| Abarca López, R. | MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST | ICAS2020_1049 |
| Abdul Hamid, M.F. | CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGN | ICAS2020_1310 |
| Abramovich, H. | THE VIBRATION CORRELATION TECHNIQUE – A RELIABLE NONDESTRUCTIVE TOOL TO PREDICT BUCKLING LOADS | ICAS2020_0270 |
| Abu Talib, A.R. | CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGN | ICAS2020_1310 |
| Abu-Zurayk, M. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Ackley, J. | MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS | ICAS2020_1237 |
| Ai, J.L. | DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE | ICAS2020_1135 |
| Alaimo, A. | A STOCHASTIC ROBUSTNESS VERIFICATION OF NLG SIMPLE ADAPTIVE SHIMMY SUPPRESSION SYSTEM | ICAS2020_0662 |
| Alexandrov, S.V. | LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICS | ICAS2020_0107 |
| Alharasees, O. | OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT | ICAS2020_0638 |
| Allaio, D. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION | ICAS2020_1222 |
| Alves, W.M. | FLUID-STRUCTURE INTERACTION ANALYSIS OF ELASTIC EFFECTS OF A TRANSPORT AIRCRAFT FITTED WITH WINGLETS | ICAS2020_0999 |
| Amelyushkin, I.A. | EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE | ICAS2020_0894 |
| Amiryants, G.A. | THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATOR | ICAS2020_0212 |
| An, Y. | RESEARCH ON FUNCTIONAL HAZARD ASSESSMENT TECHNOLOGY OF MILITARY AIRCRAFT | ICAS2020_0795 |
| Andira, M.A. | FURTHER DEVELOPMENT OF COMPUTATIONAL STUDY ON COANDA BLANKET CURVATURE EFFECTS ON HALF SPHERICAL COANDA DEVICE | ICAS2020_0906 |
| Andreeva-Mori, A. | IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTION | ICAS2020_0202 |
| Annes da Silva, R.G. | NASA-CRM LATERAL-DIRECTIONAL STABILITY DERIVATIVES COMPARISON BETWEEN SEMI-EMPIRICAL, VORTEX LATTICE AND PANEL METHOD | ICAS2020_1190 |
| Aprovitola, A. | OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE | ICAS2020_0164 |
| Aquilini, C. | MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST | ICAS2020_1049 |
| Arai, M. | IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP | ICAS2020_0557 |
| Arizono, H. | ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT FOR MORPHING WINGS | ICAS2020_0540 |
| Aruna, S.T. | SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOY | ICAS2020_1052 |
| Atanasov, G. | CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT | ICAS2020_0185 |
| Atanasov, G. | ASSESSMENT OF THREE COMMUTER AIRCRAFT CONCEPTS FROM A TRANSPORT SYSTEM PERSPECTIVE | ICAS2020_0207 |
| Atkin, C. | AN OBJECTIVE APPROACH FOR MEASURING INTERMITTENCY IN THE TRANSITIONAL BOUNDARY LAYER | ICAS2020_0149 |
| Atkin, C.J. | VIBRATION INDUCED EXCITATION OF INSTABILITY WAVES IN A BLASIUS FLOW | ICAS2020_0890 |
| Augello, R. | ACCURATE BUCKLING AND POST-BUCKLING ANALYSIS OF COMPOSITE STIFFENED PANELS | ICAS2020_1124 |
| Augousti, A.T. | FAILURE PROCESS IDENTIFICATION IN C/SIC SAMPLES WITH A RANGE OF TENSILE PERFORMANCE USING ACOUSTIC EMISSION | ICAS2020_0364 |
| Azevedo, J.L.F. | STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERS | ICAS2020_0725 |
| Azevedo, J.L.F. | A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONS | ICAS2020_0734 |
| Bagassi, S. | ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELS | ICAS2020_0508 |
| Bagassi, S. | FUTURE PERSPECTIVES ON VR & AR | ICAS2020_1290 |
| Bai, J. | AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION | ICAS2020_0071 |
| Bai, J. | TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR | ICAS2020_0357 |
| Bai, C. | STRUCTURAL VIBRATION CONTROL BY USING THE ENERGY FROM DIFFERENT MODES | ICAS2020_0383 |
| Bai, Z. | PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2020_0398 |
| Bai, J.-Q. | DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHT | ICAS2020_0714 |
| Bai, Z. | APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROL | ICAS2020_0978 |
| Bai, J. | TWISTOR BASED 6-DOF DISTRIBUTED ADAPTIVE LEADER-FOLLOWING CONTROL FOR MULTIPLE RIGID SPACECRAFT FORMATION | ICAS2020_1089 |
| Bai, X. | SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICS | ICAS2020_1134 |
| Bai, J.Q. | TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR | ICAS2020_1247 |
| Baldon, C. | S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE | ICAS2020_0455 |
| Baldon, C. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| Balunov, K. | MATHEMATICAL MODELS FOR ANALYSIS AND OPTIMIZATION OF AIRCRAFT STRUCTURAL COMPONENTS TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION | ICAS2020_0593 |
| Bando, M. | MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMS | ICAS2020_0945 |
| Bao, M.-X. | ULTRASONIC DE-ICING SYSTEM DESIGN METHODS BASED ON RESONANCE AND IMPEDANCE MATCHING | ICAS2020_1148 |
| Barberis, B. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| Barbieri, R. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION | ICAS2020_1222 |
| Bartasevicius, J. | FLIGHT TESTING OF 65KG T-FLEX SUBSCALE DEMONSTRATOR | ICAS2020_0707 |
| Basov, V. | MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS | ICAS2020_0089 |
| Bastos, T.M.B. | TASK ALLOCATION ALGORITHMS FOR A COOPERATIVE DRONE PARCEL DELIVERY SYSTEM | ICAS2020_1306 |
| Batra, A. | ASSESSING THE ENVIRONMENTAL IMPACT OF AIRCRAFT TAXIING TECHNOLOGIES | ICAS2020_1162 |
| Bautin, A. | MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS | ICAS2020_0089 |
| Bayandor, J. | REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACT | ICAS2020_1014 |
| Bazhenov, S. | THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEM | ICAS2020_0239 |
| Becker, R.-G. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Bergkvist, M. | FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE | ICAS2020_1032 |
| Berlowitz, I. | no paper provided | ICAS2020_0010 |
| Berres, A. | IMPACT OF NEW TECHNOLOGIES ON AIRCRAFT SYSTEMS | ICAS2020_0050 |
| Bessonov, P. | METHODS FOR CALCULATING THE FATIGUE DAMAGE OF A STRUCTURE FOR VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS | ICAS2020_0576 |
| Bezuevsky, A.V. | RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIME | ICAS2020_0963 |
| Bi, L. | SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRID | ICAS2020_0315 |
| Bi, S.Q. | THE FINITE ELEMENT MODELLING OF BOLTED STRUCTURE BETWEEN SELECTIVE LASER MELTING ALUMINIUM AND COMPOSITE PLATES | ICAS2020_0880 |
| Bian, J. | MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATION | ICAS2020_0397 |
| Biedermann, J. | FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESS | ICAS2020_0134 |
| Bihai, H. | AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERING | ICAS2020_0053 |
| Bijjahalli, S. | A NOVEL DETECT-AND-AVOID APPROACH FOR UAS IN URBAN ENVIRONMENTS | ICAS2020_0970 |
| Bil, C. | OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTION | ICAS2020_0311 |
| Blinnik, B.S. | AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONS | ICAS2020_1242 |
| Bodmer, D. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Bogatyrev, V. | INCREASING THE EFFECTIVENESS OF AN AERODYNAMICALLY BALANCED CONTROL SURFACE ON A MODIFIED AIRFOIL WITH REDUCED DRAG | ICAS2020_0784 |
| Bogenberger, K. | VERTIPORT PLACEMENT METHOD BASED ON MOBILITY SURVEY DATA | ICAS2020_1133 |
| Boggero, L. | THE APPLICATION OF THE AGILE 4.0 MBSE ARCHITECTURAL FRAMEWORK FOR THE MODELING OF SYSTEM STAKEHOLDERS, NEEDS AND REQUIREMENTS | ICAS2020_0193 |
| Boggero, L. | ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES | ICAS2020_1259 |
| Bolart, C. | VALIDATING SURROGATE MODELS AND ICORPORATING UNCERTAINTY QUANTIFICATION IN MULTI-ELEMENTS AIRFOIL DESIGN OPTIMISATION | ICAS2020_0248 |
| Bonnici, M. | TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSER | ICAS2020_0081 |
| Bortolotto, L. | AEROELASTIC RESPONSE CALCULATION USING DUHAMEL INTEGRAL AND ITS APPLICATIONS | ICAS2020_1126 |
| Bosnyakov, I. | VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING | ICAS2020_0033 |
| Bosnyakov, S. | VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING | ICAS2020_0033 |
| Bottino, N. | S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE | ICAS2020_0455 |
| Bragado-Aldana, E. | ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONS | ICAS2020_0253 |
| Braun, R. | HYBRID MODELLING FOR FULL MISSION SIMULATION | ICAS2020_0980 |
| Breard, C. | SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCES | ICAS2020_0743 |
| Breitsamter, C. | ANALYSIS OF A WING-TIP-MOUNTED SMALL-SCALE PROPELLER CONFIGURATION UNDER NON-AXIAL INFLOW CONDITIONS | ICAS2020_0116 |
| Breitsamter, C. | EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS | ICAS2020_0227 |
| Breitsamter, C. | TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON WAKE VORTEX IMPACT BY OSCILLATING FLAPS | ICAS2020_0595 |
| Bremm, M. | DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL AERODYNAMIC LIFT MECHANISM | ICAS2020_0863 |
| Brusberg, P. | LANDING PLATFORM FOR URBAN AIR MOBILITY VEHICLES INTEGRATED INTO PARKING LOT INFRASTRUCTURE IN DENSELY BUILT-UP AREAS | ICAS2020_1217 |
| Budinger, M. | DESIGN OPTIMIZATION OF MULTIROTOR DRONES IN FORWARD FLIGHT | ICAS2020_0781 |
| Budzko, V.I. | CREATING A MULTI-FUNCTIONAL EXPERT ANALYTICAL SYSTEM IN THE AIRCRAFT INDUSTRY AND THE FORMATION OF GENERAL REQUIREMENTS | ICAS2020_0857 |
| Burger, U. | MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONS | ICAS2020_0019 |
| Bussemaker, J.H. | SYSTEM ARCHITECTURE DESIGN SPACE MODELING AND OPTIMIZATION ELEMENTS | ICAS2020_0203 |
| Bykerk, T. | LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE | ICAS2020_0165 |
| Büscher, A. | FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANE | ICAS2020_1048 |
| Cabaleiro, C. | ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES | ICAS2020_1259 |
| Cabanac, J.-P. | THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS | ICAS2020_1235 |
| Cai, H.-Y. | STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATOR | ICAS2020_0305 |
| Cai, Z.Y. | RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DIS | ICAS2020_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 6 | ICAS2020_1224 |
| Camilleri, R. | ASSESSING THE ENVIRONMENTAL IMPACT OF AIRCRAFT TAXIING TECHNOLOGIES | ICAS2020_1162 |
| Campillo-Borras, E. | HARMONIZING SUSTAINABLE AVIATION RESEARCH AMONG IFAR ORGANIZATIONS | ICAS2020_1302 |
| Campolo, G. | APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS | ICAS2020_0454 |
| Campos, L.M.B.C. | ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATION | ICAS2020_0989 |
| Campos, L.M.B.C. | ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHS | ICAS2020_0990 |
| Cantanna, G. | S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE | ICAS2020_0455 |
| Cao, J. | EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES | ICAS2020_0093 |
| Cao, J.-A. | RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUE | ICAS2020_0273 |
| Cao, G.Z. | NUMERICAL SIMULATION OF RIDGE ICE AND AERODYNAMIC EFFECT UNDER THERMAL ANTI-ICE | ICAS2020_1179 |
| Carlsson, B. | FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE | ICAS2020_1032 |
| Carpenter, K. | REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACT | ICAS2020_1014 |
| Carrera, E. | ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADS | ICAS2020_0479 |
| Carrera, E. | ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELS | ICAS2020_0508 |
| Carrera, E. | ACCURATE BUCKLING AND POST-BUCKLING ANALYSIS OF COMPOSITE STIFFENED PANELS | ICAS2020_1124 |
| Carrone, F. | S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE | ICAS2020_0455 |
| Carvalho, L.M.M.O. | A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONS | ICAS2020_0734 |
| Castro, S.G.P. | ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURES | ICAS2020_0337 |
| Catalano, F.M. | HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORS | ICAS2020_0988 |
| Cato, A. | ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME | ICAS2020_0985 |
| Caurin, G.A.P. | USAGE OF MQTT, ROS, AND AWS IN THE MANUFACTURING PROCESS OF AIRCRAFTS | ICAS2020_1223 |
| Cavalcante, J. | ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME | ICAS2020_0985 |
| Celestini, D. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| Celli, M.-A. | THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS | ICAS2020_1235 |
| Cen, F. | VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL | ICAS2020_0313 |
| Cen, F. | WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONS | ICAS2020_0483 |
| Cen, F. | NONLINEAR UNSTEADY AERODYNAMIC MODELING AND LONGITUDINAL STABILITY ANALYSIS FOR AN AIRCRAFT MODEL | ICAS2020_1104 |
| Cerino, G. | ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT | ICAS2020_1258 |
| Cerny, M. | ANALYSIS OF A WING-TIP-MOUNTED SMALL-SCALE PROPELLER CONFIGURATION UNDER NON-AXIAL INFLOW CONDITIONS | ICAS2020_0116 |
| Cestino, E. | APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS | ICAS2020_0454 |
| Cestino, E. | S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE | ICAS2020_0455 |
| Cestino, E. | DESIGN OF A VERTICAL DITCHING TEST | ICAS2020_0763 |
| Chai, Y.-G. | RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERING | ICAS2020_0633 |
| Chang, C. | DESIGN AND VERIFICATION OF ENERGY-ABSORBING STRUCTURE OF CORRUGATED BEAM BASED ON SPECIFIC FAILURE MODE | ICAS2020_0187 |
| Chang, M. | TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR | ICAS2020_0357 |
| Chang, M. | DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHT | ICAS2020_0714 |
| Chang, S. | SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TEST | ICAS2020_0744 |
| Chang, L.-F. | A METHOD OF MANEUVER IDENTIFICATION AND TRAJECTORY PREDICTION FOR AGILE TARGET | ICAS2020_0948 |
| Chang, M. | TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR | ICAS2020_1247 |
| Chartier, N. | MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS | ICAS2020_1237 |
| Che, Y.X. | APPLICATION OF MBSE IN AERO-ENGINE STRUCTURAL PARAMETER CALCULATING SYSTEM | ICAS2020_0720 |
| Chedrik, A.V. | THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATOR | ICAS2020_0212 |
| Chedrik, V. | MATHEMATICAL MODELS FOR ANALYSIS AND OPTIMIZATION OF AIRCRAFT STRUCTURAL COMPONENTS TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION | ICAS2020_0593 |
| Chen, C. | A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS | ICAS2020_0036 |
| Chen, Y.-H. | MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSOR | ICAS2020_0138 |
| Chen, D. | CONCEPTUAL DESIGN OF A FIXED-WING AQUATIC UAV USING KNOWLEDGE BASED ENGINEERING | ICAS2020_0154 |
| Chen, Y. | EFFECT OF COMPLEX FLOW PROFILES AT COMBUSTOR EXIT ON TURBINE CHARACTERISTICS | ICAS2020_0257 |
| Chen, F. | FLIGHT MANAGEMENT SYSTEM REQUIREMENT ANALYSIS FOR TRAJECTORY BASED OPERATION | ICAS2020_0292 |
| Chen, L. | BROADBAND MICROWAVE ABSORBING HONEYCOMB CORE MATERIAL WITH ACTIVE CARBON AS DELEGATES | ICAS2020_0308 |
| Chen, H. | SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRID | ICAS2020_0315 |
| Chen, A. | MECHANISM DESIGN AND AERODYNAMIC RESEARCH OF RETRACTABLE FOLDING FLAPPING WING | ICAS2020_0333 |
| Chen, P. | MEMS-BASED DISTRIBUTED NAVIGATION SYSTEM | ICAS2020_0344 |
| Chen , B. | AERODYNAMIC NOISE SIMULATION OF CIVIL AIRCRAFT LANDING GEARS BASED ON LES-SMARGORINSKY MODEL | ICAS2020_0351 |
| Chen, X. | APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATION | ICAS2020_0352 |
| Chen, X. | STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEM | ICAS2020_0366 |
| Chen, X. | ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAM | ICAS2020_0378 |
| Chen, C. | ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAM | ICAS2020_0378 |
| Chen, Q. | ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAM | ICAS2020_0378 |
| Chen, Y.-N. | TURBINE STRUCTURE ANALYSIS AND IMPROVEMENT OF A HIGH-SPEED ROTOR WITH MULTI-DISK AND MULTI-SUPPORT | ICAS2020_0391 |
| Chen, Y.-N. | MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATION | ICAS2020_0397 |
| Chen, C. | EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIOURS OF RESOLVENT MODE | ICAS2020_0414 |
| Chen, X. | EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIOURS OF RESOLVENT MODE | ICAS2020_0414 |
| Chen, Y. | EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR | ICAS2020_0429 |
| Chen, Z.-L. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Chen, Y.-C. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Chen, B. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Chen, Y. | DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAIN | ICAS2020_0503 |
| Chen, F. | DEFORMATION ANALYSIS OF C-SPAR COMPOSITE STRUCTURE DURING THE PREFORMING PROCESSING | ICAS2020_0599 |
| Chen, P. | DEFORMATION ANALYSIS OF C-SPAR COMPOSITE STRUCTURE DURING THE PREFORMING PROCESSING | ICAS2020_0599 |
| Chen, J.W. | A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT | ICAS2020_0650 |
| Chen, X.M. | DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISK | ICAS2020_0713 |
| Chen, C. | CO-SIMULATION OF SYSML AND SIMULINK/MODELICA USING FMI | ICAS2020_0803 |
| Chen, C. | PRECISION ANALYSIS AND INDEX DISTRIBUTION SYSTEM DESIGN OF AVIONICS SYSTEM BASED ON BP NEURAL NETWORK | ICAS2020_0808 |
| Chen, H. | INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINE | ICAS2020_0845 |
| Chen, B. | AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESS | ICAS2020_0899 |
| Chen, Q. | RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTION | ICAS2020_0909 |
| Chen, X.L. | RESEARCH OF THE HYPERSONIC BOUNDARY LAYER INSTABILITIES AND TRANSITION WITH THERMAL-CHEMICAL NON-EQUILIBRIUM EFFECTS | ICAS2020_0944 |
| Chen, X. | MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGN | ICAS2020_0965 |
| Chen, Z.-J. | AN INTEGRATED METHOD FOR ACCURATE IDENTIFICATION AND DYNAMIC MONITORING OF BUILDINGS IN AERODROME OBSTACLE FREE SPACE | ICAS2020_1061 |
| Chen, Y.X. | ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION | ICAS2020_1074 |
| Chen, Y.C. | BENEFIT ANALYSIS OF AIR REFUELING IN ULTRA LONG ROUTE AIRLINER OPERATION | ICAS2020_1101 |
| Chen, X. | CLOUD-BASED ENVIRONMENT FOR AIRCRAFT DESIGN COLLABORATION | ICAS2020_1123 |
| Chen, Z.Y. | FAST ITERATIVE SIMULATION OF AIRLINER WING PLANFORM CONCEPTUAL DESIGN | ICAS2020_1155 |
| Chen , Z.T. | ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGS | ICAS2020_1171 |
| Chen, Y.Z. | NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATION | ICAS2020_1250 |
| Chen, P. | ASCENT TRAJECTORY OPTIMIZATION OF HYPERSONIC VEHICLE USING SWARM INTELLIGENT METHOD | ICAS2020_1266 |
| Chen, Y. | FLIGHT TEST ON THE ICING OF CIVIL AIRCRAFT | ICAS2020_1284 |
| Cheng, P. | EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTS | ICAS2020_0040 |
| Cheng, W. | RESEARCH ON ARCHITECTURE FRAMEWORK MODEL BASED EVALUATION INDEX FOR AVIATION SCIENCE & TECHNOLOGY MANAGEMENT | ICAS2020_0077 |
| Cheng, W.Y. | A CONTRASTIVE STUDY OF STANDARD SPECIFICATION FOR TECHNOLOGY READINESS ASSESSMENT | ICAS2020_0252 |
| Cheng, Y. | HYBRID IGNITION PROBABILITY METHOD TO PREDICT THE IGNITION PERFORMANCE OF A GAS TURBINE COMBUSTOR | ICAS2020_0259 |
| Cheng, Y. | A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDING | ICAS2020_0282 |
| Cheng, W. | VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING | ICAS2020_0284 |
| Cheng, M. | SUPERSONIC AEROELASTIC ANALYSIS OF AN ALL-MOVABLE WING WITH FREE PLAY | ICAS2020_0393 |
| Cheng, Y. | ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM FOR COMPLICATED PRODUCTS ENGINEERING | ICAS2020_0433 |
| Cheng, L.K. | RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFT | ICAS2020_0706 |
| Cheng, J.A. | RESEARCH ON UNSTEADY AERODYNAMIC MODELS AT HIGH ANGLES OF ATTACK BASED ON NONLINEAR REGRESSION | ICAS2020_1152 |
| Chernousov, V.I. | STUDY ON AERODYNAMIC CHARACTERISTICS OF LIGHT CONVERTIBLE AIRCRAFT MODEL | ICAS2020_0810 |
| Choi, J. | A STUDY ON DEEP LEARNING BASED AUTOMATED AERIAL DOCKING SYSTEM | ICAS2020_1305 |
| Chu, S. | HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSES | ICAS2020_0096 |
| Churkina, T.E. | OPTIMAL TRAJECTORY DEPENDENCE ON THE ATMOSPHERE MODEL FOR THE SUN-POWERED AIRPLANE | ICAS2020_0448 |
| Chuvakhov, P.V. | STABILIZATION OF SUPERSONIC BOUNDARY LAYERS IN THE PRESENCE OF FAVORABLE PRESSURE GRADIENT | ICAS2020_0656 |
| Chuvakhov, P.V. | MECHANISMS OF NATURAL LAMINAR-TURBULENT TRANSITION ON AN UNSWEPT WING IN SUPERSONIC FLIGHT | ICAS2020_0657 |
| Ciampa, P.D. | THE APPLICATION OF THE AGILE 4.0 MBSE ARCHITECTURAL FRAMEWORK FOR THE MODELING OF SYSTEM STAKEHOLDERS, NEEDS AND REQUIREMENTS | ICAS2020_0193 |
| Ciampa, P.D. | SYSTEM ARCHITECTURE DESIGN SPACE MODELING AND OPTIMIZATION ELEMENTS | ICAS2020_0203 |
| Ciampa, P.D. | ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES | ICAS2020_1259 |
| Ciampa, P.D. | ICAS DIGITAL PIONEERING INITIATIVE AND FUTURE PERSPECTIVES ON MDO & MBSE | ICAS2020_1288 |
| Cibrario Bertolotti, S. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS | ICAS2020_1219 |
| Cigal, N. | EXPLORATION OF AERIAL FIREFIGHTING FLEET EFFECTIVENESS AND COST BY SYSTEM OF SYSTEMS SIMULATIONS | ICAS2020_0997 |
| Cinefra, M. | ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELS | ICAS2020_0508 |
| Civera, M. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS | ICAS2020_1219 |
| Civera, M. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION | ICAS2020_1222 |
| Clark, C. | AERODYNAMIC ANALYSIS OF A HIGH SPEED TEST RIG FOR USE IN ENGINE TEST FACILITIES | ICAS2020_0016 |
