COMPLETE AUTHOR LIST HYPERLINKED TO PAPERS



Aaltonen, J.FUEL CELLS AND NOVEL THERMAL MANAGEMENT ADVANCEMENTS REQUIRED FOR AVIATIONICAS2022_0079
Abdelmoula, F.THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALEICAS2022_0328
Abdelmoula, F.IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPTICAS2022_0627
Abe, K.COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHODICAS2022_0416
Abhyankar, K.INVESTIGATION ON INTEGRATING RECYCLABILITY AS A FUNCTION AT THE DESIGN PHASE OF COMPLEX-LOADED STRUCTURAL COMPONENTSICAS2022_0125
Abu Salem, K.CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGEICAS2022_0148
Abu-Zurayk, M.APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFTICAS2022_0892
Adler, E.J.AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATIONICAS2022_0593
Adler, E.J.TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATIONICAS2022_0905
Ahn, S.A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSBICAS2022_0222
Ahn, H.J.SAFE REINFORCEMENT LEARNING BASED MULTI-ROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLESICAS2022_0539
Akatsuka, J.FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLETICAS2022_0830
Akman, T.REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFTICAS2022_0797
Alaimo, A.RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALSICAS2022_0218
Alarcon, D.S.DEEP REINFORCEMENT LEARNING FOR EVTOL HOVERING CONTROLICAS2022_0291
Alfredsson, J.HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICSICAS2022_0707
Allan, M.VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATAICAS2022_0124
Allan, M.COMPUTATIONALLY ECONOMICAL METHODS FOR LANDING GEAR NOISE SIMULATIONSICAS2022_0317
Allegaert, E.TEMPLATE-BASED SYNTHESIS OF 3D SYSTEMS FOR MBSEICAS2022_0724
Allen, N.J.IMPACT OF NASCENT TECHNOLOGIES ON THE SUSTAINABILITY ATTRIBUTES OF AN EVOLUTIONARY SINGLE-AISLE AIRCRAFTICAS2022_0543
Allouis, C.A NEW FACILITY FOR HYPERSONIC FLOW SIMULATION DRIVEN BY A HIGH VELOCITY OXYGEN FUEL GUNICAS2022_0437
Almeida, S.F.M.NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIALICAS2022_0059
Almeida, M.A. USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTIONICAS2022_0389
Almeida, L.E.N.EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINEICAS2022_0676
Alonso, G.IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONSICAS2022_0360
Altar Inceer, A.PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINEICAS2022_0782
Alves, L.ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNERICAS2022_0887
Amadori, K.ZERO-EMISSION REGIONAL AVIATION IN SWEDENICAS2022_0650
Amadori, K.UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENTICAS2022_0659
Ammann, N.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
An, Z.HUMAN-MACHINE FUNCTION ALLOCATION METHOD FOR SINGLE PILOT OPERATION USING HESITANT FUZZY 2-TUPLE LINGUISTIC INFORMATIONICAS2022_0493
Anderini, U.HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICSICAS2022_0707
Andersson, J.INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM ALLOY 780ICAS2022_0206
Andersson, P.DEMONSTRATING AN APPROACH FOR MULTIDISCIPLINARY SET BASED DESIGN WITHIN AN AEROSPACE RESEARCH PROJECT - DEFAINEICAS2022_0661
Andreeva-Mori, A.INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONSICAS2022_0904
Andreeva-Mori, A.OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSEICAS2022_0909
Andreeva-Mori, A.AN INTERNATIONAL RESEARCH PERSPECTIVE ON AIRSPACE INTEGRATION IN THE FRAMEWORK OF URBAN AIR MOBILITYICAS2022_0948
Andrés, E.AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGSICAS2022_0020
Andrews, C.HYBRID ELECTRIC PROPULSION DEVELOPMENT FOR COMMERCIAL AVIATIONICAS2022_0944
Andronikos, T.ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUPICAS2022_0335
Ansumali, S.TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHODICAS2022_0630
Anvid, D.H.A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFTICAS2022_0453
Anyu , B.AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNELICAS2022_0411
Aprovitola, A.AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLESICAS2022_0241
Aprovitola, A.AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLEICAS2022_0259
Arcidiacono, S.TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHODICAS2022_0630
Ariaseta, A.INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM ALLOY 780ICAS2022_0206
Ariyarit, A.AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATIONICAS2022_0413
Arjoni, D.HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICSICAS2022_0707
Armani, U.APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDSICAS2022_0643
Armanini, S.F.URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH NON-COOPERATIVE AIRSPACE USERSICAS2022_0567
Armanini, S.F.EVALUATION AND QUANTIFICATION OF THE POTENTIAL CONSEQUENCES OF BIRD STRIKES IN URBAN AIR MOBILITYICAS2022_0629
Arnoult, G.OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACTICAS2022_0843
Arthur, J.J.UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATIONICAS2022_0774
Arvidson, S.EFFECT OF LES LENGTH SCALE AND NUMERICAL SCHEME IN HYBRID RANS-LES OF FREE SHEAR LAYER FLOWSICAS2022_0684
Asai, M.EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETSICAS2022_0243
Aschwanden, P.POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORSICAS2022_0347
Assato, M.PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINEICAS2022_0782
Asseman, P.OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGNICAS2022_0550
Atif, M.HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONSICAS2022_0894
Atinault, O.OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACTICAS2022_0843
Atkin, C.J. STABILITY OF A LAMINAR BOUNDARY LAYER OVER LOCALISED SURFACE INDENTATIONICAS2022_0697
Augello, R.A GLOBAL/LOCAL ELEMENT-WISE APPROACH FOR THE BUCKLING AND POST-BUCKLING ANALYSIS OF THIN MULTILAYERED STRUCTURESICAS2022_0253
Autenrieb, J.COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACSICAS2022_0505
Avanzini, G.SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSISICAS2022_0370
Avellán, R.ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATORICAS2022_0382
Avellan, R.MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEMICAS2022_0832
Aydin, E.CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACHICAS2022_0102
Aydin, S.M.AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPESICAS2022_0381
Azevedo, J.L.F.ON THE INFLUENCE OF GRADIENT RECONSTRUCTION PROCEDURES OVER THE ACCURACY OF FINITE VOLUME BASED SCHEMESICAS2022_0191
Azevedo, J.L.F.A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTSICAS2022_0672
Azevedo, J.L.F.STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWSICAS2022_0726
Azevedo, J.L.FAUTOMATIC FREE-FORM DEFORMATION AS GEOMETRIC PARAMETERIZATION FOR AERODYNAMIC DESIGNICAS2022_0749
Azzara, R.NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF UNSTIFFENED AND STIFFENED STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGSICAS2022_0220
Baba, I.DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITESICAS2022_0448
Babetto, L.SORA-BASED RISK ASSESSMENT FOR CARGO UNMANNED AERIAL VEHICLES IN THE UAM FRAMEWORKICAS2022_0240
Bae, J.-S.ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGIONICAS2022_0827
Bagassi, S.VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTSICAS2022_0247
Bagassi, S.V/A-R AIR GESTURES HMI INTERACTION IN AIRPORT CONTROL TOWERSICAS2022_0452
Bagassi, S.AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACHICAS2022_0478
Bagassi, S.POTENTIAL OF EXTENDED REALITY IN ENGINEERING AND CHALLENGES OF UNCONVENTIONAL VEHICLE DESIGNICAS2022_0966
Bagdatli, B.SYSTEM LEVEL IDENTIFICATION OF CRITICAL UNCERTAINTIES TO ENABLE VALIDATION EXPERIMENTSICAS2022_0935
Bahrami, F.TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMSICAS2022_0604
Bai, J.Q.AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORKICAS2022_0199
Balack, P.IMPACT OF THE NUMBER OF WING STATIONS ON THE TWIST DISTRIBUTION OF A BWB CONCEPTUAL AIRCRAFT DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTIONICAS2022_0854
Balchanos, M.A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFTICAS2022_0453
Baldochi, L. A.USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTIONICAS2022_0389
Bando, M.ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOWICAS2022_0476
Bando, M.INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCEICAS2022_0796
Bang, H.INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFTICAS2022_0346
Bang, H.-C.FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSIONICAS2022_0438
Bang, H.C.SAFE REINFORCEMENT LEARNING BASED MULTI-ROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLESICAS2022_0539
Banks-Davies, L.EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILTROTOR AIRCRAFTICAS2022_0530
Bao, C.AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNELICAS2022_0411
Barakos, G.ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUPICAS2022_0335
Barbarino, M.COMPARISON OF ANALYTICAL SEMI-EMPIRICAL MODEL FOR JET NOISE PREDICTIONICAS2022_0855
Barbosa, D.F.C. EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINEICAS2022_0676
Barbosa, L.M.F.METHODOLOGIES AND EXAMPLE OF CONCEPTUAL DESIGN FOR A FOOT-LAUNCHABLE SPORT SAILPLANEICAS2022_0893
Baron, C.TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONESICAS2022_0655
Barragan Montes, R.DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELSICAS2022_0648
Barrier, R.AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTSICAS2022_0058
Barrier, R.LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANESICAS2022_0339
Bartasevicius, J.COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAVICAS2022_0367
Bartoli, N.A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORKICAS2022_0618
Batra, A.SERIES OR PARALLEL HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEMS? CASE STUDIES OF THE ATR42 AND ATR72ICAS2022_0163
Batra, A.KINETIC ENERGY RECOVERY FROM A LANDING AIRCRAFT: ENERGY ANALYSIS, ENVIRONMENTAL AND ECONOMIC PROSPECTSICAS2022_0821
Bauer, T.IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPTICAS2022_0627
Baumann, S.MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACEICAS2022_0574
Bayandor, J.HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE STRIKE ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFTICAS2022_0718
Bayandor, J.DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURESICAS2022_0734
Bayram, K.FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURESICAS2022_0958
Beamer, C.LATEST DEVELOPMENTS IN HIGH PRESSURE HEAT TREATMENT OF AEROSPACE COMPONENTSICAS2022_0026
Becker, D.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
Beckert, F.VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERINGICAS2022_0063
Beijer, B.THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENTICAS2022_0615
Ben Salah, N.NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050ICAS2022_0801
Benad, J.DESIGN OF A FLYING V SUBSONIC TRANSPORTICAS2022_0358
Bénard, E.SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIESICAS2022_0084
Benard, E.OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGNICAS2022_0550
Benard, E.AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGSICAS2022_0560
Bennehard, Q.OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACTICAS2022_0843
Berend, N.FLIGHT EXPERIMENTS FOR THE ALTAIR SEMI-REUSABLE AIR-LAUNCH SYSTEM WITH THE DEMONSTRATOR EOLEICAS2022_0541
Berlowitz, I.ELECTRICALLY POWERED LANDING GEAR SYSTEM FOR TRANSPORT AIRCRAFT TAXIINGICAS2022_0003
Berlowitz, I.TRANSPORT AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM AIR QUALITY IMPROVEMENTICAS2022_0055
Bernardini, G.SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSISICAS2022_0370
Berschik, M.C.A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLEICAS2022_0791
Bertling Tjernberg, L.MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACTICAS2022_0369
Bertling-Tjernberg, L.MORE ELECTRIC AIRPLANE: CASE STUDY STOCKHOLM - COPENHAGENICAS2022_0506
Bertram, O.COUPLING OF MODEL-BASED SYSTEMS ENGINEERING AND SAFETY ANALYSIS IN CONCEPTUAL AIRCRAFT SYSTEM DESIGNICAS2022_0082
Bhurat, S.NUCLEAR POWERED AIR-BREATHING ELECTRIC THRUSTERS USED IN UAVS FOR EXTRA-TERRESTRIAL APPLICATIONSICAS2022_0019
Bidinotto, J.H.DEEP REINFORCEMENT LEARNING FOR EVTOL HOVERING CONTROLICAS2022_0291
Bieber, P.AVIATION SECURITY CONCERNSICAS2022_0918
Biedermann, J.VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERINGICAS2022_0063
Biedermann, J.EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXTICAS2022_0254
Bielsky, T.SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGNICAS2022_0665
Bil, C.DOOR-TO-DOOR TRAVEL PLANNER FOR IMPROVED TRAVELER EXPERIENCE USING DIGITAL TWIN CONCEPTICAS2022_0011
Bilger, M.A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCEICAS2022_0332
Billson, M.STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECTICAS2022_0480
Billson, M.IDENTIFICATION OF CRITICAL ACOUSTIC MODES FOR AN OPEN BOX CAVITY WITH ADJUSTABLE DEPTHICAS2022_0696
Binante, V.CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGEICAS2022_0148
Binetti, T.STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIESICAS2022_0336
Birberg, J.REAL-TIME IDENTIFICATION OF USER ACTIONS IN COMPUTER-AIDED MANUFACTURING USING MACHINE LEARNING AND COMPUTER VISIONICAS2022_0534
Birch, D.M.WALL INTERFERENCE CORRECTIONS USING NONLINEAR LEAST-SQUARES OPTIMISATIONICAS2022_0378
Biron, A.VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGSICAS2022_0207
Bisagni, C.INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGYICAS2022_0685
Bischof, P.S.DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACKICAS2022_0677
Bjursten Carlsson, C.STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATIONICAS2022_0903
Bladh, P.GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONSICAS2022_0265
Blecken, M.A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLEICAS2022_0791
Bloise, N.ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITIONICAS2022_0085
Boden, B.RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORKICAS2022_0702
Boggero, L.METHODOLOGY FOR THE AUTOMATED PRELIMINARY CERTIFICATION OF ON-BOARD SYSTEMS ARCHITECTURES THROUGH REQUIREMENTS ANALYSISICAS2022_0327
Boggero, L.SYSTEMS ARCHITECTING: A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0 PROJECTICAS2022_0365
Boggero, L.AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATIONICAS2022_0593
Boggero, L.THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENTICAS2022_0615
Boggero, L.A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORKICAS2022_0618
Boggero, L.POTENTIAL OF EXTENDED REALITY IN ENGINEERING AND CHALLENGES OF UNCONVENTIONAL VEHICLE DESIGNICAS2022_0966
Bohnert, P.DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFTICAS2022_0566
