COMPLETE AUTHOR LIST HYPERLINKED TO PAPERS



Abarca López, R.MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TESTICAS2020_1049
Abdul Hamid, M.F.CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGNICAS2020_1310
Abramovich, H.THE VIBRATION CORRELATION TECHNIQUE – A RELIABLE NONDESTRUCTIVE TOOL TO PREDICT BUCKLING LOADSICAS2020_0270
Abu Talib, A.R.CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGNICAS2020_1310
Abu-Zurayk, M.COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGNICAS2020_0693
Ackley, J.MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSISICAS2020_1237
Ai, J.L.DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASEICAS2020_1135
Alaimo, A.A STOCHASTIC ROBUSTNESS VERIFICATION OF NLG SIMPLE ADAPTIVE SHIMMY SUPPRESSION SYSTEMICAS2020_0662
Alexandrov, S.V.LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICSICAS2020_0107
Alharasees, O.OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENTICAS2020_0638
Allaio, D.DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATIONICAS2020_1222
Alves, W.M.FLUID-STRUCTURE INTERACTION ANALYSIS OF ELASTIC EFFECTS OF A TRANSPORT AIRCRAFT FITTED WITH WINGLETSICAS2020_0999
Amelyushkin, I.A.EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACEICAS2020_0894
Amiryants, G.A.THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATORICAS2020_0212
An, Y.RESEARCH ON FUNCTIONAL HAZARD ASSESSMENT TECHNOLOGY OF MILITARY AIRCRAFTICAS2020_0795
Andira, M.A.FURTHER DEVELOPMENT OF COMPUTATIONAL STUDY ON COANDA BLANKET CURVATURE EFFECTS ON HALF SPHERICAL COANDA DEVICEICAS2020_0906
Andreeva-Mori, A.IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTIONICAS2020_0202
Annes da Silva, R.G.NASA-CRM LATERAL-DIRECTIONAL STABILITY DERIVATIVES COMPARISON BETWEEN SEMI-EMPIRICAL, VORTEX LATTICE AND PANEL METHODICAS2020_1190
Aprovitola, A.OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLEICAS2020_0164
Aquilini, C.MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TESTICAS2020_1049
Arai, M.IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTPICAS2020_0557
Arizono, H.ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT FOR MORPHING WINGSICAS2020_0540
Aruna, S.T.SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOYICAS2020_1052
Atanasov, G.CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFTICAS2020_0185
Atanasov, G.ASSESSMENT OF THREE COMMUTER AIRCRAFT CONCEPTS FROM A TRANSPORT SYSTEM PERSPECTIVEICAS2020_0207
Atkin, C.AN OBJECTIVE APPROACH FOR MEASURING INTERMITTENCY IN THE TRANSITIONAL BOUNDARY LAYERICAS2020_0149
Atkin, C.J.VIBRATION INDUCED EXCITATION OF INSTABILITY WAVES IN A BLASIUS FLOWICAS2020_0890
Augello, R.ACCURATE BUCKLING AND POST-BUCKLING ANALYSIS OF COMPOSITE STIFFENED PANELSICAS2020_1124
Augousti, A.T.FAILURE PROCESS IDENTIFICATION IN C/SIC SAMPLES WITH A RANGE OF TENSILE PERFORMANCE USING ACOUSTIC EMISSIONICAS2020_0364
Azevedo, J.L.F.STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERSICAS2020_0725
Azevedo, J.L.F.A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONSICAS2020_0734
Bagassi, S.ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELSICAS2020_0508
Bagassi, S.FUTURE PERSPECTIVES ON VR & ARICAS2020_1290
Bai, J.AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATIONICAS2020_0071
Bai, J.TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTORICAS2020_0357
Bai, C.STRUCTURAL VIBRATION CONTROL BY USING THE ENERGY FROM DIFFERENT MODESICAS2020_0383
Bai, Z.PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFTICAS2020_0398
Bai, J.-Q.DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHTICAS2020_0714
Bai, Z.APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROLICAS2020_0978
Bai, J.TWISTOR BASED 6-DOF DISTRIBUTED ADAPTIVE LEADER-FOLLOWING CONTROL FOR MULTIPLE RIGID SPACECRAFT FORMATIONICAS2020_1089
Bai, X.SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICSICAS2020_1134
Bai, J.Q.TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTORICAS2020_1247
Baldon, C.S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANEICAS2020_0455
Baldon, C.TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55XICAS2020_0766
Balunov, K.MATHEMATICAL MODELS FOR ANALYSIS AND OPTIMIZATION OF AIRCRAFT STRUCTURAL COMPONENTS TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTIONICAS2020_0593
Bando, M.MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMSICAS2020_0945
Bao, M.-X.ULTRASONIC DE-ICING SYSTEM DESIGN METHODS BASED ON RESONANCE AND IMPEDANCE MATCHINGICAS2020_1148
Barberis, B.TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55XICAS2020_0766
Barbieri, R.DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATIONICAS2020_1222
Bartasevicius, J.FLIGHT TESTING OF 65KG T-FLEX SUBSCALE DEMONSTRATORICAS2020_0707
Basov, V.MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTSICAS2020_0089
Bastos, T.M.B.TASK ALLOCATION ALGORITHMS FOR A COOPERATIVE DRONE PARCEL DELIVERY SYSTEMICAS2020_1306
Batra, A.ASSESSING THE ENVIRONMENTAL IMPACT OF AIRCRAFT TAXIING TECHNOLOGIESICAS2020_1162
Bautin, A.MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTSICAS2020_0089
Bayandor, J.REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACTICAS2020_1014
Bazhenov, S.THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEMICAS2020_0239
Becker, R.-G.COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGNICAS2020_0693
Bergkvist, M.FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSUREICAS2020_1032
Berlowitz, I.MULTI-MISSION TANKER-TRANSPORT CONVERSIONICAS2020_0010
Berres, A.IMPACT OF NEW TECHNOLOGIES ON AIRCRAFT SYSTEMSICAS2020_0050
Bessonov, P.METHODS FOR CALCULATING THE FATIGUE DAMAGE OF A STRUCTURE FOR VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADSICAS2020_0576
Bezuevsky, A.V.RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIMEICAS2020_0963
Bi, L.SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRIDICAS2020_0315
Bi, S.Q.THE FINITE ELEMENT MODELLING OF BOLTED STRUCTURE BETWEEN SELECTIVE LASER MELTING ALUMINIUM AND COMPOSITE PLATESICAS2020_0880
Bian, J.MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATIONICAS2020_0397
Biedermann, J.FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESSICAS2020_0134
Bihai, H.AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERINGICAS2020_0053
Bijjahalli, S.A NOVEL DETECT-AND-AVOID APPROACH FOR UAS IN URBAN ENVIRONMENTSICAS2020_0970
Bil, C.OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTIONICAS2020_0311
Blinnik, B.S.AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONSICAS2020_1242
Bodmer, D.H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURSICAS2020_0840
Bogatyrev, V.INCREASING THE EFFECTIVENESS OF AN AERODYNAMICALLY BALANCED CONTROL SURFACE ON A MODIFIED AIRFOIL WITH REDUCED DRAGICAS2020_0784
Bogenberger, K.VERTIPORT PLACEMENT METHOD BASED ON MOBILITY SURVEY DATAICAS2020_1133
Boggero, L.THE APPLICATION OF THE AGILE 4.0 MBSE ARCHITECTURAL FRAMEWORK FOR THE MODELING OF SYSTEM STAKEHOLDERS, NEEDS AND REQUIREMENTSICAS2020_0193
Boggero, L.ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINESICAS2020_1259
Bolart, C.VALIDATING SURROGATE MODELS AND ICORPORATING UNCERTAINTY QUANTIFICATION IN MULTI-ELEMENTS AIRFOIL DESIGN OPTIMISATIONICAS2020_0248
Bonnici, M.TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSERICAS2020_0081
Bortolotto, L.AEROELASTIC RESPONSE CALCULATION USING DUHAMEL INTEGRAL AND ITS APPLICATIONSICAS2020_1126
Bosnyakov, I.VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTINGICAS2020_0033
Bosnyakov, S.VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTINGICAS2020_0033
Bottino, N.S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANEICAS2020_0455
Bragado-Aldana, E.ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONSICAS2020_0253
Braun, R.HYBRID MODELLING FOR FULL MISSION SIMULATIONICAS2020_0980
Breard, C.SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCESICAS2020_0743
Breitsamter, C.ANALYSIS OF A WING-TIP-MOUNTED SMALL-SCALE PROPELLER CONFIGURATION UNDER NON-AXIAL INFLOW CONDITIONSICAS2020_0116
Breitsamter, C.EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGSICAS2020_0227
Breitsamter, C.TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON WAKE VORTEX IMPACT BY OSCILLATING FLAPSICAS2020_0595
Bremm, M.DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL AERODYNAMIC LIFT MECHANISMICAS2020_0863
Brusberg, P.LANDING PLATFORM FOR URBAN AIR MOBILITY VEHICLES INTEGRATED INTO PARKING LOT INFRASTRUCTURE IN DENSELY BUILT-UP AREASICAS2020_1217
Budinger, M.DESIGN OPTIMIZATION OF MULTIROTOR DRONES IN FORWARD FLIGHTICAS2020_0781
Budzko, V.I.CREATING A MULTI-FUNCTIONAL EXPERT ANALYTICAL SYSTEM IN THE AIRCRAFT INDUSTRY AND THE FORMATION OF GENERAL REQUIREMENTSICAS2020_0857
Burger, U.MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONSICAS2020_0019
Bussemaker, J.H.SYSTEM ARCHITECTURE DESIGN SPACE MODELING AND OPTIMIZATION ELEMENTSICAS2020_0203
Bykerk, T.LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLEICAS2020_0165
Büscher, A.FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANEICAS2020_1048
Cabaleiro, C.ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINESICAS2020_1259
Cabanac, J.-P.THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONSICAS2020_1235
