJECTIVE REINFORCEMENT LEARNING FOR WIDE-SPEED-REGIME AIRFOIL OPTIMIZATION | ICAS2026_0393 |
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| Zhang, M.X. | STUDY ON DAMAGE SEVERITY ASSESSMENT METHODS FOR ASYMMETRICALLY DAMAGED LOITERING MUNITIONS | ICAS2026_0306 |
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| Zhang, W. | FLIGHT-TEST DATA-DRIVEN HIGH-ANGLE-OF-ATTACK DYNAMICS MODELING VIA LSTM-POLYNOMIAL HYBRID APPROACH | ICAS2026_0269 |
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| Zhang, Y.F. | DATA-DRIVEN TURBULENCE MODELING FOR MULTI-MECHANISM SEPARATED FLOWS OVER ICED AIRFOILS | ICAS2026_0112 |
| Zhang, Y.G. | INVESTIGATION ON THE HIGH-EFFICIENCY PROPULSION MECHANISMS OF DUCK-WEBBED PADDLING FOR BIOINSPIRED AIRCRAFT APPLICATIONS | ICAS2026_0182 |
| Zhang, Y.S. | STUDY ON DAMAGE SEVERITY ASSESSMENT METHODS FOR ASYMMETRICALLY DAMAGED LOITERING MUNITIONS | ICAS2026_0306 |
| Zhang, Y.X. | FEMTOSECOND LASER PAINT STRIPPING ON AIRCRAFT COATINGS: EXPERIMENTAL AND NUMERICAL ASSESSMENT | ICAS2026_0159 |
| Zhang, Z. | PHYSICS-INFORMED NEURAL NETWORK BASED MODELING OF DYNAMIC BEHAVIOR OF AERIAL REFUELING HOSE | ICAS2026_0109 |
| Zhang, Z. | FLIGHT-TEST DATA-DRIVEN HIGH-ANGLE-OF-ATTACK DYNAMICS MODELING VIA LSTM-POLYNOMIAL HYBRID APPROACH | ICAS2026_0269 |
| Zhang, Z. | RESEARCH ON FLIGHT DYNAMICS AND CONTROL CHARACTERISTICS OF MULTI-UAV WINGTIP-LINKED FLIGHT | ICAS2026_0815 |
| Zhang, Z. | VANE-LESS 3D WIND ESTIMATION FOR FIXED-WING UAVS: A PHYSICS-AUGMENTED TEMPORAL RESIDUAL NETWORK APPROACH | ICAS2026_0859 |
| Zhang, Z.P. | REYNOLDS NUMBER EFFECTS OF A BIRD-FEATHER-INSPIRED POROUS-MEDIUM AIRFOIL | ICAS2026_0168 |
| Zhao, B. | MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK | ICAS2026_0493 |
| Zhao, C.L. | PILOT WORKLOAD PROFILES UNDER CONTINUOUS MULTI-TASKING AND SPARSE EVENTS VIGILANCE | ICAS2026_0091 |
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| Zhao, H. | FLIGHT-TEST DATA-DRIVEN HIGH-ANGLE-OF-ATTACK DYNAMICS MODELING VIA LSTM-POLYNOMIAL HYBRID APPROACH | ICAS2026_0269 |
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| Zhao, H. | MULTI-SCALE LINEAR FEATURE MODULATION DEEP NEURAL OPERATOR FOR RAPID PRESSURE COEFFICIENT PREDICTION | ICAS2026_0473 |
| Zhao, H. | MULTI-FIDELITY BAYESIAN NEURAL NETWORKS FOR STEALTH/AERODYNAMIC DATA FUSION METHOD | ICAS2026_0485 |
| Zhao, H. | SUPERVISED DIMENSIONALITY-REDUCED MULTI-FIDELITY SURROGATE MODEL ASSISTED HIGH-DIMENSIONAL NATURAL LAMINAR FLOW OPTIMIZATION | ICAS2026_0502 |