| Coppola, M. | APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS | ICAS2020_0454 |
| Corpino, S. | ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT | ICAS2020_1258 |
| Corpino, S. | ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES | ICAS2020_1259 |
| Cosenza, D. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS | ICAS2020_1219 |
| Costa, U. | ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME | ICAS2020_0985 |
| Costa, T.L. | ROBUST CONTROL OF UNMANNED AERIAL VEHICLE WITH TILT ROTORS AND CAMERA | ICAS2020_1006 |
| Croce, J.A.G. | HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORS | ICAS2020_0988 |
| Cui, F. | AERODYNAMICS CHARACTERISTICS STUDY ON A NATURE LAMINAR FLOW AIRFOIL OF NEAR-SPACE VEHICLE AT LOW REYNOLDS NUMBERS | ICAS2020_0021 |
| Cui, D. | RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM | ICAS2020_0413 |
| Cui, P.-C. | STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESH | ICAS2020_0686 |
| Cui, Y. | A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTS | ICAS2020_0833 |
| Cui, H. | THE FINITE ELEMENT MODELLING OF BOLTED STRUCTURE BETWEEN SELECTIVE LASER MELTING ALUMINIUM AND COMPOSITE PLATES | ICAS2020_0880 |
| Cui, X.-D. | METHODS OF DIRECTIONAL COARSENING FOR UNSTRUCTURED GRIDS AND APPLICATIONS | ICAS2020_1261 |
| Cutrone, L. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Czajkowski, L. | PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER | ICAS2020_0747 |
| da Silva, R.G. | STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERS | ICAS2020_0725 |
| da Silva, R.G. | A CONTRIBUTION TO THE SIMULATION OF TRANSITIONAL FLOWS OVER AEROSPACE CONFIGURATIONS | ICAS2020_0734 |
| Dala, L. | NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES | ICAS2020_0556 |
| Dandois, J. | NUMERICAL SIMULATIONS OF TRANSONIC BUFFET ON A HALF WING-BODY CONFIGURATION | ICAS2020_0612 |
| Daverschot, D. | STRUCTURAL HEALTH MONITORING - THE ROUTE TO CONDITION BASED MAINTENANCE | ICAS2020_0347 |
| De Gaspari, A. | AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE | ICAS2020_0631 |
| De Lucas Bodas, S. | EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION | ICAS2020_0171 |
| De Lucas Bodas, S. | STUDY OF THE BENEFITS OF A SEMI-MORPHING WING CONCEPT | ICAS2020_0216 |
| De Negri, V. | CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS | ICAS2020_0110 |
| De Pieri, E.R. | ROBUST CONTROL OF UNMANNED AERIAL VEHICLE WITH TILT ROTORS AND CAMERA | ICAS2020_1006 |
| De Simone, V. | THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE | ICAS2020_0493 |
| Degenhardt, R. | ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURES | ICAS2020_0337 |
| Degenhardt, R. | IFAR - INFRASTRUCTURE DATABASE | ICAS2020_1051 |
| Delbecq, S. | DESIGN OPTIMIZATION OF MULTIROTOR DRONES IN FORWARD FLIGHT | ICAS2020_0781 |
| Dell 'Amico, A. | EVALUATION ASPECT MAPPING FOR ACTUATION SYSTEM DESIGN | ICAS2020_1210 |
| Dell'Amico, A. | CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS | ICAS2020_0110 |
| Dell'Amico, A. | AN ONTOLOGICAL APPROACH FOR CLASSIFYING AIRCRAFT ACTUATORS | ICAS2020_1209 |
| Deng, X. | EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTS | ICAS2020_0040 |
| Deng, W.-L. | TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT | ICAS2020_0271 |
| Deng, W.-Q. | TURBINE STRUCTURE ANALYSIS AND IMPROVEMENT OF A HIGH-SPEED ROTOR WITH MULTI-DISK AND MULTI-SUPPORT | ICAS2020_0391 |
| Deng, P.Y. | INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHM | ICAS2020_0408 |
| Deng, M.-C. | RESEARCH OF LABYRINTH SEALS MEASUREMENT-BASED PROBABILITISTIC ANALYSIS METHOD FOR TURBOFAN INTERNAL AIR SYSTEM | ICAS2020_0531 |
| Deng, Y.C. | A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONS | ICAS2020_0712 |
| Denisov, S. | STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION | ICAS2020_0106 |
| Dessertenne, F. | CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM | ICAS2020_0659 |
| Di Fede, F. | ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT | ICAS2020_1258 |
| Di Ianni, L. | DESIGN OF A VERTICAL DITCHING TEST | ICAS2020_0763 |
| Di Ianni, L. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| DI Pasquale, D. | BLENDED WING BODY (BWB) PLANFORM MULTIDISCIPLINARY OPTIMISATION (MDO) FOR EARLY STAGE AIRCRAFT DESIGN USING MODEL BASED ENGINEERING | ICAS2020_0244 |
| Di Pasquale, D. | VALIDATING SURROGATE MODELS AND ICORPORATING UNCERTAINTY QUANTIFICATION IN MULTI-ELEMENTS AIRFOIL DESIGN OPTIMISATION | ICAS2020_0248 |
| Ding, D. | AIRCRAFT INFLIGHT ICING DETECTION AND DIAGNOSIS METHODS | ICAS2020_0163 |
| Ding, Q. | STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION | ICAS2020_0416 |
| Ding, Y.-L. | FAST METHOD AND AN INTEGRATED CODE FOR SONIC BOOM PREDICTION OF SUPERSONIC COMMERCIAL AIRCRAFT | ICAS2020_0600 |
| Ding, F. | AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE | ICAS2020_0663 |
| Ding , X.B. | IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEM | ICAS2020_0723 |
| Ding, Y. | BIONIC LIGHT-WEIGHT GRID SURFACE WING STRUCTURE DESIGN FOR A SOLAR-POWERED UAV | ICAS2020_0731 |
| Ding, S.L. | NUMERICAL STUDY OF DITCHING CHARACTERISTICS OF BWB AIRCRAFT | ICAS2020_1178 |
| Dinh Nguyen, D. | AIR TRAFFIC MANAGEMENT OF DRONES INTEGRATED INTO THE SMART CITIES | ICAS2020_0456 |
| Djojodihardjo, H. | FURTHER DEVELOPMENT OF COMPUTATIONAL STUDY ON COANDA BLANKET CURVATURE EFFECTS ON HALF SPHERICAL COANDA DEVICE | ICAS2020_0906 |
| Djojodihardjo, H. | CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGN | ICAS2020_1310 |
| Doberts, A.C. | LANDING PLATFORM FOR URBAN AIR MOBILITY VEHICLES INTEGRATED INTO PARKING LOT INFRASTRUCTURE IN DENSELY BUILT-UP AREAS | ICAS2020_1217 |
| Dong, Y. | THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE | ICAS2020_0095 |
| Dong, W. | A SIMPLIFIED MODEL FOR THE SIMULATION OF SYNERGISTIC AIR-BREATHING ROCKET ENGINE | ICAS2020_0160 |
| Dong, W. | AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERS | ICAS2020_0541 |
| Dong, X. | RESEARCH ON SELECTION METHODS FOR AIRCRAFT LANDING GEAR SYSTEM HEALTH FEATURE PARAMETERS | ICAS2020_0581 |
| Dong, L. | AN AGILE PRACTICE OF AVIONICS SYSTEM DEVELOPMENT | ICAS2020_0609 |
| Dong, D.N. | A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEM | ICAS2020_0764 |
| Dong, L.T. | AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESS | ICAS2020_0774 |
| Dong, Y. | COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING | ICAS2020_0836 |
| Dong, C. | INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINE | ICAS2020_0845 |
| Dong, J. | STUDY ON THE FATIGUE SCATTER FACTOR UNDER SEVERE LOAD SPECTRUM | ICAS2020_0904 |
| Dong, Y.Q. | DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE | ICAS2020_1135 |
| Dong, C. | AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE | ICAS2020_1144 |
| dos Santos, M. | MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS | ICAS2020_1237 |
| Dou, G.H. | NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH-SPEED VEHICLES | ICAS2020_1157 |
| Dowell, E. | A BENCHMARK METHOD FOR PREDICTING OBLIQUE SHOCK STRUCTURE | ICAS2020_0072 |
| Du, H. | THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT | ICAS2020_0181 |
| Du, Y.-M. | TRANSITION PREDICTION FOR TRANSPORT AIRCRAFT CONFIGURATIONS BASED ON OVERSET GRID | ICAS2020_0286 |
| Du, X. | AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING | ICAS2020_0348 |
| Du, L. | ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM FOR COMPLICATED PRODUCTS ENGINEERING | ICAS2020_0433 |
| Du, J.-N. | EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODEL | ICAS2020_0619 |
| Du, Y.X. | MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION | ICAS2020_0805 |
| Du, Y.X. | A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTS | ICAS2020_0833 |
| Du, X.F. | STUDY ON THE OUT-OF-PLANE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT 350°C | ICAS2020_1072 |
| Du, S.Y. | NUMERICAL SIMULATION STUDY ON BOUNDARY LAYER FLOW AND DRAG REDUCTION CHARACTERISTICS OF RIBLETS | ICAS2020_1140 |
| Du, Y.-X. | COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION | ICAS2020_1176 |
| Du, Q. | NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATION | ICAS2020_1250 |
| Duan, S. | STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TESTING | ICAS2020_0039 |
| Dubinskii, S. | STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION | ICAS2020_0106 |
| Dubinskii, S. | METHODS FOR CALCULATING THE FATIGUE DAMAGE OF A STRUCTURE FOR VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS | ICAS2020_0576 |
| Dui, H. | STUDY ON THE FATIGUE SCATTER FACTOR UNDER SEVERE LOAD SPECTRUM | ICAS2020_0904 |
| Dui, H.N. | AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS | ICAS2020_0939 |
| Dupuy, E. | THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS | ICAS2020_1235 |
| Dziubinski, A. | THE USE OF REVERSE ENGINEERING AND COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A LOW COST SATELLITE LAUNCH SYSTEM | ICAS2020_1221 |
| Dähne, S. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Eek, M. | CONNECTING SYSTEM SIMULATION TO AIRCRAFT CONCEPT DEVELOPMENT | ICAS2020_1229 |
| Efremov, A.V. | THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERS | ICAS2020_0176 |
| Egorov, I.V. | HYBRID NUMERICAL SCHEMES IN PREDICTION OF HIGH-SPEED LAMINAR-TURBULENT TRANSITION | ICAS2020_0529 |
| Eguea, J.P. | HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORS | ICAS2020_0988 |
| Eguea, J.P. | HOW CAN A CAMBER MORPHING WINGLET CONTRIBUTE TO MAKING AVIATION GREENER | ICAS2020_1304 |
| Eitelberg, G. | ANALYSIS OF THRUST-SCALED ACOUSTIC EMISSIONS OF AIRCRAFT PROPELLERS AND THEIR DEPENDENCE ON PROPULSIVE EFFICIENCY | ICAS2020_0751 |
| El Fassi, S. | APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATION | ICAS2020_0352 |
| El'Youssef, E.S. | ROBUST CONTROL OF UNMANNED AERIAL VEHICLE WITH TILT ROTORS AND CAMERA | ICAS2020_1006 |
| El-Jabi, R. | INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSIS | ICAS2020_1213 |
| El-Salamony, M. | STUDY OF SMALL UAVS DISTURBED MOTION NATURAL FREQUENCIES USING EXTENDED EXPERIMENTAL DATASETS | ICAS2020_0498 |
| Emara, M. | MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS | ICAS2020_1237 |
| Entzinger, J.O. | AN OVERVIEW OF FLARE TECHNIQUES AND FLARE TRAINING METHODS | ICAS2020_0919 |
| Ernst, G. | FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANE | ICAS2020_1048 |
| Esmaeili, A. | ENERGY HARVESTING FROM PIEZOELECTRIC FRINGES AT THE TRAILING-EDGE OF A FINITE WING WITH LEADING-EDGE TUBERCLES | ICAS2020_0979 |
| Fan, Y. | INCORPORTING KNOWLEDGE COVERAGE MEASUREMENT INTO KNOWLEDGE TRANSFORMATION FROM DATA FOR KNOWLEDGE ACCUMULATION | ICAS2020_0343 |
| Fan, L. | EXPERIMENTAL INVESTIGATION OF THE CHN-T1 MODEL IN FL-13 WIND TUNNEL OF CARDC AND DNW-LLF FACILITY | ICAS2020_0492 |
| Fan, Y. | RESEARCH OF LABYRINTH SEALS MEASUREMENT-BASED PROBABILITISTIC ANALYSIS METHOD FOR TURBOFAN INTERNAL AIR SYSTEM | ICAS2020_0531 |
| Fan, Z.L. | DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISK | ICAS2020_0713 |
| Fan, W.-C. | IMPROVED STOCHASTIC PERTURBATION ALGORITHM FOR GENERALIZED REPEATED EIGENVALUES PROBLEM BASED ON SURROGATE MODEL | ICAS2020_0780 |
| Fan, X.Q. | A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODY | ICAS2020_1099 |
| Fan, Z.L. | INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBER | ICAS2020_1185 |
| Fang, H. | EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS | ICAS2020_0147 |
| Fang, Y.-N. | IMPROVED STOCHASTIC PERTURBATION ALGORITHM FOR GENERALIZED REPEATED EIGENVALUES PROBLEM BASED ON SURROGATE MODEL | ICAS2020_0780 |
| Fedorov, A.V. | MECHANISMS OF NATURAL LAMINAR-TURBULENT TRANSITION ON AN UNSWEPT WING IN SUPERSONIC FLIGHT | ICAS2020_0657 |
| Fedorov, A. | NUMERICAL SIMULATION OF THREE-DIMENSIONAL DISTURBANCES EVOLUTION IN SUPERSONIC FLOW OVER A WAVY SURFACE | ICAS2020_0968 |
| Feng, J. | STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TESTING | ICAS2020_0039 |
| Feng, S. | PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTS | ICAS2020_0392 |
| Feng, H.H. | BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES | ICAS2020_0574 |
| Feng, X.-D. | RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED | ICAS2020_0661 |
| Feng, K. | STUDY ON THE METHOD OF DETERMINING SKIN WAVINESS REQUIREMENT OF CIVIL AIRCRAFT | ICAS2020_1065 |
| Ferretto, D. | THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE | ICAS2020_0493 |
| Ferretto, D. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Ferretto, D. | INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISER | ICAS2020_1195 |
| Fichera, S. | MODEL REDUCTION AND STOCHASTIC UPDATING OF A VIBRATING SYSTEM | ICAS2020_0916 |
| Figat, M. | LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE | ICAS2020_0030 |
| Fioriti, M. | ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT | ICAS2020_1258 |
| Fioriti, M. | ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES | ICAS2020_1259 |
| Franke, F. | MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONS | ICAS2020_0019 |
| Franzoni, F. | ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURES | ICAS2020_0337 |
| Fregnani, J.A.T.G. | AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER'S PROGRAM COST | ICAS2020_1005 |
| Froehler, B. | CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT | ICAS2020_0185 |
| Frulla, G. | APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS | ICAS2020_0454 |
| Fu, J. | VIRTUAL PROTOTYPING OF ELECTRICAL THSA FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS | ICAS2020_0196 |
| Fu, Y. | CONCEPT OF A NEW SYSTEM SYNTHESIZING METEOROLOGICAL AND OROGRAPHIC INFLUENCES ON THE AIRPLANE SAFE ENERGY ENVELOPE | ICAS2020_1193 |
| Fualdes, C. | THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS | ICAS2020_1235 |
| Fuchs, M. | FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESS | ICAS2020_0134 |
| Fujii, Y. | IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP | ICAS2020_0557 |
| Funes Sebastian, D.E. | EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION | ICAS2020_0171 |
| Funes Sebastian, D.E. | STUDY OF THE BENEFITS OF A SEMI-MORPHING WING CONCEPT | ICAS2020_0216 |
| Fusaro, R. | THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE | ICAS2020_0493 |
| Fusaro, R. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Fusaro, R. | TECHNOLOGY ROADMAPS FOR THE DEVELOPMENT OF FUTURE HIGH-SPEED TRANSPORTATION SYSTEMS | ICAS2020_0958 |
| Fusaro, R. | INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISER | ICAS2020_1195 |
| Gallani, M.A. | IMPLEMENTATION OF DISTRIBUTED ELECTRIC PROPULSION ON A GENERAL AVIATION AIRCRAFT | ICAS2020_1025 |
| Gao, L.M. | A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS | ICAS2020_0036 |
| Gao, Z.H. | SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHOD | ICAS2020_0094 |
| Gao, F.-L. | MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSOR | ICAS2020_0138 |
| Gao, Y.W. | APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITION | ICAS2020_0264 |
| Gao, Z.-H. | TRANSITION PREDICTION FOR TRANSPORT AIRCRAFT CONFIGURATIONS BASED ON OVERSET GRID | ICAS2020_0286 |
| Gao, Z.-J. | EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR THE “AEROSTRUCT” WING OPTIMIZATION PLATFORM | ICAS2020_0350 |
| Gao, Z.-H. | STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEM | ICAS2020_0366 |
| Gao, Z.H. | DECOUPLING CONTROL LAW DESIGN FOR OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWING | ICAS2020_0384 |
| Gao, F.L. | EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR | ICAS2020_0429 |
| Gao, Y.-W. | ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL | ICAS2020_0516 |
| Gao, F. | THE RESEARCH ON PROPELLER NOISE PREDICTION METHOD FOR TURBOPROP AIRCRAFT | ICAS2020_0544 |
| Gao, Z. | AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION | ICAS2020_0591 |
| Gao, Z.-H. | EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2020_0620 |
| Gao, X.L. | RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTION | ICAS2020_0909 |
| Gao, J.X. | NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTS | ICAS2020_1183 |
| Gao, J.X. | NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WING | ICAS2020_1240 |
| Gao, Z. | AN ACCELERATION METHODOLOGY BASED ON DISTURBANCE REGION UPDATE METHOD FOR STEADY COMPRESSIBLE FLOWS | ICAS2020_1263 |
| Gao, Z.X. | LARGE-EDDY SIMULATION OF A SWIRLING AVIATION KEROSENE SPRAY FLAME USING 3-COMPONENT SURROGATE FUELS | ICAS2020_1264 |
| Gao, L. | MODEL BASED DESIGN AND PRACTICE FOR AVIONICS SYSTEM | ICAS2020_1298 |
| Gao, X.H. | IMPLEMENTATION MECHANISM OF UAS INTEROPERABILITY BASED ON ARCHITECTURE META-MODEL | ICAS2020_1308 |
| Gardi, A. | A NOVEL DETECT-AND-AVOID APPROACH FOR UAS IN URBAN ENVIRONMENTS | ICAS2020_0970 |
| Gardi, A. | ARTIFICIAL INTELLIGENCE AND HUMAN-MACHINE INTERACTIONS FOR STREAM-BASED AIR TRAFFIC FLOW MANAGEMENT | ICAS2020_1009 |
| Garry, K. | TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSER | ICAS2020_0081 |
| Gavel, H. | CONNECTING SYSTEM SIMULATION TO AIRCRAFT CONCEPT DEVELOPMENT | ICAS2020_1229 |
| Gavva, L.M. | KINEMATIC MODEL OF REFINED THEORY AND EXACT ANALYTICAL SOLUTIONS OF STATIC AND BUCKLING PROBLEMS OF STRUCTURALLY-ANISOTROPIC COMPOSITE PANELS OF AIRCRAFT | ICAS2020_0294 |
| Ge, W. | VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING | ICAS2020_0284 |
| Gebhardt, A. | TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFT | ICAS2020_1260 |
| Geisler, R. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Gendre, D. | REAL TIME IMPACT LOCALIZATION USING MODAL SUPERPOSITION - APPLICATION TO A COMPOSITE AIRCRAFT FUSELAGE | ICAS2020_0125 |
| Geng, X. | ANALYSIS OF THRUST-SCALED ACOUSTIC EMISSIONS OF AIRCRAFT PROPELLERS AND THEIR DEPENDENCE ON PROPULSIVE EFFICIENCY | ICAS2020_0751 |
| Geng, X. | TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGY | ICAS2020_1170 |
| Giacobini de Souza, A. | OPTIMIZATION OF LONGITUDINAL CONTROL OF AN AGRICULTURAL UAV USING LQR-PID CONTROL | ICAS2020_1187 |
| Gibson, T. | BLADE - NATURAL LAMINAR FLOW FLIGHT TESTING | ICAS2020_0220 |
| Gil Annes da Silva, R. | OPTIMIZATION OF LONGITUDINAL CONTROL OF AN AGRICULTURAL UAV USING LQR-PID CONTROL | ICAS2020_1187 |
| Gili, P. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS | ICAS2020_1219 |
| Gili, A. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS | ICAS2020_1219 |
| Gili, P. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION | ICAS2020_1222 |
| Go, T.H. | NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER | ICAS2020_0555 |
| Goertz, S. | ROBUST DESIGN OF 3D SHOCK CONTROL BUMPS TO TRANSPORT AIRCRAFT UNDER REALISTIC UNCERTAINTIES | ICAS2020_0279 |
| Góes, L.C.S. | IMPLEMENTATION OF DISTRIBUTED ELECTRIC PROPULSION ON A GENERAL AVIATION AIRCRAFT | ICAS2020_1025 |
| Goetzendorf-Grabowski, T. | LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE | ICAS2020_0030 |
| Goinis, G. | THE POTENTIAL OF CASING TREATMENTS FOR TRANSONIC COMPRESSORS: EVALUATION BASED ON AXIAL-SLOT AND ROTOR BLADE OPTIMIZATION | ICAS2020_1054 |
| Golberg, F.D. | THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS | ICAS2020_0881 |
| Goldhahn, E. | DESIGN AND PERFORMANCE OF A LOW FAN-PRESSURE-RATIO PROPULSION SYSTEM | ICAS2020_1058 |
| Gomes Pereira Sarmento, A. | OPTIMIZATION OF LONGITUDINAL CONTROL OF AN AGRICULTURAL UAV USING LQR-PID CONTROL | ICAS2020_1187 |
| Gómez-Escalonilla Martín, J. | A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES | ICAS2020_0562 |
| Gong, C. | EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS | ICAS2020_0147 |
| Gong, A.L. | NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH-SPEED VEHICLES | ICAS2020_1157 |
| Gonzalez, R.C. | ON THE ASSESSMENT OF CFD METHODS FOR VORTICAL FLOWS | ICAS2020_0080 |
| Gordin, M.V. | CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS | ICAS2020_0974 |
| Gori, O. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Gori, O. | INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISER | ICAS2020_1195 |
| Gottfried, S. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Goutaudier, D. | REAL TIME IMPACT LOCALIZATION USING MODAL SUPERPOSITION - APPLICATION TO A COMPOSITE AIRCRAFT FUSELAGE | ICAS2020_0125 |
| Gowree, E.R. | VIBRATION INDUCED EXCITATION OF INSTABILITY WAVES IN A BLASIUS FLOW | ICAS2020_0890 |
| Granlund, R. | DESIGN OF SIMULATION-BASED PILOT TRAINING SYSTEMS USING MACHINE LEARNING AGENTS | ICAS2020_0130 |
| Grava, A. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION | ICAS2020_1222 |
| Grendene, S. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| Grewe, V. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Grigorev, A.V. | RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIME | ICAS2020_0963 |
| Grilli, G. | DESIGN OF A VERTICAL DITCHING TEST | ICAS2020_0763 |
| Gros, V. | CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM | ICAS2020_0659 |
| Gu, Z. | STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TESTING | ICAS2020_0039 |
| Gu, W.-T. | THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT | ICAS2020_0181 |
| Gu, J. | THE RESEARCH ON PROPELLER NOISE PREDICTION METHOD FOR TURBOPROP AIRCRAFT | ICAS2020_0544 |
| Guan, L. | CONCEPTUAL DESIGN OF A FIXED-WING AQUATIC UAV USING KNOWLEDGE BASED ENGINEERING | ICAS2020_0154 |