Cai, H.-Y.STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATORICAS2020_0305
Cai, Z.Y.RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DISICAS2020_0865
Cai, H.Y.STUDY ON THE STATISTICAL CHARACTERISTICS OF SKIN FRICTION OF SHOCK WAVE/ TURBULENT BOUDARY LAYER INTERATION IN A HOLLOW FLARE CONFIGURATION AT MACH 6ICAS2020_1224
Camilleri, R.ASSESSING THE ENVIRONMENTAL IMPACT OF AIRCRAFT TAXIING TECHNOLOGIESICAS2020_1162
Campillo-Borras, E.HARMONIZING SUSTAINABLE AVIATION RESEARCH AMONG IFAR ORGANIZATIONSICAS2020_1302
Campolo, G.APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTSICAS2020_0454
Campos, L.M.B.C.ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATIONICAS2020_0989
Campos, L.M.B.C.ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHSICAS2020_0990
Cantanna, G.S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANEICAS2020_0455
Cao, J.EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLESICAS2020_0093
Cao, J.-A.RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUEICAS2020_0273
Cao, G.Z.NUMERICAL SIMULATION OF RIDGE ICE AND AERODYNAMIC EFFECT UNDER THERMAL ANTI-ICEICAS2020_1179
Carlsson, B.FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSUREICAS2020_1032
Carpenter, K.REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACTICAS2020_1014
Carrera, E.ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADSICAS2020_0479
Carrera, E.ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELSICAS2020_0508
Carrera, E.ACCURATE BUCKLING AND POST-BUCKLING ANALYSIS OF COMPOSITE STIFFENED PANELSICAS2020_1124
Carrone, F.S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANEICAS2020_0455
Carvalho, L.M.M.O.A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONSICAS2020_0734
Castro, S.G.P.ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURESICAS2020_0337
Catalano, F.M.HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORSICAS2020_0988
Cato, A.ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIMEICAS2020_0985
Caurin, G.A.P.USAGE OF MQTT, ROS, AND AWS IN THE MANUFACTURING PROCESS OF AIRCRAFTSICAS2020_1223
Cavalcante, J.ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIMEICAS2020_0985
Celestini, D.TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55XICAS2020_0766
Celli, M.-A.THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONSICAS2020_1235
Cen, F.VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNELICAS2020_0313
Cen, F.WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONSICAS2020_0483
Cen, F.NONLINEAR UNSTEADY AERODYNAMIC MODELING AND LONGITUDINAL STABILITY ANALYSIS FOR AN AIRCRAFT MODELICAS2020_1104
Cerino, G.ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFTICAS2020_1258
Cerny, M.ANALYSIS OF A WING-TIP-MOUNTED SMALL-SCALE PROPELLER CONFIGURATION UNDER NON-AXIAL INFLOW CONDITIONSICAS2020_0116
Cestino, E.APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTSICAS2020_0454
Cestino, E.S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANEICAS2020_0455
Cestino, E.DESIGN OF A VERTICAL DITCHING TESTICAS2020_0763
Chai, Y.-G.RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERINGICAS2020_0633
Chang, C.DESIGN AND VERIFICATION OF ENERGY-ABSORBING STRUCTURE OF CORRUGATED BEAM BASED ON SPECIFIC FAILURE MODEICAS2020_0187
Chang, M.TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTORICAS2020_0357
Chang, M.DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHTICAS2020_0714
Chang, S.SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TESTICAS2020_0744
Chang, L.-F.A METHOD OF MANEUVER IDENTIFICATION AND TRAJECTORY PREDICTION FOR AGILE TARGETICAS2020_0948
Chang, M.TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTORICAS2020_1247
Chartier, N.MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSISICAS2020_1237
Che, Y.X.APPLICATION OF MBSE IN AERO-ENGINE STRUCTURAL PARAMETER CALCULATING SYSTEMICAS2020_0720
Chedrik, A.V.THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATORICAS2020_0212
Chedrik, V.MATHEMATICAL MODELS FOR ANALYSIS AND OPTIMIZATION OF AIRCRAFT STRUCTURAL COMPONENTS TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTIONICAS2020_0593
Chen, C.A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESSICAS2020_0036
Chen, Y.-H.MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSORICAS2020_0138
Chen, D.CONCEPTUAL DESIGN OF A FIXED-WING AQUATIC UAV USING KNOWLEDGE BASED ENGINEERINGICAS2020_0154
Chen, Y.EFFECT OF COMPLEX FLOW PROFILES AT COMBUSTOR EXIT ON TURBINE CHARACTERISTICSICAS2020_0257
Chen, F.FLIGHT MANAGEMENT SYSTEM REQUIREMENT ANALYSIS FOR TRAJECTORY BASED OPERATIONICAS2020_0292
Chen, L.BROADBAND MICROWAVE ABSORBING HONEYCOMB CORE MATERIAL WITH ACTIVE CARBON AS DELEGATESICAS2020_0308
Chen, H.SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRIDICAS2020_0315
Chen, A.MECHANISM DESIGN AND AERODYNAMIC RESEARCH OF RETRACTABLE FOLDING FLAPPING WINGICAS2020_0333
Chen, P.MEMS-BASED DISTRIBUTED NAVIGATION SYSTEMICAS2020_0344
Chen , B.AERODYNAMIC NOISE SIMULATION OF CIVIL AIRCRAFT LANDING GEARS BASED ON LES-SMARGORINSKY MODELICAS2020_0351
Chen, X.APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATIONICAS2020_0352
Chen, X.STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEMICAS2020_0366
Chen, X.ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAMICAS2020_0378
Chen, C.ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAMICAS2020_0378
Chen, Q.ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAMICAS2020_0378
Chen, Y.-N.TURBINE STRUCTURE ANALYSIS AND IMPROVEMENT OF A HIGH-SPEED ROTOR WITH MULTI-DISK AND MULTI-SUPPORTICAS2020_0391
Chen, Y.-N.MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATIONICAS2020_0397
Chen, C.EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIOURS OF RESOLVENT MODEICAS2020_0414
Chen, X.EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIOURS OF RESOLVENT MODEICAS2020_0414
Chen, Y.EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSORICAS2020_0429
Chen, Z.-L.PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITYICAS2020_0495
Chen, Y.-C.PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITYICAS2020_0495
Chen, B.PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITYICAS2020_0495
Chen, Y.DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAINICAS2020_0503
Chen, F.DEFORMATION ANALYSIS OF C-SPAR COMPOSITE STRUCTURE DURING THE PREFORMING PROCESSINGICAS2020_0599
Chen, P.DEFORMATION ANALYSIS OF C-SPAR COMPOSITE STRUCTURE DURING THE PREFORMING PROCESSINGICAS2020_0599
Chen, J.W.A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFTICAS2020_0650
Chen, X.M.DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISKICAS2020_0713
Chen, C.CO-SIMULATION OF SYSML AND SIMULINK/MODELICA USING FMIICAS2020_0803
Chen, C.PRECISION ANALYSIS AND INDEX DISTRIBUTION SYSTEM DESIGN OF AVIONICS SYSTEM BASED ON BP NEURAL NETWORKICAS2020_0808
Chen, H.INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINEICAS2020_0845
Chen, B.AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESSICAS2020_0899
Chen, Q.RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTIONICAS2020_0909
Chen, X.L.RESEARCH OF THE HYPERSONIC BOUNDARY LAYER INSTABILITIES AND TRANSITION WITH THERMAL-CHEMICAL NON-EQUILIBRIUM EFFECTSICAS2020_0944
Chen, X.MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGNICAS2020_0965
Chen, Z.-J.AN INTEGRATED METHOD FOR ACCURATE IDENTIFICATION AND DYNAMIC MONITORING OF BUILDINGS IN AERODROME OBSTACLE FREE SPACEICAS2020_1061
Chen, Y.X.ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTIONICAS2020_1074
Chen, Y.C.BENEFIT ANALYSIS OF AIR REFUELING IN ULTRA LONG ROUTE AIRLINER OPERATIONICAS2020_1101
Chen, X.CLOUD-BASED ENVIRONMENT FOR AIRCRAFT DESIGN COLLABORATIONICAS2020_1123
Chen, Z.Y.FAST ITERATIVE SIMULATION OF AIRLINER WING PLANFORM CONCEPTUAL DESIGNICAS2020_1155
Chen , Z.T.ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGSICAS2020_1171
Chen, Y.Z.NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATIONICAS2020_1250
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Gao, Y.W.APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITIONICAS2020_0264
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Gu, J.THE RESEARCH ON PROPELLER NOISE PREDICTION METHOD FOR TURBOPROP AIRCRAFTICAS2020_0544
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He, R.FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSUREICAS2020_1032
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Hua, J.AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATIONICAS2020_0071
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Iodice, P.ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFTICAS2020_1258
Irgaleev, I.K.THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERSICAS2020_0176
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Isyanov, A.THE CAPABILITIES OF AUTOMATION OF MDAO PROBLEM STATEMENT AT COLLABORATIVE CONCEPTUAL DESIGN OF THE PROPULSION SYSTEM USING OPEN SOURCE SOFTWARE TOOLSICAS2020_1022
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Jia, Z.BROADBAND MICROWAVE ABSORBING HONEYCOMB CORE MATERIAL WITH ACTIVE CARBON AS DELEGATESICAS2020_0308