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| Zhao, L. | RECEPTIVITY OF NON-MODAL STREAKS IN HYPERSONIC BLUNT BOUNDARY LAYERS: FROM NUMERICS TO ASYMPTOTICS | ICAS2026_0070 |
| Zhao, L. | QUANTIFYING LAND AERIAL RESCUE DEMAND INTENSITY: A DATA-DRIVEN MODELING APPROACH FOR DEFINING THE AIR-GROUND OPERATIONAL BOUNDARY | ICAS2026_0298 |
| Zhao, L. | SYSTEM EFFECTIVENESS EVALUATION OF CHINA'S AVIATION EMERGENCY COMMUNICATION SYSTEM | ICAS2026_0322 |
| Zhao, L. | PERFORMANCE DEGRADATION ASSESSMENT METHOD FOR AERO-ENGINES ACROSS THE FULL-LIFE-CYCLE BASED ON DIGITAL TWIN | ICAS2026_0856 |
| Zhao, L.Q. | HIGH-PRECISION EDDY-CURRENT TIP CLEARANCE SENSOR WITHEXCEPTIONALHEAT RESISTANCE | ICAS2026_0483 |
| Zhao, R. | GEOMETRICALLY EXACT MODEL OF CANTILEVER BEAM UNDERGOING LARGE DEFLECTION AND LINEARIZED DYNAMICS CHARACTERIZATION | ICAS2026_0071 |
| Zhao, R. | PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA | ICAS2026_0624 |
| Zhao, S.J. | AN EMBEDDED PHYSICS-INFORMED NEURAL NETWORK (PINN) FRAMEWORK FOR HIGH-FIDELITY REAL-TIME SIMULATION OF A FLIGHT CONTROL SURFACE ACTUATION SYSTEM | ICAS2026_0715 |
| Zhao, X. | DESIGN AND INVESTIGATION OF A SHORT-TO-MEDIUM-RANGE AIRCRAFT WITH LIQUID HYDROGEN AND SAF MULTI-FUEL PROPULSION | ICAS2026_0073 |
| Zhao, Y. | UNIFIED SEPARATION ASSURANCE FOR MULTI-UAV OPERATIONS: RISK-CALIBRATED BASELINES AND FAULT-AWARE ADAPTIVE RESOLUTION | ICAS2026_0554 |
| Zhao, Y. | NUMERICAL INVESTIGATION OF GUST LOAD ALLEVIATION FOR WINGS WITH PASSIVELY RELEASED FFWT | ICAS2026_0785 |
| Zhao, Y. | COMPARATIVE ANALYSIS OF DIFFERENT NUMERICAL SIMULATION METHODS FOR PROPELLER SLIPSTREAM | ICAS2026_0795 |
| Zhao, Y. | AILERON EFFICIENCY ANALYSIS OF FLEXIBLE HIGH-ASPECT-RATIO WING | ICAS2026_0796 |
| Zhao, Z.Y. | PERFORMANCE DEGRADATION ANALYSIS OF RESOLVER FAULTS IN ELECTRO-MECHANICAL ACTUATOR | ICAS2026_0784 |
| Zheng, C. | STATIC GROUND EFFECT OF HIGH-ASPECT-RATIO WINGS | ICAS2026_0295 |
| Zheng, H. | NUMERICAL SIMULATION OF SUPERCOOLED LARGE DROPLET IMPINGEMENT ON ROTATING FAN BLADES | ICAS2026_0242 |
| Zheng, H.R. | JET-INDUCED SWIRLING FLOW AND WALL HEAT TRANSFER FOR AERO-ENGINE NACELLE SWIRL ANTI-ICING SYSTEM | ICAS2026_0339 |
| Zheng, X.S. | AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH | ICAS2026_1015 |
| Zheng, Y. | ANOMALY B-VALUE DETECTION AND EXCLUSION OF GBAS BASED ON WAVELET MULTI-RESOLUTION ANALYSIS | ICAS2026_0028 |