Boisard, R.ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUPICAS2022_0335
Boni , I.STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIESICAS2022_0336
Boni , L.FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSESICAS2022_0692
Bonnin, V.O.SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART I: INITIAL DESIGNSICAS2022_0248
Bonnin, V.O.SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART II: SENSITIVITY ANALYSISICAS2022_0481
Bontoft, E.K.AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORKICAS2022_0199
Boogaart, T.E.INSTALLATION PENALTY OF AERO-ENGINES ON NARROW BODY AIRCRAFTICAS2022_0246
Bordeneuve-Guibe, J.A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERSICAS2022_0568
Borghi, M.“CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATIONICAS2022_0345
Borodacz, K.IMPACT OF MOTION-DEPENDENT ERRORS ON THE ACCURACY OF AN UNAIDED STRAPDOWN INERTIAL NAVIGATION SYSTEMICAS2022_0742
Boscagli, L.A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLESICAS2022_0162
Botero-Bolivar, L.AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF THE NACA 0008 AIRFOILICAS2022_0128
Boucher, M.J.UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATIONICAS2022_0774
Boussuge, J.-F.LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANESICAS2022_0339
Bovecchi, F.FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSESICAS2022_0692
Bowen Varela, J.AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGSICAS2022_0020
Boyer, J.IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPTICAS2022_0627
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Bramsiepe, K.WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSESICAS2022_0663
Brancalion, J.F.B.COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMSICAS2022_0340
Braune, M.WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSESICAS2022_0663
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Brazier, F.ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEMICAS2022_0368
Breitamter, C.STRAKE SECTION IMPACT ON HYBRID-DELTA-WING AERODYNAMICSICAS2022_0075
Breitsamter, C.TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WINGICAS2022_0037
Breitsamter, C.WING BUFFET PRESSURE LOAD PREDICTION BASED ON A HYBRID DEEP LEARNING MODELICAS2022_0043
Breitsamter, C.WIND-TUNNEL TEST ON LEADING-EDGE VORTEX OF LOW-ASPECT-RATIO FLAPPING PLATESICAS2022_0154
Breitsamter, C.EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSISICAS2022_0250
Bremm, M.EXPERIMENTS TO INVESTIGATE LIFT PRODUCTION MECHANISMS ON OSCILLATING TRAILING-EDGE FLAPSICAS2022_0780
Bremmers, F.VALIDATION OF SCALED FLIGHT TESTINGICAS2022_0375
Brentjes, A.INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRDICAS2022_0653
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Bringhenti, C.EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINEICAS2022_0676
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Broatch, A.NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINESICAS2022_0224
Brodersen, O.APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFTICAS2022_0892
Broehan, J.SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGNICAS2022_0665
Bronsvoort, J.TRAJECTORY-BASED OPERATIONS TO IMPROVE LONG-RANGE AIR TRAFFIC FLOW MANAGEMENTICAS2022_0087
Bronz, M.A STUDY OF HIGH-LIFT DEVICES FOR LOW REYNOLDS NUMBER APPLICATIONSICAS2022_0312
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Bruno, M.ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFTICAS2022_0234
Bu, C.DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNELICAS2022_0045
Bu, C.EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WINGICAS2022_0078
Budinger, M.STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMSICAS2022_0151
Budinger, M.PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURESICAS2022_0289
Budinger, M.A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONSICAS2022_0383
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Burger, U.A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONSICAS2022_0030
Burger, K.DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFTICAS2022_0622
Burschyk, T.RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORKICAS2022_0702
Buschhaus, M.USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAMICAS2022_0116
Busse, D.O.FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSESICAS2022_0692
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Bussemaker, J.H.AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATIONICAS2022_0593
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Buszyk, M.AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTSICAS2022_0058
Buszyk, M.LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANESICAS2022_0339
Byun, K.-H.ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGIONICAS2022_0827
Bång, M.ATCO STRATEGIES IN TACTICAL TBO: A SIMULATOR STUDYICAS2022_0285
Bång, M.HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICSICAS2022_0707
Cabac, Y.RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORKICAS2022_0702
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Cabaleiro, C.METHODOLOGY FOR THE AUTOMATED PRELIMINARY CERTIFICATION OF ON-BOARD SYSTEMS ARCHITECTURES THROUGH REQUIREMENTS ANALYSISICAS2022_0327
Cabaleiro, C.CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECTICAS2022_0350
Caivano, A.WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICAICAS2022_0280
Cakir, B.O.HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONSICAS2022_0572
Calavera, L.R.THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIESICAS2022_0915
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Cambertoni, R.ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFTICAS2022_0234
Camilleri, R.SERIES OR PARALLEL HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEMS? CASE STUDIES OF THE ATR42 AND ATR72ICAS2022_0163
Camilleri, R.KINETIC ENERGY RECOVERY FROM A LANDING AIRCRAFT: ENERGY ANALYSIS, ENVIRONMENTAL AND ECONOMIC PROSPECTSICAS2022_0821
Campillo Borrás, E.FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATIONICAS2022_0708
Campos, L.M.B.C.ON LATERAL-LONGITUDINAL CONTROL COUPLING FOR SHORT- AND LONG-FUSELAGE BWB AIRCRAFT CONFIGURATIONSICAS2022_0733
Can, A.G.DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFTICAS2022_0921
Candell, O.GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONSICAS2022_0265
Cantanna, G.CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODELICAS2022_0341
Cao, M.-G.RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTUREICAS2022_0510
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Capitao Patrao, A.NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCTICAS2022_0236
Caprdja, K.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
Caramazza, A.CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODELICAS2022_0341
Carbonneau, X.ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEMICAS2022_0368
Carbonneau, X.UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLSICAS2022_0611
Cardoso, M.M.UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIOICAS2022_0729
Cardoso Júnior, M.M.EXPLORATORY STUDY OF MENTAL WORKLOAD IN HELICOPTER AIR-TO-GROUND ROCKET FIRINGICAS2022_0077
Cardoso Junior, M.M.A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAYICAS2022_0723
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Carias, E.K.T.VALIDATION STUDY OF BLUNTED AND SHARP CONES AT HYPERSONIC SPEEDICAS2022_0147
Carlsson, B.FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSUREICAS2022_0028
Carlsson, M.EFFECT OF LES LENGTH SCALE AND NUMERICAL SCHEME IN HYBRID RANS-LES OF FREE SHEAR LAYER FLOWSICAS2022_0684
Carreño Ruiz, M.ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITIONICAS2022_0085
Carrera, E.NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF UNSTIFFENED AND STIFFENED STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGSICAS2022_0220
Carrera, E.A GLOBAL/LOCAL ELEMENT-WISE APPROACH FOR THE BUCKLING AND POST-BUCKLING ANALYSIS OF THIN MULTILAYERED STRUCTURESICAS2022_0253
Carrera, E.DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU)ICAS2022_0295
Carvalho, A.H.O.COMPETITIVITY, STRATEGY AND VALUE ON AIRPORTS A METHOD OF DIAGNOSIS, SUGGESTIONS AND ACTIONS FOR INTERNATIONAL AIRPORTS WITH A CASE STUDY OF CNFICAS2022_0022
Carvalho, L.O.USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTIONICAS2022_0389
Castaño, M.GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONSICAS2022_0265
Castellanos, R.AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGSICAS2022_0020
Castino, F.MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACEICAS2022_0574
Castro, S.G.P.OPTIMAL DESIGN OF STIFFENED PANELS UNDER BUCKLING CONSTRAINTS: A DESIGN METHODOLOGY CONSIDERING CAD-BASED PARAMETERIZATION WITH SIMULTANEOUS LAYOUT AND SIZING OPTIMIZATIONICAS2022_0393
Castro, B.M.STUDY OF EFFECTS ON THE WING'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPANICAS2022_0889
Catalano, F.M.EXPERIMENTAL STUDIES ON THE INTERACTION BETWEEN PROPELLERS AND WINGICAS2022_0262
Catalano, F.M.EXPERIMENTAL INVESTIGATION OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTIONICAS2022_0431
Catalano, F.M.EXPLORATION OF BOX-WING AIRCRAFT CONCEPT USING HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATIONICAS2022_0446
Catalano, F.M.PUSHER PROPELLER INFLUENCE ON A LAMINAR WING TRANSITION LOCATION USING INFRARED THERMOGRAPHYICAS2022_0678
Caurin, G.THE BENEFIT OF BILATERAL RESEARCH NETWORKS - THE SARC AND BARINET INITIATIVES AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICSICAS2022_0681
Cavalieri, V.DESIGN AND EXPERIMENTAL TESTING OF A DROOP NOSE MORPHING FOR ADVANCED REGIONAL AIRCRAFTICAS2022_0861
Cecrdle, J.UPDATING OF JET TRAINER AIRCRAFT DYNAMIC MODEL TO RESULTS OF GROUND VIBRATION TESTICAS2022_0044
Celso Greco Junior, P.VISCOUS CORRECTION FOR HIGH ORDER IMMERSED INTERFACE METHOD FOR COMPRESSIBLE TRANSONIC FLOWSICAS2022_0260
Cerino, G.REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATIONICAS2022_0323
Cerón-Muñoz, H.D.EXPERIMENTAL INVESTIGATION OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTIONICAS2022_0431
Cerulus, N.ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNERICAS2022_0887
Cervenka, M.TREND MONITORING OF TURBOPROP ENGINESICAS2022_0094
Cestino, E.WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICAICAS2022_0280
Cestino, E.A STUDENT TEAM BASED TEACHING APPROACH: THE TEAM S55 EXPERIENCEICAS2022_0315
Cestino, E.CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODELICAS2022_0341
Cestino, E.NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMSICAS2022_0396
Cha, J.-H.DOPAMINE-COATED UHMWPE/HYDROGEN-RICH BENZOXAZINE COMPOSITES FOR SPACE RADIATION SHIELDINGICAS2022_0101
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Chalke, A.-P.AEROELASTIC TAILORING OF COMPRESSOR BLADESICAS2022_0507
Chalon Morgan, C.DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELSICAS2022_0648
Chalon Morgan, C.FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURESICAS2022_0958
Chao, G.RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTIONICAS2022_0760
Chapman, J.W.UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATIONICAS2022_0774
Chau, T.EXPLORATION OF BOX-WING AIRCRAFT CONCEPT USING HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATIONICAS2022_0446
Chau, T.A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATION TO THE STRUT-BRACED-WING AND HYBRID-WING-BODY CONFIGURATIONSICAS2022_0748
Chau, T.UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATIONICAS2022_0774
Chen, Y.DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISKICAS2022_0032
Chen, H.EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WINGICAS2022_0078
Chen, L.DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENTICAS2022_0321
Chen, X.SET-BASED DESIGN COORDINATION BETWEEN COUPLED SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVEICAS2022_0372
Chen, Y.-H.EXPERIMENTAL STUDY ON THE EFFECT OF INTERSTAGE BLEEDING ON THE PERFORMANCE OF FULL-SCALE MULTISTAGE AXIAL COMPRESSORICAS2022_0495
Chen, Y.EXPERIMENTAL STUDY OF FLAT BAFFLE INLET TOTAL-PRESSURE DISTORTION IN A THREE-STAGE FANICAS2022_0502
Chen, B.INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNELICAS2022_0547
Chen, Q.A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFTICAS2022_0584
Chen, R.TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMSICAS2022_0604
Chen, R.DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATIONICAS2022_0753
Chen, Q.COOPERATIVE PATH PLANNING AND ADJUSTING STRATEGY FOR UAVS WITH STRICT TIME CONSTRAINSICAS2022_0781
Chen, H.DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACEICAS2022_0785
Chernoray, V.THE INFLUENCE OF THE VANE LEAN ON THE FLOW IN A TURBINE REAR STRUCTUREICAS2022_0514
Cheung, R.C.M.LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPSICAS2022_0524
Chiba, K.INFLUENCES OF CHANGING THE INSTALLING POSITIONS OF MULTIPLE WINGLETS ON AERODYNAMIC CHARACTERISTICSICAS2022_0459
Choi, H.A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSBICAS2022_0222
Christoffels, L.THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITIONICAS2022_0268
Chu, D.-L.DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEMICAS2022_0818
Chudý, P.UNMANNED AERIAL VEHICLE\\\'S TRAJECTORY OPTIMIZATION IN CONSTRAINED ENVIRONMENTSICAS2022_0717
Chudy, P.LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFTICAS2022_0719
Chudy, P.PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELSICAS2022_0721
Chunlei, Z.NUMERICAL INVESTIGATION ON TURBINE SHROUD FILM COOLING HEAT TRANSFER PERFORMANCE OF TURBINE BLADE WITH GROOVE TIPICAS2022_0203
Cicolini, P.NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITCH ANGLEICAS2022_0355
Cimini, C.A.DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES USING NEURAL NETWORKS AND HYBRID DATAICAS2022_0705
Cinefra, M.VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTSICAS2022_0247
Cinnela , P.NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTSICAS2022_0349
Cipolla, V.CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARDS THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY AND CLIMATE CHANGEICAS2022_0148
Clair, V.AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTSICAS2022_0058
Clark, J.P.REALISTIC HYDROGEN-BASED SOLUTIONS FOR SUSTAINABLE AVIATIONICAS2022_0963
Clifford, D.COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMSICAS2022_0399
Clinca, G.“CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATIONICAS2022_0345
Coelho Leite Fava, T.DIRECT NUMERICAL SIMULATIONS OF A THICK, ROTATING AIRFOIL AT A LOW REYNOLDS NUMBERICAS2022_0680
Coil, J.FATIGUE CRACK PROPAGATION IN ADDITIVELY MANUFACTURED POLYMER PARTSICAS2022_0777