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Jiang, M.CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFTICAS2020_0231
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Jiang, B.NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAPICAS2020_1149
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Jin, H.-L.APPLICATION OF A SKEWED-SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSORICAS2020_0543
Jin, H.-L.DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSORICAS2020_0632
Jin, H.-L.MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGNICAS2020_0965
Jin, D.STUDY ON THE METHOD OF DETERMINING SKIN WAVINESS REQUIREMENT OF CIVIL AIRCRAFTICAS2020_1065
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Li, C.STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATORICAS2020_0305
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Li, G.EXPERIMENTAL STUDY ON CRITICAL HEAT FLUX CHARACTERISTICS OF R134A FLOW BOILING IN A HORIZONTAL 2.1 MM TUBE UNDER HYPERGRAVITYICAS2020_0510
Li, Z.AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERSICAS2020_0541
Li, Z.-P.DISTORTION PLATE DESIGN, SIMULATION VALIDATION AND TEST SCHEME FOR STABILITY ANALYSIS ON A FAN COMPONENT OF AN AEROENGINEICAS2020_0636
Li, X.F.A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFTICAS2020_0650
Li, B.STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESHICAS2020_0686
Li, W.B.EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADEICAS2020_0704
Li, K.C.EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADEICAS2020_0704
Li, M.DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHTICAS2020_0714
Li, X.IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEMICAS2020_0723
Li, L.AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVESICAS2020_0794
Li, Q.RESEARCH ON FUNCTIONAL HAZARD ASSESSMENT TECHNOLOGY OF MILITARY AIRCRAFTICAS2020_0795
Li, B.F.CO-SIMULATION OF SYSML AND SIMULINK/MODELICA USING FMIICAS2020_0803
Li, Q.MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATIONICAS2020_0805
Li, K.T.DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMINGICAS2020_0822
Li, D.DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERSICAS2020_0839
Li, H.-J.DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERSICAS2020_0839
Li, X.X.INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINEICAS2020_0845
Li, G.Y.AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESSICAS2020_0899
Li, Z.H.RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTIONICAS2020_0909
Li, X.H.SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODELICAS2020_0928
Li, M.INVESTIGATION OF AERODYNAMIC INTERACTIONS BETWEEN NACA0012 AIRFOILS IN TANDEMICAS2020_1063
Li, F.TWISTOR BASED 6-DOF DISTRIBUTED ADAPTIVE LEADER-FOLLOWING CONTROL FOR MULTIPLE RIGID SPACECRAFT FORMATIONICAS2020_1089
Li, C.AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLESICAS2020_1109
Li, X.C.A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINEICAS2020_1114
Li, H.-Y.AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESSICAS2020_1118
Li, F.EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0ICAS2020_1122
Li, D.AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGINGICAS2020_1132
Li, H.LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINTICAS2020_1145
Li, Y.LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINTICAS2020_1145
Li, R.NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAPICAS2020_1149
Li, Y.B.NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTSICAS2020_1183
Li, Y.B.NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WINGICAS2020_1240
Liang, S.Q.ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSISICAS2020_0269
Liang, C.MODELING AND SIMULATION APPLICATION THROUGHOUT THE AERO-ENGINE LIFE CYCLEICAS2020_0290
Liang, Y.-Q.RESEARCH OF LABYRINTH SEALS MEASUREMENT-BASED PROBABILITISTIC ANALYSIS METHOD FOR TURBOFAN INTERNAL AIR SYSTEMICAS2020_0531
Liang, Y.AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVESICAS2020_0794
Liang, C.-H.EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0ICAS2020_1122
Liao, F.AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDINGICAS2020_0348
Liao, Y.STUDY ON THE FATIGUE SCATTER FACTOR UNDER SEVERE LOAD SPECTRUMICAS2020_0904
Liebhardt, B.FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFTICAS2020_0238
Liebhardt, B.H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURSICAS2020_0840
Limonin, M.V.SPECIALIZED SOFTWARE DEVELOPMENT FOR BUILDING BLOCK APPROACH INTEGRATION IN FULL-SCALE STATIC TESTSICAS2020_1117
Lin, Y.-F.AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESSICAS2020_1118
Lin, Y.-F.HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILSICAS2020_1125
Lin, Y.-F.FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATIONICAS2020_1127
Lin, D.MULTI-UAV TRAJECTORY PLANNING BASED ON COORDINATION VARIABLESICAS2020_1139
Ling, S.-B.EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR THE “AEROSTRUCT” WING OPTIMIZATION PLATFORMICAS2020_0350
Linke, F.H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURSICAS2020_0840
Lipanov, A.M.PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSETICAS2020_0949
Lipatov, I.I.PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSETICAS2020_0949
Lippoldt, K.VERTIPORT PLACEMENT METHOD BASED ON MOBILITY SURVEY DATAICAS2020_1133
Liu, N.AN IMPROVED IDENTIFICATION METHOD FOR ACTUATOR LOOP OF AIRCRAFT ENGINE CONTROL SYSTEMICAS2020_0027
Liu, Q.EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTSICAS2020_0040
Liu, Z.EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTSICAS2020_0040
Liu, R.P.THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLEICAS2020_0052
Liu, D.NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING WITH SLOTTED-TIPICAS2020_0102
Liu, L.AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLESICAS2020_0168
Liu, Y.DESIGN AND RESEARCH ON SAFETY ANALYSIS TOOL FOR AVIONICS SYSTEMICAS2020_0186
Liu, Y.J.ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSISICAS2020_0269
Liu, G.A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATESICAS2020_0272
Liu, Y.C.A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDINGICAS2020_0282
Liu, X.EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSORICAS2020_0291
Liu, P.-X.STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATORICAS2020_0305
Liu, Z.VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNELICAS2020_0313
Liu, C.INCORPORTING KNOWLEDGE COVERAGE MEASUREMENT INTO KNOWLEDGE TRANSFORMATION FROM DATA FOR KNOWLEDGE ACCUMULATIONICAS2020_0343
Liu, Z.MEMS-BASED DISTRIBUTED NAVIGATION SYSTEMICAS2020_0344
Liu, Y.DECOUPLING CONTROL LAW DESIGN FOR OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWINGICAS2020_0384
Liu, Y.PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTSICAS2020_0392
Liu, J.DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINEICAS2020_0401
Liu, H.STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATIONICAS2020_0416
Liu, D.-N.PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNELICAS2020_0418
Liu, H.-Y.PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGNICAS2020_0463
Liu, F.AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHINGICAS2020_0476
Liu, Z.WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONSICAS2020_0483
Liu, Z.A STUDY OF SONIC BOOM TEST WITH NOZZLE PLUME INTERACTIONSICAS2020_0500
Liu, Y.MODELING AND DYNAMICS STABILITY ANALYSIS FOR A BLENDED-WING-BODY AIRCRAFTICAS2020_0525
Liu, X.MODELING AND DYNAMICS STABILITY ANALYSIS FOR A BLENDED-WING-BODY AIRCRAFTICAS2020_0525
Liu, L.ASSEMBLY QUALITY OPTIMIZATION APPROACH FOR LARGE-SCALE ACTIVE COMPONENTS BASED ON REVERSE ENGINEERINGICAS2020_0542
Liu, F.BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURESICAS2020_0574
Liu, J.-Y.EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODELICAS2020_0619
Liu, T.RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BEDICAS2020_0661
Liu, J.AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLEICAS2020_0663
Liu, Y.APPLICATION OF REINFORCEMENT LEARNING IN 1-D AERODYNAMIC DESIGN OF AXIAL COMPRESSORICAS2020_0678
Liu, H.J.BIONIC LIGHT-WEIGHT GRID SURFACE WING STRUCTURE DESIGN FOR A SOLAR-POWERED UAVICAS2020_0731
Liu, P.ANALYSIS OF THRUST-SCALED ACOUSTIC EMISSIONS OF AIRCRAFT PROPELLERS AND THEIR DEPENDENCE ON PROPULSIVE EFFICIENCYICAS2020_0751
Liu, Q.Y.AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESSICAS2020_0774
Liu, S.-S.NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODELICAS2020_0796
Liu, L.MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATIONICAS2020_0805
Liu, Q.C.PRECISION ANALYSIS AND INDEX DISTRIBUTION SYSTEM DESIGN OF AVIONICS SYSTEM BASED ON BP NEURAL NETWORKICAS2020_0808
Liu, P.Q.MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORKICAS2020_0849
Liu, H.-L.RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLESICAS2020_0851
Liu, Y.M.RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DISICAS2020_0865
Liu, Z.-Q.MULTIFIDELITY AERODYNAMIC/STEALTH DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFTICAS2020_0878
Liu, L.Y.THE FINITE ELEMENT MODELLING OF BOLTED STRUCTURE BETWEEN SELECTIVE LASER MELTING ALUMINIUM AND COMPOSITE PLATESICAS2020_0880