| Zhong, C.H. | HIGH-ALTITUDE PERFORMANCE AND ONE-DIMENSIONAL MODELING OF A DUAL-ROTOR GEROTOR PUMP FOR AEROENGINE LUBRICATION SYSTEMS | ICAS2026_0352 |
| Zhong, J. | COMPARATIVE DESIGN OF SBW AIRCRAFT WITH AERODYNAMIC SHAPE OPTIMIZATION FOR THREE DIFFERENT PROPULSION LAYOUTS | ICAS2026_0078 |
| Zhou, C. | PROPULSIVE EFFICIENCY AND ENERGY ANALYSIS OF AIRCRAFT CONCEPTS WITH AFT-FUSELAGE BOUNDARY-LAYER-INGESTION | ICAS2026_1112 |
| Zhou, K.Y. | A ROTOR TRANSITION PREDICTION METHOD BASED ON GALILEAN INVARIANCE AND THE C1 CROSSFLOW TRANSITION CRITERION | ICAS2026_0463 |
| Zhou, L. | INVESTIGATION OF PLUME NON-EQUILIBRIUM INFRARED RADIATION CHARACTERISTICS AT DIFFERENT MACH NUMBERS | ICAS2026_0043 |
| Zhou, L. | AERODYNAMIC EFFECT OF PITCHING MOTION FOR FLAPPING AIRFOIL ACROSS DIFFERENT SWEEPING TRAJECTORIES | ICAS2026_0542 |
| Zhou, L. | NUMERICAL INVESTIGATION OF GEOMETRIC EFFECTS ON INFRARED CHARACTERISTICS OF MULTI-STREAM SERPENTINE NOZZLES | ICAS2026_0788 |
| Zhou, L.B. | MULTI-BODY DYNAMIC MODELING OF A BIRD-LIKE FLAPPING-WING VEHICLE: ANALYSIS OF FLAPPING-AERODYNAMIC COUPLING EFFECTS | ICAS2026_0191 |
| Zhou, Z. | AERODYNAMIC EFFECTS OF DISTRIBUTED PROPULSION WING CONFIGURATION PARAMETERS | ICAS2026_0062 |
| Zhou, Z. | INVESTIGATION OF DISTRIBUTED PROPELLER PROPULSIVE CHARACTERISTICS UNDER NON-AXIAL INFLOW | ICAS2026_0108 |
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| Zhou, Z. | DATA-DRIVEN AERODYNAMIC MODEL OF THE DISTRIBUTED PROPULSION WING | ICAS2026_0297 |
| Zhou, Z. | AUTONOMOUS FLIGHT AND INTELLIGENT TARGET LOCALIZATION FOR JUNGLE RECONNAISSANCE UAVS | ICAS2026_0649 |
| Zhou, Z. | WIND FIELD PERCEPTION AND FEATURE PREDICTION FOR LOW-ALTITUDE SMALL FIXED-WING UAVS TOWARDS ENERGY HARVESTING | ICAS2026_0742 |
| Zhou, Z. | RESEARCH ON FLIGHT DYNAMICS AND CONTROL CHARACTERISTICS OF MULTI-UAV WINGTIP-LINKED FLIGHT | ICAS2026_0815 |
| Zhou, Z. | VANE-LESS 3D WIND ESTIMATION FOR FIXED-WING UAVS: A PHYSICS-AUGMENTED TEMPORAL RESIDUAL NETWORK APPROACH | ICAS2026_0859 |
| Zhou, Z. | RAPID FLIGHT DYNAMICS EVALUATION OF STRONGLY COUPLED DISTRIBUTED PROPULSION | ICAS2026_0874 |
| Zhu, N.H. | AUTONOMOUS FLIGHT AND INTELLIGENT TARGET LOCALIZATION FOR JUNGLE RECONNAISSANCE UAVS | ICAS2026_0649 |
| Zhu, P.-F. | STUDY ON THE INJECTOR JETTING CHARACTERISTICS FOR VENTILATION EFFICIENCY OPTIMIZATION IN AIRCRAFT ENGINE LUBRICATION SYSTEMS | ICAS2026_0849 |