Colli, A.ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUPICAS2022_0335
Condomines, J.-P.PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY IMPLEMENTED UNDER ASWINGICAS2022_0318
Cooper, J.E.LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPSICAS2022_0524
Corcione, S.REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATIONICAS2022_0323
Corsi, M.V/A-R AIR GESTURES HMI INTERACTION IN AIRPORT CONTROL TOWERSICAS2022_0452
Cortes, R.G.EXPLORATORY STUDY OF MENTAL WORKLOAD IN HELICOPTER AIR-TO-GROUND ROCKET FIRINGICAS2022_0077
Cortes, R.G.DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCYICAS2022_0662
Coskun, S.DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT – LIFE CYCLE ASSESSMENT ACTIVITIES AT ECOTECH / CLEANSKY 2ICAS2022_0895
Couilleaux, A.NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINESICAS2022_0224
Coustols, P.THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIESICAS2022_0915
Coustols, E.PROGRESS IN WING DESIGN, STATUS AND PERSPECTIVESICAS2022_0926
Cristea, G.C.TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINSICAS2022_0822
Cubas, J.IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONSICAS2022_0360
Cuerno-Rejado, C.ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORAICAS2022_0699
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Cui, Z.DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATIONICAS2022_0143
Cui, P.DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATIONICAS2022_0753
Cumnuantip, S.A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATORICAS2022_0826
Cusati, V.TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASSICAS2022_0641
Cutrone, L.AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECTICAS2022_0235
D'Alesio, P.WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAPICAS2022_0232
D'Amico, F.A.“CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATIONICAS2022_0345
Da Ronch, A.COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMSICAS2022_0399
da Silva, E.T.A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAYICAS2022_0723
da Silva, R.G.STUDY OF THE EFFECTS OF NUMERICAL MODEL ENHANCEMENTS FOR AEROSTRUCTURAL ANALYSIS IN TRANSONIC FLOWSICAS2022_0726
da Silva, E.T.UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIOICAS2022_0729
da Silva, G.A.L.LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIPICAS2022_0869
da Silva, R.G.A.IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTINGICAS2022_0873
Dahlmann, K.A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIESICAS2022_0853
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Danielson, L.STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATIONICAS2022_0903
Daroukh, M.STUDY OF THE IMPACT OF AZIMUTHAL FLOW DISTORTION ON IN-DUCT ACOUSTIC PROPAGATION USING A MULTIMODAL FORMULATIONICAS2022_0666
Das, S.NUCLEAR POWERED AIR-BREATHING ELECTRIC THRUSTERS USED IN UAVS FOR EXTRA-TERRESTRIAL APPLICATIONSICAS2022_0019
Das, R.NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMSICAS2022_0396
Das, T.S.G.DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT – LIFE CYCLE ASSESSMENT ACTIVITIES AT ECOTECH / CLEANSKY 2ICAS2022_0895
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De Crescenzio, F.AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACHICAS2022_0478
de Faria, A.R.ASSESSMENT OF FAILURE UNDER LONGITUDINAL COMPRESSION OF UNIDIRECTIONAL COMPOSITES WITH IN-PLANE FIBER MISALIGNMENTICAS2022_0343
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De Franssu, H.TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINEICAS2022_0006
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de Graaf, S.DEVELOPMENT OF A CONTROLS APPROACH FOR FUEL CELL-POWERED ALL-ELECTRIC AERO ENGINES BASED ON AN FHAICAS2022_0366
de Gruijl, W.RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERSICAS2022_0489
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de Negri, V.J.THE BENEFIT OF BILATERAL RESEARCH NETWORKS - THE SARC AND BARINET INITIATIVES AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICSICAS2022_0681
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de Oliveirra, G.L.A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENTICAS2022_0523
de Oliveirra, G.EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMASICAS2022_0526
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de Paula, T.R.UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIOICAS2022_0729
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de Santana, L.D.INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRDICAS2022_0653
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de Saqui-Sannes, P.TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONESICAS2022_0655
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De Visscher, I.DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELSICAS2022_0648
De Visscher, I.FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURESICAS2022_0958
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Deng, J.RESEARCH ON CROSSTALK CHARACTERISTICS OF AIRCRAFT ELECTRICAL CABLEICAS2022_0503
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Di Stasio, M.MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFTICAS2022_0649
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Dickey, E.D.TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATIONICAS2022_0397
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Diette, C.OPEN FAN ENGINE ARCHITECTURE FOR NEXT GENERATION SMRICAS2022_0925
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Ding, C.RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAVICAS2022_0107
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Donelli, G.A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORKICAS2022_0618
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Duval, M.N.DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACKICAS2022_0677
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Feng, S.EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WINGICAS2022_0078
Feng, D.STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATORICAS2022_0313
Feng, S.FREE FLIGHT TEST IN HORIZONTAL WIND TUNNEL WITH POWERED AIRCRAFTICAS2022_0423
Feng, S.DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACEICAS2022_0785
Fernandes, V.P.PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WINGICAS2022_0694
Fernberg, P.FATIGUE DAMAGE MODEL OF HIGH TEMPERATURE POLYMER COMPOSITES IN AERO-ENGINESICAS2022_0831
Ferrari, S.DESIGNING SUSTAINABLE AVIATION SOLUTIONS WITH DIGITAL TWIN APPROACHICAS2022_0967
Ferreira, L.P.S.DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES USING NEURAL NETWORKS AND HYBRID DATAICAS2022_0705
Ferreto, D.MATHEMATICAL MODELLING AND ANALYSIS OF THERMAL MANAGEMENT SYSTEM ARCHITECTURE FOR HYPERSONIC AIRCRAFTICAS2022_0730
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Ferretto, D.HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONSICAS2022_0572
Ferro, M.LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIPICAS2022_0869
Feuerle, T.FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURESICAS2022_0958
Feurich, P.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
Fezans, N.LANDING SIMULATION OF A HIGH-ALTITUDE PLATFORM WITH SKID-TYPE LANDING GEAR – FLIGHT PROCEDURE, CONTROLLER, AND LOADSICAS2022_0364
Fezans, N.COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACSICAS2022_0505
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Figat, M.PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLEICAS2022_0395
Filho, A.J.D.USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTIONICAS2022_0389
Filippatos, A.INVESTIGATION ON INTEGRATING RECYCLABILITY AS A FUNCTION AT THE DESIGN PHASE OF COMPLEX-LOADED STRUCTURAL COMPONENTSICAS2022_0125
Filippi, M.NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF UNSTIFFENED AND STIFFENED STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGSICAS2022_0220
Finck, T.DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORSICAS2022_0264
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Fioriti, M.METHODOLOGY FOR THE AUTOMATED PRELIMINARY CERTIFICATION OF ON-BOARD SYSTEMS ARCHITECTURES THROUGH REQUIREMENTS ANALYSISICAS2022_0327
Fioriti, M.CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECTICAS2022_0350
Fischer, M.FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATIONICAS2022_0708
Fischer, O.J.P.ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACHICAS2022_0817
Fischer, C.IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTINGICAS2022_0873
Fitzgerald, L.K.A STATIC STABILITY COMPARISON OF WIND TUNNEL AND COMPUTATIONAL FLUID DYNAMICS METHODSICAS2022_0384
Flassig, P.ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISKICAS2022_0532
Flores-Peña, P.ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORAICAS2022_0699
Fonseca, G.C.NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIALICAS2022_0059
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Fornaseri, F.“CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATIONICAS2022_0345
Forsberg, H.A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCEICAS2022_0332
Forsyth, P.NUMERICAL SIMULATION OF ICE ACCRETION ON A PITOT TUBEICAS2022_0130
Forte, M.STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCEICAS2022_0583
Fouda, M.AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATIONICAS2022_0593
Francois, C.OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACTICAS2022_0843
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Frezet, A.TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINEICAS2022_0006
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Fujii, K.OPTIMIZATION OF AIRCRAFT FLIGHT PATHS CONSIDERING THE CONFLICTING PARAMETERS OF ECONOMY AND SAFETYICAS2022_0652
Fukumine, Y.ESTIMATION OF EVTOL FLIGHT PERFORMANCE USING ROTORCRAFT THEORYICAS2022_0408
Funk, P.GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONSICAS2022_0265
Funk, P.USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTIONICAS2022_0389
Fureby, C.LARGE EDDY SIMULATION OF RAMJET TO SCRAMJET TRANSITIONICAS2022_0188
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Fusaro, R.COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATIONICAS2022_0342
Fusaro, R.LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASESICAS2022_0498
Fusaro, R.HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONSICAS2022_0572
Fusaro, R.AERODATABASE DEVELOPMENT AND INTEGRATION OF SUPERSONIC/HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROJECTICAS2022_0596
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Gangoli Rao, A.DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFTICAS2022_0622
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Gao, F.ANALYSIS OF THE AERODYNAMIC CHARACTERISTICS AND ITS INFLUENCE OF TURBOMACHINERY IN TRANSITION STATEICAS2022_0603
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García-Tíscar, J.NON-INTRUSIVE AEROTHERMAL CHARACTERIZATION OF SURFACE HEAT EXCHANGERS FOR TURBOFAN AEROENGINESICAS2022_0224
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Gastaldo, G.STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMSICAS2022_0151
Gastaldo, G.PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURESICAS2022_0289
Gatlin, G.M.TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATIONICAS2022_0397
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Gemma, R.THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIESICAS2022_0915
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Genrup, M.ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATORICAS2022_0382
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Gerdes, I.THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITIONICAS2022_0268
Gessner, M.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
Ghelani, R.A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFTICAS2022_0703
Ghika, S.WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLEICAS2022_0215
Giacomossi, L.COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMSICAS2022_0340
Gibertini, G.ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUPICAS2022_0335
Gibertini, G.EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING THE WIND TUNNEL: HELICOPTER SHIP LANDING CASEICAS2022_0625
Gierszewski, D.REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFTICAS2022_0797
Gierszewski, D.AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFTICAS2022_0835
Giese, K.THE NEW RESEARCH AIRCRAFT ISTAR - EXPERIMENTAL FLIGHT CONTROL SYSTEMICAS2022_0439
Gijsman, F.INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRDICAS2022_0653
Girard, G.FUTURE COMBAT AIR SYSTEMS: REQUIREMENTS AND TECHNOLOGIESICAS2022_0940
Gkoutzamanis, V.G.MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENTICAS2022_0943
Glabeke, G.WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAPICAS2022_0232
Glodic, N.STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALLICAS2022_0351
Glodic, N.AEROELASTIC TAILORING OF COMPRESSOR BLADESICAS2022_0507
Glodic, N.MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEMICAS2022_0832
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Góes, L.C.S.SYNTHETIC AIR DATA - A COMPARATIVE PRACTICAL STUDYICAS2022_0536
Góes, L.C.S.PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WINGICAS2022_0694
Góes, L.C.S.IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTINGICAS2022_0873
Góes, L.C.S.OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEMICAS2022_0891
Goetz, C.VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERINGICAS2022_0063
Goetzendorf-Grabowski , T.PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLEICAS2022_0395
Goetzendorf-Grabowski, T.MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIESICAS2022_0462
Goetzendorf-Grabowski, T.OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANEICAS2022_0576
Golan, O.TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATIONICAS2022_0036
Gollnick, V.CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACHICAS2022_0102
Gollnick, V.ASSESSMENT OF REAL-TIME DATA TRANSMISSION VIA AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC OCEANIC AIRSPACEICAS2022_0168
Gollnick, V.ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITYICAS2022_0233
Gollnick, V.MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACEICAS2022_0574
Gollnick, V.INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGIONICAS2022_0840
Gomez-Escalonilla, J.TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURESICAS2022_0012
Gong, R.INTEGRATE ONLINE QUERY&DEFENSE INTO PROJECT BASED LEARNING TO PROMPT ENGINEERING AUTHENTIC EXPERIENCESICAS2022_0284
Gonschorek, J.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