Liu, F.AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESSICAS2020_0899
Liu, D.L.AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTSICAS2020_0939
Liu, Z.-W.A METHOD OF MANEUVER IDENTIFICATION AND TRAJECTORY PREDICTION FOR AGILE TARGETICAS2020_0948
Liu, Y.Z.TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLEICAS2020_1110
Liu, F.A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINEICAS2020_1114
Liu, Y.EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0ICAS2020_1122
Liu, X.NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAPICAS2020_1149
Liu, S.S.A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTIONICAS2020_1160
Liu, Z.K.A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTIONICAS2020_1160
Liu, X.A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTIONICAS2020_1160
Liu, X.P.TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGYICAS2020_1170
Liu, L.COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTIONICAS2020_1176
Liu, P.Q.NUMERICAL STUDY OF DITCHING CHARACTERISTICS OF BWB AIRCRAFTICAS2020_1178
Liu, J.-Y.A REDUNDANT ADAPTIVE NAVIGATION METHOD BASED ON DYNAMIC PERFORMANCE EVALUATION FOR AEROSPACE VEHICLEICAS2020_1180
Liu, X.CONCEPT OF A NEW SYSTEM SYNTHESIZING METEOROLOGICAL AND OROGRAPHIC INFLUENCES ON THE AIRPLANE SAFE ENERGY ENVELOPEICAS2020_1193
Liu, L.RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGEICAS2020_1203
Liu, C.RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGEICAS2020_1203
Liu, P.X.STUDY ON THE STATISTICAL CHARACTERISTICS OF SKIN FRICTION OF SHOCK WAVE/ TURBULENT BOUDARY LAYER INTERATION IN A HOLLOW FLARE CONFIGURATION AT MACH 6ICAS2020_1224
Liu, L.B.RESEARCH ON AIRCRAFT-LEVEL PHYSICAL INTEGRATION VERIFICATION TEST TECHNOLOGYICAS2020_1232
Liu, Y.X.INVESTIGATION OF VARIABLE GEOMETRIES ON THE OPERABILITY AND AIRCRAFT LEVEL PERFORMANCE OF A THREE-SHAFT TURBOFAN ENGINE FOR ENTRY INTO SERVICE 2050ICAS2020_1249
Liu, Y.X.NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATIONICAS2020_1250
Liu, P.ESTIMATION OF STATIC AND DYNAMIC FLOATATION CHARACTERISTICS DURING AIRCRAFT DITCHINGICAS2020_1255
Liu, A.A DEEP LEARNING AND ONTOLOGY BASED FRAMEWORK FOR TEXTUAL REQUIREMENTS ANALYSIS AND CONCEPTUAL MODEL GENERATIONICAS2020_1293
Loiodice, L.TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55XICAS2020_0766
Lone, M.M.ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONSICAS2020_0253
Lone, M.RAPID THEORETICAL EVALUATION OF FORMATION FLIGHT PERFORMANCEICAS2020_0648
Lowenberg, M.H. NONLINEAR UNSTEADY AERODYNAMIC MODELING AND LONGITUDINAL STABILITY ANALYSIS FOR AN AIRCRAFT MODELICAS2020_1104
Lu, J.A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFTICAS2020_0097
Lu, Y.-H.MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATIONICAS2020_0397
Lu, M.H.STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTIONICAS2020_0598
Lu, S.DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISKICAS2020_0713
Lubrina, P.MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TESTICAS2020_1049
Luderer, O.VALIDATION OF AN AERODYNAMIC MODEL FOR THE ANALYSIS OF SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRICAL PROPULSIONICAS2020_0145
Luna, L.S.USAGE OF MQTT, ROS, AND AWS IN THE MANUFACTURING PROCESS OF AIRCRAFTSICAS2020_1223
Luo, Z.EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTSICAS2020_0040
Luo, Y.COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWSICAS2020_0114
Luo, S.CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELLICAS2020_0285
Luo, X.PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGNICAS2020_0463
Luo, K.AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSORICAS2020_0538
Luo, B.A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOSICAS2020_1309
Lv, S.A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATESICAS2020_0272
Lv, S.EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOYICAS2020_0400
Lv, P.NUMERICAL SIMULATION OF LOCAL LONG SHALLOW CAVITY EFFECT ON THE STABILITY OF A HYPERSONIC BOUNDARY LAYERICAS2020_1189
Lühder, W.MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENTICAS2020_0523
Lyrio, J.A.A.STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERSICAS2020_0725
Ma, K.ESTIMATION OF THREE-DIMENSIONAL BOUNDARY LAYER VELOCITY PROFILES ON SWEPT WINGS AND BLENDED WING BODIESICAS2020_0078
Ma, K.THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHTICAS2020_0181
Ma, Y.PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFTICAS2020_0398
Ma, Y.PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFTICAS2020_0398
Ma, C.RESEARCH ON SELECTION METHODS FOR AIRCRAFT LANDING GEAR SYSTEM HEALTH FEATURE PARAMETERSICAS2020_0581
Ma, H.L.EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADEICAS2020_0704
Ma, X.-P.AERODYNAMIC AND STRUCTURAL DESIGN OF THE COMPOSITE PROPELLER FOR NEAR SPACE VEHICLESICAS2020_0722
Ma, H.S.DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMINGICAS2020_0822
Ma, C.BENEFIT ANALYSIS OF AIR REFUELING IN ULTRA LONG ROUTE AIRLINER OPERATIONICAS2020_1101
Ma, G.-W.EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0ICAS2020_1122
Ma, J.Y.DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASEICAS2020_1135
Ma, C.THE STUDY ON ANTI-ICING AREAS OF LEADING-EDGE SLATS IN MODERN CIVIL AIRCRAFTICAS2020_1154
Ma, C.FAST ITERATIVE SIMULATION OF AIRLINER WING PLANFORM CONCEPTUAL DESIGNICAS2020_1155
Magerramova, L.DEVELOPMENT OF ADVANCED DESIGNS OF GAS TURBINE ENGINES FROM POWDER COMPOSITIONSICAS2020_0924
Maina, M.HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTUREICAS2020_0236
Malik, Z.INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSISICAS2020_1213
Malyutin, V.A.THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATORICAS2020_0212
Mamaev, V.ADVANCED WEAK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATINGICAS2020_0037
Manfriani, L.CONCEPT OF A NEW SYSTEM SYNTHESIZING METEOROLOGICAL AND OROGRAPHIC INFLUENCES ON THE AIRPLANE SAFE ENERGY ENVELOPEICAS2020_1193
Mao, J.ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META-MODELICAS2020_0200
Mao, J.GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHODICAS2020_0489
Maqsood, A.NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBERICAS2020_0555
Maqsood, A.NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICESICAS2020_0556
Mare, J.-C.VIRTUAL PROTOTYPING OF ELECTRICAL THSA FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONSICAS2020_0196
Marin, G.ATTENTION: TARGET AND ACTUAL - THE CONTROLLER FOCUSICAS2020_0012
Marini, M.THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLEICAS2020_0493
Marini, M.H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURSICAS2020_0840
Marini, M.INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISERICAS2020_1195
Maritano, G.APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTSICAS2020_0454
Markov, S.EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTSICAS2020_0750
Marques, J.M.G.ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATIONICAS2020_0989
Marques, J.M.G.ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHSICAS2020_0990
Martensson, H.AERODYNAMIC ANALYSIS OF A HIGH SPEED TEST RIG FOR USE IN ENGINE TEST FACILITIESICAS2020_0016
Martin, M.NUMERICAL SIMULATIONS OF TRANSONIC BUFFET ON A HALF WING-BODY CONFIGURATIONICAS2020_0612
Martinez, J.H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURSICAS2020_0840
Masse, G.THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONSICAS2020_1235
Masuda, K.LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAVICAS2020_0150
Matsumura, Y.MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMSICAS2020_0945
Matsuno, Y.IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTIONICAS2020_0202
Mattos, B.S.FLUID-STRUCTURE INTERACTION ANALYSIS OF ELASTIC EFFECTS OF A TRANSPORT AIRCRAFT FITTED WITH WINGLETSICAS2020_0999
Mattos, B.S.AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER'S PROGRAM COSTICAS2020_1005
Mavris, D.N.AN EXERCISE IN DEVELOPING A SUPERVISED ANOMALY DETECTION MODEL WITH AUTOMATICALLY ENGINEERED FEATURESICAS2020_0467
Mavris, D.N.TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNINGICAS2020_0649
Mavris, D.N.MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSISICAS2020_1237
Mavris, D.QUANTIFICATION OF OPERATIONAL EFFECTIVENESS FOR TECHNOLOGY EVALUATIONICAS2020_1241
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Qiu, D.-B.DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSORICAS2020_0632
Qiu, H.-C.IMPROVED STOCHASTIC PERTURBATION ALGORITHM FOR GENERALIZED REPEATED EIGENVALUES PROBLEM BASED ON SURROGATE MODELICAS2020_0780
Qiu, D.-B.MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGNICAS2020_0965
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Qui, F.A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONSICAS2020_0712
Qui, X.BASED ON SYSTEMS ENGINEERING PROCESS THE CIVIL AIRCRAFT PROJECT PRODUCT BREAKDOWN STRUCTURE DEVELOPMENT RESEARCHICAS2020_1018
Qui, X.D.THE CIVIL AIRCRAFT DEVELOPMENT PROJECT RISK MANAGEMENT RESEARCHICAS2020_1244
Rachdi, A.INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSISICAS2020_1213
Raczko, K.PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVERICAS2020_0747