| Guelailia, A. | PASSIVE FLEXIBLE WINGTIP AREA FOR IMPROVING AIRLINERS CRUISE EFFICIENCY AND GUST ALLEVIATION | ICAS2020_0360 |
| Guenov, M.D. | CLOUD-BASED ENVIRONMENT FOR AIRCRAFT DESIGN COLLABORATION | ICAS2020_1123 |
| Gueraiche, D. | PASSIVE FLEXIBLE WINGTIP AREA FOR IMPROVING AIRLINERS CRUISE EFFICIENCY AND GUST ALLEVIATION | ICAS2020_0360 |
| Guerra Crespo, J.J. | EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION | ICAS2020_0171 |
| Guha, A. | METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WING | ICAS2020_0085 |
| Gui, Y.W. | MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION | ICAS2020_0805 |
| Gui, Y.W. | A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTS | ICAS2020_0833 |
| Gui, Y.-W. | GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOW | ICAS2020_1073 |
| Gui, Y.W. | A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTION | ICAS2020_1160 |
| Gui, Y.-W. | COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION | ICAS2020_1176 |
| Guo, J. | STATISTICS AND ANALYSIS OF MANUFACTURING DEFECTS AND DAMAGE OF HELICOPTER COMPOSITE STRUCTURES | ICAS2020_0188 |
| Guo, Q.-L. | STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATOR | ICAS2020_0305 |
| Guo, T. | VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL | ICAS2020_0313 |
| Guo, J. | AN ADJOINT-BASDF AERO-STRUCTURAL DESIGN OPTIMIZATION METHOD USING DYNAMIC MESH TECHNOLOGY | ICAS2020_0317 |
| Guo, Y. | RESEARCH ON SELECTION METHODS FOR AIRCRAFT LANDING GEAR SYSTEM HEALTH FEATURE PARAMETERS | ICAS2020_0581 |
| Guo, S.-P. | RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERING | ICAS2020_0633 |
| Guo, S. | AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE | ICAS2020_0663 |
| Guo, W. | RESEARCH ON TRAJECTORY OPTIMIZATION TECHNOLOGY CONSIDERING METEOROLOGICAL INFORMATION PREDICTION | ICAS2020_0823 |
| Guo, Y. | COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING | ICAS2020_0836 |
| Guo, H. | MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORK | ICAS2020_0849 |
| Guo, Q. | AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGING | ICAS2020_1132 |
| Guo, Q.-L. | A NUMEIRCAL PREDICTION OF THE AIRCRAFT ICING METEOROLOGICAL ENVIRONMENT | ICAS2020_1156 |
| Guo, L.B. | NUMERICAL SIMULATION OF RIDGE ICE AND AERODYNAMIC EFFECT UNDER THERMAL ANTI-ICE | ICAS2020_1179 |
| Görtz, S. | MULTI-AXIS MANEUVER SIMULATION FOR SYSTEM IDENTIFICATION OF FLEXIBLE TRANSPORT AIRCRAFT BY HIGH-FIDELITY METHODS | ICAS2020_0206 |
| Görtz, S. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Haixia, L. | STUDY ON THE AIRWORTHINESS AND COMFORTABLENESS REQUIREMENTS OF AIRCRAFT CABIN AIR CONTAMINATIONS | ICAS2020_0761 |
| Han, Y.Z. | A STRUCTURE DESIGN OF CFRP REAR PRESSURE BULKHEAD WITHOUT STIFFENERS | ICAS2020_0109 |
| Han, J.-H. | EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK-ABSORBING INSERT | ICAS2020_0157 |
| Han, J.H. | EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACK | ICAS2020_0182 |
| Han, C.-L. | FLIGHT MANAGEMENT SYSTEM REQUIREMENT ANALYSIS FOR TRAJECTORY BASED OPERATION | ICAS2020_0292 |
| Han, Z.-H. | EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR THE “AEROSTRUCT” WING OPTIMIZATION PLATFORM | ICAS2020_0350 |
| Han, Z.-H. | NATURAL-LAMINAR-FLOW AIRFOIL DESIGN OPTIMIZATION CONSIDERING CROSSFLOW INSTABILITY WHEN CONFIGURED ON A SWEPT WING | ICAS2020_0472 |
| Han, Z.-H. | AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHING | ICAS2020_0476 |
| Han, J.J. | EXPERIMENTAL STUDY ON CRITICAL HEAT FLUX CHARACTERISTICS OF R134A FLOW BOILING IN A HORIZONTAL 2.1 MM TUBE UNDER HYPERGRAVITY | ICAS2020_0510 |
| Han, Z.-H. | FAST METHOD AND AN INTEGRATED CODE FOR SONIC BOOM PREDICTION OF SUPERSONIC COMMERCIAL AIRCRAFT | ICAS2020_0600 |
| Han, Z.-H. | IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC MODELING PROBLEMS | ICAS2020_0787 |
| Han, Z.-H. | DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS | ICAS2020_0839 |
| Han, Z.-H. | MULTIFIDELITY AERODYNAMIC/STEALTH DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT | ICAS2020_0878 |
| Hang, X. | APPLICATION OF REINFORCEMENT LEARNING IN 1-D AERODYNAMIC DESIGN OF AXIAL COMPRESSOR | ICAS2020_0678 |
| Hanjie, J. | DESIGN OF A HYBRID VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO CIVIL AVIATION AIR TRAFFIC CONTROL SYSTEM | ICAS2020_0468 |
| Hao, L.-S. | ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL | ICAS2020_0516 |
| Hao, B. | A STUDY ON TRAINING NEEDS ANALYSIS (TNA) METHOD FOR MILITARY AIRCRAFT | ICAS2020_0602 |
| Hao, X. | THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDE-BODY CIVIL TRANSPORT | ICAS2020_0676 |
| Hao, D. | NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODEL | ICAS2020_0796 |
| Harla, R. | INVESTIGATIONS ON LANDING GEAR SHOCK ABSORBER ACTIVE FORCE CONTROL | ICAS2020_0513 |
| Hartmann, J. | FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFT | ICAS2020_0238 |
| Hauglustaine, D. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Hayashi, M. | ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME | ICAS2020_0985 |
| He, G.Y. | THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLE | ICAS2020_0052 |
| He, Y. | ON AIRCRAFT OPERATIONAL INTEGRITY | ICAS2020_0225 |
| He, C.-J. | COMPREHENSIVE REDUNDANCY MANAGEMENT AND VERIFICATION STRATEGY FOR TASK-BASED AIR MANAGEMENT SYSTEM | ICAS2020_0485 |
| He, F. | EXPERIMENTAL STUDY ON SUPERSONIC CAVITY ACOUSTICS | ICAS2020_0708 |
| He, Y.Q. | A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONS | ICAS2020_0712 |
| He, R. | FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE | ICAS2020_1032 |
| He, S.M. | ADRC BASED HIGH MANEUVERING FLIGHT CONTROL LAW DESIGN FOR UAV | ICAS2020_1088 |
| He, K. | NONLINEAR UNSTEADY AERODYNAMIC MODELING AND LONGITUDINAL STABILITY ANALYSIS FOR AN AIRCRAFT MODEL | ICAS2020_1104 |
| He, S. | MULTI-UAV TRAJECTORY PLANNING BASED ON COORDINATION VARIABLES | ICAS2020_1139 |
| He, S. | LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINT | ICAS2020_1145 |
| He, Y. | LARGE-EDDY SIMULATION OF A SWIRLING AVIATION KEROSENE SPRAY FLAME USING 3-COMPONENT SURROGATE FUELS | ICAS2020_1264 |
| Heckmeier, F.M. | TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON WAKE VORTEX IMPACT BY OSCILLATING FLAPS | ICAS2020_0595 |
| Heidari Soreshjani, M. | MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT WINGLET | ICAS2020_0402 |
| Heintz, F. | DESIGN OF SIMULATION-BASED PILOT TRAINING SYSTEMS USING MACHINE LEARNING AGENTS | ICAS2020_0130 |
| Herman, M. | THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS | ICAS2020_1235 |
| Hernandes, J.A. | FLUID-STRUCTURE INTERACTION ANALYSIS OF ELASTIC EFFECTS OF A TRANSPORT AIRCRAFT FITTED WITH WINGLETS | ICAS2020_0999 |
| Hernandes, J.A. | AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER'S PROGRAM COST | ICAS2020_1005 |
| Hernandez, S. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Hernik, B. | LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE | ICAS2020_0030 |
| Herrera de la Cruz , J. | A NOVEL APPROACH FOR TURNAROUND TIME ALLOCATION BASED ON REINFORCEMENT LEARNING | ICAS2020_1015 |
| Herzog, N. | ANALYSIS OF A WING-TIP-MOUNTED SMALL-SCALE PROPELLER CONFIGURATION UNDER NON-AXIAL INFLOW CONDITIONS | ICAS2020_0116 |
| Hesse, C. | FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESS | ICAS2020_0134 |
| Hesse, C. | CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT | ICAS2020_0185 |
| Higasa, K. | DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS | ICAS2020_0032 |
| Hilton, S. | A NOVEL DETECT-AND-AVOID APPROACH FOR UAS IN URBAN ENVIRONMENTS | ICAS2020_0970 |
| Hirschmann, K. | EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS | ICAS2020_0227 |
| Hofmann, J. | AERODYNAMIC AND STRUCTURAL MODELING IN THE ROTORCRAFT MULTI-PHYSICS SIMULATION VAST | ICAS2020_0584 |
| Hokamoto, S. | MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMS | ICAS2020_0945 |
| Hornung, M. | COST AND BENEFIT OF SCHEDULED STRUCTURAL HEALTH MONITORING FOR COMMERCIAL AIRCRAFT | ICAS2020_0117 |
| Hornung, M. | PROPELLER WAKE - OBJECT INTERACTION USING A FREE WAKE MODEL UTILIZING LOCAL MESH SEPARATION | ICAS2020_0209 |
| Hornung, M. | DEVELOPMENTS TOWARDS A TOOLCHAIN FOR UAV FLIGHT DYNAMIC MODELS IN EARLY DESIGN | ICAS2020_0552 |
| Hornung, M. | STATIC AEROELASTIC TAILORING OF A HIGH-ASPECT-RATIO-WING FOR A SAILPLANE WITH A FORWARD MORPHING WING SECTION | ICAS2020_0575 |
| Hornung, M. | FLIGHT TESTING OF 65KG T-FLEX SUBSCALE DEMONSTRATOR | ICAS2020_0707 |
| Hou, P. | THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE | ICAS2020_0095 |
| Hou, N. | DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINE | ICAS2020_0401 |
| Hozumi, K. | ENDURANCE ANALYSIS OF BATTERY-POWERED MULTICOPTERS: DERIVATION OF PROPER CUT-OFF VOLTAGE USING DC MOTOR MODEL | ICAS2020_0769 |
| Hu, X.-Z. | PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNEL | ICAS2020_0418 |
| Hu, H. | GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHOD | ICAS2020_0489 |
| Hu, D. | GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHOD | ICAS2020_0489 |
| Hu, B. | ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL | ICAS2020_0516 |
| Hu, C. | THE RESEARCH ON PROPELLER NOISE PREDICTION METHOD FOR TURBOPROP AIRCRAFT | ICAS2020_0544 |
| Hu, T. | ANALYSIS OF THRUST-SCALED ACOUSTIC EMISSIONS OF AIRCRAFT PROPELLERS AND THEIR DEPENDENCE ON PROPULSIVE EFFICIENCY | ICAS2020_0751 |
| Hu, X. | RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DIS | ICAS2020_0865 |
| Hu, J. | RESEARCH ON FAULT DIAGNOSIS AND FAILURE RECONFIGURATION OF FLUSH AIR DATA SENSING | ICAS2020_1064 |
| Hu, S. | AN ACCELERATION METHODOLOGY BASED ON DISTURBANCE REGION UPDATE METHOD FOR STEADY COMPRESSIBLE FLOWS | ICAS2020_1263 |
| Hua, J. | AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION | ICAS2020_0071 |
| Hua, R. | SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRID | ICAS2020_0315 |
| Huai, Y. | AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVES | ICAS2020_0794 |
| Huang, H. | STATISTICS AND ANALYSIS OF MANUFACTURING DEFECTS AND DAMAGE OF HELICOPTER COMPOSITE STRUCTURES | ICAS2020_0188 |
| Huang, J.F. | DESIGN AND PERFORMANCE RESEARCH OF ARTIFICIAL ELECTROMAGNETIC STRUCTURE WITH TRANSMISSION AND ABSORPTION CHARACTERISTICS | ICAS2020_0208 |
| Huang, X.-X. | RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUE | ICAS2020_0273 |
| Huang, J.-T. | AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING | ICAS2020_0348 |
| Huang, J.-T. | STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEM | ICAS2020_0366 |
| Huang, J. | ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAM | ICAS2020_0378 |
| Huang, J.-T. | EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIOURS OF RESOLVENT MODE | ICAS2020_0414 |
| Huang, T. | STRUCTURAL HEALTH MONITORING OF SANDWICH STRUCTURES WITH LATTICE CORES IN AIRCRAFT DESIGN: CHALLENGES AND POTENTIAL | ICAS2020_0518 |
| Huang, W. | AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE | ICAS2020_0663 |
| Huang, Z. | SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODEL | ICAS2020_0928 |
| Huang, H.Y. | STUDY ON THE OUT-OF-PLANE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT 350°C | ICAS2020_1072 |
| Huang, Y.Z. | LARGE-EDDY SIMULATION OF A SWIRLING AVIATION KEROSENE SPRAY FLAME USING 3-COMPONENT SURROGATE FUELS | ICAS2020_1264 |
| Huang, W.-D. | ASCENT TRAJECTORY OPTIMIZATION OF HYPERSONIC VEHICLE USING SWARM INTELLIGENT METHOD | ICAS2020_1266 |
| Hull, A. | QUANTIFICATION OF OPERATIONAL EFFECTIVENESS FOR TECHNOLOGY EVALUATION | ICAS2020_1241 |
| Hupe, J. | ICAO ADDRESSING CLIMATE CHANGE AND WILDFIRES | ICAS2020_1311 |
| Hwang, D.-H. | EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK-ABSORBING INSERT | ICAS2020_0157 |
| Hühne, C. | MODELS AND METHODS FOR DRONE STRIKE LOAD PREDICTIONS | ICAS2020_0019 |
| Hällqvist, R. | CONNECTING SYSTEM SIMULATION TO AIRCRAFT CONCEPT DEVELOPMENT | ICAS2020_1229 |
| Häßy, J. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Hörnschemeyer, R. | DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL AERODYNAMIC LIFT MECHANISM | ICAS2020_0863 |
| Iavecchia, P. | APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS | ICAS2020_0454 |
| Iavecchia, P. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| Ii, Y. | THE FLOW AND HEAT TRANSFER OF ANALYSIS TO ANNULAR CAVITY IN ENGINE CASE | ICAS2020_1251 |
| Ikeda, T. | ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT FOR MORPHING WINGS | ICAS2020_0540 |
| Ikeda, T. | IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP | ICAS2020_0557 |
| Ilic, C. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Illenberger, G. | STATIC AEROELASTIC TAILORING OF A HIGH-ASPECT-RATIO-WING FOR A SAILPLANE WITH A FORWARD MORPHING WING SECTION | ICAS2020_0575 |
| Imamura, T. | UNSTEADY FLOW SIMULATION AROUND MAIN LANDING GEAR USING HIERARCHICAL CARTESIAN GRID METHOD WITH IMMERSED BOUNDARY METHOD | ICAS2020_0677 |
| Indelicato, R. | S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE | ICAS2020_0455 |
| Iodice, P. | ON-BOARD SYSTEM ARCHITECTURES FOR HYBRID/ALL-ELECTRIC REGIONAL AIRCRAFT | ICAS2020_1258 |
| Irgaleev, I.K. | THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERS | ICAS2020_0176 |
| Ishikawa, T. | IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP | ICAS2020_0557 |
| Ishioka, S. | LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV | ICAS2020_0150 |
| Ishmuratov, F. | EFFECTS OF ELASTICITY, VISCOSITY AND BOUNDARY LAYER TRANSITION ON AEROELASTICITY CHARACTERISTICS OF LAMINAR WINGS | ICAS2020_0961 |
| Isnardi, I. | MODEL REDUCTION AND STOCHASTIC UPDATING OF A VIBRATING SYSTEM | ICAS2020_0916 |
| Ispir, A.C. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Isyanov, A. | THE CAPABILITIES OF AUTOMATION OF MDAO PROBLEM STATEMENT AT COLLABORATIVE CONCEPTUAL DESIGN OF THE PROPULSION SYSTEM USING OPEN SOURCE SOFTWARE TOOLS | ICAS2020_1022 |
| Itoh, E. | DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS | ICAS2020_0032 |
| Itoh, Y. | ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF PROPELLER AT LOW ADVANCE RATIO USING A WHIRING ARM | ICAS2020_0470 |
| Iuspa, L. | OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE | ICAS2020_0164 |
| Ivanov, M. | ADVANCED WEAK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING | ICAS2020_0037 |
| Ivanov, I.I. | AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONS | ICAS2020_1242 |
| Jahangirian, A. | MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT FUSELAGE | ICAS2020_0232 |
| Jahangirian, A. | MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT WINGLET | ICAS2020_0402 |
| Jansen, T.M. | LANDING PLATFORM FOR URBAN AIR MOBILITY VEHICLES INTEGRATED INTO PARKING LOT INFRASTRUCTURE IN DENSELY BUILT-UP AREAS | ICAS2020_1217 |
| Ji, W. | EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS | ICAS2020_0147 |
| Ji, W.T. | FLOW AND HEAT TRANSFER MECHANISM OF JET IMPINGEMENT COOLING ONTO MID-CHORD REGINE OF TWISTED BLADE | ICAS2020_1106 |
| Jia, Z. | BROADBAND MICROWAVE ABSORBING HONEYCOMB CORE MATERIAL WITH ACTIVE CARBON AS DELEGATES | ICAS2020_0308 |
| Jia, Z.Y. | A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEM | ICAS2020_0764 |
| Jia, H.-Y. | NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODEL | ICAS2020_0796 |
| Jia, Q. | RESEARCH ON FAULT DIAGNOSIS AND FAILURE RECONFIGURATION OF FLUSH AIR DATA SENSING | ICAS2020_1064 |
| Jia, S. | A POLE CONFIGURATION CONTROLLER FOR FIXED HEIGHT CONTROL OF TILT ROTOR AIRCRAFT | ICAS2020_1228 |
| Jiang, Y.M. | RESEARCH ON THE PRESSURE COMFORT OF PILOT HELMETS | ICAS2020_0180 |
| Jiang, M. | CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFT | ICAS2020_0231 |
| Jiang, Y. | WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONS | ICAS2020_0483 |
| Jiang, C. | APPLICATION OF REINFORCEMENT LEARNING IN 1-D AERODYNAMIC DESIGN OF AXIAL COMPRESSOR | ICAS2020_0678 |
| Jiang, M. | EXPERIMENTAL STUDY ON SUPERSONIC CAVITY ACOUSTICS | ICAS2020_0708 |
| Jiang, X. | SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TEST | ICAS2020_0744 |
| Jiang, W.Y. | MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOW | ICAS2020_1078 |
| Jiang, B. | NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAP | ICAS2020_1149 |
| Jiang, C. | AN ACCELERATION METHODOLOGY BASED ON DISTURBANCE REGION UPDATE METHOD FOR STEADY COMPRESSIBLE FLOWS | ICAS2020_1263 |
| Jiang, C.W. | LARGE-EDDY SIMULATION OF A SWIRLING AVIATION KEROSENE SPRAY FLAME USING 3-COMPONENT SURROGATE FUELS | ICAS2020_1264 |
| Jiao, J. | RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES | ICAS2020_0162 |
| Jiao, J. | AERODYNAMIC AND STRUCTURAL DESIGN OF THE COMPOSITE PROPELLER FOR NEAR SPACE VEHICLES | ICAS2020_0722 |
| Jiao, Z.X. | ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION | ICAS2020_1074 |
| Jiao, Z.X. | MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOW | ICAS2020_1078 |
| Jiao, Z.X. | ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGS | ICAS2020_1171 |
| Jin, H. | EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR | ICAS2020_0291 |
| Jin, L. | RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM | ICAS2020_0413 |
| Jin, H.-L. | APPLICATION OF A SKEWED-SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSOR | ICAS2020_0543 |
| Jin, H.-L. | DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSOR | ICAS2020_0632 |
| Jin, H.-L. | MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGN | ICAS2020_0965 |
| Jin, D. | STUDY ON THE METHOD OF DETERMINING SKIN WAVINESS REQUIREMENT OF CIVIL AIRCRAFT | ICAS2020_1065 |
| Jin, W. | FLOW AND HEAT TRANSFER MECHANISM OF JET IMPINGEMENT COOLING ONTO MID-CHORD REGINE OF TWISTED BLADE | ICAS2020_1106 |
| Jin, T. | LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINT | ICAS2020_1145 |
| Jin, W. | NUMERICAL STUDY ON COOLING CHARACTERISTICS IN CHANNELS WITH PIN FIN ARRAYS UNDER HIGH TEMPERATURE/PRESSURE CONDITIONS | ICAS2020_1151 |
| Jing, L. | ANALYSIS AND SOLUTION RESEARCH OF THE AIR DATA LOSSFROM AIRCRAFT FOR ENGINE CONTROL | ICAS2020_0004 |
| Jing, L. | THE STUDY OF UNMANNED AERIAL VEHICLE FLYING QUALITIES FLIGHT TEST METHOD BASED ON TIME-DELAY EVALUATION | ICAS2020_0710 |
| Johansson, C. | CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS | ICAS2020_0110 |
| Jokinen, J. | THE INFLUENCE OF THE NUMBER OF ADHESIVE PLIES (FM 300-2) ON FRACTURE PROPERTIES | ICAS2020_0295 |
| Jokinen, J. | ADJUSTED SHAPES OF ADHESIVELY BONDED REPAIR PATCHES FOR THE EARLY INDICATION OF DEBOND IN FIGHTER AIRCRAFT STRUCTURES | ICAS2020_0297 |
| Jokinen, J. | REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACT | ICAS2020_1014 |
| Jouannet, C. | FUTURE PERSPECTIVES ON SOSE | ICAS2020_1291 |
| Julian, M. | DESIGN AND PERFORMANCE OF A LOW FAN-PRESSURE-RATIO PROPULSION SYSTEM | ICAS2020_1058 |
| Julistina, R. | FURTHER DEVELOPMENT OF COMPUTATIONAL STUDY ON COANDA BLANKET CURVATURE EFFECTS ON HALF SPHERICAL COANDA DEVICE | ICAS2020_0906 |
| Jung, S. | AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING | ICAS2020_0959 |
| Juracka, J. | BIRD STRIKE SIMULATIONS IN MSC.SOFTWARE: CORRELATION BETWEEN THE EXPERIMENTS AND SIMULATIONS | ICAS2020_0017 |
| Jünemann, M. | VALIDATION OF AN AERODYNAMIC MODEL FOR THE ANALYSIS OF SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRICAL PROPULSION | ICAS2020_0145 |
| Kale, U. | TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRID-ELECTRIC AIRCRAFT | ICAS2020_0635 |
| Kale, U. | OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT | ICAS2020_0638 |
| Kan, A.V. | CREATING A MULTI-FUNCTIONAL EXPERT ANALYTICAL SYSTEM IN THE AIRCRAFT INDUSTRY AND THE FORMATION OF GENERAL REQUIREMENTS | ICAS2020_0857 |
| Kanerva, M. | THE INFLUENCE OF THE NUMBER OF ADHESIVE PLIES (FM 300-2) ON FRACTURE PROPERTIES | ICAS2020_0295 |
| Kanerva, M. | ADJUSTED SHAPES OF ADHESIVELY BONDED REPAIR PATCHES FOR THE EARLY INDICATION OF DEBOND IN FIGHTER AIRCRAFT STRUCTURES | ICAS2020_0297 |
| Kanerva, M. | REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACT | ICAS2020_1014 |
| Kang, J. | STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTION | ICAS2020_0598 |
| Kang, M.-H. | HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILS | ICAS2020_1125 |
| Karas, O. | EFFECTS OF ELASTICITY, VISCOSITY AND BOUNDARY LAYER TRANSITION ON AEROELASTICITY CHARACTERISTICS OF LAMINAR WINGS | ICAS2020_0961 |
| Karskanov, S.A. | PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSET | ICAS2020_0949 |
| Kato, F. | DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS | ICAS2020_0032 |
| Kavabata, L. | ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME | ICAS2020_0985 |
| Kazarinov, G.G. | CREATING A MULTI-FUNCTIONAL EXPERT ANALYTICAL SYSTEM IN THE AIRCRAFT INDUSTRY AND THE FORMATION OF GENERAL REQUIREMENTS | ICAS2020_0857 |
| Khaletskii, I. | METHODS OF PROGRAMMED THRUST MANAGEMENT FOR NOISE REDUCTION OF SUPERSONIC CIVIL AIRCRAFT | ICAS2020_1017 |
| Khrabrov, A.N. | INFLUENCE OF AERODYNAMIC ASYMMETRY ON SPIN PARAMETERS OF THE COMMON RESEARCH MODEL | ICAS2020_0532 |
| Kier, T. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Kim, S. | AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING | ICAS2020_0959 |
| Kim, Y. | AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING | ICAS2020_0959 |
| Kirby, M. | MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS | ICAS2020_1237 |