González, P.J.DESIGN OF STABILITY AUGMENTATION SYSTEMS FOR A FLEXIBLE AIRCRAFT USING LQ OUTPUT-FEEDBACK CONTROL VIA LMIICAS2022_0623
González, P.J.TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONSICAS2022_0657
González, P.J.LPV/LFR CONTROL FOR ACTIVE FLUTTER SUPPRESSION OF A SMART AIRFOIL MODELICAS2022_0816
González, P.J.A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATORICAS2022_0826
González Lozano, B.NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCTICAS2022_0236
Gorgues, A.AN ASSESSMENT OF REDUCED-ORDER AND MACHINE LEARNING MODELS FOR STEADY TRANSONIC FLOW PREDICTION ON WINGSICAS2022_0020
Gori, O.SIMPLIFIED MODELS FOR THE PRELIMINARY AERODYNAMIC CHARACTERIZATION OF HIGH-SPEED VEHICLES TO SUPPORT MISSION ANALYSISICAS2022_0551
Gori, O.HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONSICAS2022_0572
Gowree, E.STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCEICAS2022_0583
Gowree, E.R.UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLSICAS2022_0611
Gowree, E.R.STABILITY OF A LAMINAR BOUNDARY LAYER OVER LOCALISED SURFACE INDENTATIONICAS2022_0697
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Gray, A.L.A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATION TO THE STRUT-BRACED-WING AND HYBRID-WING-BODY CONFIGURATIONSICAS2022_0748
Gray, A.C.TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATIONICAS2022_0905
Graziani, S.LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASESICAS2022_0498
Gregg, R.TOWARDS CERTIFICATION BY ANALYSIS FOR FLIGHT CHARACTERISTICSICAS2022_0956
Grendene, S.STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIESICAS2022_0336
Grendysa, W.A NEW APPROACH TO SHAPING THE PUSHROD TUBE AS THE MAIN COMPONENT OF THE CONTROL SYSTEM, OPTIMIZATION, AND MANUFACTURING TECHNOLOGY.ICAS2022_0616
Grewe, V.MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGNICAS2022_0602
Griffin, P.C.A STATIC STABILITY COMPARISON OF WIND TUNNEL AND COMPUTATIONAL FLUID DYNAMICS METHODSICAS2022_0384
Grimaldi, G.DEVELOPMENT OF A CONCEPTUAL DESIGN TOOL TO PREDICT PERFORMANCE OF HYDROGEN FUELLED PRECOOLED AIRBREATHING ROCKET ENGINESICAS2022_0152
Grimme, W.DESIGN AND ECO-EFFICIENCY ASSESSMENT OF A PEOPLE-MOVER AIRCRAFT IN COMPARISON TO STATE-OF-THE-ART NARROW BODY AIRCRAFTICAS2022_0304
Gringinger, E.AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTSICAS2022_0693
Groot Koerkamp, L.H.INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRDICAS2022_0653
Grundström, M.DESIGNING SUSTAINABLE AVIATION SOLUTIONS WITH DIGITAL TWIN APPROACHICAS2022_0967
Gryazev, V.APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDSICAS2022_0643
Grün, G.USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAMICAS2022_0116
Grünewald, M.CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACHICAS2022_0102
Grönstedt, T.LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTIONICAS2022_0088
Grönstedt, T.ENVIRONMENTAL ASSESSMENT OF NOISE ABATEMENT APPROACH TRAJECTORIESICAS2022_0671
Grönstedt, T.PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINEICAS2022_0782
Grönstedt, T.SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045ICAS2022_0804
Grönstedt, T.MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEMICAS2022_0832
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Guagliardo, D.NUMERICAL MODELING OF FLUID-STRUCTURE INTERACTION OF A 3D WEDGE DURING WATER IMPACT WITH VARIATION OF VELOCITY AND PITCH ANGLEICAS2022_0355
Guarino, G.TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHODICAS2022_0427
Guedes, M.J.M.LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIPICAS2022_0869
Guenov, M.D.SET-BASED DESIGN COORDINATION BETWEEN COUPLED SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVEICAS2022_0372
Guerrero i Almirall, A.ZONAL MODEL BASED AIRCRAFT PASSENGER THERMAL COMFORT COMPARATIVE STUDYICAS2022_0338
Guglieri, G.ADAPTIVE PATH PLANNING FOR SPRAYING UAS IN VINEYARD UNDER VARIABLE WIND CONDITIONICAS2022_0085
Guida, M.MECHANICAL CHARACTERIZATION OF A COMPOSITE STRUCTURAL BATTERY LAMINATEICAS2022_0690
Guiterrez Salas, M.MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEMICAS2022_0832
Gulizzi, V.TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHODICAS2022_0427
Gulizzi, V.HIGH-ORDER ACCURATE EMBEDDED-BOUNDARY DISCONTINUOUS GALERKIN METHODS FOR INVISCID GAS DYNAMICSICAS2022_0735
Guo, T.EXPERIMENTAL INVESTIGATION ON TRANSPORT AIRPLANE LONGITUDINAL STABILITY ENHANCEMENT IN CRITICAL ICING CONDITIONICAS2022_0270
Guo, D.DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIALICAS2022_0290
Guo, F.MOTION STROKE DESIGN ON FLEXIBLE ASSEMBLY TOOLING FOR MULTIPLE AIRCRAFT COMPONENTSICAS2022_0314
Guo, X.EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF COMPOSITE SHIELD ON THE ELECTROTHERMAL ANTI-ICING SYSTEMSICAS2022_0537
Guocheng, Z.AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNELICAS2022_0411
Gupta, P.CONCEPTUAL DESIGN AND SIZING FOR A FIXED WING UAV FOR EXPLORATION OVER MARSICAS2022_0210
Gurtov, A.A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATIONICAS2022_0704
Gustafsson, M.GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONSICAS2022_0265
Gustafsson, B.STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECTICAS2022_0480
Gutierrez Salas, M.AEROELASTIC TAILORING OF COMPRESSOR BLADESICAS2022_0507
Gürlük, H.THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITIONICAS2022_0268
Görtz, A.THERMODYNAMIC POTENTIAL OF TURBOFAN ENGINES WITH DIRECT COMBUSTION OF HYDROGENICAS2022_0499
Görtz, S.APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFTICAS2022_0892
Hackbarth, H.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
Hackenberg, D.L.INTERNATIONAL SCIENTIFIC ASSESSMENT ON URBAN AIR MOBILITY AS A CONTRIBUTION TO FUTURE AVIATION STANDARDSICAS2022_0949
Hackström, M.AERODYNAMIC DEVELOPMENT OF SAAB FCAS UNMANNED SUPERSONIC COMBAT AIRCRAFTICAS2022_0570
Hagemann, S.ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITYICAS2022_0233
Hagström, M.THE GROUP OF RESPONSABLES "FLIGHT MECHANICS, SYSTEMS AND INTEGRATION (GOR FM)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIESICAS2022_0912
Hahn, S.H.GENERATION OF TERRAIN PROFILE FOR TERRAIN FOLLOWINGICAS2022_0538
Haldar, D.IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIESICAS2022_0334
Haldar, D.MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACTICAS2022_0369
Halila, G.L.O.A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTSICAS2022_0672
Hallander, P.SMART SKIN FOR AEW AIRCRAFTICAS2022_0048
Hammer, S.IDENTIFICATION OF CRITICAL ACOUSTIC MODES FOR AN OPEN BOX CAVITY WITH ADJUSTABLE DEPTHICAS2022_0696
Han, Y.-J.DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLEICAS2022_0108
Han, J.-H.DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLEICAS2022_0108
Han, Y.-J.OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNINGICAS2022_0109
Han, J.-H.OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNINGICAS2022_0109
Han, J.-S.WIND-TUNNEL TEST ON LEADING-EDGE VORTEX OF LOW-ASPECT-RATIO FLAPPING PLATESICAS2022_0154
Han, S.-Q.A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEMEICAS2022_0157
Han, Z.-H.A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEMEICAS2022_0157
Han, S.-Q.A NUMERICAL METHOD FOR STUDY ON THE AERO-ELASTICITY OF AIR-TO-AIR MISSILES IN OVER-THE-SHOULDER LAUNCHICAS2022_0311
Han, Z.-H.UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODELICAS2022_0330
Han, S.NUMERICAL PREDICTION OF FOCUS BOOM GENERATED BY MANEUVERSICAS2022_0410
Han, S.IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFTICAS2022_0421
Han, Z.-H.EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTOR GENERATIONICAS2022_0548
Han, S.-Q.HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACKICAS2022_0555
Han, Z.-H.HIGH-ACCURATE NUMERICAL SIMULATION FOR VORTEX FLOW OVER A SLENDER MISSILE AT HIGH ANGLE OF ATTACKICAS2022_0555
Han, Z.-H.A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFTICAS2022_0584
Hanak, J.PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELSICAS2022_0721
Handal-Rivera, C.D.DESIGN OF AN ADVANCED EMPENNAGE AND REAR FUSELAGE CONCEPT FOR A COMMERCIAL AIRCRAFTICAS2022_0227
Handojo, V.LOADS ANALYSIS AND STRUCTURAL OPTIMIZATION OF A LONG-RANGE TRANSPORT CONFIGURATION WITH HYBRID LAMINAR FLOW CONTROLICAS2022_0158
Handojo, V.XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEMICAS2022_0228
Hang, H.-Y.RESEARCH ON THE EFFECT OF THE PROCESS FIRST SHOT PEENING STRENGTHENING THEN SHOT PEENING FORMING ON FATIGUE STRENGTH OF 7050 HIGH-STRENGTH ALUMINUM ALLOYICAS2022_0316
Hanifi, A.PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFTICAS2022_0126
Hanifi, A.ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND DISTURBANCE LEVELSICAS2022_0571
Hanifi, A.REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYERICAS2022_0605
Hanifi, A.ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATIONICAS2022_0635
Hanifi, A.DIRECT NUMERICAL SIMULATIONS OF A THICK, ROTATING AIRFOIL AT A LOW REYNOLDS NUMBERICAS2022_0680
Hanisch, L.V.A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTSICAS2022_0850
Hao, C.NUMERICAL INVESTIGATION ON TURBINE SHROUD FILM COOLING HEAT TRANSFER PERFORMANCE OF TURBINE BLADE WITH GROOVE TIPICAS2022_0203
Harada, A.CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H-INFINITY STRUCTURE WITH GWOICAS2022_0428
Harada, M.STUDY ON THE APPLICATION OF EMULSIFIED FUEL IN SMALL JET ENGINESICAS2022_0751
Harada, M.EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENTICAS2022_0756
Hardell, H.PERFORMANCE EVALUATION OF THE ARRIVAL OPERATIONS IN TERMINAL AREAICAS2022_0825
Harey, C.DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURESICAS2022_0734
Hariansyah, M.A.DEEP LEARNING TECHNIQUES FOR HIGH-DIMENSIONAL SURROGATE-BASED AERODYNAMIC DESIGNICAS2022_0187
Harrison, N.A.TRANSONIC TRUSS-BRACED WING VISION VEHICLE TECHNOLOGY MATURATIONICAS2022_0397
Harrison, E.D.A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFTICAS2022_0453
Harrison, N.A.MDAO OF A TRANSONIC TRUSS-BRACED WING VISION VEHICLEICAS2022_0807
Hartl, P.EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSISICAS2022_0250
Hartman, S.A.INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRDICAS2022_0653
Hartmann, J.ELIMINATING CLIMATE IMPACT FROM AVIATION – REVIEW OF PROMISING AIRCRAFT CONCEPTS AND ENABLING TECHNOLOGY BRICKSICAS2022_0716
Hasan, Y.J.LANDING SIMULATION OF A HIGH-ALTITUDE PLATFORM WITH SKID-TYPE LANDING GEAR – FLIGHT PROCEDURE, CONTROLLER, AND LOADSICAS2022_0364
Hatamoto, A.EXPERIMENTAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS OF DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATORICAS2022_0877
Hausmann, P.IMAGE SEGMENTATION BASED EMERGENCY LANDING FOR AUTONOMOUS AND AUTOMATED UNMANNED AERIAL VEHICLESICAS2022_0725
Hayböck, S.EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSISICAS2022_0250
He, P.AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGSICAS2022_0560
He, Y.-B.EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECKICAS2022_0847
Healy, F.LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPSICAS2022_0524
Heberle, G.EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMASICAS2022_0526
Hecker, P.FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURESICAS2022_0958
Heersema, N.UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATIONICAS2022_0774
Hegde, A.INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFTICAS2022_0326
Heger, R.THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIESICAS2022_0917
Heidebrecht, A.DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFTICAS2022_0622
Heiets, I.DOOR-TO-DOOR TRAVEL PLANNER FOR IMPROVED TRAVELER EXPERIENCE USING DIGITAL TWIN CONCEPTICAS2022_0011
Helgesen, B.FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSUREICAS2022_0028
Henke, M.A CREDIBILITY-BASED CRITERION FOR THE ASSESSMENT OF FUTURISTIC AIRCRAFT CONCEPTSICAS2022_0850
Henne, U.NUMERICAL AND EXPERIMENTAL INVESTIGATIONS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODELICAS2022_0720
Henningson, D.AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGESICAS2022_0104
Henningson, D.S.ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND DISTURBANCE LEVELSICAS2022_0571
Henningson, D.S.REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYERICAS2022_0605
Henningson, D.S.ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATIONICAS2022_0635
Henningson, D.DIRECT NUMERICAL SIMULATIONS OF A THICK, ROTATING AIRFOIL AT A LOW REYNOLDS NUMBERICAS2022_0680
Henningson, D.AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 2ICAS2022_0946
Hermetz, J.FLIGHT EXPERIMENTS FOR THE ALTAIR SEMI-REUSABLE AIR-LAUNCH SYSTEM WITH THE DEMONSTRATOR EOLEICAS2022_0541
Herrmann, U.NOVEL PATHWAYS TO SUSTAINABLE AVIATIONICAS2022_0688
Herzog, E.HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENTICAS2022_0434
Hesse, C.EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXTICAS2022_0254
Hesse, J.-T.PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONSICAS2022_0820
Higasa, K.ASSESSMENT AND CONTROL OF ARRIVAL FLOW AND WAITING TIME APPLYING GT/GI/ST+GI TIME-VARYING QUEUING MODELICAS2022_0132
Hillebrecht, A.ASSESSMENT OF REAL-TIME DATA TRANSMISSION VIA AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC OCEANIC AIRSPACEICAS2022_0168
Hillebrecht, A.CLUSTER STRUCTURE AND GATEWAY AVAILABILITY OF AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC AIRSPACEICAS2022_0293
Hiraiwa, H.ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOWICAS2022_0476
Hjorth, J.A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCEICAS2022_0332
Hoarau, Y.USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC PERFORMANCE OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFTICAS2022_0251
Hoeijmakers, H.W.M.INVESTIGATION FLAPPING-FLIGHT AERODYNAMICS OF A ROBOTIC BIRDICAS2022_0653
Hokamoto, S.ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOWICAS2022_0476
Hokamoto, S.INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCEICAS2022_0796
Holmgren, E.IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIESICAS2022_0334
Holmgren, E.MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACTICAS2022_0369
Holzapfel, F.REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFTICAS2022_0797
Holzapfel, F.AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFTICAS2022_0835
Holzapfel, F.EXTENSION OF THE CAPABILITIES OF AN AUTOMATIC LANDING SYSTEM WITH PROCEDURES MOTIVATED BY VISUAL-FLIGHT-RULESICAS2022_0841
Homan, J.FATIGUE OF NOTCHED STANDARD SPECIMENS – THE INFLUENCE OF THE STRESS GRADIENT ON THE S-N CURVE IN AL2024ICAS2022_0561
Homola, J.INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONSICAS2022_0904
Homola, J. OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSEICAS2022_0909