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Rajaram, D.AN EXERCISE IN DEVELOPING A SUPERVISED ANOMALY DETECTION MODEL WITH AUTOMATICALLY ENGINEERED FEATURESICAS2020_0467
Rakhmankulov, D.Y.CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERSICAS2020_0974
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Rataj, J.ATTENTION: TARGET AND ACTUAL - THE CONTROLLER FOCUSICAS2020_0012
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Reichenwallner, C.EVALUATION ASPECT MAPPING FOR ACTUATION SYSTEM DESIGNICAS2020_1210
Ren, J.X.THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLEICAS2020_0052
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Riaz, R.NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBERICAS2020_0555
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Riaz, A.CLOUD-BASED ENVIRONMENT FOR AIRCRAFT DESIGN COLLABORATIONICAS2020_1123
Ricci, S.AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGEICAS2020_0631
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Rodera Garcia, O.REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACTICAS2020_1014
Rodriguez Diaz, M.A.GAZE-BASED INTERFACE FOR FLIGHT CONTROL: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEMICAS2020_0645
Rodriguez Diaz, M.A.FITT’S LAW WITH EYE TRACKING ON A FLIGHT SIMULATOR COCKPITICAS2020_0982
Rodriguez-Sanz, A.A NOVEL APPROACH FOR TURNAROUND TIME ALLOCATION BASED ON REINFORCEMENT LEARNINGICAS2020_1015
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Rogalski, T.AIRCRAFT FLIGHT CONTROL SYSTEM FOR AEROBATIC FLIGHTICAS2020_0073
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Sapienza, V.S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANEICAS2020_0455
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Shi, X.VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WINGICAS2020_0284
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Shi, Y.A.A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTSICAS2020_0833
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Shi, H.Y.RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DISICAS2020_0865
Shi, J.RESEARCH ON FAULT DIAGNOSIS AND FAILURE RECONFIGURATION OF FLUSH AIR DATA SENSINGICAS2020_1064
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Sinnige, T.ANALYSIS OF THRUST-SCALED ACOUSTIC EMISSIONS OF AIRCRAFT PROPELLERS AND THEIR DEPENDENCE ON PROPULSIVE EFFICIENCYICAS2020_0751
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Skryabin, A.THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEMICAS2020_0239
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Song, B.-F.RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLESICAS2020_0162
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Song, W.B.A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WINGICAS2020_0256
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Song, W.-P.FAST METHOD AND AN INTEGRATED CODE FOR SONIC BOOM PREDICTION OF SUPERSONIC COMMERCIAL AIRCRAFTICAS2020_0600
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Song, Z.Y.TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGYICAS2020_1170
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Stalewski, W.IMPROVEMENT OF HELICOPTER PERFORMANCE THROUGH PULSE AIR JETS BLOWN FROM THE TRAILING EDGE OF MAIN ROTOR BLADESICAS2020_0301
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Wang, B.THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDE-BODY CIVIL TRANSPORTICAS2020_0676
Wang, H.A SUBJECTIVE EVALUATION METHOD OF AIRCRAFT VIBRATION IN FLIGHT TESTICAS2020_0684
Wang, Y.Y.EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADEICAS2020_0704
Wang, H.F.RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFTICAS2020_0706
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Wang, F.THE STUDY OF UNMANNED AERIAL VEHICLE FLYING QUALITIES FLIGHT TEST METHOD BASED ON TIME-DELAY EVALUATIONICAS2020_0710
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Wang, W.H.SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCESICAS2020_0743
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Wang, D.DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMINGICAS2020_0822
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Wang, Y.J.STUDY ON THE FATIGUE SCATTER FACTOR UNDER SEVERE LOAD SPECTRUMICAS2020_0904
Wang, W.K.RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTIONICAS2020_0909
Wang, H.W.SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODELICAS2020_0928
Wang, R.APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROLICAS2020_0978
Wang, H.ON THE DEVELOPMENT OF FUSELAGE WEIGHT ESTIMATION TOOL INTO AIRCRAFT MULTIDISCIPLINARY DESIGN ENVIRONMENTICAS2020_1068
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Wang, H.NUMERICAL ANALYSIS METHOD OF CIVIL AIRCRAFT DITCHING FLOATING PERFORMANCEICAS2020_1069
Wang, H.NUMERICAL ANALYSIS METHOD OF CIVIL AIRCRAFT DITCHING FLOATING PERFORMANCEICAS2020_1069
Wang, D.STUDY ON THE OUT-OF-PLANE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT 350°CICAS2020_1072
Wang, W.S.ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTIONICAS2020_1074
Wang, L.MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOWICAS2020_1078
Wang, Y.A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODYICAS2020_1099
Wang, Z.G.A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODYICAS2020_1099
Wang, Y.-H.NUMERICAL STUDY OF HIGH TEMPERATURE TRANSVERSE PULSE JET IN THE SUPERSONIC COMBUSTION CHAMBERICAS2020_1100
Wang, X.AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLESICAS2020_1109
Wang, X.Z.TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLEICAS2020_1110
Wang, T.-Y.EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0ICAS2020_1122
Wang, C.EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0ICAS2020_1122
Wang, J.X.EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACEICAS2020_1138
Wang, X.P.AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLEICAS2020_1144
Wang, Z.-W.INFLUENCE OF SHOCK TRAIN ON HEAT FLUX DISTRIBUTION OF A CIRCULAR CONSTANT-AREA ISOLATORICAS2020_1146
Wang, Y.H.THE STUDY ON ANTI-ICING AREAS OF LEADING-EDGE SLATS IN MODERN CIVIL AIRCRAFTICAS2020_1154
Wang, R.A REDUNDANT ADAPTIVE NAVIGATION METHOD BASED ON DYNAMIC PERFORMANCE EVALUATION FOR AEROSPACE VEHICLEICAS2020_1180
Wang, L.F.RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGEICAS2020_1203
Wang, Y.A POLE CONFIGURATION CONTROLLER FOR FIXED HEIGHT CONTROL OF TILT ROTOR AIRCRAFTICAS2020_1228
Wang, M.NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATIONICAS2020_1250
Wang, Z.-Y.ASCENT TRAJECTORY OPTIMIZATION OF HYPERSONIC VEHICLE USING SWARM INTELLIGENT METHODICAS2020_1266
Wang, Y.-L.ASCENT TRAJECTORY OPTIMIZATION OF HYPERSONIC VEHICLE USING SWARM INTELLIGENT METHODICAS2020_1266
Wang, Y.H.A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOSICAS2020_1309
Wangai, A.W.TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRID-ELECTRIC AIRCRAFTICAS2020_0635
Wassink, P.CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFTICAS2020_0185
Wassink, P.ASSESSMENT OF THREE COMMUTER AIRCRAFT CONCEPTS FROM A TRANSPORT SYSTEM PERSPECTIVEICAS2020_0207
Watanabe, M.ENDURANCE ANALYSIS OF BATTERY-POWERED MULTICOPTERS: DERIVATION OF PROPER CUT-OFF VOLTAGE USING DC MOTOR MODELICAS2020_0769
Watanabe, A.ENDURANCE ANALYSIS OF BATTERY-POWERED MULTICOPTERS: DERIVATION OF PROPER CUT-OFF VOLTAGE USING DC MOTOR MODELICAS2020_0769
Webster, K.INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSISICAS2020_1213
Wegener, P.INTEGRATION OF FUSELAGE-MOUNTED OVER-WING ENGINES ON A MID-RANGE AIRCRAFTICAS2020_1194
Wei, D.AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLESICAS2020_0168
Wei, B.B.APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITIONICAS2020_0264
Wei, X.MEMS-BASED DISTRIBUTED NAVIGATION SYSTEMICAS2020_0344
Wei, B.-B.ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOILICAS2020_0516
Wei, H.F.BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURESICAS2020_0574
Wei, Z.B.IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEMICAS2020_0723
Wei, D.MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATIONICAS2020_0805
Wei, D.A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTSICAS2020_0833
Wei, H.F.A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINEICAS2020_1114
Weigel, P.TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFTICAS2020_1260
Weiss, F.AERODYNAMIC AND STRUCTURAL MODELING IN THE ROTORCRAFT MULTI-PHYSICS SIMULATION VASTICAS2020_0584
Wen, Q.AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSORICAS2020_0538
Wen, P.C.AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISIONICAS2020_0591
Wen, J.R.DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASEICAS2020_1135
Willert, C.MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENTICAS2020_0523
Witt, T.LANDING PLATFORM FOR URBAN AIR MOBILITY VEHICLES INTEGRATED INTO PARKING LOT INFRASTRUCTURE IN DENSELY BUILT-UP AREASICAS2020_1217
Woehler, S.FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFTICAS2020_0238
Wojtas, M.PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVERICAS2020_0747
Wolkov, A.VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTINGICAS2020_0033