| Kiszkowiak, L. | EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS | ICAS2020_0101 |
| Kiszkowiak, L. | THE USE OF REVERSE ENGINEERING AND COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A LOW COST SATELLITE LAUNCH SYSTEM | ICAS2020_1221 |
| Kleinert, J. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Klimmek, T. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Kling, F. | OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT | ICAS2020_0638 |
| Knopp, T. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Knöös Franzén, L. | CONNECTING SYSTEM SIMULATION TO AIRCRAFT CONCEPT DEVELOPMENT | ICAS2020_1229 |
| Koeberle, S.J. | DEVELOPMENTS TOWARDS A TOOLCHAIN FOR UAV FLIGHT DYNAMIC MODELS IN EARLY DESIGN | ICAS2020_0552 |
| Koeberle, S.J. | FLIGHT TESTING OF 65KG T-FLEX SUBSCALE DEMONSTRATOR | ICAS2020_0707 |
| Kolman, E.M. | SPECIALIZED SOFTWARE DEVELOPMENT FOR BUILDING BLOCK APPROACH INTEGRATION IN FULL-SCALE STATIC TESTS | ICAS2020_1117 |
| Kong, W. | RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLES | ICAS2020_0851 |
| Kong, X.-F. | AN INTEGRATED METHOD FOR ACCURATE IDENTIFICATION AND DYNAMIC MONITORING OF BUILDINGS IN AERODROME OBSTACLE FREE SPACE | ICAS2020_1061 |
| Kong, Y. | NONLINEAR UNSTEADY AERODYNAMIC MODELING AND LONGITUDINAL STABILITY ANALYSIS FOR AN AIRCRAFT MODEL | ICAS2020_1104 |
| Kong, C.H. | FAST ITERATIVE SIMULATION OF AIRLINER WING PLANFORM CONCEPTUAL DESIGN | ICAS2020_1155 |
| Korzhnev, V. | EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS | ICAS2020_0750 |
| Kostenko, V. | STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION | ICAS2020_0106 |
| Kou, M. | A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT | ICAS2020_0097 |
| Kratt, E. | DEVELOPMENT OF ADVANCED DESIGNS OF GAS TURBINE ENGINES FROM POWDER COMPOSITIONS | ICAS2020_0924 |
| Kreerenko, O. | SYNERGETIC CONTROLS OF THE SYSTEM “CARRIER AIRCRAFT - UPPER-STAGE ROCKET“ | ICAS2020_1001 |
| Krob, D. | TOWARDS AGILE SYSTEMS ENGINEERING: AN ITERATIVE & COLLABORATIVE APPROACH FOR COMPLEX SYSTEMS DEVELOPMENT | ICAS2020_1294 |
| Krumbein, A. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Krus, P. | CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS | ICAS2020_0110 |
| Krus, P. | GAZE-BASED INTERFACE FOR FLIGHT CONTROL: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEM | ICAS2020_0645 |
| Krus, P. | HYBRID MODELLING FOR FULL MISSION SIMULATION | ICAS2020_0980 |
| Krus, P. | FITT’S LAW WITH EYE TRACKING ON A FLIGHT SIMULATOR COCKPIT | ICAS2020_0982 |
| Krus, P. | AN ONTOLOGICAL APPROACH FOR CLASSIFYING AIRCRAFT ACTUATORS | ICAS2020_1209 |
| Krus, P. | EVALUATION ASPECT MAPPING FOR ACTUATION SYSTEM DESIGN | ICAS2020_1210 |
| Krutov, A.A. | STUDY ON AERODYNAMIC CHARACTERISTICS OF LIGHT CONVERTIBLE AIRCRAFT MODEL | ICAS2020_0810 |
| Krzysiak, A. | EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS | ICAS2020_0101 |
| Kudrov, M.A. | EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE | ICAS2020_0894 |
| Kurulyuk, D.V. | SPECIALIZED SOFTWARE DEVELOPMENT FOR BUILDING BLOCK APPROACH INTEGRATION IN FULL-SCALE STATIC TESTS | ICAS2020_1117 |
| Kuvshinov, V.M. | DESIGN TECHNIQUE OF INTEGRAL ALGORITHMS OF HELICOPTER FBW CONTROL SYSTEM | ICAS2020_0534 |
| Kuzmina, S. | EFFECTS OF ELASTICITY, VISCOSITY AND BOUNDARY LAYER TRANSITION ON AEROELASTICITY CHARACTERISTICS OF LAMINAR WINGS | ICAS2020_0961 |
| Källström, J. | DESIGN OF SIMULATION-BASED PILOT TRAINING SYSTEMS USING MACHINE LEARNING AGENTS | ICAS2020_0130 |
| La Rocca, G. | FUTURE PERSPECTIVES ON KBE & AI | ICAS2020_1289 |
| Labzin, I. | EXPERIENCE OF BELARUS IN USING HELICOPTER TECHNOLOGY FOR FOREST FIREFIGHTING | ICAS2020_1313 |
| Lakshmi, R.V. | SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOY | ICAS2020_1052 |
| Lammers, K. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Lang, X. | COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING | ICAS2020_0836 |
| Lang, X.-Y. | NUMERICAL SIMULATION OF PITCHING MOTION EFFECTS ON THE AERODYNAMIC PERFORMANCE OF DRAGONFLY-LIKE FLAPPING WING | ICAS2020_1150 |
| Lang, X.Y. | NUMERICAL SIMULATION OF SWEEPING MOTION EFFECTS ON THE HOVERING DRAGONFLIES | ICAS2020_1167 |
| Lang, X.Y. | AERODYNAMIC ANALYSIS OF DRAGONFLY WINGS SPACE DISTRIBUTION ON THREE-DIMENSIONAL DURING HOVERING FLIGHT | ICAS2020_1172 |
| Larsson, F. | CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS | ICAS2020_0110 |
| Larsson, F. | AN ONTOLOGICAL APPROACH FOR CLASSIFYING AIRCRAFT ACTUATORS | ICAS2020_1209 |
| Larsson, F. | EVALUATION ASPECT MAPPING FOR ACTUATION SYSTEM DESIGN | ICAS2020_1210 |
| Lawson, S. | HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTURE | ICAS2020_0236 |
| Lee, H.K. | TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNING | ICAS2020_0649 |
| Lee, J. | AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING | ICAS2020_0959 |
| Lee, H. | AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING | ICAS2020_0959 |
| Lee, C.-H. | AN ACCELERATION METHODOLOGY BASED ON DISTURBANCE REGION UPDATE METHOD FOR STEADY COMPRESSIBLE FLOWS | ICAS2020_1263 |
| Lehmann, O. | INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSIS | ICAS2020_1213 |
| Lei, K. | TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT | ICAS2020_0271 |
| Lei, T. | EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2020_0620 |
| Lei, J. | FLOW AND HEAT TRANSFER MECHANISM OF JET IMPINGEMENT COOLING ONTO MID-CHORD REGINE OF TWISTED BLADE | ICAS2020_1106 |
| Leng, Y. | ATMOSPHERIC TURBULENCE EFFECTS ON SONIC BOOM PROPAGATION | ICAS2020_0349 |
| Leng, L.-T. | RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED | ICAS2020_0661 |
| Leng, J. | SHAPE MORPHING SMART STRUCTURES: MECHANICS, MATERIALS AND APPLICATIONS | ICAS2020_1281 |
| Lertworawanich, P. | ARTIFICIAL INTELLIGENCE AND HUMAN-MACHINE INTERACTIONS FOR STREAM-BASED AIR TRAFFIC FLOW MANAGEMENT | ICAS2020_1009 |
| Levchenko, E.A. | SPECIALIZED SOFTWARE DEVELOPMENT FOR BUILDING BLOCK APPROACH INTEGRATION IN FULL-SCALE STATIC TESTS | ICAS2020_1117 |
| Li, C. | A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS | ICAS2020_0036 |
| Li, J. | ADVANCED WEAK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING | ICAS2020_0037 |
| Li, Y. | AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION | ICAS2020_0071 |
| Li, X. | AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION | ICAS2020_0071 |
| LI, P. | TRANSFER PATH ANALYSIS OF RANDOM VIBRATION LOADS | ICAS2020_0086 |
| Li, C. | EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES | ICAS2020_0093 |
| Li, G. | HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSES | ICAS2020_0096 |
| Li, Z.Y. | A STRUCTURE DESIGN OF CFRP REAR PRESSURE BULKHEAD WITHOUT STIFFENERS | ICAS2020_0109 |
| Li, H. | COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS | ICAS2020_0114 |
| Li, L. | FRACTURE CRITERION ANALYSIS AND CRACK GROWTH PROPERTY OF MIXED-MODE CRACK EXPERIMENTS | ICAS2020_0118 |
| Li, C. | EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS | ICAS2020_0147 |
| Li, Y. | CONCEPTUAL DESIGN OF A FIXED-WING AQUATIC UAV USING KNOWLEDGE BASED ENGINEERING | ICAS2020_0154 |
| Li, Y. | CONCEPTUAL DESIGN OF A FIXED-WING AQUATIC UAV USING KNOWLEDGE BASED ENGINEERING | ICAS2020_0154 |
| Li, Q. | AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLES | ICAS2020_0168 |
| Li, J. | DESIGN AND VERIFICATION OF ENERGY-ABSORBING STRUCTURE OF CORRUGATED BEAM BASED ON SPECIFIC FAILURE MODE | ICAS2020_0187 |
| Li, J. | STATISTICS AND ANALYSIS OF MANUFACTURING DEFECTS AND DAMAGE OF HELICOPTER COMPOSITE STRUCTURES | ICAS2020_0188 |
| Li, Y.F. | EFFECT OF COMPLEX FLOW PROFILES AT COMBUSTOR EXIT ON TURBINE CHARACTERISTICS | ICAS2020_0257 |
| Li, D. | APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITION | ICAS2020_0264 |
| Li, M.Q. | ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS | ICAS2020_0269 |
| Li, C. | VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING | ICAS2020_0284 |
| Li, H. | MODELING AND SIMULATION APPLICATION THROUGHOUT THE AERO-ENGINE LIFE CYCLE | ICAS2020_0290 |
| Li, X. | MODELING AND SIMULATION APPLICATION THROUGHOUT THE AERO-ENGINE LIFE CYCLE | ICAS2020_0290 |
| Li, W.-H. | FLIGHT MANAGEMENT SYSTEM REQUIREMENT ANALYSIS FOR TRAJECTORY BASED OPERATION | ICAS2020_0292 |
| Li, C. | STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATOR | ICAS2020_0305 |
| Li, Y. | AN ADJOINT-BASDF AERO-STRUCTURAL DESIGN OPTIMIZATION METHOD USING DYNAMIC MESH TECHNOLOGY | ICAS2020_0317 |
| Li, Y. | MECHANISM DESIGN AND AERODYNAMIC RESEARCH OF RETRACTABLE FOLDING FLAPPING WING | ICAS2020_0333 |
| Li, Q. | AERODYNAMIC NOISE SIMULATION OF CIVIL AIRCRAFT LANDING GEARS BASED ON LES-SMARGORINSKY MODEL | ICAS2020_0351 |
| Li, K. | STRUCTURAL VIBRATION CONTROL BY USING THE ENERGY FROM DIFFERENT MODES | ICAS2020_0383 |
| Li, H. | DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEM | ICAS2020_0386 |
| Li, Y.L. | DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINE | ICAS2020_0401 |
| Li, M. | STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION | ICAS2020_0416 |
| Li, W.-B. | PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGN | ICAS2020_0463 |
| Li, J. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Li, D. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Li, X. | A STUDY OF SONIC BOOM TEST WITH NOZZLE PLUME INTERACTIONS | ICAS2020_0500 |
| Li, H. | DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAIN | ICAS2020_0503 |
| Li, G. | EXPERIMENTAL STUDY ON CRITICAL HEAT FLUX CHARACTERISTICS OF R134A FLOW BOILING IN A HORIZONTAL 2.1 MM TUBE UNDER HYPERGRAVITY | ICAS2020_0510 |
| Li, Z. | AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERS | ICAS2020_0541 |
| Li, Z.-P. | DISTORTION PLATE DESIGN, SIMULATION VALIDATION AND TEST SCHEME FOR STABILITY ANALYSIS ON A FAN COMPONENT OF AN AEROENGINE | ICAS2020_0636 |
| Li, X.F. | A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT | ICAS2020_0650 |
| Li, B. | STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESH | ICAS2020_0686 |
| Li, W.B. | EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADE | ICAS2020_0704 |
| Li, K.C. | EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADE | ICAS2020_0704 |
| Li, M. | DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHT | ICAS2020_0714 |
| Li, X. | IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEM | ICAS2020_0723 |
| Li, L. | AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVES | ICAS2020_0794 |
| Li, Q. | RESEARCH ON FUNCTIONAL HAZARD ASSESSMENT TECHNOLOGY OF MILITARY AIRCRAFT | ICAS2020_0795 |
| Li, B.F. | CO-SIMULATION OF SYSML AND SIMULINK/MODELICA USING FMI | ICAS2020_0803 |
| Li, Q. | MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION | ICAS2020_0805 |
| Li, K.T. | DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMING | ICAS2020_0822 |
| Li, D. | DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS | ICAS2020_0839 |
| Li, H.-J. | DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS | ICAS2020_0839 |
| Li, X.X. | INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINE | ICAS2020_0845 |
| Li, G.Y. | AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESS | ICAS2020_0899 |
| Li, Z.H. | RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTION | ICAS2020_0909 |
| Li, X.H. | SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODEL | ICAS2020_0928 |
| Li, M. | INVESTIGATION OF AERODYNAMIC INTERACTIONS BETWEEN NACA0012 AIRFOILS IN TANDEM | ICAS2020_1063 |
| Li, F. | TWISTOR BASED 6-DOF DISTRIBUTED ADAPTIVE LEADER-FOLLOWING CONTROL FOR MULTIPLE RIGID SPACECRAFT FORMATION | ICAS2020_1089 |
| Li, C. | AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLES | ICAS2020_1109 |
| Li, X.C. | A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINE | ICAS2020_1114 |
| Li, H.-Y. | AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESS | ICAS2020_1118 |
| Li, F. | EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0 | ICAS2020_1122 |
| Li, D. | AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGING | ICAS2020_1132 |
| Li, H. | LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINT | ICAS2020_1145 |
| Li, Y. | LEARNING-BASED MIDCOURSE GUIDANCE FOR VELOCITY MAXIMIZATION WITH ANGULAR CONSTRAINT | ICAS2020_1145 |
| Li, R. | NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAP | ICAS2020_1149 |
| Li, Y.B. | NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTS | ICAS2020_1183 |
| Li, Y.B. | NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WING | ICAS2020_1240 |
| Liang, S.Q. | ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS | ICAS2020_0269 |
| Liang, C. | MODELING AND SIMULATION APPLICATION THROUGHOUT THE AERO-ENGINE LIFE CYCLE | ICAS2020_0290 |
| Liang, Y.-Q. | RESEARCH OF LABYRINTH SEALS MEASUREMENT-BASED PROBABILITISTIC ANALYSIS METHOD FOR TURBOFAN INTERNAL AIR SYSTEM | ICAS2020_0531 |
| Liang, Y. | AN INTELLIGENT STRUCTURED CHIMERA GRID APPROACH FOR MOVING OBJECTIVES | ICAS2020_0794 |
| Liang, C.-H. | EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0 | ICAS2020_1122 |
| Liao, F. | AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING | ICAS2020_0348 |
| Liao, Y. | STUDY ON THE FATIGUE SCATTER FACTOR UNDER SEVERE LOAD SPECTRUM | ICAS2020_0904 |
| Liebhardt, B. | FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFT | ICAS2020_0238 |
| Liebhardt, B. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Limonin, M.V. | SPECIALIZED SOFTWARE DEVELOPMENT FOR BUILDING BLOCK APPROACH INTEGRATION IN FULL-SCALE STATIC TESTS | ICAS2020_1117 |
| Lin, Y.-F. | AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESS | ICAS2020_1118 |
| Lin, Y.-F. | HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILS | ICAS2020_1125 |
| Lin, Y.-F. | FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATION | ICAS2020_1127 |
| Lin, D. | MULTI-UAV TRAJECTORY PLANNING BASED ON COORDINATION VARIABLES | ICAS2020_1139 |
| Ling, S.-B. | EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR THE “AEROSTRUCT” WING OPTIMIZATION PLATFORM | ICAS2020_0350 |
| Linke, F. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Lipanov, A.M. | PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSET | ICAS2020_0949 |
| Lipatov, I.I. | PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSET | ICAS2020_0949 |
| Lippoldt, K. | VERTIPORT PLACEMENT METHOD BASED ON MOBILITY SURVEY DATA | ICAS2020_1133 |
| Liu, N. | AN IMPROVED IDENTIFICATION METHOD FOR ACTUATOR LOOP OF AIRCRAFT ENGINE CONTROL SYSTEM | ICAS2020_0027 |
| Liu, Q. | EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTS | ICAS2020_0040 |
| Liu, Z. | EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTS | ICAS2020_0040 |
| Liu, R.P. | THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLE | ICAS2020_0052 |
| Liu, D. | NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING WITH SLOTTED-TIP | ICAS2020_0102 |
| Liu, L. | AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLES | ICAS2020_0168 |
| Liu, Y. | DESIGN AND RESEARCH ON SAFETY ANALYSIS TOOL FOR AVIONICS SYSTEM | ICAS2020_0186 |
| Liu, Y.J. | ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS | ICAS2020_0269 |
| Liu, G. | A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES | ICAS2020_0272 |
| Liu, Y.C. | A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDING | ICAS2020_0282 |
| Liu, X. | EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR | ICAS2020_0291 |
| Liu, P.-X. | STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATOR | ICAS2020_0305 |
| Liu, Z. | VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL | ICAS2020_0313 |
| Liu, C. | INCORPORTING KNOWLEDGE COVERAGE MEASUREMENT INTO KNOWLEDGE TRANSFORMATION FROM DATA FOR KNOWLEDGE ACCUMULATION | ICAS2020_0343 |
| Liu, Z. | MEMS-BASED DISTRIBUTED NAVIGATION SYSTEM | ICAS2020_0344 |
| Liu, Y. | DECOUPLING CONTROL LAW DESIGN FOR OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWING | ICAS2020_0384 |
| Liu, Y. | PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTS | ICAS2020_0392 |
| Liu, J. | DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINE | ICAS2020_0401 |
| Liu, H. | STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION | ICAS2020_0416 |
| Liu, D.-N. | PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNEL | ICAS2020_0418 |
| Liu, H.-Y. | PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGN | ICAS2020_0463 |
| Liu, F. | AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHING | ICAS2020_0476 |
| Liu, Z. | WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONS | ICAS2020_0483 |
| Liu, Z. | A STUDY OF SONIC BOOM TEST WITH NOZZLE PLUME INTERACTIONS | ICAS2020_0500 |
| Liu, Y. | MODELING AND DYNAMICS STABILITY ANALYSIS FOR A BLENDED-WING-BODY AIRCRAFT | ICAS2020_0525 |
| Liu, X. | MODELING AND DYNAMICS STABILITY ANALYSIS FOR A BLENDED-WING-BODY AIRCRAFT | ICAS2020_0525 |
| Liu, L. | ASSEMBLY QUALITY OPTIMIZATION APPROACH FOR LARGE-SCALE ACTIVE COMPONENTS BASED ON REVERSE ENGINEERING | ICAS2020_0542 |
| Liu, F. | BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES | ICAS2020_0574 |
| Liu, J.-Y. | EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODEL | ICAS2020_0619 |
| Liu, T. | RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED | ICAS2020_0661 |
| Liu, J. | AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE | ICAS2020_0663 |
| Liu, Y. | APPLICATION OF REINFORCEMENT LEARNING IN 1-D AERODYNAMIC DESIGN OF AXIAL COMPRESSOR | ICAS2020_0678 |
| Liu, H.J. | BIONIC LIGHT-WEIGHT GRID SURFACE WING STRUCTURE DESIGN FOR A SOLAR-POWERED UAV | ICAS2020_0731 |
| Liu, P. | ANALYSIS OF THRUST-SCALED ACOUSTIC EMISSIONS OF AIRCRAFT PROPELLERS AND THEIR DEPENDENCE ON PROPULSIVE EFFICIENCY | ICAS2020_0751 |
| Liu, Q.Y. | AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESS | ICAS2020_0774 |
| Liu, S.-S. | NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODEL | ICAS2020_0796 |
| Liu, L. | MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION | ICAS2020_0805 |
| Liu, Q.C. | PRECISION ANALYSIS AND INDEX DISTRIBUTION SYSTEM DESIGN OF AVIONICS SYSTEM BASED ON BP NEURAL NETWORK | ICAS2020_0808 |
| Liu, P.Q. | MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORK | ICAS2020_0849 |
| Liu, H.-L. | RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLES | ICAS2020_0851 |
| Liu, Y.M. | RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DIS | ICAS2020_0865 |
| Liu, Z.-Q. | MULTIFIDELITY AERODYNAMIC/STEALTH DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT | ICAS2020_0878 |
| Liu, L.Y. | THE FINITE ELEMENT MODELLING OF BOLTED STRUCTURE BETWEEN SELECTIVE LASER MELTING ALUMINIUM AND COMPOSITE PLATES | ICAS2020_0880 |
| Liu, F. | AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESS | ICAS2020_0899 |
| Liu, D.L. | AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS | ICAS2020_0939 |
| Liu, Z.-W. | A METHOD OF MANEUVER IDENTIFICATION AND TRAJECTORY PREDICTION FOR AGILE TARGET | ICAS2020_0948 |
| Liu, Y.Z. | TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLE | ICAS2020_1110 |
| Liu, F. | A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINE | ICAS2020_1114 |
| Liu, Y. | EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0 | ICAS2020_1122 |
| Liu, X. | NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAP | ICAS2020_1149 |
| Liu, S.S. | A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTION | ICAS2020_1160 |
| Liu, Z.K. | A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTION | ICAS2020_1160 |
| Liu, X. | A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTION | ICAS2020_1160 |
| Liu, X.P. | TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGY | ICAS2020_1170 |
| Liu, L. | COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION | ICAS2020_1176 |
| Liu, P.Q. | NUMERICAL STUDY OF DITCHING CHARACTERISTICS OF BWB AIRCRAFT | ICAS2020_1178 |
| Liu, J.-Y. | A REDUNDANT ADAPTIVE NAVIGATION METHOD BASED ON DYNAMIC PERFORMANCE EVALUATION FOR AEROSPACE VEHICLE | ICAS2020_1180 |
| Liu, X. | CONCEPT OF A NEW SYSTEM SYNTHESIZING METEOROLOGICAL AND OROGRAPHIC INFLUENCES ON THE AIRPLANE SAFE ENERGY ENVELOPE | ICAS2020_1193 |
| Liu, L. | RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGE | ICAS2020_1203 |
| Liu, C. | RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGE | ICAS2020_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 6 | ICAS2020_1224 |
| Liu, L.B. | RESEARCH ON AIRCRAFT-LEVEL PHYSICAL INTEGRATION VERIFICATION TEST TECHNOLOGY | ICAS2020_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 2050 | ICAS2020_1249 |
| Liu, Y.X. | NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATION | ICAS2020_1250 |
| Liu, P. | ESTIMATION OF STATIC AND DYNAMIC FLOATATION CHARACTERISTICS DURING AIRCRAFT DITCHING | ICAS2020_1255 |
| Liu, A. | A DEEP LEARNING AND ONTOLOGY BASED FRAMEWORK FOR TEXTUAL REQUIREMENTS ANALYSIS AND CONCEPTUAL MODEL GENERATION | ICAS2020_1293 |
| Loiodice, L. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| Lone, M.M. | ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONS | ICAS2020_0253 |
| Lone, M. | RAPID THEORETICAL EVALUATION OF FORMATION FLIGHT PERFORMANCE | ICAS2020_0648 |
| Lowenberg, M.H. | NONLINEAR UNSTEADY AERODYNAMIC MODELING AND LONGITUDINAL STABILITY ANALYSIS FOR AN AIRCRAFT MODEL | ICAS2020_1104 |
| Lu, J. | A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT | ICAS2020_0097 |
| Lu, Y.-H. | MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATION | ICAS2020_0397 |