Honda, S.AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATIONICAS2022_0192
Hong, H.REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFTICAS2022_0797
Hoogreef, M.F.M.INSTALLATION PENALTY OF AERO-ENGINES ON NARROW BODY AIRCRAFTICAS2022_0246
Hoogreef, M.F.M. SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART I: INITIAL DESIGNSICAS2022_0248
Hoogreef, M.F.M.SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART II: SENSITIVITY ANALYSISICAS2022_0481
Hoogreef, M.DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFTICAS2022_0622
Hopkins, S.FUTURE COMBAT AIRCRAFT SYSTEM THE COMPLEXITY OF THE SKILLS EQUATIONICAS2022_0901
Horak, M.TREND MONITORING OF TURBOPROP ENGINESICAS2022_0094
Horinouchi, S.CONCEPT DESIGN OF A LOW BOOM SSBJ TO SATISFY SOCIAL ACCEPTANCEICAS2022_0762
Hornung, M.THE INFLUENCE OF THE MODEL PARAMETERS OF LI-ION BATTERIES ON THE WIRING HARNESS PERFORMANCE OF EVTOL AIRCRAFTICAS2022_0113
Hornung, M.MORPHING FORWARD WING SECTION SKIN DESIGN FOR A SAILPLANE CONSIDERING WING BENDINGICAS2022_0178
Hornung, M.COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAVICAS2022_0367
Hornung, M.SUCCESSIVE KNOWLEDGE BUILDUP AND TRANSFER DURING THE ANALYSIS OF SCALED UAV WINGS BY MEANS OF MACHINE LEARNINGICAS2022_0521
Hosseini, S.WING LOADING PROCESS IN KNOWLEDGE-BASED AIRCRAFT DESIGN AND OPTIMIZATION FRAMEWORKICAS2022_0519
Hou, P.TASK ALLOCATION METHOD FOR COMPLEX RECONNAISSANCE AREA BY MULTIPLE UAVSICAS2022_0195
Hua, Y.DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATIONICAS2022_0143
Huang, Y.-L.RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHPICAS2022_0200
Huang, D.-Q.RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHPICAS2022_0200
Huang, H.Y.STUDY ON MECHANICAL PROPERTIES OF CARBON FIBER RESIN MATRIX COMPOSITE BOLTED JOINT STRUCTURE AT HIGH TEMPERATUREICAS2022_0278
Huang, H.Y.DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIALICAS2022_0290
Huang, W.DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENTICAS2022_0321
Huang, Y.INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCEICAS2022_0796
Hueso-Rebassa, J.OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELSICAS2022_0167
Huete, J.PROPULSION SYSTEM INTEGRATION FOR A FIRST GENERATION HYDROGEN CIVIL AIRLINER?ICAS2022_0950
Hunger, R.THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITIONICAS2022_0268
Hyde, L.ARRIVING AT CERTIFIABLE NOVEL AIRLINER USING LIQUID HYDROGEN & EFFICIENCY METRICSICAS2022_0373
Hühne, C.A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONSICAS2022_0030
Hällqvist, R.HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENTICAS2022_0434
Hällqvist, R.MODEL FIDELITY AND ITS INFLUENCE ON AIRCRAFT CONCEPTUAL DESIGNICAS2022_0477
Häßy, J.KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND MASS ESTIMATION OF RUBBER AERO ENGINESICAS2022_0497
Häßy, J.IMPACT OF THE NUMBER OF WING STATIONS ON THE TWIST DISTRIBUTION OF A BWB CONCEPTUAL AIRCRAFT DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTIONICAS2022_0854
Hörnschemeyer, R.VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIRICAS2022_0083
Hörnschemeyer, R.EXPERIMENTS TO INVESTIGATE LIFT PRODUCTION MECHANISMS ON OSCILLATING TRAILING-EDGE FLAPSICAS2022_0780
Iafrati, A.ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODYICAS2022_0385
Ibron, C.LES OF COMBUSTION DYNAMICS IN AN ETHYLENE-HYDROGEN-AIR RAMJETICAS2022_0786
Ignatyev, D.FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIESICAS2022_0520
Ignatyev, D.I.GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMPICAS2022_0644
Ikeda, T.WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS)ICAS2022_0814
Ilic, C.APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFTICAS2022_0892
Ilina, S.TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINSICAS2022_0822
Imamura, T.UNSTEADY TURBULENT FLOW SIMULATION OF ROTOR BLADES ON MOVING CARTESIAN GRIDS USING RECURSIVE FITTING APPROACHICAS2022_0790
Inal, T.A FAULT INTEGRATOR BASED VOTE&MONITOR DESIGN FOR GRACEFULL DEGRADATION IN MULTIPLE REDUNDANT SAFETY CRITICAL SYSTEMSICAS2022_0472
Inasawa, A.EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETSICAS2022_0243
Iovieno, M.HEAT TRANSFER ENHANCEMENT BY SUSPENDED PARTICLES IN A TURBULENT SHEARLESS FLOWICAS2022_0711
Ireland, C.J.A GLOBAL APPROACH TO ASSESSING THE CLIMATE RESILIENCE OF AIRPORTSICAS2022_0922
Isikveren, A.T.DEVELOPMENT OF A HYDROGEN-POWERED FUSELAGE-MOUNTED BLI PROPULSOR ADD-ON FOR PASSENGER AIRCRAFTICAS2022_0622
Ispir, A.C.HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONSICAS2022_0572
Itoh, E.DEVELOPING A DEPARTURE QUEUE MODEL FOR INTEGRATED ARRIVAL AND DEPARTURE OPERATION OF RUNWAYSICAS2022_0106
Itoh, E.ASSESSMENT AND CONTROL OF ARRIVAL FLOW AND WAITING TIME APPLYING GT/GI/ST+GI TIME-VARYING QUEUING MODELICAS2022_0132
Itoh, E.APPLYING MACHINE LEARNING TO TAXI-TIME PREDICTION ATTOKYO INTERNATIONAL AIRPORTICAS2022_0267
Itoh, E.MACHINE LEARNING METHODS ENSURING BOTH PERFORMANCE AND INTERPRETABILITY OF ESTIMATING AIRCRAFT ARRIVAL TIMESICAS2022_0271
Itoh, E.AIR TRAFFIC SIMULATION ACROSS FIR IN JAPAN USING CELLULAR AUTOMATONICAS2022_0401
Itoh, E.REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMICICAS2022_0486
Iuspa, L.AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLESICAS2022_0241
Iuspa, L.AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLEICAS2022_0259
Ivchenko, M.DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGINGICAS2022_0447
Iwami, Y.WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS)ICAS2022_0814
Iwanizki, M.IMPACT OF THE NUMBER OF WING STATIONS ON THE TWIST DISTRIBUTION OF A BWB CONCEPTUAL AIRCRAFT DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTIONICAS2022_0854
Iwata, D.DEVELOPING A DEPARTURE QUEUE MODEL FOR INTEGRATED ARRIVAL AND DEPARTURE OPERATION OF RUNWAYSICAS2022_0106
Izuka, J.H.EXPERIMENTAL AND NUMERICAL ANALYSIS OF A PRE-STRESSED TENSEGRITY MEMBRANEICAS2022_0038
Jacob, M.C.UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLSICAS2022_0611
Jacobson, M.DEMONSTRATING AN APPROACH FOR MULTIDISCIPLINARY SET BASED DESIGN WITHIN AN AEROSPACE RESEARCH PROJECT - DEFAINEICAS2022_0661
Jameel, M.DEMAND PATTERN INFLUENCE ON RELATION OF TURNAROUND DURATION AND GATE OCCUPATION DEPENDING ON AVAILABLE RESOURCESICAS2022_0122
Jameel, M.THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITIONICAS2022_0268
Jan, R.PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY IMPLEMENTED UNDER ASWINGICAS2022_0318
Jang, Y.H.EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAVICAS2022_0488
Jansen, R.UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATIONICAS2022_0774
Jaroslawski, T.STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCEICAS2022_0583
Jax, T.POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORSICAS2022_0347
Jeaong, H.J.EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAVICAS2022_0488
Jentink, H.VALIDATION OF SCALED FLIGHT TESTINGICAS2022_0375
Jentys, M.M.TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WINGICAS2022_0037
Jesudasan, R.PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFTICAS2022_0126
Jesus, L.D.USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTIONICAS2022_0389
Jeyarai, A.CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECTICAS2022_0350
Jeyaraj, A.K.SYSTEMS ARCHITECTING: A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0 PROJECTICAS2022_0365
Jézégou, J.FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFTICAS2022_0214
Jezegou, J.OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGNICAS2022_0550
Ji, Z.A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTHICAS2022_0142
Ji, Z.DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATIONICAS2022_0143
Ji, H.-B.RESEARCH ON FLOW HEAT TRANSFER CHARACTERISTICS OF HEAT EXCHANGER BASED ON BIONIC FRACTAL STRUCTUREICAS2022_0510
Jia, D.S.AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORKICAS2022_0199
Jia, Q.EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONEICAS2022_0256
Jia, B.-B.SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSORICAS2022_0589
Jia, X.ELECTROMAGNETIC INTERFERENCE SHIELDING EFFECTIVENESS OF THE THIN CARBON NANOFIBERS/ SILICON CARBIDE FABRICS COMPOSITESICAS2022_0608
Jiang, X.STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGERICAS2022_0072
Jiang, X.EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONEICAS2022_0256
Jiang, T.MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATIONICAS2022_0544
Jiang, L.-Y.SAND EROSION MODELING IN GENERIC COMPRESSOR RIG TESTINGICAS2022_0945
Jiao, Y.INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNELICAS2022_0547
Jin, T.EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRINGICAS2022_0632
Jochims Lau, C.A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENTICAS2022_0523
Jochims Lau, C.EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMASICAS2022_0526
Johann, S.USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAMICAS2022_0116
Johansson, A.IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIESICAS2022_0334
Johansson, A.MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACTICAS2022_0369
Johansson, E.FLIGHT DYNAMICS SIMULATION AND FCS AUTO-GENERATION IN THE CONCEPTUAL DESIGN PHASE OF AN UNSTABLE SUPERSONIC AIRCRAFTICAS2022_0458
Johansson, P.STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECTICAS2022_0480
Johansson, U.STATUS OF GKN AEROSPACE\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECTICAS2022_0480
Johansson, A.MORE ELECTRIC AIRPLANE: CASE STUDY STOCKHOLM - COPENHAGENICAS2022_0506
Johansson, B.HMI-HUFLAB – A BRAZILIAN - SWEDISH INITIATIVE IN HUMAN FACTORS FOR AERONAUTICSICAS2022_0707
Johnson, M. INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONSICAS2022_0904
Johnson, M. OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSEICAS2022_0909
Jokinen, J.FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHODICAS2022_0754
Joksimovic, A.AIRCRAFT FLEET MODELS USING A BOTTOM-UP APPROACH FOR SIMULATING AVIATION TECHNOLOGICAL PROSPECTIVE SCENARIOSICAS2022_0117
Joksimovic, A.ENERGY-BASED SYSTEM ARCHITECTURE DESIGN - ENVIRONMENTAL CONTROL SYSTEMICAS2022_0368
Jonsson, I.NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCTICAS2022_0236
Jonsson, I.EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCTICAS2022_0788
Jonsson, I.MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEMICAS2022_0832
Jordao, R.TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMSICAS2022_0604
Josefsson, B.STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATIONICAS2022_0903
Jouannet, C.ZERO-EMISSION REGIONAL AVIATION IN SWEDENICAS2022_0650
Jouannet, C.UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENTICAS2022_0659
Jouannet, C.SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045ICAS2022_0804
Jouannet, C.ICAS DIGITAL PIONEERING INITIATIVE AND SYSTEM OF SYSTEM CHALLENGESICAS2022_0964
Jung, C.-G.CONVEX PROGRAMMING-BASED OPTIMAL THREE-DIMENSIONAL MID-COURSE GUIDANCE WITH LOSSLESS CONVEXIFICATIONICAS2022_0810
Jung, Y.META-REINFORCEMENT LEARNING-BASED FAULT TOLERANT CONTROL FOR A QUADROTOR WITH A SEVERE LOSS OF ROTORICAS2022_0879
Júnior, M.M.C. DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCYICAS2022_0662
Juracka, J.TREND MONITORING OF TURBOPROP ENGINESICAS2022_0094
Justin, C.Y.ZERO-EMISSION REGIONAL AVIATION IN SWEDENICAS2022_0650
Justin, C.Y.REGIONAL AIR MOBILITY MARKET STUDYICAS2022_0872
Jäger, M.LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEMICAS2022_0144
Kacik, D.OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANEICAS2022_0576
Kahlo, H.DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFTICAS2022_0921
Kai, J.-M.A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERSICAS2022_0568
Kalfas, A.I.MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENTICAS2022_0943
Kalra, R.ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORAICAS2022_0699
Kanazaki, M.AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATIONICAS2022_0413
Kanerva, M.FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHODICAS2022_0754
Kang, M.-H.INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEXICAS2022_0417
Kapidzic, Z.INCREMENTAL FATIGUE DAMAGE MODEL: APPLICATION TO PLANE PROBLEMS WITH NON-PROPORTIONAL LOADINGICAS2022_0111
Karabasov, S.A.APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDSICAS2022_0643
Karagoz, F.A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFTICAS2022_0453
Kartal, M.R.FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIESICAS2022_0520
Kasemsri, R.AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATIONICAS2022_0413
Kashitani, M.ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICESICAS2022_0145
Katagiri, K.WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS)ICAS2022_0814
Kato, F.APPLYING MACHINE LEARNING TO TAXI-TIME PREDICTION ATTOKYO INTERNATIONAL AIRPORTICAS2022_0267
Kaya, M.AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPESICAS2022_0381
Kaysser-Pyzalla, A.FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATIONICAS2022_0708
Kazula, S.DEVELOPMENT OF A CONTROLS APPROACH FOR FUEL CELL-POWERED ALL-ELECTRIC AERO ENGINES BASED ON AN FHAICAS2022_0366
Kelly, M.A.MODEL-BASED SYSTEMS ENGINEERING FOR FUTURE DIGITAL FLIGHT LINESICAS2022_0919
Kerlin, U.CERTIFICATION BY ANALYSIS - SOME THOUGHTSICAS2022_0954
Kern, J.S.ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND DISTURBANCE LEVELSICAS2022_0571
Keye, S.CAD DEFORMATION FOR THE CONSIDERATION OF AEROELASTIC EFFECTSICAS2022_0557
Keßler, M.ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUPICAS2022_0335
Khan, S.A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATIONICAS2022_0704
Khanal, P.SMART SKIN FOR AEW AIRCRAFTICAS2022_0048
Khankwa, K.AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATIONICAS2022_0413
Khorrami, M.R.TOWARD A COMMUNITY NOISE ASSESSMENT OF SINGLE-AISLE AIRCRAFT WITH HYBRID-ELECTRIC PROPULSIONICAS2022_0953
Kiehn, D.COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACSICAS2022_0505
Kienberger, M.USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAMICAS2022_0116
Kienberger, M.ZONAL MODEL VALIDATION FOR AN ENVIRONMENTALLY FRIENDLY AIRCRAFT CARGO FIRE PROTECTION SYSTEM WITH CONTAINERIZED LOADICAS2022_0159
Kienitz, K.H.FLIGHT CONTROLLABILITY ANALYSIS IN TIGHT FORMATION AND CRUISE FLIGHT FOR FUEL SAVINGICAS2022_0273
Kier, T.EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERSICAS2022_0656
Kierbel, D.VALIDATION OF SCALED FLIGHT TESTINGICAS2022_0375
Kierbel, D.CLEAN-SKY 2 LARGE PASSENGER AIRCRAFT PLATFORM 1 ADVANCED ENGINE AND AIRCRAFT CONFIGURATIONSICAS2022_0464
Kierulf, B.CRITICAL REVIEW OF SOUNDING ROCKET FLIGHT DATA AND COMPUTATIONAL FLUID DYNAMICS EFFORTSICAS2022_0414