Wong, P.W.C.HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTUREICAS2020_0236
Wu, C.H.COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWSICAS2020_0114
Wu, H.MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSORICAS2020_0138
Wu, H.EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIVICAS2020_0140
Wu, J.-T.TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINTICAS2020_0271
Wu, X.-H.RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUEICAS2020_0273
Wu, M.RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHMICAS2020_0413
Wu, L.RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHMICAS2020_0413
Wu, J.T.RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORYICAS2020_0514
Wu, T.AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERSICAS2020_0541
Wu, J.M.BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURESICAS2020_0574
Wu, J.-F.DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSORICAS2020_0632
Wu, F.RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BEDICAS2020_0661
Wu, W.H.DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISKICAS2020_0713
Wu, X.-J.NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODELICAS2020_0796
Wu, B.BASED ON SYSTEMS ENGINEERING PROCESS THE CIVIL AIRCRAFT PROJECT PRODUCT BREAKDOWN STRUCTURE DEVELOPMENT RESEARCHICAS2020_1018
Wu, J.M.FLOW AND HEAT TRANSFER MECHANISM OF JET IMPINGEMENT COOLING ONTO MID-CHORD REGINE OF TWISTED BLADEICAS2020_1106
Wu, J.M.A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINEICAS2020_1114
Wu, J.-M.NUMERICAL STUDY ON COOLING CHARACTERISTICS IN CHANNELS WITH PIN FIN ARRAYS UNDER HIGH TEMPERATURE/PRESSURE CONDITIONSICAS2020_1151
Wu, W.H.INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBERICAS2020_1185
Wu, B.THE CIVIL AIRCRAFT DEVELOPMENT PROJECT RISK MANAGEMENT RESEARCHICAS2020_1244
Wu, F.DEPLOY SYSTEM ENGINEERING METHODS IN AIRBORNE GUIDANCE NAVIGATION CONTROL DOMAINICAS2020_1296
Wunderlich, T.COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGNICAS2020_0693
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Xia, Z.H.EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACKICAS2020_0182
Xia, D.W.SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TESTICAS2020_0744
Xia, P.AN OVERVIEW OF HELICOPTER DEVELOPMENT IN CHINA AND SOME NEW HELICOPTER TECHNOLOGIESICAS2020_1282
Xiao, G.M.AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLESICAS2020_0168
Xiao, W.HYBRID IGNITION PROBABILITY METHOD TO PREDICT THE IGNITION PERFORMANCE OF A GAS TURBINE COMBUSTORICAS2020_0259
Xiao, G.M.MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATIONICAS2020_0805
Xiao, G.M.A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTSICAS2020_0833
Xiao, G.-M.COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTIONICAS2020_1176
Xiao, Z.-Y.METHODS OF DIRECTIONAL COARSENING FOR UNSTRUCTURED GRIDS AND APPLICATIONSICAS2020_1261
Xie, H.PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTSICAS2020_0392
Xie, H.RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DISICAS2020_0865
Xie, Y.ARTIFICIAL INTELLIGENCE AND HUMAN-MACHINE INTERACTIONS FOR STREAM-BASED AIR TRAFFIC FLOW MANAGEMENTICAS2020_1009
Xie, R.X.A LOCAL CORRELATION-BASED ALGEBRAIC TRANSITION MODEL WITH COMPRESSIBILITY AND CROSSFLOW CORRECTIONICAS2020_1098
Xing, C.RESEARCH ON ARCHITECTURE FRAMEWORK MODEL BASED EVALUATION INDEX FOR AVIATION SCIENCE & TECHNOLOGY MANAGEMENTICAS2020_0077
Xing, C.G.A CONTRASTIVE STUDY OF STANDARD SPECIFICATION FOR TECHNOLOGY READINESS ASSESSMENTICAS2020_0252
Xing, P.P.MODEL-BASED VIRTUAL INTEGRATED TEST METHOD FOR AVIONICS SYSTEMICAS2020_1212
Xiong, Z.EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODELICAS2020_0619
Xiong, B.A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODYICAS2020_1099
Xiong, Z.A REDUNDANT ADAPTIVE NAVIGATION METHOD BASED ON DYNAMIC PERFORMANCE EVALUATION FOR AEROSPACE VEHICLEICAS2020_1180
Xu, J.F.A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESSICAS2020_0036
Xu, J.RESEARCH ON ARCHITECTURE FRAMEWORK MODEL BASED EVALUATION INDEX FOR AVIATION SCIENCE & TECHNOLOGY MANAGEMENTICAS2020_0077
Xu, J.RESEARCH ON THE PRESSURE COMFORT OF PILOT HELMETSICAS2020_0180
Xu, X.W.EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACKICAS2020_0182
Xu, A.ENABLING THE SMART SHOP FLOOR THROUGH THE INTEGRATION OF IOT AND AUTONOMOUS INTELLIGENCEICAS2020_0310
Xu, M.AN ADJOINT-BASDF AERO-STRUCTURAL DESIGN OPTIMIZATION METHOD USING DYNAMIC MESH TECHNOLOGYICAS2020_0317
Xu, L.DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEMICAS2020_0386
Xu, Y.-L.MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATIONICAS2020_0397
Xu, J.H.STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERICAS2020_0436
Xu, Z.-M.NATURAL-LAMINAR-FLOW AIRFOIL DESIGN OPTIMIZATION CONSIDERING CROSSFLOW INSTABILITY WHEN CONFIGURED ON A SWEPT WINGICAS2020_0472
Xu, C.-Z.AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHINGICAS2020_0476
Xu, Y.DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAINICAS2020_0503
Xu, C.-Z.IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC MODELING PROBLEMSICAS2020_0787
Xu, J.-H.DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERSICAS2020_0839
Xu, H.INVESTIGATION OF AERODYNAMIC INTERACTIONS BETWEEN NACA0012 AIRFOILS IN TANDEMICAS2020_1063
Xu, Y.X.STUDY ON THE OUT-OF-PLANE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT 350°CICAS2020_1072
Xu, S.C.A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODYICAS2020_1099
Xuan, L.BROADBAND MICROWAVE ABSORBING HONEYCOMB CORE MATERIAL WITH ACTIVE CARBON AS DELEGATESICAS2020_0308
Xue, B.INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHMICAS2020_0408
Xue, H.Z.AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESSICAS2020_0774
Xue, B.PRECISION ANALYSIS AND INDEX DISTRIBUTION SYSTEM DESIGN OF AVIONICS SYSTEM BASED ON BP NEURAL NETWORKICAS2020_0808
Xue, P.INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINEICAS2020_0845
Xue, G.-L.A METHOD OF MANEUVER IDENTIFICATION AND TRAJECTORY PREDICTION FOR AGILE TARGETICAS2020_0948
Xue, T.DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASEICAS2020_1135
Xue, B.A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOSICAS2020_1309
Yan, C.Y.MULTIPOINT OPTIMIZATION OF TRANSONIC NATURAL LAMINAR FLOW NACELLESICAS2020_0501
Yan, Z.K.SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TESTICAS2020_0744
Yan, P.AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESSICAS2020_0774
Yang, W.Q.NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING WITH SLOTTED-TIPICAS2020_0102
Yang, M.-S.EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIVICAS2020_0140
Yang, W.NUMERICAL SIMULATION ON AERODYNAMIC CHARACTERISTICS OF BIONIC CORRUGATED FLAPPING WINGICAS2020_0155
Yang, J.EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK-ABSORBING INSERTICAS2020_0157
Yang, X.A SIMPLIFIED MODEL FOR THE SIMULATION OF SYNERGISTIC AIR-BREATHING ROCKET ENGINEICAS2020_0160
Yang, Q.A SIMPLIFIED MODEL FOR THE SIMULATION OF SYNERGISTIC AIR-BREATHING ROCKET ENGINEICAS2020_0160
Yang, X.F.AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLESICAS2020_0168
Yang, Y.A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATESICAS2020_0272
Yang, Y.VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WINGICAS2020_0284
Yang , W.MECHANISM DESIGN AND AERODYNAMIC RESEARCH OF RETRACTABLE FOLDING FLAPPING WINGICAS2020_0333
Yang, C.PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTSICAS2020_0392
Yang, X.EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOYICAS2020_0400
Yang, D.EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOYICAS2020_0400
Yang, H.RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHMICAS2020_0413
Yang, X.D.AERODYNAMIC OPTIMIZATION DESIGN OF DOUBLE BLUNT ROTOR AIRFOIL WITH LARGE THICKNESS IN FORWARD AND REVERSE FLOWICAS2020_0424
Yang, M.S.EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSORICAS2020_0429
Yang, X.D.STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERICAS2020_0436
Yang, J.-H.COMPREHENSIVE REDUNDANCY MANAGEMENT AND VERIFICATION STRATEGY FOR TASK-BASED AIR MANAGEMENT SYSTEMICAS2020_0485
Yang, Y.-J.AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGEICAS2020_0631
Yang, C.AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGEICAS2020_0631
Yang, C.-Q.RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BEDICAS2020_0661
Yang, Y.A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONSICAS2020_0712
Yang, J.-B.AERODYNAMIC AND STRUCTURAL DESIGN OF THE COMPOSITE PROPELLER FOR NEAR SPACE VEHICLESICAS2020_0722
Yang, X.F.MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATIONICAS2020_0805
Yang, X.-W.NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATIONICAS2020_0826
Yang, W.-Q.NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATIONICAS2020_0826
Yang, W.COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WINGICAS2020_0836
Yang, Y.F.INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINEICAS2020_0845
Yang, C.-G.RESEARCH ON STRUCTURAL DESIGN OF TAIL BOOM FOR AN UNMANNED HELICOPTERICAS2020_1062
Yang, Y.-X.EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0ICAS2020_1122