| Lu, M.H. | STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTION | ICAS2020_0598 |
| Lu, S. | DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISK | ICAS2020_0713 |
| Lubrina, P. | MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST | ICAS2020_1049 |
| Luderer, O. | VALIDATION OF AN AERODYNAMIC MODEL FOR THE ANALYSIS OF SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRICAL PROPULSION | ICAS2020_0145 |
| Luna, L.S. | USAGE OF MQTT, ROS, AND AWS IN THE MANUFACTURING PROCESS OF AIRCRAFTS | ICAS2020_1223 |
| Luo, Z. | EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTS | ICAS2020_0040 |
| Luo, Y. | COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS | ICAS2020_0114 |
| Luo, S. | CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELL | ICAS2020_0285 |
| Luo, X. | PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGN | ICAS2020_0463 |
| Luo, K. | AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR | ICAS2020_0538 |
| Luo, B. | A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOS | ICAS2020_1309 |
| Lv, S. | A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES | ICAS2020_0272 |
| Lv, S. | EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY | ICAS2020_0400 |
| Lv, P. | NUMERICAL SIMULATION OF LOCAL LONG SHALLOW CAVITY EFFECT ON THE STABILITY OF A HYPERSONIC BOUNDARY LAYER | ICAS2020_1189 |
| Lühder, W. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Lyrio, J.A.A. | STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERS | ICAS2020_0725 |
| Ma, K. | ESTIMATION OF THREE-DIMENSIONAL BOUNDARY LAYER VELOCITY PROFILES ON SWEPT WINGS AND BLENDED WING BODIES | ICAS2020_0078 |
| Ma, K. | THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT | ICAS2020_0181 |
| Ma, Y. | PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2020_0398 |
| Ma, Y. | PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2020_0398 |
| Ma, C. | RESEARCH ON SELECTION METHODS FOR AIRCRAFT LANDING GEAR SYSTEM HEALTH FEATURE PARAMETERS | ICAS2020_0581 |
| Ma, H.L. | EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADE | ICAS2020_0704 |
| Ma, X.-P. | AERODYNAMIC AND STRUCTURAL DESIGN OF THE COMPOSITE PROPELLER FOR NEAR SPACE VEHICLES | ICAS2020_0722 |
| Ma, H.S. | DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMING | ICAS2020_0822 |
| Ma, C. | BENEFIT ANALYSIS OF AIR REFUELING IN ULTRA LONG ROUTE AIRLINER OPERATION | ICAS2020_1101 |
| Ma, G.-W. | EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0 | ICAS2020_1122 |
| Ma, J.Y. | DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE | ICAS2020_1135 |
| Ma, C. | THE STUDY ON ANTI-ICING AREAS OF LEADING-EDGE SLATS IN MODERN CIVIL AIRCRAFT | ICAS2020_1154 |
| Ma, C. | FAST ITERATIVE SIMULATION OF AIRLINER WING PLANFORM CONCEPTUAL DESIGN | ICAS2020_1155 |
| Magerramova, L. | DEVELOPMENT OF ADVANCED DESIGNS OF GAS TURBINE ENGINES FROM POWDER COMPOSITIONS | ICAS2020_0924 |
| Maina, M. | HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTURE | ICAS2020_0236 |
| Malik, Z. | INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSIS | ICAS2020_1213 |
| Malyutin, V.A. | THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATOR | ICAS2020_0212 |
| Mamaev, V. | ADVANCED WEAK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING | ICAS2020_0037 |
| Manfriani, L. | CONCEPT OF A NEW SYSTEM SYNTHESIZING METEOROLOGICAL AND OROGRAPHIC INFLUENCES ON THE AIRPLANE SAFE ENERGY ENVELOPE | ICAS2020_1193 |
| Mao, J. | ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META-MODEL | ICAS2020_0200 |
| Mao, J. | GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHOD | ICAS2020_0489 |
| Maqsood, A. | NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER | ICAS2020_0555 |
| Maqsood, A. | NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES | ICAS2020_0556 |
| Mare, J.-C. | VIRTUAL PROTOTYPING OF ELECTRICAL THSA FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS | ICAS2020_0196 |
| Marin, G. | ATTENTION: TARGET AND ACTUAL - THE CONTROLLER FOCUS | ICAS2020_0012 |
| Marini, M. | THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE | ICAS2020_0493 |
| Marini, M. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Marini, M. | INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISER | ICAS2020_1195 |
| Maritano, G. | APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS | ICAS2020_0454 |
| Markov, S. | EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS | ICAS2020_0750 |
| Marques, J.M.G. | ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATION | ICAS2020_0989 |
| Marques, J.M.G. | ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHS | ICAS2020_0990 |
| Martensson, H. | AERODYNAMIC ANALYSIS OF A HIGH SPEED TEST RIG FOR USE IN ENGINE TEST FACILITIES | ICAS2020_0016 |
| Martin, M. | NUMERICAL SIMULATIONS OF TRANSONIC BUFFET ON A HALF WING-BODY CONFIGURATION | ICAS2020_0612 |
| Martinez, J. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Masse, G. | THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS | ICAS2020_1235 |
| Masuda, K. | LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV | ICAS2020_0150 |
| Matsumura, Y. | MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMS | ICAS2020_0945 |
| Matsuno, Y. | IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTION | ICAS2020_0202 |
| Mattos, B.S. | FLUID-STRUCTURE INTERACTION ANALYSIS OF ELASTIC EFFECTS OF A TRANSPORT AIRCRAFT FITTED WITH WINGLETS | ICAS2020_0999 |
| Mattos, B.S. | AIRLINE NETWORK-AIRPLANE INTEGRATED OPTIMIZATION CONSIDERING MANUFACTURER'S PROGRAM COST | ICAS2020_1005 |
| Mavris, D.N. | AN EXERCISE IN DEVELOPING A SUPERVISED ANOMALY DETECTION MODEL WITH AUTOMATICALLY ENGINEERED FEATURES | ICAS2020_0467 |
| Mavris, D.N. | TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNING | ICAS2020_0649 |
| Mavris, D.N. | MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS | ICAS2020_1237 |
| Mavris, D. | QUANTIFICATION OF OPERATIONAL EFFECTIVENESS FOR TECHNOLOGY EVALUATION | ICAS2020_1241 |
| Mei, Q. | MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATION | ICAS2020_0397 |
| Melnikov, Y. | MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS | ICAS2020_0089 |
| Men, W.W. | DESIGN AND PERFORMANCE RESEARCH OF ARTIFICIAL ELECTROMAGNETIC STRUCTURE WITH TRANSMISSION AND ABSORPTION CHARACTERISTICS | ICAS2020_0208 |
| Meng, S. | SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRID | ICAS2020_0315 |
| Meng, M. | ACTIVITY CHARACTERISTICS AND THE MECHANISM OF MESO-MICRO SCALE DISTURBANCES IN THE EAST ASIAN SUBTROPICAL UPPER-LEVEL JET STREAM | ICAS2020_0378 |
| Meng, X.H. | DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINE | ICAS2020_0401 |
| Meng, X.-X. | DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHT | ICAS2020_0714 |
| Menga, E. | MODEL REDUCTION AND STOCHASTIC UPDATING OF A VIBRATING SYSTEM | ICAS2020_0916 |
| Meyer, J. | OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTION | ICAS2020_0311 |
| Meyer, M. | TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFT | ICAS2020_1260 |
| Mi, J.C. | RESEARCH ON THE PRESSURE COMFORT OF PILOT HELMETS | ICAS2020_0180 |
| Mi, B.-G. | MODELING AND DYNAMICS STABILITY ANALYSIS FOR A BLENDED-WING-BODY AIRCRAFT | ICAS2020_0525 |
| Mi, B.-G. | SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICS | ICAS2020_1134 |
| Mi, B.G. | RESEARCH ON UNSTEADY AERODYNAMIC MODELS AT HIGH ANGLES OF ATTACK BASED ON NONLINEAR REGRESSION | ICAS2020_1152 |
| Miao, G. | EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY | ICAS2020_0400 |
| Miao, T. | AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESS | ICAS2020_0899 |
| Miao, H.-Y. | INFLUENCE OF SHOCK TRAIN ON HEAT FLUX DISTRIBUTION OF A CIRCULAR CONSTANT-AREA ISOLATOR | ICAS2020_1146 |
| Miao, B. | ULTRASONIC DE-ICING SYSTEM DESIGN METHODS BASED ON RESONANCE AND IMPEDANCE MATCHING | ICAS2020_1148 |
| Mieloszyk, J. | LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE | ICAS2020_0030 |
| Mikhalyn , I.S. | CREATING A MULTI-FUNCTIONAL EXPERT ANALYTICAL SYSTEM IN THE AIRCRAFT INDUSTRY AND THE FORMATION OF GENERAL REQUIREMENTS | ICAS2020_0857 |
| Mikhaylov, S. | VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING | ICAS2020_0033 |
| Mileshin, V. | EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS | ICAS2020_0750 |
| Miller, A.B. | EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE | ICAS2020_0894 |
| Mindt, M. | AERODYNAMIC AND STRUCTURAL MODELING IN THE ROTORCRAFT MULTI-PHYSICS SIMULATION VAST | ICAS2020_0584 |
| Mirzoyan, A. | METHODS OF PROGRAMMED THRUST MANAGEMENT FOR NOISE REDUCTION OF SUPERSONIC CIVIL AIRCRAFT | ICAS2020_1017 |
| Mirzoyan, L. | THE CAPABILITIES OF AUTOMATION OF MDAO PROBLEM STATEMENT AT COLLABORATIVE CONCEPTUAL DESIGN OF THE PROPULSION SYSTEM USING OPEN SOURCE SOFTWARE TOOLS | ICAS2020_1022 |
| Mirzoyan, A. | THE CAPABILITIES OF AUTOMATION OF MDAO PROBLEM STATEMENT AT COLLABORATIVE CONCEPTUAL DESIGN OF THE PROPULSION SYSTEM USING OPEN SOURCE SOFTWARE TOOLS | ICAS2020_1022 |
| Mirzoyan, A. | PROPOSAL FOR INTERNATIONAL FIRE AVIATION SERVICE UNDER THE AUSPICES OF ICAO TO IMPROVE WORLD WILDFIRE MANAGEMENT | ICAS2020_1307 |
| Mischke, R. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Mistri, S.R. | METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WING | ICAS2020_0085 |
| Mo, W.-J. | RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUE | ICAS2020_0273 |
| Mo, D. | INVESTIGATION OF VARIABLE GEOMETRIES ON THE OPERABILITY AND AIRCRAFT LEVEL PERFORMANCE OF A THREE-SHAFT TURBOFAN ENGINE FOR ENTRY INTO SERVICE 2050 | ICAS2020_1249 |
| Mo, D. | NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATION | ICAS2020_1250 |
| Moberg, B. | ERAS- EVALUATION OF REALISTIC APPROACH SCENARIOS FOR MINIMAL NOISE - PRELIMINARY FINDINGS | ICAS2020_0409 |
| Moeljadi, M.A. | FURTHER DEVELOPMENT OF COMPUTATIONAL STUDY ON COANDA BLANKET CURVATURE EFFECTS ON HALF SPHERICAL COANDA DEVICE | ICAS2020_0906 |
| Moerland, E. | COLLABORATIVE AIRCRAFT DESIGN TECHNIQUES IN RESEARCH | ICAS2020_1299 |
| Mohd Rafie, A.S. | CIRCULATION CONTROL AIRCRAFT: RECENT DEVELOPMENTS OF THE CHANNEL-WING DESIGN | ICAS2020_1310 |
| Mori, R. | ANALYSIS OF PILOT OPERATIONAL STRATEGY DIFFERENCE USING NEURAL NETWORK | ICAS2020_0533 |
| Mori, T. | POINT MERGE SYSTEM AND ARRIVAL METERING SYNERGY EFFECT ESTIMATION OF INBOUND FLIGHT EFFICIENCY AT TOKYO INTERNATIONAL (HANEDA) AIRPORT | ICAS2020_1205 |
| Moruzzi, M.C. | ATTENUATION OF NOISE IN THE CABIN OF A REGIONAL AIRCRAFT BY METAMATERIAL TRIM PANELS | ICAS2020_0508 |
| Moschetta, J.-M. | DESIGN OPTIMIZATION OF MULTIROTOR DRONES IN FORWARD FLIGHT | ICAS2020_0781 |
| Mottershead, J.E. | MODEL REDUCTION AND STOCHASTIC UPDATING OF A VIBRATING SYSTEM | ICAS2020_0916 |
| Mou, Y. | CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFT | ICAS2020_0231 |
| Mou, B. | METHODS OF DIRECTIONAL COARSENING FOR UNSTRUCTURED GRIDS AND APPLICATIONS | ICAS2020_1261 |
| Muniz Neves, A. | OPTIMIZATION OF LONGITUDINAL CONTROL OF AN AGRICULTURAL UAV USING LQR-PID CONTROL | ICAS2020_1187 |
| Munthahar, S.A. | AUTONOMOUS CONFLICT RESOLUTION ALGORITHM BASED ON ELLIPTIC GEOMETRY | ICAS2020_0735 |
| Myasnikov, V.Y. | AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONS | ICAS2020_1242 |
| Na, Z.Z. | EFFECT OF COMPLEX FLOW PROFILES AT COMBUSTOR EXIT ON TURBINE CHARACTERISTICS | ICAS2020_0257 |
| Naeem, N. | EXPLORATION OF AERIAL FIREFIGHTING FLEET EFFECTIVENESS AND COST BY SYSTEM OF SYSTEMS SIMULATIONS | ICAS2020_0997 |
| Nagel, B. | FORMALIZED KNOWLEDGE MANAGEMENT FOR THE AIRCRAFT CABIN DESIGN PROCESS | ICAS2020_0134 |
| Nagel, B. | THE APPLICATION OF THE AGILE 4.0 MBSE ARCHITECTURAL FRAMEWORK FOR THE MODELING OF SYSTEM STAKEHOLDERS, NEEDS AND REQUIREMENTS | ICAS2020_0193 |
| Nagel, B. | SYSTEM ARCHITECTURE DESIGN SPACE MODELING AND OPTIMIZATION ELEMENTS | ICAS2020_0203 |
| Nagel, B. | EXPLORATION OF AERIAL FIREFIGHTING FLEET EFFECTIVENESS AND COST BY SYSTEM OF SYSTEMS SIMULATIONS | ICAS2020_0997 |
| Nagel, B. | ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES | ICAS2020_1259 |
| Nagel, B. | COLLABORATIVE AIRCRAFT DESIGN TECHNIQUES IN RESEARCH | ICAS2020_1299 |
| Nalianda, D. | INVESTIGATION OF VARIABLE GEOMETRIES ON THE OPERABILITY AND AIRCRAFT LEVEL PERFORMANCE OF A THREE-SHAFT TURBOFAN ENGINE FOR ENTRY INTO SERVICE 2050 | ICAS2020_1249 |
| Narbona Gonzalez, J. | EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION | ICAS2020_0171 |
| Naruoka, M. | BAYESIAN APPROACH TO SIMULTANEOUS STATIC AND DYNAMIC FLIGHT CHARACTERISTICS MODELING | ICAS2020_0814 |
| Neild, S.A. | NONLINEAR UNSTEADY AERODYNAMIC MODELING AND LONGITUDINAL STABILITY ANALYSIS FOR AN AIRCRAFT MODEL | ICAS2020_1104 |
| Nerosky, L.A.R. | IMPLEMENTATION OF DISTRIBUTED ELECTRIC PROPULSION ON A GENERAL AVIATION AIRCRAFT | ICAS2020_1025 |
| Neuteboom, M. | AERODYNAMIC ANALYSIS OF A HIGH SPEED TEST RIG FOR USE IN ENGINE TEST FACILITIES | ICAS2020_0016 |
| Nguen, N.K. | HYBRID NUMERICAL SCHEMES IN PREDICTION OF HIGH-SPEED LAMINAR-TURBULENT TRANSITION | ICAS2020_0529 |
| Nguyen, N. | MATHEMATICAL MODELS FOR ANALYSIS AND OPTIMIZATION OF AIRCRAFT STRUCTURAL COMPONENTS TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION | ICAS2020_0593 |
| Nguyen, D.D. | TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRID-ELECTRIC AIRCRAFT | ICAS2020_0635 |
| Nian, P. | NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION | ICAS2020_0826 |
| Nicke, E. | THE POTENTIAL OF CASING TREATMENTS FOR TRANSONIC COMPRESSORS: EVALUATION BASED ON AXIAL-SLOT AND ROTOR BLADE OPTIMIZATION | ICAS2020_1054 |
| Nicolosi, G. | DESIGN OF A VERTICAL DITCHING TEST | ICAS2020_0763 |
| Nie, B. | VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL | ICAS2020_0313 |
| Nie, W.-J. | TURBINE STRUCTURE ANALYSIS AND IMPROVEMENT OF A HIGH-SPEED ROTOR WITH MULTI-DISK AND MULTI-SUPPORT | ICAS2020_0391 |
| Nie, B.-W. | PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNEL | ICAS2020_0418 |
| Nie, T.-Y. | EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODEL | ICAS2020_0619 |
| Nie, T.-Y. | A REDUNDANT ADAPTIVE NAVIGATION METHOD BASED ON DYNAMIC PERFORMANCE EVALUATION FOR AEROSPACE VEHICLE | ICAS2020_1180 |
| Niemeyer, P. | IMPACT OF NEW TECHNOLOGIES ON AIRCRAFT SYSTEMS | ICAS2020_0050 |
| Ning, Y. | STUDY ON THE AIRWORTHINESS AND COMFORTABLENESS REQUIREMENTS OF AIRCRAFT CABIN AIR CONTAMINATIONS | ICAS2020_0761 |
| Ning, D. | A POLE CONFIGURATION CONTROLLER FOR FIXED HEIGHT CONTROL OF TILT ROTOR AIRCRAFT | ICAS2020_1228 |
| Niu, J. | AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGING | ICAS2020_1132 |
| Niu, Y.-B. | INFLUENCE OF SHOCK TRAIN ON HEAT FLUX DISTRIBUTION OF A CIRCULAR CONSTANT-AREA ISOLATOR | ICAS2020_1146 |
| Niu, J.-J. | A NUMEIRCAL PREDICTION OF THE AIRCRAFT ICING METEOROLOGICAL ENVIRONMENT | ICAS2020_1156 |
| Novara, M. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Novelli, P. | COLLABORATIVE AIRCRAFT DESIGN EXERCISE BEYOND IFAR | ICAS2020_1301 |
| Novikov, A.V. | HYBRID NUMERICAL SCHEMES IN PREDICTION OF HIGH-SPEED LAMINAR-TURBULENT TRANSITION | ICAS2020_0529 |
| Novikov, A. | NUMERICAL SIMULATION OF THREE-DIMENSIONAL DISTURBANCES EVOLUTION IN SUPERSONIC FLOW OVER A WAVY SURFACE | ICAS2020_0968 |
| Nunes, T. | IFAR-X COLLABORATIVE AIRCRAFT DESIGN EXERCISE ON ENVIRONMENTALLY COMPATIBLE TRANSPORT AIRCRAFT | ICAS2020_1300 |
| Nuño , M. | STRUCTURAL HEALTH MONITORING OF SANDWICH STRUCTURES WITH LATTICE CORES IN AIRCRAFT DESIGN: CHALLENGES AND POTENTIAL | ICAS2020_0518 |
| Näsman, P. | ERAS- EVALUATION OF REALISTIC APPROACH SCENARIOS FOR MINIMAL NOISE - PRELIMINARY FINDINGS | ICAS2020_0409 |
| Ochi, Y. | ESTIMATION OF WIND BY ESTIMATING DERIVATIVES OF A LATERAL-DIRECTIONAL MOTION MODEL | ICAS2020_0752 |
| Ohneiser, O. | ATTENTION: TARGET AND ACTUAL - THE CONTROLLER FOCUS | ICAS2020_0012 |
| Okfen, P. | OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTION | ICAS2020_0311 |
| Okubo, K. | AN OVERVIEW OF FLARE TECHNIQUES AND FLARE TRAINING METHODS | ICAS2020_0919 |
| Olejnik, A. | EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS | ICAS2020_0101 |
| Olejnik, A. | THE USE OF REVERSE ENGINEERING AND COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A LOW COST SATELLITE LAUNCH SYSTEM | ICAS2020_1221 |
| Olenev, V. | INTEGRATED ON-BOARD NETWORKS FOR NEXT GENERATION AVIONICS | ICAS2020_0577 |
| Olsson, S. | FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE | ICAS2020_1032 |
| Oprea, A. | CONNECTING SYSTEM SIMULATION TO AIRCRAFT CONCEPT DEVELOPMENT | ICAS2020_1229 |
| Ordy, B. | CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM | ICAS2020_0659 |
| Orlando, C. | A STOCHASTIC ROBUSTNESS VERIFICATION OF NLG SIMPLE ADAPTIVE SHIMMY SUPPRESSION SYSTEM | ICAS2020_0662 |
| Osipova, S.L. | INFLUENCE OF VARIABLE WALL PERFORATION RATIO ON BOUNDARY LAYER PARAMETERS AT TRANSONIC SPEEDS | ICAS2020_0249 |
| Ossorio Contreras, V. | EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION | ICAS2020_0171 |
| Ovdienko, M.A. | UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM | ICAS2020_0451 |
| Ovdienko, M.A. | CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS | ICAS2020_0974 |
| Pagani, A. | ACCURATE BUCKLING AND POST-BUCKLING ANALYSIS OF COMPOSITE STIFFENED PANELS | ICAS2020_1124 |
| Pagliaroli, T. | NUMERICAL SIMULATION OF LOCAL LONG SHALLOW CAVITY EFFECT ON THE STABILITY OF A HYPERSONIC BOUNDARY LAYER | ICAS2020_1189 |
| Pagliuca, G. | BLENDED WING BODY (BWB) PLANFORM MULTIDISCIPLINARY OPTIMISATION (MDO) FOR EARLY STAGE AIRCRAFT DESIGN USING MODEL BASED ENGINEERING | ICAS2020_0244 |
| Pan, B. | CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELL | ICAS2020_0285 |
| Pan, S.Z. | AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS | ICAS2020_0939 |
| Pan, X.L. | RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGE | ICAS2020_1203 |
| Pan, G.Y. | THE FLOW AND HEAT TRANSFER OF ANALYSIS TO ANNULAR CAVITY IN ENGINE CASE | ICAS2020_1251 |
| Panfilov, S.V. | MODELING AND SIMULATION OF DUSTY GAS FLOW IN AERODYNAMICS | ICAS2020_0441 |
| Pang, X.Y. | DESIGN AND PERFORMANCE RESEARCH OF ARTIFICIAL ELECTROMAGNETIC STRUCTURE WITH TRANSMISSION AND ABSORPTION CHARACTERISTICS | ICAS2020_0208 |
| Pang, C. | TRANSITION PREDICTION FOR TRANSPORT AIRCRAFT CONFIGURATIONS BASED ON OVERSET GRID | ICAS2020_0286 |
| Pang, R. | NUMERICAL INVESTIGATION ON FLOW INTERFERENCE BETWEEN BLENDED-WING-BODY AIRCRAFT AND OVERHANGING NACELLE | ICAS2020_0417 |
| Pang, R. | NUMERICAL SIMULATION STUDY ON BOUNDARY LAYER FLOW AND DRAG REDUCTION CHARACTERISTICS OF RIBLETS | ICAS2020_1140 |
| Pant, R.S. | METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WING | ICAS2020_0085 |
| Papantoni, V. | ASSESSMENT OF THREE COMMUTER AIRCRAFT CONCEPTS FROM A TRANSPORT SYSTEM PERSPECTIVE | ICAS2020_0207 |
| Paraschivoiu, D. | IFAR - INFRASTRUCTURE DATABASE | ICAS2020_1051 |
| Paris, C. | THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS | ICAS2020_1235 |
| Park, H.-S. | EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK-ABSORBING INSERT | ICAS2020_0157 |
| Paryshev, S.E. | THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATOR | ICAS2020_0212 |
| Pawellek, S. | FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANE | ICAS2020_1048 |
| Payan, A. | MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS | ICAS2020_1237 |
| Pedras, M.H.J. | AEROELASTIC RESPONSE CALCULATION USING DUHAMEL INTEGRAL AND ITS APPLICATIONS | ICAS2020_1126 |
| Pei, Y. | NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION | ICAS2020_0826 |
| Peng, H.F. | STATISTICS AND ANALYSIS OF MANUFACTURING DEFECTS AND DAMAGE OF HELICOPTER COMPOSITE STRUCTURES | ICAS2020_0188 |
| Peng, S.-H. | MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST | ICAS2020_1049 |
| Peng, S.E. | FLOW AND HEAT TRANSFER MECHANISM OF JET IMPINGEMENT COOLING ONTO MID-CHORD REGINE OF TWISTED BLADE | ICAS2020_1106 |
| Peng, S.-E. | NUMERICAL STUDY ON COOLING CHARACTERISTICS IN CHANNELS WITH PIN FIN ARRAYS UNDER HIGH TEMPERATURE/PRESSURE CONDITIONS | ICAS2020_1151 |
| Pereira, E.P. | ENERGY HARVESTING FROM PIEZOELECTRIC FRINGES AT THE TRAILING-EDGE OF A FINITE WING WITH LEADING-EDGE TUBERCLES | ICAS2020_0979 |
| Petiot, E. | THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS | ICAS2020_1235 |
| Petsch, M. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Petukhov, A.A. | THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS | ICAS2020_0881 |
| Pezzella, G. | OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE | ICAS2020_0164 |
| Pezzella, G. | LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE | ICAS2020_0165 |
| Pflüger, J. | EXPERIMENTAL INVESTIGATIONS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS | ICAS2020_0227 |
| Philipp, F. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Piana, P. | APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS | ICAS2020_0454 |
| Piana, P. | DESIGN OF A VERTICAL DITCHING TEST | ICAS2020_0763 |
| Pigusov, E.A. | STUDY ON AERODYNAMIC CHARACTERISTICS OF LIGHT CONVERTIBLE AIRCRAFT MODEL | ICAS2020_0810 |
| Pinon, O.J. | MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS | ICAS2020_1237 |
| Pinon Fischer, O.J. | AN EXERCISE IN DEVELOPING A SUPERVISED ANOMALY DETECTION MODEL WITH AUTOMATICALLY ENGINEERED FEATURES | ICAS2020_0467 |
| Pinon Fischer, O.J. | TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNING | ICAS2020_0649 |