Kikura, I.FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLETICAS2022_0830
Kilian, T.AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WINICAS2022_0155
Kim, C.-G.DOPAMINE-COATED UHMWPE/HYDROGEN-RICH BENZOXAZINE COMPOSITES FOR SPACE RADIATION SHIELDINGICAS2022_0101
Kim, T.G.PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTSICAS2022_0141
Kim, Y.J.PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTSICAS2022_0141
Kim, S.K.PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTSICAS2022_0141
Kim, S.A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSBICAS2022_0222
Kim, J.A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSBICAS2022_0222
Kim, L.INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFTICAS2022_0346
Kim, Y.J.FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTERICAS2022_0420
Kim, T.G.FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTERICAS2022_0420
Kim, S.K.FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTERICAS2022_0420
Kim, L.-S.FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSIONICAS2022_0438
Kim, D.A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFTICAS2022_0453
Kim, S.K.EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAVICAS2022_0488
Kim, Y.NEURAL-NETWORK ADAPTIVE DECENTRALIZED FORMATION CONTROLICAS2022_0490
Kim, B.S.NEURAL-NETWORK ADAPTIVE DECENTRALIZED FORMATION CONTROLICAS2022_0490
Kim, J.OPENVSP BASED AERODYNAMIC DESIGN OPTIMIZATION TOOL BUILDING METHOD AND ITS APPLICATION TO TAILLESS UAVICAS2022_0858
Kim, S.-H.META-REINFORCEMENT LEARNING-BASED FAULT TOLERANT CONTROL FOR A QUADROTOR WITH A SEVERE LOSS OF ROTORICAS2022_0879
Kim, Y.META-REINFORCEMENT LEARNING-BASED FAULT TOLERANT CONTROL FOR A QUADROTOR WITH A SEVERE LOSS OF ROTORICAS2022_0879
Kimura, K.HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXAICAS2022_0444
Kiris, C.C.UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATIONICAS2022_0774
Kishimoto, N.WIND TUNNEL EXPERIMENT OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS) AND BLACK KITE (MILVUS MIGRANS)ICAS2022_0814
Kiszkowiak, L.THE USE OF COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A NEW GENERATION LIGHT COMBAT AIRPLANEICAS2022_0371
Klaproth, T.SUCCESSIVE KNOWLEDGE BUILDUP AND TRANSFER DURING THE ANALYSIS OF SCALED UAV WINGS BY MEANS OF MACHINE LEARNINGICAS2022_0521
Klein, M.OPEN CAVITY SIMULATIONS UNDER SIDESLIP FLOW CONDITIONSICAS2022_0173
Klein, M.INVESTIGATION OF LEADING-EDGE VORTICES ON A TRIPLE-DELTA-WING CONFIGURATION USING SCALE-ADAPTIVE SIMULATIONICAS2022_0528
Klein, C.NUMERICAL AND EXPERIMENTAL INVESTIGATIONS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODELICAS2022_0720
Kleine, V.G.ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATIONICAS2022_0635
Kleineberg, M.DESIGN,MANUFACTURING & CERTIFICATION STRATEGIES FOR INNOVATIVE HYDROGEN STORAGE SYSTEMS TO ENABLE ZERO EMISSION AVIATIONICAS2022_0962
Klimczyk, W.PROPELLER AEROACOUSTIC MODELS IN VARIABLE-FIDELITY DESIGN OPTIMIZATIONICAS2022_0710
Klimmek, T.LOADS ANALYSIS AND STRUCTURAL OPTIMIZATION OF A LONG-RANGE TRANSPORT CONFIGURATION WITH HYBRID LAMINAR FLOW CONTROLICAS2022_0158
Klimmek, T.AEROELASTIC MODELING, LOADS ANALYSIS AND STRUCTURAL DESIGN OF A FIGHTER AIRCRAFTICAS2022_0161
Klimmek, T.A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATORICAS2022_0826
Kloock-Schreiber, D.INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGIONICAS2022_0840
Kluenker, C.DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORSICAS2022_0264
Klöckner, A.FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATIONICAS2022_0708
Kniebel, B.SORA-BASED RISK ASSESSMENT FOR CARGO UNMANNED AERIAL VEHICLES IN THE UAM FRAMEWORKICAS2022_0240
Knoblauch, B.DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFTICAS2022_0921
Knöös Franzén, L.ONTOLOGY-ASSISTED AIRCRAFT CONCEPT GENERATIONICAS2022_0352
Kobayashi, E.INFLUENCES OF CHANGING THE INSTALLING POSITIONS OF MULTIPLE WINGLETS ON AERODYNAMIC CHARACTERISTICSICAS2022_0459
Kobayashi, K.INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONSICAS2022_0904
Kobayashi, K. OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSEICAS2022_0909
Kobiki, N.HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXAICAS2022_0444
Kong, G.DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATIONICAS2022_0753
Kontos, G.PILOT TRAINING CHALLENGES FOR ADVANCED AIR MOBILITYICAS2022_0675
Kopardekar, P.INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONSICAS2022_0904
Kopardekar, P.OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSEICAS2022_0909
Korn, B.THE GROUP OF RESPONSABLES "FLIGHT MECHANICS, SYSTEMS AND INTEGRATION (GOR FM)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIESICAS2022_0912
Kos, J.NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050ICAS2022_0801
Koschel, S.AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATIONICAS2022_0747
Koschlik, A.-K.DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTSICAS2022_0868
Kostek, A.ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUPICAS2022_0335
Koyama, T.DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITESICAS2022_0448
Kraft, T.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
Krammer, C.REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFTICAS2022_0797
Kratz, J.L.UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATIONICAS2022_0774
Krause, D.A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLEICAS2022_0791
Krause, D.PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONSICAS2022_0820
Krawczyk, K.TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D PRINTED EPOXY RESINSICAS2022_0822
Krishnaswamy, S.MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURINGICAS2022_0176
Krus, P.ONTOLOGY-ASSISTED AIRCRAFT CONCEPT GENERATIONICAS2022_0352
Krus, P.A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROLICAS2022_0513
Krus, P.MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIESICAS2022_0575
Krus, P.ENVIRONMENTAL AGENT-BASED MODELLING FOR A FIREFIGHTING SYSTEM OF SYSTEMSICAS2022_0645
Krus, P.THE BENEFIT OF BILATERAL RESEARCH NETWORKS - THE SARC AND BARINET INITIATIVES AND THE BRAZILIAN SWEDISH COLLABORATION IN AERONAUTICSICAS2022_0681
Krus, P.SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045ICAS2022_0804
Krus, P.HYBRID ELECTRIC PROPULSION SYSTEM OPTIMIZATION FOR A COMMUTER AIRCRAFTICAS2022_0874
Krus, P.CRITICALITY AND COMFORT ZONE SUPPORTING DESIGN CHOICES TO ACHIEVE SUSTAINABLE REQUIREMENTS: THE CASE OF ELECTRIC AIRCRAFTICAS2022_0875
Kruse, M.AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WINICAS2022_0155
Krüger, W.WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSESICAS2022_0663
Krüger, W.R.A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATORICAS2022_0826
Kuchar, R.EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATIONICAS2022_0467
Kuelper, N.SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGNICAS2022_0665
Kuenz, A.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
Kumawat, H.A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLEICAS2022_0791
Kurita, M.EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETSICAS2022_0243
Kurka, P.R.G.EXPERIMENTAL AND NUMERICAL ANALYSIS OF A PRE-STRESSED TENSEGRITY MEMBRANEICAS2022_0038
Kurtulus, D.F.AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATIONICAS2022_0593
Kusunose, K.ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICESICAS2022_0145
Kwiecien, A.COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS OBTAINED BY ANALYTICAL, PANEL AND CFD METHODICAS2022_0353
Kwiek, A.PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLEICAS2022_0395
Kwiek, A.MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIESICAS2022_0462
Kügler, D.FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATIONICAS2022_0708
Kyriakopoulos, M.EUROPEAN AVIATION RESEARCH AND INNOVATION TOWARDS CLIMATE NEUTRALITYICAS2022_0959
Kållberg, F.AERODYNAMIC DEVELOPMENT OF SAAB FCAS UNMANNED SUPERSONIC COMBAT AIRCRAFTICAS2022_0570
Kötter, A.DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT – LIFE CYCLE ASSESSMENT ACTIVITIES AT ECOTECH / CLEANSKY 2ICAS2022_0895
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Labans, E.INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGYICAS2022_0685
Laliberté, J.FATIGUE CRACK PROPAGATION IN ADDITIVELY MANUFACTURED POLYMER PARTSICAS2022_0777
Lamkin, A.H.R.COUPLED AEROPROPULSIVE ANALYSIS AND OPTIMIZATION OF A HIGH BYPASS TURBOFAN ENGINEICAS2022_0390
Lammen, W.NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050ICAS2022_0801
Lammering, T.DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACKICAS2022_0677
Langer, M.FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURESICAS2022_0958
Langer, M.FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURESICAS2022_0961
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Larsson, R.ANALYSIS OF THE EFFECT OF FLOW TRANSITION OVER THE WINGS OF THE BLADE DEMONSTRATORICAS2022_0150
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Larsson, F.MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIESICAS2022_0575
Larsson, F.AN EVALUATION METHOD FOR AIRCRAFT ACTUATION SYSTEMS OPERATIONAL COSTICAS2022_0601
Larsson, R.REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYERICAS2022_0605
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Lee, S.-G.OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNINGICAS2022_0109
Lee, D.INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFTICAS2022_0346
Lee, S.AIRCRAFT DESIGN PARAMETER ESTIMATION USING DATA-DRIVEN MACHINE LEARNING MODELSICAS2022_0435
Lee, D.-W.FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSIONICAS2022_0438
Lee, H.J.GENERATION OF TERRAIN PROFILE FOR TERRAIN FOLLOWINGICAS2022_0538
Lee, S.C.GENERATION OF TERRAIN PROFILE FOR TERRAIN FOLLOWINGICAS2022_0538
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Lee, J.-J.DESIGN STUDY OF BRAKE MECHANICAL CONTROL SYSTEM OF UAVICAS2022_0778
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Lefevre, L.ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUPICAS2022_0335
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Lei, Z.OPERATIONAL FEASIBILITY STUDY OF AIR TAXI SERVICE USING EVTOLICAS2022_0474
Leißling, D.THE NEW RESEARCH AIRCRAFT ISTAR - EXPERIMENTAL FLIGHT CONTROL SYSTEMICAS2022_0439
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Li, X.DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENTICAS2022_0321
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Li, H.-Y.INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEXICAS2022_0417
Li, H.-Y.A FAST PREDICTION METHOD FOR DROPPING WATER OF FIRE FIGHTING AIRCRAFT BASED ON EXTERNAL BALLISTICS OF PARTICLESICAS2022_0422
Li, Z.-P.REDESIGNING AND SIMULATION EVALUATION ON LARGE-FLOW HIGH-TEMPERATURE HIGH-PRESSURE BYPASS SURGE-OUT SYSTEMICAS2022_0487
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Li, H.-X.SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSORICAS2022_0589
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Li, F.-R.RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTIONICAS2022_0760
Li, H.AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFTICAS2022_0795
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Liscouët-Hanke, S.SYSTEMS ARCHITECTING: A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0 PROJECTICAS2022_0365
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Liu, Y.DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISKICAS2022_0032
Liu, G.STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGERICAS2022_0072
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Liu, L.STRUCTURAL DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WINGICAS2022_0139
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Liu, H.DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATIONICAS2022_0143
Liu, J.RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHPICAS2022_0200
Liu, Y.INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN THE V103 CASCADEICAS2022_0204
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Liu, P.Q.NUMERICAL STUDY ON WATER DISPLACEMENT DRAG CHARACTERISTICS OF AIRCRAFT ELASTIC TIRE ON CONTAMINATED RUNWAYSICAS2022_0329
Liu, P.SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATIONICAS2022_0386
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Liu, Q.-H.EQUIVALENT CALCULATION METHOD OF FLYOVER NOISE LEVEL OF CUTBACK TAKE-OFF FOR CIVIL JET AIRPLANE AIRWORTHINESS CERTIFICATIONICAS2022_0626
Liu, Y.J.RESEARCH ON THE DUCTILE FRACTURE OF AL7085 AND TC11 UNDER COMPLEX STRESS STATEICAS2022_0862
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Luckring, J.M.CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIESICAS2022_0934
Ludena Cervantes, T.J. NEURAL-NETWORK ADAPTIVE DECENTRALIZED FORMATION CONTROLICAS2022_0490
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Lundbladh, A.MULTIPOINT AERODYNAMIC DESIGN OF A NACELLE FOR AN ELECTRIC FANICAS2022_0138
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Lundbladh, A.SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045ICAS2022_0804
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Luo, R.SMART SKIN FOR AEW AIRCRAFTICAS2022_0048
Luo, M.A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTHICAS2022_0142
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Lyu, S.A DAMAGE RECOGNITION METHOD OF COMPOSITE STRUCTURES USING ARTIFICIAL DEFECTIONSICAS2022_0052
Lößle, F.ROTOR / ROTOR AERODYNAMIC INTERACTIONS - A GARTEUR ACTION GROUPICAS2022_0335
Ma, Z.DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNELICAS2022_0045
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Ma, T.-L.DESIGN AND EFFICIENCY ANALYSIS OF EVTOL CONTRA-ROTATING PROPELERICAS2022_0060
Ma, T.-L.RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAVICAS2022_0107
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Machado Cardoso Junior, M.LONG TOUCHDOWN THROUGH A SAFETY-II PERSPECTIVEICAS2022_0185
MacManus, D.G.A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKEICAS2022_0127
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Mansfield, N.MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHTICAS2022_0115
Mantegna, G.RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALSICAS2022_0218
Marciello, V.TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASSICAS2022_0641
Marciello, V.MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFTICAS2022_0649
Mariani, R.PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFTICAS2022_0126
Mariani, R.WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLEICAS2022_0215
Mariani, R.DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGINGICAS2022_0447
Marini, M.AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECTICAS2022_0235