Yang, X.H.DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASEICAS2020_1135
Yang, Z.EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACEICAS2020_1138
Yang, G.J.NUMERICAL SIMULATION STUDY ON BOUNDARY LAYER FLOW AND DRAG REDUCTION CHARACTERISTICS OF RIBLETSICAS2020_1140
Yang, X.INFLUENCE OF SHOCK TRAIN ON HEAT FLUX DISTRIBUTION OF A CIRCULAR CONSTANT-AREA ISOLATORICAS2020_1146
Yang, W.-Q.NUMERICAL SIMULATION OF PITCHING MOTION EFFECTS ON THE AERODYNAMIC PERFORMANCE OF DRAGONFLY-LIKE FLAPPING WINGICAS2020_1150
Yang, Y.J.NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH-SPEED VEHICLESICAS2020_1157
Yang, W.Q.NUMERICAL SIMULATION OF SWEEPING MOTION EFFECTS ON THE HOVERING DRAGONFLIESICAS2020_1167
Yang, W.Q.AERODYNAMIC ANALYSIS OF DRAGONFLY WINGS SPACE DISTRIBUTION ON THREE-DIMENSIONAL DURING HOVERING FLIGHTICAS2020_1172
Yang, X.-F.COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTIONICAS2020_1176
Yang, W.Q.NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTSICAS2020_1183
Yang, W.INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBERICAS2020_1185
Yang, J.J.NUMERICAL SIMULATION OF LOCAL LONG SHALLOW CAVITY EFFECT ON THE STABILITY OF A HYPERSONIC BOUNDARY LAYERICAS2020_1189
Yang, W.Q.NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WINGICAS2020_1240
Yao, X.H.A STRUCTURE DESIGN OF CFRP REAR PRESSURE BULKHEAD WITHOUT STIFFENERSICAS2020_0109
Yao, L.J.FAILURE PROCESS IDENTIFICATION IN C/SIC SAMPLES WITH A RANGE OF TENSILE PERFORMANCE USING ACOUSTIC EMISSIONICAS2020_0364
Yao, Y.M.AERODYNAMIC OPTIMIZATION DESIGN OF DOUBLE BLUNT ROTOR AIRFOIL WITH LARGE THICKNESS IN FORWARD AND REVERSE FLOWICAS2020_0424
Yao, R.FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATIONICAS2020_1127
Yao, J.NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAPICAS2020_1149
Yao, Z.C.RESEARCH ON AIRCRAFT-LEVEL PHYSICAL INTEGRATION VERIFICATION TEST TECHNOLOGYICAS2020_1232
Ye , Z.DESIGN OF A HYBRID VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO CIVIL AVIATION AIR TRAFFIC CONTROL SYSTEMICAS2020_0468
Yerramalli, C.S.METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WINGICAS2020_0085
Yi, S.H.EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACKICAS2020_0182
Yi , M.DESIGN OF A HYBRID VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO CIVIL AVIATION AIR TRAFFIC CONTROL SYSTEMICAS2020_0468
Yin, Y.K.A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WINGICAS2020_0256
Yin, Q.RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUEICAS2020_0273
Yin, Y.EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSORICAS2020_0291
Yin, Y.-H.RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNINGICAS2020_0388
Yin, Y.-Q.APPLICATION OF A SKEWED-SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSORICAS2020_0543
Yin, Y.-Q.DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSORICAS2020_0632
Yin, Y.-Q.MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGNICAS2020_0965
Yin, S.SMART CIVIL AVIATION TRANSPORTATION SYSTEMICAS2020_1283
Ying, J.Y.STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTIONICAS2020_0598
Yokosu, A.IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTPICAS2020_0557
Yokoyama, N.DECENTRALIZED CONFLICT DETECTION AND RESOLUTION METHOD ACCOUNTING FOR UNCERTAINTIES OF TRAJECTORIESICAS2020_0885
Yoshikawa, N.FEEDBACK ERROR LEARNING WITH ENHANCED SAMPLING: NEURAL FAULT TOLERANT CONTROLLER OF AIRCRAFTICAS2020_0613
You, K.AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESSICAS2020_1118
You, K.HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILSICAS2020_1125
You, Q.A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTIONICAS2020_1160
You, Q.COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTIONICAS2020_1176
Yu, G.F.A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDINGICAS2020_0282
Yu, J.NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODELICAS2020_0796
Yu, J.-Y.SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICSICAS2020_1134
Yu, L.INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBERICAS2020_1185
Yu, X.THE FLOW AND HEAT TRANSFER OF ANALYSIS TO ANNULAR CAVITY IN ENGINE CASEICAS2020_1251
Yuan, S.Q.COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWSICAS2020_0114
Yuan, X.-X.STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATORICAS2020_0305
Yuan, X.SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRIDICAS2020_0315
Yuan, K.SUPERSONIC AEROELASTIC ANALYSIS OF AN ALL-MOVABLE WING WITH FREE PLAYICAS2020_0393
Yuan, C.-S.PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITYICAS2020_0495
Yuan, M.L.SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODELICAS2020_0928
Yuan, X.X.STUDY ON THE STATISTICAL CHARACTERISTICS OF SKIN FRICTION OF SHOCK WAVE/ TURBULENT BOUDARY LAYER INTERATION IN A HOLLOW FLARE CONFIGURATION AT MACH 6ICAS2020_1224
Zakharchenko, V.S.UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEMICAS2020_0451
Zakharchenko, V.S.CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERSICAS2020_0974
Zalewski, P.THE USE OF REVERSE ENGINEERING AND COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A LOW COST SATELLITE LAUNCH SYSTEMICAS2020_1221
Zang, J.SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATIONICAS2020_0549
Zaplana Manzano, L.A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURESICAS2020_0562
Zappino, E.ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADSICAS2020_0479
Zeng, Q.EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLESICAS2020_0093
Zeng, L.COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTIONICAS2020_1176
Zhan, Z.J.INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHMICAS2020_0408
Zhan, H.MODELING AND DYNAMICS STABILITY ANALYSIS FOR A BLENDED-WING-BODY AIRCRAFTICAS2020_0525
Zhan, H.SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICSICAS2020_1134
Zhan, H.RESEARCH ON UNSTEADY AERODYNAMIC MODELS AT HIGH ANGLES OF ATTACK BASED ON NONLINEAR REGRESSIONICAS2020_1152
Zhan, Z.J.A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOSICAS2020_1309
Zhang, H.AERODYNAMICS CHARACTERISTICS STUDY ON A NATURE LAMINAR FLOW AIRFOIL OF NEAR-SPACE VEHICLE AT LOW REYNOLDS NUMBERSICAS2020_0021
Zhang, G.AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATIONICAS2020_0071
Zhang, G.HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSESICAS2020_0096
Zhang, J.A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFTICAS2020_0097
Zhang, S.H.COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWSICAS2020_0114
Zhang, W.FRACTURE CRITERION ANALYSIS AND CRACK GROWTH PROPERTY OF MIXED-MODE CRACK EXPERIMENTSICAS2020_0118
Zhang, Z.-B.MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSORICAS2020_0138
Zhang, Z.-B.EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIVICAS2020_0140
Zhang, W.VIRTUAL PROTOTYPING OF ELECTRICAL THSA FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONSICAS2020_0196
Zhang, Q.RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREASICAS2020_0219
Zhang, L.A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDINGICAS2020_0282
Zhang, Y.VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WINGICAS2020_0284
Zhang, S.VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WINGICAS2020_0284
Zhang, R.MECHANISM DESIGN AND AERODYNAMIC RESEARCH OF RETRACTABLE FOLDING FLAPPING WINGICAS2020_0333
Zhang, S.AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDINGICAS2020_0348
Zhang, K.-S.EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR THE “AEROSTRUCT” WING OPTIMIZATION PLATFORMICAS2020_0350
Zhang, Y.Z.FAILURE PROCESS IDENTIFICATION IN C/SIC SAMPLES WITH A RANGE OF TENSILE PERFORMANCE USING ACOUSTIC EMISSIONICAS2020_0364
Zhang, Y.DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEMICAS2020_0386
Zhang, Y.-F.RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNINGICAS2020_0388
Zhang, W.PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFTICAS2020_0398
Zhang, Y.PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFTICAS2020_0398
Zhang, Z.B.EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSORICAS2020_0429
Zhang, Y.AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHINGICAS2020_0476
Zhang, L.WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONSICAS2020_0483
Zhang, H.EXPERIMENTAL INVESTIGATION OF THE CHN-T1 MODEL IN FL-13 WIND TUNNEL OF CARDC AND DNW-LLF FACILITYICAS2020_0492
Zhang, S.PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITYICAS2020_0495
Zhang, Y.-J.PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITYICAS2020_0495
Zhang, Y.-Z.PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITYICAS2020_0495
Zhang, B.-Q.PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITYICAS2020_0495
Zhang, Y.F.MULTIPOINT OPTIMIZATION OF TRANSONIC NATURAL LAMINAR FLOW NACELLESICAS2020_0501
Zhang, M.H.MULTIPOINT OPTIMIZATION OF TRANSONIC NATURAL LAMINAR FLOW NACELLESICAS2020_0501
Zhang, M.NUMERICAL INVESTIGATION OF NACELLE INTAKE FLOW DISTORTION AT CROSSWIND CONDITIONSICAS2020_0504
Zhang, H.RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORYICAS2020_0514
Zhang, W.AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSORICAS2020_0538
Zhang, X.-Y.EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFTICAS2020_0620