| Plezer, J.F. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Pochkin, I. | EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS | ICAS2020_0750 |
| Podaruev, V. | VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING | ICAS2020_0033 |
| Pogorelov, I.O. | MECHANISMS OF NATURAL LAMINAR-TURBULENT TRANSITION ON AN UNSWEPT WING IN SUPERSONIC FLIGHT | ICAS2020_0657 |
| Polla, A. | DESIGN OF A VERTICAL DITCHING TEST | ICAS2020_0763 |
| Pollet, F. | DESIGN OPTIMIZATION OF MULTIROTOR DRONES IN FORWARD FLIGHT | ICAS2020_0781 |
| Pongsakornsathien, N. | ARTIFICIAL INTELLIGENCE AND HUMAN-MACHINE INTERACTIONS FOR STREAM-BASED AIR TRAFFIC FLOW MANAGEMENT | ICAS2020_1009 |
| Popov, S. | PASSIVE FLEXIBLE WINGTIP AREA FOR IMPROVING AIRLINERS CRUISE EFFICIENCY AND GUST ALLEVIATION | ICAS2020_0360 |
| Postaru, R. | ATTENTION: TARGET AND ACTUAL - THE CONTROLLER FOCUS | ICAS2020_0012 |
| Potapov, Y.F. | EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE | ICAS2020_0894 |
| Pott-Pollenske, M. | NOISE REDUCTION AT FLAP SIDE EDGE AND UNDERCARRIAGE | ICAS2020_1047 |
| Preis, L. | VERTIPORT PLACEMENT METHOD BASED ON MOBILITY SURVEY DATA | ICAS2020_1133 |
| Presto, F. | FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFT | ICAS2020_0238 |
| Prince, S. | ESTIMATION OF THREE-DIMENSIONAL BOUNDARY LAYER VELOCITY PROFILES ON SWEPT WINGS AND BLENDED WING BODIES | ICAS2020_0078 |
| Prince, S.A. | ON THE ASSESSMENT OF CFD METHODS FOR VORTICAL FLOWS | ICAS2020_0080 |
| Prince, S. | TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSER | ICAS2020_0081 |
| Prodan, M. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| Prusik, J. | AIRCRAFT FLIGHT CONTROL SYSTEM FOR AEROBATIC FLIGHT | ICAS2020_0073 |
| Pu, S.M. | RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFT | ICAS2020_0706 |
| Puranik, T.G. | AN EXERCISE IN DEVELOPING A SUPERVISED ANOMALY DETECTION MODEL WITH AUTOMATICALLY ENGINEERED FEATURES | ICAS2020_0467 |
| Puranik, T.G. | TOWARDS AN ONLINE PREDICTIVE MODEL OF AIRCRAFT ENERGY STATE USING SUPERVISED MACHINE LEARNING | ICAS2020_0649 |
| Puranik, T.G. | MACHINE LEARNING ENABLED TURBULENCE PREDICTION USING FLIGHT DATA FOR SAFETY ANALYSIS | ICAS2020_1237 |
| Pärnänen, T. | REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACT | ICAS2020_1014 |
| Qasem, J. | ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME | ICAS2020_0985 |
| Qi, C. | L1 ADAPTIVE CONTROL AUGMENTATION FOR A FLEXIBLE AIR-BREATHING HYPERSONIC VEHICLE MODEL | ICAS2020_0197 |
| Qi, S.-J. | THE STUDY OF UNMANNED AERIAL VEHICLE FLYING QUALITIES FLIGHT TEST METHOD BASED ON TIME-DELAY EVALUATION | ICAS2020_0710 |
| Qian, W.-Q. | AIRCRAFT INFLIGHT ICING DETECTION AND DIAGNOSIS METHODS | ICAS2020_0163 |
| Qian, Z. | VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING | ICAS2020_0284 |
| Qian, Z. | ATMOSPHERIC TURBULENCE EFFECTS ON SONIC BOOM PROPAGATION | ICAS2020_0349 |
| Qian, Z. | A STUDY OF SONIC BOOM TEST WITH NOZZLE PLUME INTERACTIONS | ICAS2020_0500 |
| Qian, G.P. | STUDY ON THE METHOD OF DETERMINING SKIN WAVINESS REQUIREMENT OF CIVIL AIRCRAFT | ICAS2020_1065 |
| Qian, G.-P. | NUMERICAL STUDY OF HIGH TEMPERATURE TRANSVERSE PULSE JET IN THE SUPERSONIC COMBUSTION CHAMBER | ICAS2020_1100 |
| Qian, G.P. | THE STUDY ON ANTI-ICING AREAS OF LEADING-EDGE SLATS IN MODERN CIVIL AIRCRAFT | ICAS2020_1154 |
| Qiao, J.-L. | FAST METHOD AND AN INTEGRATED CODE FOR SONIC BOOM PREDICTION OF SUPERSONIC COMMERCIAL AIRCRAFT | ICAS2020_0600 |
| Qiao, L. | A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT | ICAS2020_0650 |
| Qiu, D. | EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR | ICAS2020_0291 |
| Qiu, L. | DECOUPLING CONTROL LAW DESIGN FOR OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWING | ICAS2020_0384 |
| Qiu, A.X. | NUMERICAL INVESTIGATION ON FLOW INTERFERENCE BETWEEN BLENDED-WING-BODY AIRCRAFT AND OVERHANGING NACELLE | ICAS2020_0417 |
| Qiu, D.-B. | APPLICATION OF A SKEWED-SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSOR | ICAS2020_0543 |
| Qiu, D.-B. | DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSOR | ICAS2020_0632 |
| Qiu, H.-C. | IMPROVED STOCHASTIC PERTURBATION ALGORITHM FOR GENERALIZED REPEATED EIGENVALUES PROBLEM BASED ON SURROGATE MODEL | ICAS2020_0780 |
| Qiu, D.-B. | MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGN | ICAS2020_0965 |
| Qiu, B. | GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOW | ICAS2020_1073 |
| Qiu, A. | AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGING | ICAS2020_1132 |
| Qiu, B. | NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAP | ICAS2020_1149 |
| Qiu, A.-X. | A NUMEIRCAL PREDICTION OF THE AIRCRAFT ICING METEOROLOGICAL ENVIRONMENT | ICAS2020_1156 |
| Qu, Q.L. | NUMERICAL STUDY OF DITCHING CHARACTERISTICS OF BWB AIRCRAFT | ICAS2020_1178 |
| Qu, Q. | ESTIMATION OF STATIC AND DYNAMIC FLOATATION CHARACTERISTICS DURING AIRCRAFT DITCHING | ICAS2020_1255 |
| Qui, F. | A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONS | ICAS2020_0712 |
| Qui, X. | BASED ON SYSTEMS ENGINEERING PROCESS THE CIVIL AIRCRAFT PROJECT PRODUCT BREAKDOWN STRUCTURE DEVELOPMENT RESEARCH | ICAS2020_1018 |
| Qui, X.D. | THE CIVIL AIRCRAFT DEVELOPMENT PROJECT RISK MANAGEMENT RESEARCH | ICAS2020_1244 |
| Rachdi, A. | INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSIS | ICAS2020_1213 |
| Raczko, K. | PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER | ICAS2020_0747 |
| Rade, D.A. | STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERS | ICAS2020_0725 |
| Rajaram, D. | AN EXERCISE IN DEVELOPING A SUPERVISED ANOMALY DETECTION MODEL WITH AUTOMATICALLY ENGINEERED FEATURES | ICAS2020_0467 |
| Rakhmankulov, D.Y. | CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS | ICAS2020_0974 |
| Rameshbabu, R. | AN EXERCISE IN DEVELOPING A SUPERVISED ANOMALY DETECTION MODEL WITH AUTOMATICALLY ENGINEERED FEATURES | ICAS2020_0467 |
| Rasimarzabadi, F. | AERODYNAMIC ANALYSIS OF A HIGH SPEED TEST RIG FOR USE IN ENGINE TEST FACILITIES | ICAS2020_0016 |
| Rataj, J. | ATTENTION: TARGET AND ACTUAL - THE CONTROLLER FOCUS | ICAS2020_0012 |
| Ratei, P. | EXPLORATION OF AERIAL FIREFIGHTING FLEET EFFECTIVENESS AND COST BY SYSTEM OF SYSTEMS SIMULATIONS | ICAS2020_0997 |
| Rawikara, S.S. | AUTONOMOUS CONFLICT RESOLUTION ALGORITHM BASED ON ELLIPTIC GEOMETRY | ICAS2020_0735 |
| Raza, H. | REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACT | ICAS2020_1014 |
| Reichenwallner, C. | AN ONTOLOGICAL APPROACH FOR CLASSIFYING AIRCRAFT ACTUATORS | ICAS2020_1209 |
| Reichenwallner, C. | EVALUATION ASPECT MAPPING FOR ACTUATION SYSTEM DESIGN | ICAS2020_1210 |
| Ren, J.X. | THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLE | ICAS2020_0052 |
| Ren, Z. | HYBRID IGNITION PROBABILITY METHOD TO PREDICT THE IGNITION PERFORMANCE OF A GAS TURBINE COMBUSTOR | ICAS2020_0259 |
| Ren, Z.P. | RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORY | ICAS2020_0514 |
| Riaz, A. | ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONS | ICAS2020_0253 |
| Riaz, A. | APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATION | ICAS2020_0352 |
| Riaz, R. | NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER | ICAS2020_0555 |
| Riaz, R. | NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES | ICAS2020_0556 |
| Riaz, A. | CLOUD-BASED ENVIRONMENT FOR AIRCRAFT DESIGN COLLABORATION | ICAS2020_1123 |
| Ricci, S. | AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE | ICAS2020_0631 |
| Ritter, M. | MULTI-AXIS MANEUVER SIMULATION FOR SYSTEM IDENTIFICATION OF FLEXIBLE TRANSPORT AIRCRAFT BY HIGH-FIDELITY METHODS | ICAS2020_0206 |
| Riveiro Moreno, C. | NUMERICAL SIMULATIONS OF TRANSONIC BUFFET ON A HALF WING-BODY CONFIGURATION | ICAS2020_0612 |
| Rodera Garcia, O. | REVIEW OF PREDICTIVE METHODS FOR CAPTURING ONSET OF DAMAGE AND INITIAL DELAMINATION IN CARBON FIBRE REINFORCED POLYMER LAMINATES SUBJECT TO IMPACT | ICAS2020_1014 |
| Rodriguez Diaz, M.A. | GAZE-BASED INTERFACE FOR FLIGHT CONTROL: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEM | ICAS2020_0645 |
| Rodriguez Diaz, M.A. | FITT’S LAW WITH EYE TRACKING ON A FLIGHT SIMULATOR COCKPIT | ICAS2020_0982 |
| Rodriguez-Sanz, A. | A NOVEL APPROACH FOR TURNAROUND TIME ALLOCATION BASED ON REINFORCEMENT LEARNING | ICAS2020_1015 |
| Roeser, M.S. | MULTI-AXIS MANEUVER SIMULATION FOR SYSTEM IDENTIFICATION OF FLEXIBLE TRANSPORT AIRCRAFT BY HIGH-FIDELITY METHODS | ICAS2020_0206 |
| Roessler, C. | FLIGHT TESTING OF 65KG T-FLEX SUBSCALE DEMONSTRATOR | ICAS2020_0707 |
| Rogalski, T. | AIRCRAFT FLIGHT CONTROL SYSTEM FOR AEROBATIC FLIGHT | ICAS2020_0073 |
| Rogers, N. | BLADE - NATURAL LAMINAR FLOW FLIGHT TESTING | ICAS2020_0220 |
| Rohacs, D. | AIR TRAFFIC MANAGEMENT OF DRONES INTEGRATED INTO THE SMART CITIES | ICAS2020_0456 |
| Rohacs, D. | OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT | ICAS2020_0638 |
| Rohani, S.V. | MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT FUSELAGE | ICAS2020_0232 |
| Rolland, P.-C. | CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM | ICAS2020_0659 |
| Romanyuk, D.A. | MODELING AND SIMULATION OF DUSTY GAS FLOW IN AERODYNAMICS | ICAS2020_0441 |
| Romero Arana, J. | A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES | ICAS2020_0562 |
| Roncioni, P. | INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISER | ICAS2020_1195 |
| Roumeliotis, I. | INVESTIGATION OF VARIABLE GEOMETRIES ON THE OPERABILITY AND AIRCRAFT LEVEL PERFORMANCE OF A THREE-SHAFT TURBOFAN ENGINE FOR ENTRY INTO SERVICE 2050 | ICAS2020_1249 |
| Roy, R. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS | ICAS2020_1219 |
| Roy, R. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION | ICAS2020_1222 |
| Ruan, H. | AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESS | ICAS2020_0774 |
| Ruhland, J. | TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON WAKE VORTEX IMPACT BY OSCILLATING FLAPS | ICAS2020_0595 |
| Rui, Y. | EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODEL | ICAS2020_0619 |
| Ruiz Calavera, L.P. | EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION | ICAS2020_0171 |
| Ruiz Calavera, L.P. | STUDY OF THE BENEFITS OF A SEMI-MORPHING WING CONCEPT | ICAS2020_0216 |
| Rzucidlo, P. | AIRCRAFT FLIGHT CONTROL SYSTEM FOR AEROBATIC FLIGHT | ICAS2020_0073 |
| Sabater, C. | ROBUST DESIGN OF 3D SHOCK CONTROL BUMPS TO TRANSPORT AIRCRAFT UNDER REALISTIC UNCERTAINTIES | ICAS2020_0279 |
| Sabatini, R. | A NOVEL DETECT-AND-AVOID APPROACH FOR UAS IN URBAN ENVIRONMENTS | ICAS2020_0970 |
| Sabatini, R. | ARTIFICIAL INTELLIGENCE AND HUMAN-MACHINE INTERACTIONS FOR STREAM-BASED AIR TRAFFIC FLOW MANAGEMENT | ICAS2020_1009 |
| Saccone, G. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Sadraey, M.H. | ROCKETS HYBRID LAUNCH SYSTEM USING LINEAR SYNCHRONOUS ELECTRIC MOTORS | ICAS2020_0651 |
| Safwat, E. | RESEARCH ON FAULT DIAGNOSIS AND FAILURE RECONFIGURATION OF FLUSH AIR DATA SENSING | ICAS2020_1064 |
| Sakai, T. | IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP | ICAS2020_0557 |
| Salassidis, D. | PROPELLER WAKE - OBJECT INTERACTION USING A FREE WAKE MODEL UTILIZING LOCAL MESH SEPARATION | ICAS2020_0209 |
| Sampath, S. | SOL-GEL BASED ORGANIC-INORGANIC HYBRID COATINGS FOR CORROSION PROTECTION OF AEROSPACE ALUMINIUM ALLOY | ICAS2020_1052 |
| Sandoval Góes, L.C. | OPTIMIZATION OF LONGITUDINAL CONTROL OF AN AGRICULTURAL UAV USING LQR-PID CONTROL | ICAS2020_1187 |
| Sang, W.M. | NUMERICAL INVESTIGATION ON FLOW INTERFERENCE BETWEEN BLENDED-WING-BODY AIRCRAFT AND OVERHANGING NACELLE | ICAS2020_0417 |
| Sang, W.-M. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Sang, W.M. | A LOCAL CORRELATION-BASED ALGEBRAIC TRANSITION MODEL WITH COMPRESSIBILITY AND CROSSFLOW CORRECTION | ICAS2020_1098 |
| Sang, W. | AN OPTIMIZATION OF ANTI-ICING CHAMBER BASED ON POD AND KRIGING | ICAS2020_1132 |
| Sang, W.M. | NUMERICAL SIMULATION STUDY ON BOUNDARY LAYER FLOW AND DRAG REDUCTION CHARACTERISTICS OF RIBLETS | ICAS2020_1140 |
| Sang, W.-M. | A NUMEIRCAL PREDICTION OF THE AIRCRAFT ICING METEOROLOGICAL ENVIRONMENT | ICAS2020_1156 |
| Santoro, L. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| Sapienza, V. | APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS | ICAS2020_0454 |
| Sapienza, V. | S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE | ICAS2020_0455 |
| Sapienza, V. | DESIGN OF A VERTICAL DITCHING TEST | ICAS2020_0763 |
| Saponaro Piacente, A. | DESIGN OF A VERTICAL DITCHING TEST | ICAS2020_0763 |
| Saponaro Piacente, A. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| Saracoglu, B. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Sartor, F. | NUMERICAL SIMULATIONS OF TRANSONIC BUFFET ON A HALF WING-BODY CONFIGURATION | ICAS2020_0612 |
| Sasongko, R.A. | AUTONOMOUS CONFLICT RESOLUTION ALGORITHM BASED ON ELLIPTIC GEOMETRY | ICAS2020_0735 |
| Satoh, A. | ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF PROPELLER AT LOW ADVANCE RATIO USING A WHIRING ARM | ICAS2020_0470 |
| Satoh, A. | ENDURANCE ANALYSIS OF BATTERY-POWERED MULTICOPTERS: DERIVATION OF PROPER CUT-OFF VOLTAGE USING DC MOTOR MODEL | ICAS2020_0769 |
| Scano, D. | ACCURATE BUCKLING AND POST-BUCKLING ANALYSIS OF COMPOSITE STIFFENED PANELS | ICAS2020_1124 |
| Schanz, D. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Scherer, J. | ASSESSMENT OF THREE COMMUTER AIRCRAFT CONCEPTS FROM A TRANSPORT SYSTEM PERSPECTIVE | ICAS2020_0207 |
| Schlösser, P. | TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFT | ICAS2020_1260 |
| Schnell, R. | DESIGN AND PERFORMANCE OF A LOW FAN-PRESSURE-RATIO PROPULSION SYSTEM | ICAS2020_1058 |
| Schram, C. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Schroll, M. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Schröder, K.-U. | STRUCTURAL HEALTH MONITORING OF SANDWICH STRUCTURES WITH LATTICE CORES IN AIRCRAFT DESIGN: CHALLENGES AND POTENTIAL | ICAS2020_0518 |
| Schröder, A. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Schultz, M. | DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS | ICAS2020_0032 |
| Schulze, M. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Schuster, A. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Schwochow, J. | MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST | ICAS2020_1049 |
| Schülein, E. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Scigliano, R. | THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE | ICAS2020_0493 |
| Senba, A. | ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT FOR MORPHING WINGS | ICAS2020_0540 |
| Serokhvostov, S.V. | OPTIMAL TRAJECTORY DEPENDENCE ON THE ATMOSPHERE MODEL FOR THE SUN-POWERED AIRPLANE | ICAS2020_0448 |
| Serokhvostov, S. | STUDY OF SMALL UAVS DISTURBED MOTION NATURAL FREQUENCIES USING EXTENDED EXPERIMENTAL DATASETS | ICAS2020_0498 |
| Sevastyanov, F. | STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION | ICAS2020_0106 |
| Shalaev, V.I. | LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICS | ICAS2020_0107 |
| Shalaev, V.I. | SINGULARITIES IN THE NEAR-WALL REGION OF 3D BOUNDARY LAYER AND THE FLOW STRUCTURE IN ITS VICINITY | ICAS2020_0108 |
| Shang, Y. | RESEARCH ON CIVIL AIRCRAFT POWERPLANT SYSTEM EICAS MESSAGES DESIGN APPROACH | ICAS2020_0055 |
| Shang, X.-J. | THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE | ICAS2020_0095 |
| Shang, Y.X. | ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGS | ICAS2020_1171 |
| Shanygin, A. | DEVELOPMENT OF LIGHTWEIGHT HYBRID AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE STRUCTURE CONCEPTS | ICAS2020_0340 |
| Shao, C. | CURRENT PROGRESS AND FUTURE PROSPECTS OF CHINESE COMMERCIAL AIRCRAFT ENGINE DEVELOPMENT | ICAS2020_1285 |
| Shen, Y. | RESEARCH OF LABYRINTH SEALS MEASUREMENT-BASED PROBABILITISTIC ANALYSIS METHOD FOR TURBOFAN INTERNAL AIR SYSTEM | ICAS2020_0531 |
| Shen, T.L. | AUTOMATIC DETECTION TECHNOLOGY OF LARGE CIVIL AIRCRAFT BASED ON IMAGE RECOGNITION | ICAS2020_0675 |
| Shen, J. | CO-SIMULATION OF SYSML AND SIMULINK/MODELICA USING FMI | ICAS2020_0803 |
| Shen, J.S. | PRECISION ANALYSIS AND INDEX DISTRIBUTION SYSTEM DESIGN OF AVIONICS SYSTEM BASED ON BP NEURAL NETWORK | ICAS2020_0808 |
| Shen , P.F. | STUDY ON THE STATISTICAL CHARACTERISTICS OF SKIN FRICTION OF SHOCK WAVE/ TURBULENT BOUDARY LAYER INTERATION IN A HOLLOW FLARE CONFIGURATION AT MACH 6 | ICAS2020_1224 |
| Shi, G. | STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TESTING | ICAS2020_0039 |
| Shi, A. | A BENCHMARK METHOD FOR PREDICTING OBLIQUE SHOCK STRUCTURE | ICAS2020_0072 |
| Shi, X. | VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING | ICAS2020_0284 |
| Shi, Y. | EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY | ICAS2020_0400 |
| Shi, D. | EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY | ICAS2020_0400 |
| Shi, Y.A. | A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTS | ICAS2020_0833 |
| Shi, H.-C. | RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLES | ICAS2020_0851 |
| Shi, H.Y. | RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DIS | ICAS2020_0865 |
| Shi, J. | RESEARCH ON FAULT DIAGNOSIS AND FAILURE RECONFIGURATION OF FLUSH AIR DATA SENSING | ICAS2020_1064 |
| Shiva Prakasha, P. | EXPLORATION OF AERIAL FIREFIGHTING FLEET EFFECTIVENESS AND COST BY SYSTEM OF SYSTEMS SIMULATIONS | ICAS2020_0997 |
| Shvalev, Y.G. | METHODICAL STUDIES OF THE POSSIBILITY TO APPLY A NUMERICAL METHOD WITH BUILD-IN EMPIRICAL CRITERIA FOR DETERMIMING THE LAMINAR-TO-TURBULENT TRANSITION ON THE CONE SURFACE AT HIGH MACH NUMBERS | ICAS2020_0435 |
| Si, J.T. | BENEFIT ANALYSIS OF AIR REFUELING IN ULTRA LONG ROUTE AIRLINER OPERATION | ICAS2020_1101 |
| Sidorov, I. | METHODS FOR CALCULATING THE FATIGUE DAMAGE OF A STRUCTURE FOR VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS | ICAS2020_0576 |
| Sidoryuk, M.E. | INFLUENCE OF AERODYNAMIC ASYMMETRY ON SPIN PARAMETERS OF THE COMMON RESEARCH MODEL | ICAS2020_0532 |
| Siggel, M. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Silva, G.P.G. | HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORS | ICAS2020_0988 |
| Silva, R.G.A. | AEROELASTIC RESPONSE CALCULATION USING DUHAMEL INTEGRAL AND ITS APPLICATIONS | ICAS2020_1126 |
| Sinisi, M. | S55 PROJECT - CFD ANALYSIS OF AN HISTORICAL SEAPLANE | ICAS2020_0455 |
| Sinnige, T. | ANALYSIS OF THRUST-SCALED ACOUSTIC EMISSIONS OF AIRCRAFT PROPELLERS AND THEIR DEPENDENCE ON PROPULSIVE EFFICIENCY | ICAS2020_0751 |
| Skorupka, Z. | INVESTIGATIONS ON LANDING GEAR SHOCK ABSORBER ACTIVE FORCE CONTROL | ICAS2020_0513 |
| Skryabin, A. | THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEM | ICAS2020_0239 |
| Sokolov, M.P. | THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS | ICAS2020_0881 |
| Son, L.H. | ESTIMATION OF WIND BY ESTIMATING DERIVATIVES OF A LATERAL-DIRECTIONAL MOTION MODEL | ICAS2020_0752 |
| Song, G. | RESEARCH ON ARCHITECTURE FRAMEWORK MODEL BASED EVALUATION INDEX FOR AVIATION SCIENCE & TECHNOLOGY MANAGEMENT | ICAS2020_0077 |
| Song, B.F. | NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING WITH SLOTTED-TIP | ICAS2020_0102 |
| Song, B. | NUMERICAL SIMULATION ON AERODYNAMIC CHARACTERISTICS OF BIONIC CORRUGATED FLAPPING WING | ICAS2020_0155 |
| Song, B.-F. | RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES | ICAS2020_0162 |
| Song, G. | A CONTRASTIVE STUDY OF STANDARD SPECIFICATION FOR TECHNOLOGY READINESS ASSESSMENT | ICAS2020_0252 |
| Song, W.B. | A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WING | ICAS2020_0256 |
| Song, G. | VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING | ICAS2020_0284 |
| Song, B.F. | STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER | ICAS2020_0436 |
| Song, C. | PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGN | ICAS2020_0463 |
| Song, W.-P. | NATURAL-LAMINAR-FLOW AIRFOIL DESIGN OPTIMIZATION CONSIDERING CROSSFLOW INSTABILITY WHEN CONFIGURED ON A SWEPT WING | ICAS2020_0472 |
| Song, C.-X. | RESEARCH OF LABYRINTH SEALS MEASUREMENT-BASED PROBABILITISTIC ANALYSIS METHOD FOR TURBOFAN INTERNAL AIR SYSTEM | ICAS2020_0531 |
| Song, W.-P. | FAST METHOD AND AN INTEGRATED CODE FOR SONIC BOOM PREDICTION OF SUPERSONIC COMMERCIAL AIRCRAFT | ICAS2020_0600 |
| Song, B.-F. | FAST METHOD AND AN INTEGRATED CODE FOR SONIC BOOM PREDICTION OF SUPERSONIC COMMERCIAL AIRCRAFT | ICAS2020_0600 |
| Song, W.-M. | AN AGILE PRACTICE OF AVIONICS SYSTEM DEVELOPMENT | ICAS2020_0609 |
| Song, C. | AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE | ICAS2020_0631 |
| Song, C. | EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADE | ICAS2020_0704 |
| Song, B.-F. | AERODYNAMIC AND STRUCTURAL DESIGN OF THE COMPOSITE PROPELLER FOR NEAR SPACE VEHICLES | ICAS2020_0722 |
| Song, W.-P. | IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC MODELING PROBLEMS | ICAS2020_0787 |
| Song, B.-F. | NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION | ICAS2020_0826 |
| Song, W.-P. | DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS | ICAS2020_0839 |
| Song, Z.C. | MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORK | ICAS2020_0849 |
| Song, W.-P. | MULTIFIDELITY AERODYNAMIC/STEALTH DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT | ICAS2020_0878 |
| Song, F. | RESEARCH OF THE HYPERSONIC BOUNDARY LAYER INSTABILITIES AND TRANSITION WITH THERMAL-CHEMICAL NON-EQUILIBRIUM EFFECTS | ICAS2020_0944 |