Marini, M.COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATIONICAS2022_0342
Marini, M.HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONSICAS2022_0572
Marini, M.AERODATABASE DEVELOPMENT AND INTEGRATION OF SUPERSONIC/HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROJECTICAS2022_0596
Marini, M.HIGH PRESSURE HYDROGEN OXYGEN COMBUSTION KINETIC ASSESSMENT FOR AIR-BREATHING PROPULSION SUPERSONIC GREEN AVIATIONICAS2022_0845
Marino, A.HYBRID-ELECTRIC AND FULL ELECTRIC ARCHITECTURES FOR LOW-EMISSION HYBRID-ELECTRIC REGIONAL [REG] AIRCRAFTICAS2022_0930
Marion, G.TECHNOLOGY MATURATION IN CLEAN SKY 2 FOR NEXT GENERATION SMR ENGINEICAS2022_0006
Markatos, D.N.ASSESSMENT OF THE SUSTAINABILITY OF THE IMPLEMENTATION OF CIRCULAR ECONOMY PRINCIPLES IN PRODUCING AIRCRAFT STRUCTURESICAS2022_0056
Markesteijn, A.P.APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDSICAS2022_0643
Markiewicz, R.THE GROUP OF RESPONSABLES "ROTORCRAFT (RC-GOR)": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIESICAS2022_0917
Marks, T.ASSESSMENT OF REAL-TIME DATA TRANSMISSION VIA AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC OCEANIC AIRSPACEICAS2022_0168
Marks, T.CLUSTER STRUCTURE AND GATEWAY AVAILABILITY OF AD-HOC COMMUNICATION NETWORKS IN THE NORTH ATLANTIC AIRSPACEICAS2022_0293
Marouf, A.USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC PERFORMANCE OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFTICAS2022_0251
Marques, H.C.A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAYICAS2022_0723
Marques, H.C.UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIOICAS2022_0729
Marques, J.M.G.ON LATERAL-LONGITUDINAL CONTROL COUPLING FOR SHORT- AND LONG-FUSELAGE BWB AIRCRAFT CONFIGURATIONSICAS2022_0733
Martin, N.TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURESICAS2022_0012
Martina, F.MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURINGICAS2022_0176
Martini Catalano, F.LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTIONICAS2022_0088
Martins, J.R.R.A.LARGE-SCALE MULTIFIDELITY AEROSTRUCTURAL OPTIMIZATION OF A TRANSPORT AIRCRAFTICAS2022_0186
Martins, W. M.USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTIONICAS2022_0389
Martins, J.R.R.A.COUPLED AEROPROPULSIVE ANALYSIS AND OPTIMIZATION OF A HIGH BYPASS TURBOFAN ENGINEICAS2022_0390
Martins, J.R.R.A.AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATIONICAS2022_0593
Martins, J.R.R.A.TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATIONICAS2022_0905
Marzocca, P.NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMSICAS2022_0396
Marzocca, P.AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATIONICAS2022_0747
Massegur, D.COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMSICAS2022_0399
Matayoshi, N.NEW ENTRANTS’ AIRSPACE INTEGRATION IN JAPAN: JAXA’S ONGOING CONTRIBUTIONICAS2022_0907
Matesanz-Garcia, J.A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLESICAS2022_0162
Matias, C.TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATIONICAS2022_0036
Matoses Gimenez, A.DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGINGICAS2022_0447
Matthes, S.MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACEICAS2022_0574
Matunaga, M.A.L.AUTOMATIC FREE-FORM DEFORMATION AS GEOMETRIC PARAMETERIZATION FOR AERODYNAMIC DESIGNICAS2022_0749
Maulana, F.A.TURBULENCE MODELLING STUDIES OF SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE CYLINDER FLARE IN HYPERSONIC FLOWSICAS2022_0746
Mavris, D.N.A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFTICAS2022_0453
Mavris, D.N.ZERO-EMISSION REGIONAL AVIATION IN SWEDENICAS2022_0650
Mavris, D.N.ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACHICAS2022_0817
Mavris, D.N.REGIONAL AIR MOBILITY MARKET STUDYICAS2022_0872
Mavris, D.N.SYSTEM LEVEL IDENTIFICATION OF CRITICAL UNCERTAINTIES TO ENABLE VALIDATION EXPERIMENTSICAS2022_0935
Mavris, D.NEXT STEPS TOWARDS CERTIFICATION BY ANALYSIS - A DIGITAL THREAD PERSPECTIVEICAS2022_0955
Maximo, M.R.O.A.COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMSICAS2022_0340
May, M.EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONSICAS2022_0860
Mayer, F.USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAMICAS2022_0116
Meddaikar, Y.M.A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATORICAS2022_0826
Meeß, H.IMAGE SEGMENTATION BASED EMERGENCY LANDING FOR AUTONOMOUS AND AUTOMATED UNMANNED AERIAL VEHICLESICAS2022_0725
Mège, R.TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONESICAS2022_0655
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Méheut, M.OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION'S CLIMATE IMPACTICAS2022_0843
Meissner, D.VALIDATION OF SCALED FLIGHT TESTINGICAS2022_0375
Meister, J.IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPTICAS2022_0627
Mello, J.M.G.D.A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORKICAS2022_0618
Mendiguchia Meuser, M.MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACEICAS2022_0574
Mendonca, W.R.P.APPLICATION OF THE VIRTUAL CRACK CLOSURE TECHNIQUE FOR CRACKS IN BUILT-UP PANELSICAS2022_0799
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Meng, J.-H.STRUCTURAL DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WINGICAS2022_0139
Meng, D.STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATORICAS2022_0313
Metz, I.C.AN OPERATIONAL CONCEPT FOR THE INTEGRATION OF URBAN AIR MOBILITY VEHICLES INTO THE AIR TRAFFIC CONTROL PROCESSESICAS2022_0451
Metz, I.C.URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH NON-COOPERATIVE AIRSPACE USERSICAS2022_0567
Metz, I.C.EVALUATION AND QUANTIFICATION OF THE POTENTIAL CONSEQUENCES OF BIRD STRIKES IN URBAN AIR MOBILITYICAS2022_0629
Metzler, D.DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACKICAS2022_0677
Meyer, M.ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISKICAS2022_0532
Meyer, H.DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTSICAS2022_0868
Meyer, L.STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATIONICAS2022_0903
Miao, Z.THREE DIMENSIONAL PATH FOLLOWING CONTROL FOR A FIXED-WING UAV ON SO(3) WITH INPUT SATURATIONICAS2022_0049
Michler, O.REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMICICAS2022_0486
Mieloszyk, J.MEDIUM SIZE UAV AS TEST PLATFORM FOR NEW TECHNOLOGIESICAS2022_0462
Mieloszyk, J.OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANEICAS2022_0576
Migliorini, M.A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKEICAS2022_0127
Miki, H.FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLETICAS2022_0830
Milazzo, A.DEVELOPMENT AND APPLICATIONS OF A VIRTUAL HYBRID PLATFORM FOR MULTISCALE ANALYSIS OF ADVANCED STRUCTURES OF AIRCRAFT (DEVISU)ICAS2022_0295
Milazzo, A.TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHODICAS2022_0427
Milz, D.EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONSICAS2022_0860
Mingione, G.THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIESICAS2022_0915
Mirhashemi, A.UPDATE ON SUBSONIC SINGLE AFT ENGINE (SUSAN) ELECTROFAN TRADE SPACE EXPLORATIONICAS2022_0774
Mishra, C.AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFTICAS2022_0835
Mishra, C.EXTENSION OF THE CAPABILITIES OF AN AUTOMATIC LANDING SYSTEM WITH PROCEDURES MOTIVATED BY VISUAL-FLIGHT-RULESICAS2022_0841
Miura, T.VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGSICAS2022_0207
Miyake, T.NUMERICAL INVESTIGATION ON THE DOUBLE TRANSONIC DIP OF SUPERCRITICAL AIRFOIL FLUTTERICAS2022_0545
Miyazaki, S.COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHODICAS2022_0416
Mizukaki, T.NUMERICAL ANALYSIS OF PROPAGATION OF DETONATION WAVE PLUNGING ENTRY THE FUEL JET TRAIN INSIDE ROTATING DETONATION COMBUSTORICAS2022_0409
Mo, D.TWO-PHASE NUMERICAL SIMULATION INVESTIGATION ON THE EFFECTS OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCEICAS2022_0029
Mo, D.DYNAMIC STRESS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISKICAS2022_0032
Modi, P.DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFTICAS2022_0921
Moens, F.MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONSICAS2022_0546
Moerland, E.A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONSICAS2022_0700
Moerland, E.TOWARDS A SEAMLESS SIMULATION OF THE AIR TRANSPORT SYSTEMICAS2022_0732
Monge, F.THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIESICAS2022_0915
Monnier, V.A STUDY ON THE DEVELOPMENT OF THE FLOW DISTORTION DOWNSTREAM OF AN S-DUCT INTAKEICAS2022_0127
Montella, N.AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLESICAS2022_0241
Montella, N.AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLEICAS2022_0259
Moraes, L.PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINEICAS2022_0782
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Moretti, S.SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSISICAS2022_0370
Mori, R.AIRCRAFT MASS ESTIMATION USING CRUISE FLIGHT PROFILEICAS2022_0105
Moriai, H.STUDY ON THE APPLICATION OF EMULSIFIED FUEL IN SMALL JET ENGINESICAS2022_0751
Moriai, H.EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENTICAS2022_0756
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Morrison, J.NATO AVT-297 DEVELOPMENT OF A FRAMEWORK FOR VALIDATION OF COMPUTATIONAL TOOLS FOR ANALYSIS OF AIR VEHICLESICAS2022_0933
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Moruzzi, M.C.AURALIZATION OF NOISE IN A VIRTUAL REALITY AIRCRAFT CABIN FOR PASSENGER WELL-BEING USING HUMAN-CENTRED APPROACHICAS2022_0478
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Moschetta, J.-M.PREDICTING STEADY LIFT AND DRAG COEFFICIENT OF TANDEM AIRCRAFT USING PRANDTL’S EXTENDED LIFTING-LINE THEORY IMPLEMENTED UNDER ASWINGICAS2022_0318
Moschetta, J.-M.A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONSICAS2022_0383
Moschetta, J.-M.STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCEICAS2022_0583
Moura, E.A.IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTINGICAS2022_0873
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Murali, A.R.APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDSICAS2022_0643
Muraoka, K.FLIGHT VERIFICATION OF AUTOMATIC TRANSITION FOR QUAD TILT WING SMALL UAVICAS2022_0740
Muth, B.CONCEPTUAL DESIGN OF FUTURE MILITARY AIR SYSTEMS - AN EDUCATIONAL APPROACHICAS2022_0102
Muth, K.REAL-TIME CALCULATION AND ADAPTION OF CONFLICT-FREE AIRCRAFT GROUND TRAJECTORIESICAS2022_0213
Müller, B.MEASUREMENT OF NOISE AND INDOOR CLIMATE ON BOARD A TURBOPROP AIRPLANE FLIGHTICAS2022_0115
Müller, P.LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEMICAS2022_0144
Müller, J.POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORSICAS2022_0347
Månsson, P.FLIGHT DYNAMICS SIMULATION AND FCS AUTO-GENERATION IN THE CONCEPTUAL DESIGN PHASE OF AN UNSTABLE SUPERSONIC AIRCRAFTICAS2022_0458
Mårtensson, H.STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALLICAS2022_0351
Mårtensson, H.ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATORICAS2022_0382
Mårtensson, H.MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEMICAS2022_0832
Mönig, R.FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATIONICAS2022_0708
Nadjm-Tehrani, S.CONCEPT LEVEL EXPLORATION OF IMA-BASED NETWORKED PLATFORMS WITH MIXED TIME-SENSITIVE COMMUNICATION REQUIREMENTSICAS2022_0660
Naeser, J.HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENTICAS2022_0434
Nagashima, T.OPTIMIZATION OF AIRCRAFT FLIGHT PATHS CONSIDERING THE CONFLICTING PARAMETERS OF ECONOMY AND SAFETYICAS2022_0652
Nagel, B.VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERINGICAS2022_0063
Nagel, B.EXTENSIBLE AIRCRAFT FUSELAGE MODEL GENERATION FOR A MULTIDISCIPLINARY, MULTI-FIDELITY CONTEXTICAS2022_0254
Nagel, B.AUTOMATED HYBRID PROPULSION MODEL CONSTRUCTION FOR CONCEPTUAL AIRCRAFT DESIGN AND OPTIMIZATIONICAS2022_0593
Nagel, B.THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENTICAS2022_0615
Nagel, B.A VALUE-DRIVEN QUANTITATIVE FRAMEWORK COUPLING AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN BY LEVERAGING THE AGILE 4.0 MBSE-MDO FRAMEWORKICAS2022_0618
Nagel, B.A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONSICAS2022_0700
Nagel, B.RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORKICAS2022_0702
Nagel, B.FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATIONICAS2022_0708
Nagel, B.TOWARDS A SEAMLESS SIMULATION OF THE AIR TRANSPORT SYSTEMICAS2022_0732
Nagel, B.SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045ICAS2022_0804
Nagel, B.DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFTICAS2022_0921
Nagel, N.ICAS DIGITAL PIONEERING INITIATIVE AND SYSTEM OF SYSTEM CHALLENGESICAS2022_0964
Nagele-Renzl, A.USE OF THE FLIGHT TEST FACILITY MOCK-UPS IN THE EUROPEAN CLEAN SKY 2 PROGRAMICAS2022_0116
Naghibi, S.E.APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDSICAS2022_0643
Nairus, J.G.POWER/THERMAL 2030 VISION - AIR PLATFORM ELECTRIFICATIONICAS2022_0960
Nakasuka, S.DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITESICAS2022_0448
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Nambiar, S.MATHEMATICAL MODELLING AND ANALYSIS OF THERMAL MANAGEMENT SYSTEM ARCHITECTURE FOR HYPERSONIC AIRCRAFTICAS2022_0730
Nan Fernandez-Ayala, V.DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGINGICAS2022_0447
Nangia, R.K.ARRIVING AT CERTIFIABLE NOVEL AIRLINER USING LIQUID HYDROGEN & EFFICIENCY METRICSICAS2022_0373
Naruoka, M.STATISTICAL DATA SELECTION FOR BETTER FLIGHT CHARACTERISTIC MODELINGICAS2022_0430
Navarro, P.PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURESICAS2022_0289
Nepomuceno, L.M.IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTINGICAS2022_0873
Névir, M.-C.DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORSICAS2022_0264
Nghiem, Q.-H.DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEMICAS2022_0818
Nguyen, T.D.ANALYSIS OF LOW-SPEED AERODYNAMIC CHARACTERISTICS OF BUSEMANN BIPLANE AIRFOIL INSTALLED HIGH LIFT DEVICESICAS2022_0145
Nguyen, Q.-H.MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINESICAS2022_0813
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Nguyen, T.-G.DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEMICAS2022_0818
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Nguyen, P.-M.DEVELOPMENT OF THE LOW-COST AND LIMITED SPACE SEA-LEVEL RAM AIR TEST (RAT) MACH 0.8 SYSTEMICAS2022_0818
Nguyen, P.A.ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGIONICAS2022_0827
Nicolosi, G.WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICAICAS2022_0280
Nicolosi, F.REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATIONICAS2022_0323
Nicolosi, F.TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASSICAS2022_0641
Nicolosi, F.MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFTICAS2022_0649