Zhang, X.-B.EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFTICAS2020_0620
Zhang, W.EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFTICAS2020_0620
Zhang, Z.-K.AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGEICAS2020_0631
Zhang, J.DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSORICAS2020_0632
Zhang, C.A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFTICAS2020_0650
Zhang, Q.Q.THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDE-BODY CIVIL TRANSPORTICAS2020_0676
Zhang, J.STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESHICAS2020_0686
Zhang, K.-S.IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC MODELING PROBLEMSICAS2020_0787
Zhang, R.Y.RESEARCH ON TRAJECTORY OPTIMIZATION TECHNOLOGY CONSIDERING METEOROLOGICAL INFORMATION PREDICTIONICAS2020_0823
Zhang, W.W.DATA FUSION UNSTEADY AERODYNAMIC MODELING BASED ON EXPERIMENTAL DATAICAS2020_0842
Zhang, M.X.INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINEICAS2020_0845
Zhang, Q.B.RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTIONICAS2020_0909
Zhang, M.SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODELICAS2020_0928
Zhang, Z.X.AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTSICAS2020_0939
Zhang, L.X.AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTSICAS2020_0939
Zhang, K.-W.AN INTEGRATED METHOD FOR ACCURATE IDENTIFICATION AND DYNAMIC MONITORING OF BUILDINGS IN AERODROME OBSTACLE FREE SPACEICAS2020_1061
Zhang, W.RESEARCH ON FAULT DIAGNOSIS AND FAILURE RECONFIGURATION OF FLUSH AIR DATA SENSINGICAS2020_1064
Zhang, H.-Y.GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOWICAS2020_1073
Zhang, B.TWISTOR BASED 6-DOF DISTRIBUTED ADAPTIVE LEADER-FOLLOWING CONTROL FOR MULTIPLE RIGID SPACECRAFT FORMATIONICAS2020_1089
Zhang, S.S.TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLEICAS2020_1110
Zhang, H.A DYNAMIC SELF-CONTROL ERR STRATEGY FOR BI-DIRECTIONAL EVOLUTIONARY STRUCTURAL OPTIMIZATIONICAS2020_1153
Zhang, Q.A DYNAMIC SELF-CONTROL ERR STRATEGY FOR BI-DIRECTIONAL EVOLUTIONARY STRUCTURAL OPTIMIZATIONICAS2020_1153
Zhang, L.TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGYICAS2020_1170
Zhang, H.P.NUMERICAL SIMULATION OF RIDGE ICE AND AERODYNAMIC EFFECT UNDER THERMAL ANTI-ICEICAS2020_1179
Zhang, R.NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTSICAS2020_1183
Zhang, Y.D.NUMERICAL SIMULATION OF LOCAL LONG SHALLOW CAVITY EFFECT ON THE STABILITY OF A HYPERSONIC BOUNDARY LAYERICAS2020_1189
Zhang, R.NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WINGICAS2020_1240
Zhang, L.METHODS OF DIRECTIONAL COARSENING FOR UNSTRUCTURED GRIDS AND APPLICATIONSICAS2020_1261
Zhao, H.STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TESTINGICAS2020_0039
Zhao, H.SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHODICAS2020_0094
Zhao, Z.DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEMICAS2020_0386
Zhao, S.DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEMICAS2020_0386
Zhao, B.-D.PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNELICAS2020_0418
Zhao, S.-W.PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITYICAS2020_0495
Zhao, Y.Q.DEFORMATION ANALYSIS OF C-SPAR COMPOSITE STRUCTURE DURING THE PREFORMING PROCESSINGICAS2020_0599
Zhao, H.J.RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DISICAS2020_0865
Zhao, L.F.ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTIONICAS2020_1074
Zhao, L.F.MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOWICAS2020_1078
Zhao, X.AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESSICAS2020_1118
Zhao, S.-Z.AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESSICAS2020_1118
Zhao, S.-Z.HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILSICAS2020_1125
Zhao, X.HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILSICAS2020_1125
Zhao, S.-Z.FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATIONICAS2020_1127
Zhao, X.FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATIONICAS2020_1127
Zhao, L.F.ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGSICAS2020_1171
Zhao, Z.H.RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGEICAS2020_1203
Zhao, Y.X.THE FLOW AND HEAT TRANSFER OF ANALYSIS TO ANNULAR CAVITY IN ENGINE CASEICAS2020_1251
Zhao, Y.ESTIMATION OF STATIC AND DYNAMIC FLOATATION CHARACTERISTICS DURING AIRCRAFT DITCHINGICAS2020_1255
Zharenov, I.STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATIONICAS2020_0106
Zhbanov, V.A.EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACEICAS2020_0894
Zhen, H.AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERINGICAS2020_0053
Zheng, G.ADVANCED WEAK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATINGICAS2020_0037
Zheng, S.AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATIONICAS2020_0071
Zheng, W.P.EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACKICAS2020_0182
Zheng, C.VIRTUAL PROTOTYPING OF ELECTRICAL THSA FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONSICAS2020_0196
Zheng, J.-J.RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTERICAS2020_0304
Zheng, L.APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROLICAS2020_0978
Zheng, X.MULTI-UAV TRAJECTORY PLANNING BASED ON COORDINATION VARIABLESICAS2020_1139
Zhong, M.AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATIONICAS2020_0071
Zhong, S.-D.STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEMICAS2020_0366
Zhong, H.T.SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TESTICAS2020_0744
Zhou, Q.ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META-MODELICAS2020_0200
Zhou, Z.RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREASICAS2020_0219
Zhou, Y.A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATESICAS2020_0272
Zhou, Z.STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEMICAS2020_0366
Zhou, D.PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTSICAS2020_0392
Zhou, L.STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATIONICAS2020_0416
Zhou, H.ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM FOR COMPLICATED PRODUCTS ENGINEERINGICAS2020_0433
Zhou, Z.PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGNICAS2020_0463
Zhou, Z.A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFTICAS2020_0650
Zhou, N.-C.STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESHICAS2020_0686
Zhou, Z.BIONIC LIGHT-WEIGHT GRID SURFACE WING STRUCTURE DESIGN FOR A SOLAR-POWERED UAVICAS2020_0731
Zhou, Y.A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEMICAS2020_0764
Zhou, Q.CO-SIMULATION OF SYSML AND SIMULINK/MODELICA USING FMIICAS2020_0803
Zhou, Y.M.RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DISICAS2020_0865
Zhou, Z.APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROLICAS2020_0978
Zhou, W.Y.ADRC BASED HIGH MANEUVERING FLIGHT CONTROL LAW DESIGN FOR UAVICAS2020_1088
Zhou, W.J.NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH-SPEED VEHICLESICAS2020_1157
Zhou, L.C.RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGEICAS2020_1203
Zhu, G.CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFTICAS2020_0231
Zhu, Q.APPLICATION OF DEVELOPMENT ASSURANCE METHODOLOGIES TO ELECTRONIC ENGINE CONTROL SYSTEM (EECS)ICAS2020_0268
Zhu, L.-G.RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTERICAS2020_0304
Zhu, R.STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATIONICAS2020_0416
Zhu, X.ASSEMBLY QUALITY OPTIMIZATION APPROACH FOR LARGE-SCALE ACTIVE COMPONENTS BASED ON REVERSE ENGINEERINGICAS2020_0542
Zhu, J.Q.SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATIONICAS2020_0549
Zhu, Q.RESEARCH ON CERTIFICATION MANAGEMENT OF AIRCRAFT ENGINE BASED ON RISK ANALYSISICAS2020_0715
Zhu, A.-Y.RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLESICAS2020_0851
Zhu, Y.BASED ON SYSTEMS ENGINEERING PROCESS THE CIVIL AIRCRAFT PROJECT PRODUCT BREAKDOWN STRUCTURE DEVELOPMENT RESEARCHICAS2020_1018
Zhu, Y.-H.GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOWICAS2020_1073
Zhu, C.L.EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACEICAS2020_1138
Zhu, C.X.EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACEICAS2020_1138
Zhu, C.-L.ULTRASONIC DE-ICING SYSTEM DESIGN METHODS BASED ON RESONANCE AND IMPEDANCE MATCHINGICAS2020_1148
Zhu, Y.NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAPICAS2020_1149
Zhu, Z.C.NUMERICAL SIMULATION OF SWEEPING MOTION EFFECTS ON THE HOVERING DRAGONFLIESICAS2020_1167
Zhu, S.F.MODEL-BASED VIRTUAL INTEGRATED TEST METHOD FOR AVIONICS SYSTEMICAS2020_1212
Ziverts, U.ERAS- EVALUATION OF REALISTIC APPROACH SCENARIOS FOR MINIMAL NOISE - PRELIMINARY FINDINGSICAS2020_0409
Zong, W.-G.GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOWICAS2020_1073
Zou, C.H.A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDINGICAS2020_0282
Zou, L.TURBINE STRUCTURE ANALYSIS AND IMPROVEMENT OF A HIGH-SPEED ROTOR WITH MULTI-DISK AND MULTI-SUPPORTICAS2020_0391
Zou, X.-Q.APPLICATION OF A SKEWED-SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSORICAS2020_0543
Zou, C.H.AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISIONICAS2020_0591
Zuo, Y.T.AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLEICAS2020_1144