| Song, Y. | AN INTEGRATED METHOD FOR ACCURATE IDENTIFICATION AND DYNAMIC MONITORING OF BUILDINGS IN AERODROME OBSTACLE FREE SPACE | ICAS2020_1061 |
| Song, B.-F. | NUMERICAL SIMULATION OF PITCHING MOTION EFFECTS ON THE AERODYNAMIC PERFORMANCE OF DRAGONFLY-LIKE FLAPPING WING | ICAS2020_1150 |
| Song, B.F. | NUMERICAL SIMULATION OF SWEEPING MOTION EFFECTS ON THE HOVERING DRAGONFLIES | ICAS2020_1167 |
| Song, Z.Y. | TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGY | ICAS2020_1170 |
| Song, B.F. | AERODYNAMIC ANALYSIS OF DRAGONFLY WINGS SPACE DISTRIBUTION ON THREE-DIMENSIONAL DURING HOVERING FLIGHT | ICAS2020_1172 |
| Sorbilli Cardoso de Sousa, R. | NASA-CRM LATERAL-DIRECTIONAL STABILITY DERIVATIVES COMPARISON BETWEEN SEMI-EMPIRICAL, VORTEX LATTICE AND PANEL METHOD | ICAS2020_1190 |
| Soucheleau, B. | BLADE - NATURAL LAMINAR FLOW FLIGHT TESTING | ICAS2020_0220 |
| Soudakov, V.G. | THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE AEROELASTIC CHARACTERISTICS OF THE AFLONEXT PROJECT BIG-SIZE DEMONSTRATOR | ICAS2020_0212 |
| Soudakov, V. | TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFT | ICAS2020_1260 |
| Sousa, J.M.M. | ENERGY HARVESTING FROM PIEZOELECTRIC FRINGES AT THE TRAILING-EDGE OF A FINITE WING WITH LEADING-EDGE TUBERCLES | ICAS2020_0979 |
| Staack, I. | CONNECTING SYSTEM SIMULATION TO AIRCRAFT CONCEPT DEVELOPMENT | ICAS2020_1229 |
| Stalewski, W. | IMPROVEMENT OF HELICOPTER PERFORMANCE THROUGH PULSE AIR JETS BLOWN FROM THE TRAILING EDGE OF MAIN ROTOR BLADES | ICAS2020_0301 |
| Starodubtsev, M.A. | LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICS | ICAS2020_0107 |
| Stasenko, A.L. | EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE | ICAS2020_0894 |
| Steinweg, D.M. | COST AND BENEFIT OF SCHEDULED STRUCTURAL HEALTH MONITORING FOR COMMERCIAL AIRCRAFT | ICAS2020_0117 |
| Stephan, R. | DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL AERODYNAMIC LIFT MECHANISM | ICAS2020_0863 |
| Stumpf, E. | DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL AERODYNAMIC LIFT MECHANISM | ICAS2020_0863 |
| Sturm, F. | STATIC AEROELASTIC TAILORING OF A HIGH-ASPECT-RATIO-WING FOR A SAILPLANE WITH A FORWARD MORPHING WING SECTION | ICAS2020_0575 |
| Su, S. | FRACTURE CRITERION ANALYSIS AND CRACK GROWTH PROPERTY OF MIXED-MODE CRACK EXPERIMENTS | ICAS2020_0118 |
| Su, J. | CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELL | ICAS2020_0285 |
| Su, L. | ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM FOR COMPLICATED PRODUCTS ENGINEERING | ICAS2020_0433 |
| Su, C. | THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDE-BODY CIVIL TRANSPORT | ICAS2020_0676 |
| Su, Y.L. | DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISK | ICAS2020_0713 |
| Su , W. | AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE | ICAS2020_1144 |
| Su., T. | BROADBAND MICROWAVE ABSORBING HONEYCOMB CORE MATERIAL WITH ACTIVE CARBON AS DELEGATES | ICAS2020_0308 |
| Sudol, A. | QUANTIFICATION OF OPERATIONAL EFFECTIVENESS FOR TECHNOLOGY EVALUATION | ICAS2020_1241 |
| Sultan, A. | NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER | ICAS2020_0555 |
| Sun, X. | AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION | ICAS2020_0071 |
| Sun, R.J. | ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS | ICAS2020_0269 |
| Sun, X.-M. | FLIGHT MANAGEMENT SYSTEM REQUIREMENT ANALYSIS FOR TRAJECTORY BASED OPERATION | ICAS2020_0292 |
| Sun, D. | STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATOR | ICAS2020_0305 |
| Sun, H. | VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL | ICAS2020_0313 |
| Sun, Y. | TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR | ICAS2020_0357 |
| Sun, H. | WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONS | ICAS2020_0483 |
| Sun, J.G. | AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION | ICAS2020_0591 |
| Sun, C. | A STUDY ON TRAINING NEEDS ANALYSIS (TNA) METHOD FOR MILITARY AIRCRAFT | ICAS2020_0602 |
| Sun, C. | A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONS | ICAS2020_0712 |
| Sun, Y.F. | SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCES | ICAS2020_0743 |
| Sun, M.-B. | EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0 | ICAS2020_1122 |
| Sun, D. | STUDY ON THE STATISTICAL CHARACTERISTICS OF SKIN FRICTION OF SHOCK WAVE/ TURBULENT BOUDARY LAYER INTERATION IN A HOLLOW FLARE CONFIGURATION AT MACH 6 | ICAS2020_1224 |
| Sun, Y. | TRAJECTORY GENERATION AND CONTROL FOR PERCHING MANEUVERING WITH QUADROTOR | ICAS2020_1247 |
| Suntsov, P.S. | CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS | ICAS2020_0974 |
| Surace, C. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: CONTROL, ALIMENTATION, AND PROPULSION SYSTEMS | ICAS2020_1219 |
| Surace, C. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION | ICAS2020_1222 |
| Suvorova, E. | INTEGRATED ON-BOARD NETWORKS FOR NEXT GENERATION AVIONICS | ICAS2020_0577 |
| Suzuki, S. | FEEDBACK ERROR LEARNING WITH ENHANCED SAMPLING: NEURAL FAULT TOLERANT CONTROLLER OF AIRCRAFT | ICAS2020_0613 |
| Svirsky, Y. | MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS | ICAS2020_0089 |
| Svirsky, Y. | METHODS FOR CALCULATING THE FATIGUE DAMAGE OF A STRUCTURE FOR VARIOUS SPECTRA OF VIBRO-ACOUSTIC LOADS | ICAS2020_0576 |
| Süelözgen, Ö. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Symonov, V. | BIRD STRIKE SIMULATIONS IN MSC.SOFTWARE: CORRELATION BETWEEN THE EXPERIMENTS AND SIMULATIONS | ICAS2020_0017 |
| Takase, R. | LEARNING FLIGHT CONTROL SKILLS BY IMITATING EXPERT DEMONSTRATIONS | ICAS2020_1080 |
| Takenami, H. | IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP | ICAS2020_0557 |
| Tamaki, Y. | UNSTEADY FLOW SIMULATION AROUND MAIN LANDING GEAR USING HIERARCHICAL CARTESIAN GRID METHOD WITH IMMERSED BOUNDARY METHOD | ICAS2020_0677 |
| Tamayama, M. | ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT FOR MORPHING WINGS | ICAS2020_0540 |
| Tan, S. | A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT | ICAS2020_0097 |
| Tan, Z.-G. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Tang, M.T. | THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLE | ICAS2020_0052 |
| Tang, W. | AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLES | ICAS2020_0168 |
| Tang, Z. | CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELL | ICAS2020_0285 |
| Tang, J.-Y. | RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTER | ICAS2020_0304 |
| Tang, Z. | SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRID | ICAS2020_0315 |
| Tang, F.-M. | AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR | ICAS2020_0538 |
| Tang, J. | STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESH | ICAS2020_0686 |
| Tang, X.H. | RESEARCH ON CERTIFICATION MANAGEMENT OF AIRCRAFT ENGINE BASED ON RISK ANALYSIS | ICAS2020_0715 |
| Tang, J. | SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TEST | ICAS2020_0744 |
| Tang, M.-H. | RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLES | ICAS2020_0851 |
| Tang, C. | AERODYNAMIC ANALYSIS OF DRAGONFLY WINGS SPACE DISTRIBUTION ON THREE-DIMENSIONAL DURING HOVERING FLIGHT | ICAS2020_1172 |
| Tao, H. | STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TESTING | ICAS2020_0039 |
| Tao, Y.-J. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Tao, J. | RESEARCH ON AERO-ENGINE COLLABORATIVE DESIGN PROCESS BASED ON SYSTEM ENGINEERING | ICAS2020_0633 |
| Tao, H. | STUDY ON THE AIRWORTHINESS AND COMFORTABLENESS REQUIREMENTS OF AIRCRAFT CABIN AIR CONTAMINATIONS | ICAS2020_0761 |
| Tarnowski, A. | LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE | ICAS2020_0030 |
| Techmer, D. | STATIC AEROELASTIC TAILORING OF A HIGH-ASPECT-RATIO-WING FOR A SAILPLANE WITH A FORWARD MORPHING WING SECTION | ICAS2020_0575 |
| ter Meer, T. | TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFT | ICAS2020_1260 |
| Teubl, D. | FLIGHT TESTING OF 65KG T-FLEX SUBSCALE DEMONSTRATOR | ICAS2020_0707 |
| Thiele, M. | PROPELLER WAKE - OBJECT INTERACTION USING A FREE WAKE MODEL UTILIZING LOCAL MESH SEPARATION | ICAS2020_0209 |
| Thielecke, F. | VALIDATION OF AN AERODYNAMIC MODEL FOR THE ANALYSIS OF SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRICAL PROPULSION | ICAS2020_0145 |
| Tiaglik, M.S. | THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERS | ICAS2020_0176 |
| Tian, H. | COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS | ICAS2020_0114 |
| Tian, J. | CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELL | ICAS2020_0285 |
| Tian, P.Q. | RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORY | ICAS2020_0514 |
| Tian, Z.-Q. | RESEARCH ON STRUCTURAL DESIGN OF TAIL BOOM FOR AN UNMANNED HELICOPTER | ICAS2020_1062 |
| Tian, M.M. | ADRC BASED HIGH MANEUVERING FLIGHT CONTROL LAW DESIGN FOR UAV | ICAS2020_1088 |
| Tiberti, D. | TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X | ICAS2020_0766 |
| Tong, X.Y. | FAILURE PROCESS IDENTIFICATION IN C/SIC SAMPLES WITH A RANGE OF TENSILE PERFORMANCE USING ACOUSTIC EMISSION | ICAS2020_0364 |
| Tong, K. | AN INTEGRATED METHOD FOR ACCURATE IDENTIFICATION AND DYNAMIC MONITORING OF BUILDINGS IN AERODROME OBSTACLE FREE SPACE | ICAS2020_1061 |
| Tronco, M.L. | USAGE OF MQTT, ROS, AND AWS IN THE MANUFACTURING PROCESS OF AIRCRAFTS | ICAS2020_1223 |
| Troshin, A. | VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING | ICAS2020_0033 |
| Tsai, M.-H. | NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER ADVERSE SITUATIONS | ICAS2020_0482 |
| Tsirkunov, Y.M. | MODELING AND SIMULATION OF DUSTY GAS FLOW IN AERODYNAMICS | ICAS2020_0441 |
| Tsukamoto, R. | ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT FOR MORPHING WINGS | ICAS2020_0540 |
| Tufilli, R. | DESIGN OF A PROTOTYPE UNMANNED LIGHTER-THAN-AIR PLATFORM FOR REMOTE SENSING: STRUCTURAL DESIGN AND OPTIMIZATION | ICAS2020_1222 |
| Tuktarov, S. | MATHEMATICAL MODELS FOR ANALYSIS AND OPTIMIZATION OF AIRCRAFT STRUCTURAL COMPONENTS TAKING INTO CONSIDERATION OF LOCAL STRESS DISTRIBUTION | ICAS2020_0593 |
| Uchiyama, K. | LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV | ICAS2020_0150 |
| Ur Rahman, H. | NUMERICAL EVALUATION OF DYNAMIC STABILITY DERIVATIVES FOR HIGH LIFT DEVICES | ICAS2020_0556 |
| Vaganov, A.V. | LONGITUDINAL VORTEX FORMATION IN HYPERSONIC BOUNDARY LAYER ON BLUNTED DELTA WING AND ITS EFFECT ON FLOW CHARACTERISTICS | ICAS2020_0107 |
| Valpiani, F. | DESIGN OF A VERTICAL DITCHING TEST | ICAS2020_0763 |
| van Doeselaar, J. | STRUCTURAL HEALTH MONITORING - THE ROUTE TO CONDITION BASED MAINTENANCE | ICAS2020_0347 |
| Varyukhin, A.N. | UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM | ICAS2020_0451 |
| Varyukhin, A.N. | CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS | ICAS2020_0974 |
| Veerasamy, D. | AN OBJECTIVE APPROACH FOR MEASURING INTERMITTENCY IN THE TRANSITIONAL BOUNDARY LAYER | ICAS2020_0149 |
| Veerasamy, D. | UNPRECEDENTED TRANSITIONAL CHARACTERISTICS IN WAKE – BOUNDARY LAYER INTERACTION | ICAS2020_1314 |
| Vendrichoski, J.C. | ROBUST CONTROL OF UNMANNED AERIAL VEHICLE WITH TILT ROTORS AND CAMERA | ICAS2020_1006 |
| Vercella, V. | TECHNOLOGY ROADMAPS FOR THE DEVELOPMENT OF FUTURE HIGH-SPEED TRANSPORTATION SYSTEMS | ICAS2020_0958 |
| Veresnikov, G. | THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEM | ICAS2020_0239 |
| Verma, D. | BLENDED WING BODY (BWB) PLANFORM MULTIDISCIPLINARY OPTIMISATION (MDO) FOR EARLY STAGE AIRCRAFT DESIGN USING MODEL BASED ENGINEERING | ICAS2020_0244 |
| Veron, S. | CONDITION BASED MAINTENANCE (CBM) IN THE DIGITAL TRANSFORMATION STREAM | ICAS2020_0659 |
| Verstraete, D. | LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE | ICAS2020_0165 |
| Villani, E. | GAZE-BASED INTERFACE FOR FLIGHT CONTROL: RESULTS OF INITIAL EXPERIMENTS WITH THE SYSTEM | ICAS2020_0645 |
| Villani, E. | HYBRID MODELLING FOR FULL MISSION SIMULATION | ICAS2020_0980 |
| Villani, E. | FITT’S LAW WITH EYE TRACKING ON A FLIGHT SIMULATOR COCKPIT | ICAS2020_0982 |
| Vilumbrales-Garcia, R. | RAPID THEORETICAL EVALUATION OF FORMATION FLIGHT PERFORMANCE | ICAS2020_0648 |
| Vincent, A. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Viola, N. | THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE | ICAS2020_0493 |
| Viola, N. | H2020 STRATOFLY PROJECT: FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS | ICAS2020_0840 |
| Viola, N. | TECHNOLOGY ROADMAPS FOR THE DEVELOPMENT OF FUTURE HIGH-SPEED TRANSPORTATION SYSTEMS | ICAS2020_0958 |
| Viola, N. | INTEGRATION OF AN INCREASING-FIDELITY AERODYNAMIC MODELLING APPROACH IN THE CONCEPTUAL DESIGN OF HYPERSONIC CRUISER | ICAS2020_1195 |
| Viviani, A. | OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE | ICAS2020_0164 |
| Viviani, A. | LONGITUDINAL AND LATERAL-DIRECTIONAL AERODYNAMICS OF A RE-USABLE HIGH-SPEED VEHICLE | ICAS2020_0165 |
| Vlasov, A.V. | UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM | ICAS2020_0451 |
| Voevodenko, N.V. | METHODICAL STUDIES OF THE POSSIBILITY TO APPLY A NUMERICAL METHOD WITH BUILD-IN EMPIRICAL CRITERIA FOR DETERMIMING THE LAMINAR-TO-TURBULENT TRANSITION ON THE CONE SURFACE AT HIGH MACH NUMBERS | ICAS2020_0435 |
| Volkov, V.E. | THE USE OF SOFTWARE “VIRTUAL ENGINE” FOR TIMELY GAS-TURBINE ENGINE FAULT LOCALIZATIONS | ICAS2020_0881 |
| Volpe, E. | ADJOINT-BASED STUDY OF THE AERODYNAMIC CENTER SHIFT IN THE TRANSONIC FLOW REGIME | ICAS2020_0985 |
| Voronin, A.Y. | DESIGN TECHNIQUE OF INTEGRAL ALGORITHMS OF HELICOPTER FBW CONTROL SYSTEM | ICAS2020_0534 |
| Voß, C. | THE POTENTIAL OF CASING TREATMENTS FOR TRANSONIC COMPRESSORS: EVALUATION BASED ON AXIAL-SLOT AND ROTOR BLADE OPTIMIZATION | ICAS2020_1054 |
| Wahlich, M. | ACTIVE FLOW- LOADS & NOISE CONTROL ON NEXT GENERATION WING (AFLONEXT): OVERVIEW AND RESULTS | ICAS2020_1257 |
| Wahlich, M. | TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFT | ICAS2020_1260 |
| Wallin, M. | THE INFLUENCE OF THE NUMBER OF ADHESIVE PLIES (FM 300-2) ON FRACTURE PROPERTIES | ICAS2020_0295 |
| Wallin, M. | ADJUSTED SHAPES OF ADHESIVELY BONDED REPAIR PATCHES FOR THE EARLY INDICATION OF DEBOND IN FIGHTER AIRCRAFT STRUCTURES | ICAS2020_0297 |
| Wan, T. | NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER ADVERSE SITUATIONS | ICAS2020_0482 |
| Wan, Z.Q. | AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLES | ICAS2020_1109 |
| Wan, Z.Q. | TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLE | ICAS2020_1110 |
| Wan, K.D. | LARGE-EDDY SIMULATION OF A SWIRLING AVIATION KEROSENE SPRAY FLAME USING 3-COMPONENT SURROGATE FUELS | ICAS2020_1264 |
| Wang, Q. | THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLE | ICAS2020_0052 |
| Wang, G. | AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION | ICAS2020_0071 |
| Wang, H. | AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION | ICAS2020_0071 |
| Wang, B. | EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES | ICAS2020_0093 |
| Wang, G. | EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES | ICAS2020_0093 |
| Wang, M. | EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIV | ICAS2020_0140 |
| Wang, Q. | CONCEPTUAL DESIGN OF A FIXED-WING AQUATIC UAV USING KNOWLEDGE BASED ENGINEERING | ICAS2020_0154 |
| Wang, W. | NUMERICAL SIMULATION ON AERODYNAMIC CHARACTERISTICS OF BIONIC CORRUGATED FLAPPING WING | ICAS2020_0155 |
| Wang, D.-C. | RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES | ICAS2020_0162 |
| Wang, H.-F. | RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES | ICAS2020_0162 |
| Wang, Q. | AIRCRAFT INFLIGHT ICING DETECTION AND DIAGNOSIS METHODS | ICAS2020_0163 |
| Wang, X.J. | RESEARCH ON THE PRESSURE COMFORT OF PILOT HELMETS | ICAS2020_0180 |
| Wang, J.H. | RESEARCH ON THE PRESSURE COMFORT OF PILOT HELMETS | ICAS2020_0180 |
| Wang, L.-B. | THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT | ICAS2020_0181 |
| Wang, W. | THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT | ICAS2020_0181 |
| Wang, J. | ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META-MODEL | ICAS2020_0200 |
| Wang, Y.B. | EFFECT OF COMPLEX FLOW PROFILES AT COMBUSTOR EXIT ON TURBINE CHARACTERISTICS | ICAS2020_0257 |
| Wang, K. | HYBRID IGNITION PROBABILITY METHOD TO PREDICT THE IGNITION PERFORMANCE OF A GAS TURBINE COMBUSTOR | ICAS2020_0259 |
| Wang, C.X. | APPLICATION OF DEVELOPMENT ASSURANCE METHODOLOGIES TO ELECTRONIC ENGINE CONTROL SYSTEM (EECS) | ICAS2020_0268 |
| Wang, B.-W. | TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT | ICAS2020_0271 |
| Wang, B. | A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES | ICAS2020_0272 |
| Wang, L. | A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES | ICAS2020_0272 |
| Wang, Z. | VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING | ICAS2020_0284 |
| Wang, B.-W. | RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTER | ICAS2020_0304 |
| Wang, J. | INCORPORTING KNOWLEDGE COVERAGE MEASUREMENT INTO KNOWLEDGE TRANSFORMATION FROM DATA FOR KNOWLEDGE ACCUMULATION | ICAS2020_0343 |
| Wang , P. | AERODYNAMIC NOISE SIMULATION OF CIVIL AIRCRAFT LANDING GEARS BASED ON LES-SMARGORINSKY MODEL | ICAS2020_0351 |
| Wang, Y.H. | INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHM | ICAS2020_0408 |
| Wang, W.-K. | PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNEL | ICAS2020_0418 |
| Wang, B. | STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER | ICAS2020_0436 |
| Wang, L.-I. | COMPREHENSIVE REDUNDANCY MANAGEMENT AND VERIFICATION STRATEGY FOR TASK-BASED AIR MANAGEMENT SYSTEM | ICAS2020_0485 |
| Wang, L.-X. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Wang, L. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Wang, H. | ASSEMBLY QUALITY OPTIMIZATION APPROACH FOR LARGE-SCALE ACTIVE COMPONENTS BASED ON REVERSE ENGINEERING | ICAS2020_0542 |
| Wang, X.B. | STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTION | ICAS2020_0598 |
| Wang, Q. | A STUDY ON TRAINING NEEDS ANALYSIS (TNA) METHOD FOR MILITARY AIRCRAFT | ICAS2020_0602 |
| Wang, R. | EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODEL | ICAS2020_0619 |
| Wang, B. | THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDE-BODY CIVIL TRANSPORT | ICAS2020_0676 |
| Wang, H. | A SUBJECTIVE EVALUATION METHOD OF AIRCRAFT VIBRATION IN FLIGHT TEST | ICAS2020_0684 |
| Wang, Y.Y. | EFFECT OF DROPLET MVD ON ICING COLLECTION EFFICIENCY FOR A HELICOPTER BLADE | ICAS2020_0704 |
| Wang, H.F. | RESEARCH ON THE TRIGGERING CONDITIIONS OF EJECTABLE RECORDER FOR CIVIL AIRCRAFT | ICAS2020_0706 |
| Wang, M. | EXPERIMENTAL STUDY ON SUPERSONIC CAVITY ACOUSTICS | ICAS2020_0708 |
| Wang, F. | THE STUDY OF UNMANNED AERIAL VEHICLE FLYING QUALITIES FLIGHT TEST METHOD BASED ON TIME-DELAY EVALUATION | ICAS2020_0710 |
| Wang, C.X. | RESEARCH ON CERTIFICATION MANAGEMENT OF AIRCRAFT ENGINE BASED ON RISK ANALYSIS | ICAS2020_0715 |
| Wang, X.K. | RESEARCH ON CERTIFICATION MANAGEMENT OF AIRCRAFT ENGINE BASED ON RISK ANALYSIS | ICAS2020_0715 |
| Wang, Z.J. | IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEM | ICAS2020_0723 |
| Wang, W.H. | SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCES | ICAS2020_0743 |
| Wang, Q.C. | SNGR BASED FAST ANALYSIS OF SLAT TRACK NOISE SOURCES | ICAS2020_0743 |
| Wang, C.Y. | AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESS | ICAS2020_0774 |
| Wang, D. | DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMING | ICAS2020_0822 |
| Wang, X. | DATA FUSION UNSTEADY AERODYNAMIC MODELING BASED ON EXPERIMENTAL DATA | ICAS2020_0842 |
| Wang, S.Z. | INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINE | ICAS2020_0845 |
| Wang, Y. | MULTIFIDELITY AERODYNAMIC/STEALTH DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT | ICAS2020_0878 |
| Wang, Y.J. | STUDY ON THE FATIGUE SCATTER FACTOR UNDER SEVERE LOAD SPECTRUM | ICAS2020_0904 |
| Wang, W.K. | RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTION | ICAS2020_0909 |
| Wang, H.W. | SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODEL | ICAS2020_0928 |
| Wang, R. | APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROL | ICAS2020_0978 |
| Wang, H. | ON THE DEVELOPMENT OF FUSELAGE WEIGHT ESTIMATION TOOL INTO AIRCRAFT MULTIDISCIPLINARY DESIGN ENVIRONMENT | ICAS2020_1068 |
| Wang, H. | ON THE DEVELOPMENT OF FUSELAGE WEIGHT ESTIMATION TOOL INTO AIRCRAFT MULTIDISCIPLINARY DESIGN ENVIRONMENT | ICAS2020_1068 |
| Wang, H. | NUMERICAL ANALYSIS METHOD OF CIVIL AIRCRAFT DITCHING FLOATING PERFORMANCE | ICAS2020_1069 |
| Wang, H. | NUMERICAL ANALYSIS METHOD OF CIVIL AIRCRAFT DITCHING FLOATING PERFORMANCE | ICAS2020_1069 |
| Wang, D. | STUDY ON THE OUT-OF-PLANE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT 350°C | ICAS2020_1072 |
| Wang, W.S. | ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION | ICAS2020_1074 |
| Wang, L. | MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOW | ICAS2020_1078 |
| Wang, Y. | A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODY | ICAS2020_1099 |
| Wang, Z.G. | A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODY | ICAS2020_1099 |
| Wang, Y.-H. | NUMERICAL STUDY OF HIGH TEMPERATURE TRANSVERSE PULSE JET IN THE SUPERSONIC COMBUSTION CHAMBER | ICAS2020_1100 |
| Wang, X. | AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLES | ICAS2020_1109 |
| Wang, X.Z. | TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLE | ICAS2020_1110 |
| Wang, T.-Y. | EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0 | ICAS2020_1122 |