Niedermeier, D.THE NEW RESEARCH AIRCRAFT ISTAR - EXPERIMENTAL FLIGHT CONTROL SYSTEMICAS2022_0439
Nieto, A.IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONSICAS2022_0360
Nikbay, M.NATO AVT-297 DEVELOPMENT OF A FRAMEWORK FOR VALIDATION OF COMPUTATIONAL TOOLS FOR ANALYSIS OF AIR VEHICLESICAS2022_0933
Niklaß, M.MINIMIZING THE CLIMATE IMPACT OF THE NEXT GENERATION AIRCRAFT USING NOVEL CLIMATE FUNCTIONS FOR AIRCRAFT DESIGNICAS2022_0602
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Nilsson, T.LARGE EDDY SIMULATION OF RAMJET TO SCRAMJET TRANSITIONICAS2022_0188
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Radtke, J.OPEN CAVITY SIMULATIONS UNDER SIDESLIP FLOW CONDITIONSICAS2022_0173
Rafael, C.F.LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIPICAS2022_0869
Rafik, Y.PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURESICAS2022_0289
Rahman, H.OPTIMAL DESIGN OF STIFFENED PANELS UNDER BUCKLING CONSTRAINTS: A DESIGN METHODOLOGY CONSIDERING CAD-BASED PARAMETERIZATION WITH SIMULTANEOUS LAYOUT AND SIZING OPTIMIZATIONICAS2022_0393
Raj, P.REGIONAL TRANSPORT AIRCRAFT DESIGN USING TURBO-ELECTRIC DISTRIBUTED PROPULSION (TEDIP) SYSTEMICAS2022_0609
Rajaram, D.ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACHICAS2022_0817
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Rameshbabu, R.ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACHICAS2022_0817
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Ramos, P.G.EXPERIMENTAL AND NUMERICAL ANALYSIS OF A PRE-STRESSED TENSEGRITY MEMBRANEICAS2022_0038
Ramos, A.C.B.USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTIONICAS2022_0389
Ramos, B.M.A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENTICAS2022_0523
Ramos, B.M.EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMASICAS2022_0526
Rangel, R.K.HYDRO ENVIRONMENTAL AND ELECTRICAL ASSETS MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USVICAS2022_0017
Ranman, R.EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCTICAS2022_0788
Raposo, C.L.S. COMPUTATIONAL STUDY OF AIRFLOW AND DISPERSION OF AIRBORNE PATHOGENS INSIDE AN AIRCRAFT CABINICAS2022_0911
Rapp, M.NOVEL PATHWAYS TO SUSTAINABLE AVIATIONICAS2022_0688
Ratei, P.DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFTICAS2022_0921
Rath, J.-E.A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLEICAS2022_0791
Rauscher, F.VIRTUAL RECONFIGURATION AND ASSESSMENT OF AIRCRAFT CABINS USING MODEL-BASED SYSTEMS ENGINEERINGICAS2022_0063
Raute, R.SERIES OR PARALLEL HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEMS? CASE STUDIES OF THE ATR42 AND ATR72ICAS2022_0163
Raza, H.HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE STRIKE ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFTICAS2022_0718
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Razafimahazo, E.TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONESICAS2022_0655
Rebollo, M.TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURESICAS2022_0012
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Reichenwallner, C.MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIESICAS2022_0575
Reichenwallner, C.AN EVALUATION METHOD FOR AIRCRAFT ACTUATION SYSTEMS OPERATIONAL COSTICAS2022_0601
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Reinap, A.MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEMICAS2022_0832
Reiser, C.LONG TOUCHDOWN THROUGH A SAFETY-II PERSPECTIVEICAS2022_0185
Reist, T.A.A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATION TO THE STRUT-BRACED-WING AND HYBRID-WING-BODY CONFIGURATIONSICAS2022_0748
Renzoni, P.GARTEUR: NEARLY HALF A CENTURY OF EUROPEAN COLLABORATION IN AERONAUTICSICAS2022_0910
Resende, G.J.STUDY OF EFFECTS ON THE WING'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPANICAS2022_0889
Reysset, A.FAST-OAD-GA: AN OPEN-SOURCE EXTENSION FOR OVERALL AIRCRAFT DESIGN OF GENERAL AVIATION AIRCRAFTICAS2022_0214
Rezgui, D.LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPSICAS2022_0524
Rho, H.-G.ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGIONICAS2022_0827
Riabov, V.APPLICATION OF GENETIC PROGRAMMING AND ARTIFICIAL NEURAL NETWORK APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDSICAS2022_0643
Riaz, A.SET-BASED DESIGN COORDINATION BETWEEN COUPLED SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVEICAS2022_0372
Ribeiro, M.URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH NON-COOPERATIVE AIRSPACE USERSICAS2022_0567
Ribeiro, M.Y.D.DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCYICAS2022_0662
Ricardo Jr, J.A.COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMSICAS2022_0340
Ricci, S.DESIGN OF AN INNOVATIVE WING TIP FOR AEROELASTIC CONTROL: FROM SCRATCH TO FLIGHT TESTICAS2022_0436
Ricci, S.DESIGN AND EXPERIMENTAL TESTING OF A DROOP NOSE MORPHING FOR ADVANCED REGIONAL AIRCRAFTICAS2022_0861
Richter, K.THE GROUP OF RESPONSABLES "AERODYNAMICS (GOR AD)" AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIESICAS2022_0915
Rider, C.VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATAICAS2022_0124
Righi, A.R.S.A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTSICAS2022_0672
Ringertz, U.RAPID PROTOTYPING IN AIRCRAFT DESIGN USING CFD, WIND TUNNEL AND FLIGHT TESTINGICAS2022_0441
Rispoli, A.VALIDATION OF SCALED FLIGHT TESTINGICAS2022_0375
Ritter, J.DLR DESIGN CHALLENGE 2022: DESIGN OF A NEXT GENERATION VTOL FIREFIGHTING AIRCRAFTICAS2022_0921
Rivero, I.TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURESICAS2022_0012
Rizzi, A.AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGESICAS2022_0104
Rizzi, A.IMPROVING STALL CHARACTERISTICS OF UCAV WING WITH VORTEX GENERATORSICAS2022_0238
Rizzi, A.AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 2ICAS2022_0946
Rodrigues, V.A.HYDRO ENVIRONMENTAL AND ELECTRICAL ASSETS MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USVICAS2022_0017
Rodrigues, M.R.B.APPLICATION OF THE VIRTUAL CRACK CLOSURE TECHNIQUE FOR CRACKS IN BUILT-UP PANELSICAS2022_0799
Roh, C.EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAVICAS2022_0488
Romero, J.TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURESICAS2022_0012
Romero-Ramirez, R.EFFECT OF NITRIDING ON MICROSTRUCTURE AND MECHANICAL PROPERTIES ON A TI64 ALLOY FOR AEROSPACE APPLICATIONSICAS2022_0607
Roncioni, P.AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECTICAS2022_0235
Roncioni, P.HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONSICAS2022_0572
Roncioni, P.AERODATABASE DEVELOPMENT AND INTEGRATION OF SUPERSONIC/HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROJECTICAS2022_0596
Rooseleer, F.FLIGHT SIMULATION TO SUPPORT SAFETY CASE FOR PAIR-WISE WAKE TURBULENCE SEPARATION ON DEPARTURESICAS2022_0958
Rosado, T.OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEMICAS2022_0891
Rosado de Paula, T.A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAYICAS2022_0723
Rosell, D.LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTIONICAS2022_0088
Rosell, D.PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINEICAS2022_0782
Rossato, D.B.FLIGHT CONTROLLABILITY ANALYSIS IN TIGHT FORMATION AND CRUISE FLIGHT FOR FUEL SAVINGICAS2022_0273
Rossow, C.-C.FIT FOR CHANGE - DLR STRATEGY TOWARDS ZERO-EMISSION AVIATIONICAS2022_0708
Roth, Y.C.SUSTAINABLE TECHNOLOGIES FOR COMMERCIAL AIRCRAFT OF TOMORROW - INTEGRATED MULTIFUNCTIONAL FUSELAGE DEMONSTRATORICAS2022_0924
Roumeliotis, I.A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFTICAS2022_0703
Roush, K.DESIGNING FOR SECURITY: A CYBERSECURITY INTRODUCTION FOR AEROSPACE EDUCATIONICAS2022_0180
Rudolph, M.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
Ruiz, S.AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTSICAS2022_0693
Ruocco, M.MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFTICAS2022_0649
Russo, P.MECHANICAL CHARACTERIZATION OF A COMPOSITE STRUCTURAL BATTERY LAMINATEICAS2022_0690
Ryu, H.A PREPARATORY RESEARCH FOR UAM COLLISION AVOIDACE USING ADSBICAS2022_0222
Rönnberg, N.EXPECTED TEAMWORK ATTRIBUTES BETWEEN HUMAN OPERATOR AND AUTOMATION IN AIR TRAFFIC CONTROLICAS2022_0504
Saar de Moraes, R.CONCEPT LEVEL EXPLORATION OF IMA-BASED NETWORKED PLATFORMS WITH MIXED TIME-SENSITIVE COMMUNICATION REQUIREMENTSICAS2022_0660
Sabel, D.INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATIONICAS2022_0245
Sabel, D.VISION-BASED LOCALISATION FOR AUTONOMOUS AERIAL NAVIGATION IN GNSS-DENIED SITUATIONSICAS2022_0485
Saccone, G.HIGH PRESSURE HYDROGEN OXYGEN COMBUSTION KINETIC ASSESSMENT FOR AIR-BREATHING PROPULSION SUPERSONIC GREEN AVIATIONICAS2022_0845
Sachs, F.THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALEICAS2022_0328
Sadeghinia, N.INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM ALLOY 780ICAS2022_0206
Saluzzi, V.THE AGILE 4.0 MBSE-MDAO DEVELOPMENT FRAMEWORK: OVERVIEW AND ASSESSMENTICAS2022_0615
Salze, E.AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTSICAS2022_0058
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Sanchez-Moreno, F.TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINESICAS2022_0380
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Sanders, D.A SCALABLE HYDROGEN PROPULSION SYSTEM FOR CIVIL TRANSPORT AIRCRAFTICAS2022_0703
Sant'Ana, V.T.LATERAL-DIRECTIONAL AERODYNAMIC MODELLING FOR NUMERICAL RESULTS USING NEURO-FUZZY WITH DIFFERENTIAL EVOLUTIONICAS2022_0870
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Santos, R.ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNERICAS2022_0887
Sapienza, V.WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICAICAS2022_0280
Sapienza, V.A STUDENT TEAM BASED TEACHING APPROACH: THE TEAM S55 EXPERIENCEICAS2022_0315
Sapienza, S.A STUDENT TEAM BASED TEACHING APPROACH: THE TEAM S55 EXPERIENCEICAS2022_0315
Saracoglu, B.H.HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONSICAS2022_0572
Sarmento, A.G.P.PARAMETER IDENTIFICATION BY UPDATING THE STRUCTURAL MODEL OF A UAV WITH FLEXIBLE WINGICAS2022_0694
Sarmento, A.G.P.A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAYICAS2022_0723
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Sato, M.FLIGHT VERIFICATION OF AUTOMATIC TRANSITION FOR QUAD TILT WING SMALL UAVICAS2022_0740
Sato, A.STUDY ON THE APPLICATION OF EMULSIFIED FUEL IN SMALL JET ENGINESICAS2022_0751
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Schröder, D.VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIRICAS2022_0083
Schröder, B.-O.TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONSICAS2022_0657
Schuetz, C.G.AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTSICAS2022_0693
Schultz, M.DEVELOPING A DEPARTURE QUEUE MODEL FOR INTEGRATED ARRIVAL AND DEPARTURE OPERATION OF RUNWAYSICAS2022_0106
Schultz, M.REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMICICAS2022_0486
Schulz, S.EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERSICAS2022_0656
Schwalb, D.A GENERALISED MULTI-OBJECTIVE ISLAND MODEL FOR FLIGHT CONTROL SYSTEM CLEARANCESICAS2022_0275
Schwalb, D.EXPERIMENTAL INVESTIGATION OF FUEL SLOSH IN A GENERIC FIGHTER WING TANK CONFIGURATIONICAS2022_0467
Schwarz, F.MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURINGICAS2022_0176
Schwarz, C.W.THE SENS4ICE EU PROJECT – SENSORS AND CERTIFIABLE HYBRID ARCHITECTURES FOR SAFER AVIATION IN ICING ENVIRONMENT – PROJECT OVERVIEW AND INITIAL RESULTSICAS2022_0794
Schweighofer, F.REQUIREMENTS-BASED GENERATION OF OPTIMAL VERTICAL TAKEOFF AND LANDING TRAJECTORIES FOR ELECTRIC AIRCRAFTICAS2022_0797
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Schüppstuhl, T.TECHNICAL CONCEPTS FOR INSPECTING UAVS FOR DAMAGEICAS2022_0047
Schüppstuhl, T.A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLEICAS2022_0791
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Scigliano, R.COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATIONICAS2022_0342
Scott, M.J.AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATIONICAS2022_0747
Sedlacek, D.STRAKE SECTION IMPACT ON HYBRID-DELTA-WING AERODYNAMICSICAS2022_0075
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Seidler, R.B.XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEMICAS2022_0228
Seidler, R.CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOMICAS2022_0606
Sekine, K.AIR TRAFFIC SIMULATION ACROSS FIR IN JAPAN USING CELLULAR AUTOMATONICAS2022_0401
Sekler, H.SIGMOIDAL SENSING DEVICES FOR MONITORING TO IMPROVE MAINTENANCE OPERATIONS IN AERONAUTICSICAS2022_0454
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Selier, M.DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFTICAS2022_0566
Sequeira, C.VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATAICAS2022_0124
Serafini, J.SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSISICAS2022_0370
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Sezer, A.-O.NUMERICAL INVESTIGATION OF ROTORCRAFT PRESSURE ERROR CORRECTION BY UTILIZATION OF AIR DAMSICAS2022_0357
Shah, H.INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFTICAS2022_0326
Shahi, H.A PRELIMINARY STRUCTURAL DESIGN OF A FLEXIBLE FLYING DEMONSTRATORICAS2022_0826
Shang, Y.DESIGN OF AERO-ENGINE FADEC POWER SUPPLY CONTROL SYSTEM BASED ON FORWARD DESIGNICAS2022_0023
Shang, S.TWO-PHASE NUMERICAL SIMULATION INVESTIGATION ON THE EFFECTS OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCEICAS2022_0029
Sharma, S.AN INTERNATIONAL RESEARCH PERSPECTIVE ON AIRSPACE INTEGRATION IN THE FRAMEWORK OF URBAN AIR MOBILITYICAS2022_0948
Sharpe, J.VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATAICAS2022_0124
Shaw, S.CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIESICAS2022_0934
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Sheaf, C.OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELSICAS2022_0167
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Sheikh, M.Z.HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONSICAS2022_0894
Shen, Y.EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WINGICAS2022_0078
Shen, J.HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONSICAS2022_0894
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Xu, Y.IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFTICAS2022_0421
Xu, L.AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFTICAS2022_0795
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Yamada, G.COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHODICAS2022_0416
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Zhu, C.CITY-ATM – LIFE DRONE DEMONSTRATIONS OF NEW CONCEPT ELEMENTS ENABLING OPERATIONS IN URBAN AREASICAS2022_0300
Zhu, S.EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURES WITH SINGLE-SIDED REPAIRINGICAS2022_0632
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