| Zhu, P.F. | HIGH-ALTITUDE PERFORMANCE AND ONE-DIMENSIONAL MODELING OF A DUAL-ROTOR GEROTOR PUMP FOR AEROENGINE LUBRICATION SYSTEMS | ICAS2026_0352 |
| Zhu, R. | A COMPARATIVE STUDY OF THE AERODYNAMIC CHARACTERISTICS OF FOUR CONFIGURATIONS | ICAS2026_0280 |
| Zhu, R.B. | EXERGY-BASED AERODYNAMIC CHARACTERISTICS ANALYSIS OF THE NASA COMMON RESEARCH MODEL AND BWB CONFIGURATION CIVIL AIRCRAFT | ICAS2026_0373 |
| Zhu, R.B. | 2D AND 3D TRAJECTORY PLANNING FOR UAVS FORMATION SYSTEM USING DYNAMIC WINDOW APPROACH | ICAS2026_0735 |
| Zhu, R.B. | INLET OPTIMIZATION DESIGN OF A BOUNDARY LAYER INGESTION PROPULSION SYSTEM | ICAS2026_0906 |
| Zhu, S. | FEMTOSECOND LASER PAINT STRIPPING ON AIRCRAFT COATINGS: EXPERIMENTAL AND NUMERICAL ASSESSMENT | ICAS2026_0159 |
| Zhu, X. | CASCADE ADRC FOR TRAJECTORY TRACKING OF A FLYING-WING SOLAR AIRCRAFT UNDER WIND DISTURBANCES | ICAS2026_0128 |
| Zhu, X. | DATA-DRIVEN AERODYNAMIC MODEL OF THE DISTRIBUTED PROPULSION WING | ICAS2026_0297 |
| Zhu, Y. | RAPID FLIGHT DYNAMICS EVALUATION OF STRONGLY COUPLED DISTRIBUTED PROPULSION | ICAS2026_0874 |
| Zhu, Z. | MULTI-OBJECTIVE OPTIMIZATION OF AERO-ENGINE BEARING CHAMBER SCAVENGE STRUCTURE BASED ON NSGA-II | ICAS2026_0623 |
| Zhu, Z. | HYPERSONIC RECEPTIVITY TO FREESTREAM DISTURBANCES OVER A BLUNT WEDGE: A LINEARIZED NAVIER-STOKES APPROACH | ICAS2026_0653 |
| Zhu, Z.Y. | RESPONSE CHARACTERISTICS OF WINGTIP VORTEX INSTABILITY TO EXTERNAL DISTURBANCES | ICAS2026_0194 |
| Ziakos, N. | AN AUTOMATED PARAMETRIC FRAMEWORK FOR EARLY-STAGE STRUCTURAL DESIGN AND OPTIMIZATION OF COMPOSITE AIRFRAMES | ICAS2026_0948 |
| Zill, T. | FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION | ICAS2026_0888 |
| Zingg, D.W. | SWEEP ANGLE STUDY OF A STRUT-BRACED-WING REGIONAL JET WITH NATURAL LAMINAR FLOW | ICAS2026_0066 |
| Zingg, D.W. | AERODYNAMIC SHAPE OPTIMIZATION OF INFINITE SWEPT WINGS FOR NATURAL LAMINAR FLOW AT TRANSONIC CRUISE CONDITIONS | ICAS2026_0087 |
| Zintl, M. | FAMILIARIZATION, OPERATION, AND DEBRIEFING: AN ADAPTIVE AUGMENTED REALITY SUPPORT SYSTEM FOR UAV FLIGHT TESTING | ICAS2026_0204 |
| Zwane, L. | REFLECTIONS ON THE AEROSPACE ENGINEERING DEVELOPMENT PROGRAMME AT THE CSIR | ICAS2026_0549 |
| Zwingler, A. | IMPACT ASSESSMENT OF COMPONENT FAILURES IN A PEM-FUEL CELL BASED PROPULSION SYSTEM FOR AIRCRAFT APPLICATIONS FOCUSING ON WATER MANAGEMENT | ICAS2026_0139 |
| Özkan, C. | VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS | ICAS2026_0336 |