| Wang, C. | EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0 | ICAS2020_1122 |
| Wang, J.X. | EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACE | ICAS2020_1138 |
| Wang, X.P. | AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE | ICAS2020_1144 |
| Wang, Z.-W. | INFLUENCE OF SHOCK TRAIN ON HEAT FLUX DISTRIBUTION OF A CIRCULAR CONSTANT-AREA ISOLATOR | ICAS2020_1146 |
| Wang, Y.H. | THE STUDY ON ANTI-ICING AREAS OF LEADING-EDGE SLATS IN MODERN CIVIL AIRCRAFT | ICAS2020_1154 |
| Wang, R. | A REDUNDANT ADAPTIVE NAVIGATION METHOD BASED ON DYNAMIC PERFORMANCE EVALUATION FOR AEROSPACE VEHICLE | ICAS2020_1180 |
| Wang, L.F. | RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGE | ICAS2020_1203 |
| Wang, Y. | A POLE CONFIGURATION CONTROLLER FOR FIXED HEIGHT CONTROL OF TILT ROTOR AIRCRAFT | ICAS2020_1228 |
| Wang, M. | NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION ON FLUTTER AND NON-SYNCHRONOUS VIBRATION | ICAS2020_1250 |
| Wang, Z.-Y. | ASCENT TRAJECTORY OPTIMIZATION OF HYPERSONIC VEHICLE USING SWARM INTELLIGENT METHOD | ICAS2020_1266 |
| Wang, Y.-L. | ASCENT TRAJECTORY OPTIMIZATION OF HYPERSONIC VEHICLE USING SWARM INTELLIGENT METHOD | ICAS2020_1266 |
| Wang, Y.H. | A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOS | ICAS2020_1309 |
| Wangai, A.W. | TOTAL LIFE CYCLE COST AND EMISSION OF ELECTRIC, HYBRID-ELECTRIC AIRCRAFT | ICAS2020_0635 |
| Wassink, P. | CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT | ICAS2020_0185 |
| Wassink, P. | ASSESSMENT OF THREE COMMUTER AIRCRAFT CONCEPTS FROM A TRANSPORT SYSTEM PERSPECTIVE | ICAS2020_0207 |
| Watanabe, M. | ENDURANCE ANALYSIS OF BATTERY-POWERED MULTICOPTERS: DERIVATION OF PROPER CUT-OFF VOLTAGE USING DC MOTOR MODEL | ICAS2020_0769 |
| Watanabe, A. | ENDURANCE ANALYSIS OF BATTERY-POWERED MULTICOPTERS: DERIVATION OF PROPER CUT-OFF VOLTAGE USING DC MOTOR MODEL | ICAS2020_0769 |
| Webster, K. | INTEGRATION OF SPACE VEHICLE OPERATIONS INTO THE UNITED ARAB EMIRATES AIR TRAFFIC MANAGEMENT - AN IMPACT ANALYSIS | ICAS2020_1213 |
| Wegener, P. | INTEGRATION OF FUSELAGE-MOUNTED OVER-WING ENGINES ON A MID-RANGE AIRCRAFT | ICAS2020_1194 |
| Wei, D. | AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLES | ICAS2020_0168 |
| Wei, B.B. | APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITION | ICAS2020_0264 |
| Wei, X. | MEMS-BASED DISTRIBUTED NAVIGATION SYSTEM | ICAS2020_0344 |
| Wei, B.-B. | ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL | ICAS2020_0516 |
| Wei, H.F. | BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES | ICAS2020_0574 |
| Wei, Z.B. | IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEM | ICAS2020_0723 |
| Wei, D. | MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION | ICAS2020_0805 |
| Wei, D. | A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTS | ICAS2020_0833 |
| Wei, H.F. | A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINE | ICAS2020_1114 |
| Weigel, P. | TOWARDS THE INDUSTRIAL APPLICATION OF ACTIVE FLOW CONTROL AT THE PYLON/WING JUNCTION OF CIVIL AIRCRAFT | ICAS2020_1260 |
| Weiss, F. | AERODYNAMIC AND STRUCTURAL MODELING IN THE ROTORCRAFT MULTI-PHYSICS SIMULATION VAST | ICAS2020_0584 |
| Wen, Q. | AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR | ICAS2020_0538 |
| Wen, P.C. | AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION | ICAS2020_0591 |
| Wen, J.R. | DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE | ICAS2020_1135 |
| Willert, C. | MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT | ICAS2020_0523 |
| Witt, T. | LANDING PLATFORM FOR URBAN AIR MOBILITY VEHICLES INTEGRATED INTO PARKING LOT INFRASTRUCTURE IN DENSELY BUILT-UP AREAS | ICAS2020_1217 |
| Woehler, S. | FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFT | ICAS2020_0238 |
| Wojtas, M. | PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER | ICAS2020_0747 |
| Wolkov, A. | VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING | ICAS2020_0033 |
| Wong, P.W.C. | HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTURE | ICAS2020_0236 |
| Wu, C.H. | COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS | ICAS2020_0114 |
| Wu, H. | MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSOR | ICAS2020_0138 |
| Wu, H. | EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIV | ICAS2020_0140 |
| Wu, J.-T. | TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT | ICAS2020_0271 |
| Wu, X.-H. | RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUE | ICAS2020_0273 |
| Wu, M. | RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM | ICAS2020_0413 |
| Wu, L. | RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM | ICAS2020_0413 |
| Wu, J.T. | RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORY | ICAS2020_0514 |
| Wu, T. | AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERS | ICAS2020_0541 |
| Wu, J.M. | BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES | ICAS2020_0574 |
| Wu, J.-F. | DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSOR | ICAS2020_0632 |
| Wu, F. | RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED | ICAS2020_0661 |
| Wu, W.H. | DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISK | ICAS2020_0713 |
| Wu, X.-J. | NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODEL | ICAS2020_0796 |
| Wu, B. | BASED ON SYSTEMS ENGINEERING PROCESS THE CIVIL AIRCRAFT PROJECT PRODUCT BREAKDOWN STRUCTURE DEVELOPMENT RESEARCH | ICAS2020_1018 |
| Wu, J.M. | FLOW AND HEAT TRANSFER MECHANISM OF JET IMPINGEMENT COOLING ONTO MID-CHORD REGINE OF TWISTED BLADE | ICAS2020_1106 |
| Wu, J.M. | A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINE | ICAS2020_1114 |
| Wu, J.-M. | NUMERICAL STUDY ON COOLING CHARACTERISTICS IN CHANNELS WITH PIN FIN ARRAYS UNDER HIGH TEMPERATURE/PRESSURE CONDITIONS | ICAS2020_1151 |
| Wu, W.H. | INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBER | ICAS2020_1185 |
| Wu, B. | THE CIVIL AIRCRAFT DEVELOPMENT PROJECT RISK MANAGEMENT RESEARCH | ICAS2020_1244 |
| Wu, F. | DEPLOY SYSTEM ENGINEERING METHODS IN AIRBORNE GUIDANCE NAVIGATION CONTROL DOMAIN | ICAS2020_1296 |
| Wunderlich, T. | COLLABORATIVE HIGH FIDELITY AND HIGH PERFORMANCE COMPUTING-BASED MDO STRATEGIES FOR TRANSPORT AIRCRAFT DESIGN | ICAS2020_0693 |
| Xia, L. | SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHOD | ICAS2020_0094 |
| Xia, Z.H. | EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACK | ICAS2020_0182 |
| Xia, D.W. | SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TEST | ICAS2020_0744 |
| Xia, P. | AN OVERVIEW OF HELICOPTER DEVELOPMENT IN CHINA AND SOME NEW HELICOPTER TECHNOLOGIES | ICAS2020_1282 |
| Xiao, G.M. | AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLES | ICAS2020_0168 |
| Xiao, W. | HYBRID IGNITION PROBABILITY METHOD TO PREDICT THE IGNITION PERFORMANCE OF A GAS TURBINE COMBUSTOR | ICAS2020_0259 |
| Xiao, G.M. | MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION | ICAS2020_0805 |
| Xiao, G.M. | A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTS | ICAS2020_0833 |
| Xiao, G.-M. | COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION | ICAS2020_1176 |
| Xiao, Z.-Y. | METHODS OF DIRECTIONAL COARSENING FOR UNSTRUCTURED GRIDS AND APPLICATIONS | ICAS2020_1261 |
| Xie, H. | PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTS | ICAS2020_0392 |
| Xie, H. | RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DIS | ICAS2020_0865 |
| Xie, Y. | ARTIFICIAL INTELLIGENCE AND HUMAN-MACHINE INTERACTIONS FOR STREAM-BASED AIR TRAFFIC FLOW MANAGEMENT | ICAS2020_1009 |
| Xie, R.X. | A LOCAL CORRELATION-BASED ALGEBRAIC TRANSITION MODEL WITH COMPRESSIBILITY AND CROSSFLOW CORRECTION | ICAS2020_1098 |
| Xing, C. | RESEARCH ON ARCHITECTURE FRAMEWORK MODEL BASED EVALUATION INDEX FOR AVIATION SCIENCE & TECHNOLOGY MANAGEMENT | ICAS2020_0077 |
| Xing, C.G. | A CONTRASTIVE STUDY OF STANDARD SPECIFICATION FOR TECHNOLOGY READINESS ASSESSMENT | ICAS2020_0252 |
| Xing, P.P. | MODEL-BASED VIRTUAL INTEGRATED TEST METHOD FOR AVIONICS SYSTEM | ICAS2020_1212 |
| Xiong, Z. | EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODEL | ICAS2020_0619 |
| Xiong, B. | A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODY | ICAS2020_1099 |
| Xiong, Z. | A REDUNDANT ADAPTIVE NAVIGATION METHOD BASED ON DYNAMIC PERFORMANCE EVALUATION FOR AEROSPACE VEHICLE | ICAS2020_1180 |
| Xu, J.F. | A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS | ICAS2020_0036 |
| Xu, J. | RESEARCH ON ARCHITECTURE FRAMEWORK MODEL BASED EVALUATION INDEX FOR AVIATION SCIENCE & TECHNOLOGY MANAGEMENT | ICAS2020_0077 |
| Xu, J. | RESEARCH ON THE PRESSURE COMFORT OF PILOT HELMETS | ICAS2020_0180 |
| Xu, X.W. | EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACK | ICAS2020_0182 |
| Xu, A. | ENABLING THE SMART SHOP FLOOR THROUGH THE INTEGRATION OF IOT AND AUTONOMOUS INTELLIGENCE | ICAS2020_0310 |
| Xu, M. | AN ADJOINT-BASDF AERO-STRUCTURAL DESIGN OPTIMIZATION METHOD USING DYNAMIC MESH TECHNOLOGY | ICAS2020_0317 |
| Xu, L. | DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEM | ICAS2020_0386 |
| Xu, Y.-L. | MODAL DAMPING PARAMETER IDENTIFICATION METHOD BASED ON IMPROVED VMD AND ENVELOPE FITTING AND ITS APPLICATION | ICAS2020_0397 |
| Xu, J.H. | STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER | ICAS2020_0436 |
| Xu, Z.-M. | NATURAL-LAMINAR-FLOW AIRFOIL DESIGN OPTIMIZATION CONSIDERING CROSSFLOW INSTABILITY WHEN CONFIGURED ON A SWEPT WING | ICAS2020_0472 |
| Xu, C.-Z. | AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHING | ICAS2020_0476 |
| Xu, Y. | DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAIN | ICAS2020_0503 |
| Xu, C.-Z. | IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC MODELING PROBLEMS | ICAS2020_0787 |
| Xu, J.-H. | DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS | ICAS2020_0839 |
| Xu, H. | INVESTIGATION OF AERODYNAMIC INTERACTIONS BETWEEN NACA0012 AIRFOILS IN TANDEM | ICAS2020_1063 |
| Xu, Y.X. | STUDY ON THE OUT-OF-PLANE COMPRESSION PROPERTIES OF MULTISTAGE TITANIUM ALLOY LATTICE METAMATERIALS AT 350°C | ICAS2020_1072 |
| Xu, S.C. | A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODY | ICAS2020_1099 |
| Xuan, L. | BROADBAND MICROWAVE ABSORBING HONEYCOMB CORE MATERIAL WITH ACTIVE CARBON AS DELEGATES | ICAS2020_0308 |
| Xue, B. | INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHM | ICAS2020_0408 |
| Xue, H.Z. | AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESS | ICAS2020_0774 |
| Xue, B. | PRECISION ANALYSIS AND INDEX DISTRIBUTION SYSTEM DESIGN OF AVIONICS SYSTEM BASED ON BP NEURAL NETWORK | ICAS2020_0808 |
| Xue, P. | INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINE | ICAS2020_0845 |
| Xue, G.-L. | A METHOD OF MANEUVER IDENTIFICATION AND TRAJECTORY PREDICTION FOR AGILE TARGET | ICAS2020_0948 |
| Xue, T. | DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE | ICAS2020_1135 |
| Xue, B. | A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOS | ICAS2020_1309 |
| Yan, C.Y. | MULTIPOINT OPTIMIZATION OF TRANSONIC NATURAL LAMINAR FLOW NACELLES | ICAS2020_0501 |
| Yan, Z.K. | SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TEST | ICAS2020_0744 |
| Yan, P. | AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESS | ICAS2020_0774 |
| Yang, W.Q. | NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING WITH SLOTTED-TIP | ICAS2020_0102 |
| Yang, M.-S. | EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIV | ICAS2020_0140 |
| Yang, W. | NUMERICAL SIMULATION ON AERODYNAMIC CHARACTERISTICS OF BIONIC CORRUGATED FLAPPING WING | ICAS2020_0155 |
| Yang, J. | EXPERIMENTAL STUDY ON ATTENUATION PERFORMANCE OF SHOCK-ABSORBING INSERT | ICAS2020_0157 |
| Yang, X. | A SIMPLIFIED MODEL FOR THE SIMULATION OF SYNERGISTIC AIR-BREATHING ROCKET ENGINE | ICAS2020_0160 |
| Yang, Q. | A SIMPLIFIED MODEL FOR THE SIMULATION OF SYNERGISTIC AIR-BREATHING ROCKET ENGINE | ICAS2020_0160 |
| Yang, X.F. | AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLES | ICAS2020_0168 |
| Yang, Y. | A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES | ICAS2020_0272 |
| Yang, Y. | VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING | ICAS2020_0284 |
| Yang , W. | MECHANISM DESIGN AND AERODYNAMIC RESEARCH OF RETRACTABLE FOLDING FLAPPING WING | ICAS2020_0333 |
| Yang, C. | PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTS | ICAS2020_0392 |
| Yang, X. | EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY | ICAS2020_0400 |
| Yang, D. | EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY | ICAS2020_0400 |
| Yang, H. | RESEARCH ON OPTIMIZATION TECHNOLOGY FOR CONTROL PARAMETERS OF EJECTION SEAT BASED ON PSO ALGORITHM | ICAS2020_0413 |
| Yang, X.D. | AERODYNAMIC OPTIMIZATION DESIGN OF DOUBLE BLUNT ROTOR AIRFOIL WITH LARGE THICKNESS IN FORWARD AND REVERSE FLOW | ICAS2020_0424 |
| Yang, M.S. | EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR | ICAS2020_0429 |
| Yang, X.D. | STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER | ICAS2020_0436 |
| Yang, J.-H. | COMPREHENSIVE REDUNDANCY MANAGEMENT AND VERIFICATION STRATEGY FOR TASK-BASED AIR MANAGEMENT SYSTEM | ICAS2020_0485 |
| Yang, Y.-J. | AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE | ICAS2020_0631 |
| Yang, C. | AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE | ICAS2020_0631 |
| Yang, C.-Q. | RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED | ICAS2020_0661 |
| Yang, Y. | A METHOD FOR CALCULATING TORSION ANGLE OF FLEXIBLE RETICULAR TUBE AT DIFFERENT POSITIONS | ICAS2020_0712 |
| Yang, J.-B. | AERODYNAMIC AND STRUCTURAL DESIGN OF THE COMPOSITE PROPELLER FOR NEAR SPACE VEHICLES | ICAS2020_0722 |
| Yang, X.F. | MULTI-SCALE CFD/MD MODELLING OF HIGH-ENTHALPY FLOW/TPS INTERACTION AND ITS PRELIMINARY AERONAUTICAL APPLICATION | ICAS2020_0805 |
| Yang, X.-W. | NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION | ICAS2020_0826 |
| Yang, W.-Q. | NUMERICAL SIMULATION OF A BIO-INSPIRED FLEXIBLE FLAPPING-WING BASED ON EXPERIMENTAL MEASURED DEFORMATION | ICAS2020_0826 |
| Yang, W. | COMPUTATIONAL FLUID-STRUCTURE INTERACTIONS OF A 3D FLEXIBLE FLAPPING WING | ICAS2020_0836 |
| Yang, Y.F. | INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINE | ICAS2020_0845 |
| Yang, C.-G. | RESEARCH ON STRUCTURAL DESIGN OF TAIL BOOM FOR AN UNMANNED HELICOPTER | ICAS2020_1062 |
| Yang, Y.-X. | EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0 | ICAS2020_1122 |
| Yang, X.H. | DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE | ICAS2020_1135 |
| Yang, Z. | EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACE | ICAS2020_1138 |
| Yang, G.J. | NUMERICAL SIMULATION STUDY ON BOUNDARY LAYER FLOW AND DRAG REDUCTION CHARACTERISTICS OF RIBLETS | ICAS2020_1140 |
| Yang, X. | INFLUENCE OF SHOCK TRAIN ON HEAT FLUX DISTRIBUTION OF A CIRCULAR CONSTANT-AREA ISOLATOR | ICAS2020_1146 |
| Yang, W.-Q. | NUMERICAL SIMULATION OF PITCHING MOTION EFFECTS ON THE AERODYNAMIC PERFORMANCE OF DRAGONFLY-LIKE FLAPPING WING | ICAS2020_1150 |
| Yang, Y.J. | NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH-SPEED VEHICLES | ICAS2020_1157 |
| Yang, W.Q. | NUMERICAL SIMULATION OF SWEEPING MOTION EFFECTS ON THE HOVERING DRAGONFLIES | ICAS2020_1167 |
| Yang, W.Q. | AERODYNAMIC ANALYSIS OF DRAGONFLY WINGS SPACE DISTRIBUTION ON THREE-DIMENSIONAL DURING HOVERING FLIGHT | ICAS2020_1172 |
| Yang, X.-F. | COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION | ICAS2020_1176 |
| Yang, W.Q. | NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTS | ICAS2020_1183 |
| Yang, W. | INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBER | ICAS2020_1185 |
| Yang, J.J. | NUMERICAL SIMULATION OF LOCAL LONG SHALLOW CAVITY EFFECT ON THE STABILITY OF A HYPERSONIC BOUNDARY LAYER | ICAS2020_1189 |
| Yang, W.Q. | NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WING | ICAS2020_1240 |
| Yao, X.H. | A STRUCTURE DESIGN OF CFRP REAR PRESSURE BULKHEAD WITHOUT STIFFENERS | ICAS2020_0109 |
| Yao, L.J. | FAILURE PROCESS IDENTIFICATION IN C/SIC SAMPLES WITH A RANGE OF TENSILE PERFORMANCE USING ACOUSTIC EMISSION | ICAS2020_0364 |
| Yao, Y.M. | AERODYNAMIC OPTIMIZATION DESIGN OF DOUBLE BLUNT ROTOR AIRFOIL WITH LARGE THICKNESS IN FORWARD AND REVERSE FLOW | ICAS2020_0424 |
| Yao, R. | FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATION | ICAS2020_1127 |
| Yao, J. | NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAP | ICAS2020_1149 |
| Yao, Z.C. | RESEARCH ON AIRCRAFT-LEVEL PHYSICAL INTEGRATION VERIFICATION TEST TECHNOLOGY | ICAS2020_1232 |
| Ye , Z. | DESIGN OF A HYBRID VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO CIVIL AVIATION AIR TRAFFIC CONTROL SYSTEM | ICAS2020_0468 |
| Yerramalli, C.S. | METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WING | ICAS2020_0085 |
| Yi, S.H. | EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACK | ICAS2020_0182 |
| Yi , M. | DESIGN OF A HYBRID VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO CIVIL AVIATION AIR TRAFFIC CONTROL SYSTEM | ICAS2020_0468 |
| Yin, Y.K. | A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WING | ICAS2020_0256 |
| Yin, Q. | RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUE | ICAS2020_0273 |
| Yin, Y. | EFFECT OF INTER-STAGE BLEEDING ON FLOW STABILITY OF A MULTI-STAGE COMPRESSOR | ICAS2020_0291 |
| Yin, Y.-H. | RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNING | ICAS2020_0388 |
| Yin, Y.-Q. | APPLICATION OF A SKEWED-SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSOR | ICAS2020_0543 |
| Yin, Y.-Q. | DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSOR | ICAS2020_0632 |
| Yin, Y.-Q. | MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGN | ICAS2020_0965 |
| Yin, S. | SMART CIVIL AVIATION TRANSPORTATION SYSTEM | ICAS2020_1283 |
| Ying, J.Y. | STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTION | ICAS2020_0598 |
| Yokosu, A. | IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP | ICAS2020_0557 |
| Yokoyama, N. | DECENTRALIZED CONFLICT DETECTION AND RESOLUTION METHOD ACCOUNTING FOR UNCERTAINTIES OF TRAJECTORIES | ICAS2020_0885 |
| Yoshikawa, N. | FEEDBACK ERROR LEARNING WITH ENHANCED SAMPLING: NEURAL FAULT TOLERANT CONTROLLER OF AIRCRAFT | ICAS2020_0613 |
| You, K. | AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESS | ICAS2020_1118 |
| You, K. | HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILS | ICAS2020_1125 |
| You, Q. | A NOVEL RBF DATA TRANSFER METHOD BASED ON PCA GEOMETRIC FEATURE EXTRACTION | ICAS2020_1160 |
| You, Q. | COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION | ICAS2020_1176 |
| Yu, G.F. | A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDING | ICAS2020_0282 |
| Yu, J. | NONLINEAR UNSTEADY AERODYNAMIC DESCRIPTIONS BASED ON IMPROVED GOMAN’S MODEL | ICAS2020_0796 |
| Yu, J.-Y. | SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICS | ICAS2020_1134 |
| Yu, L. | INTEGRATED AERODYNAMIC DESIGN OF PROPELLER POSITION AND WING SHAPE AT A LOW REYNOLDS NUMBER | ICAS2020_1185 |
| Yu, X. | THE FLOW AND HEAT TRANSFER OF ANALYSIS TO ANNULAR CAVITY IN ENGINE CASE | ICAS2020_1251 |
| Yuan, S.Q. | COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS | ICAS2020_0114 |
| Yuan, X.-X. | STUDY ON THE HEAT FLUX OF HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROLLED BY A MICRO-RAMP VORTEX GENERATOR | ICAS2020_0305 |
| Yuan, X. | SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRID | ICAS2020_0315 |
| Yuan, K. | SUPERSONIC AEROELASTIC ANALYSIS OF AN ALL-MOVABLE WING WITH FREE PLAY | ICAS2020_0393 |
| Yuan, C.-S. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Yuan, M.L. | SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODEL | ICAS2020_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 6 | ICAS2020_1224 |
| Zakharchenko, V.S. | UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM | ICAS2020_0451 |
| Zakharchenko, V.S. | CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS | ICAS2020_0974 |
| Zalewski, P. | THE USE OF REVERSE ENGINEERING AND COMPUTATIONAL FLUID DYNAMICS METHODS IN THE PRELIMINARY DESIGN OF A LOW COST SATELLITE LAUNCH SYSTEM | ICAS2020_1221 |
| Zang, J. | SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATION | ICAS2020_0549 |
| Zaplana Manzano, L. | A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES | ICAS2020_0562 |
| Zappino, E. | ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADS | ICAS2020_0479 |
| Zeng, Q. | EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES | ICAS2020_0093 |
| Zeng, L. | COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION | ICAS2020_1176 |
| Zhan, Z.J. | INFORMATION DISTRIBUTION METHOD FOR MULTI-AIRCRAFT COOPERATION BASED ON COLLABORATIVE FILTERING ALGORITHM | ICAS2020_0408 |
| Zhan, H. | MODELING AND DYNAMICS STABILITY ANALYSIS FOR A BLENDED-WING-BODY AIRCRAFT | ICAS2020_0525 |
| Zhan, H. | SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICS | ICAS2020_1134 |
| Zhan, H. | RESEARCH ON UNSTEADY AERODYNAMIC MODELS AT HIGH ANGLES OF ATTACK BASED ON NONLINEAR REGRESSION | ICAS2020_1152 |
| Zhan, Z.J. | A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOS | ICAS2020_1309 |
| Zhang, H. | AERODYNAMICS CHARACTERISTICS STUDY ON A NATURE LAMINAR FLOW AIRFOIL OF NEAR-SPACE VEHICLE AT LOW REYNOLDS NUMBERS | ICAS2020_0021 |
| Zhang, G. | AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION | ICAS2020_0071 |
| Zhang, G. | HELICOPTER FLIGHT DYNAMICS MODELLING WITH FREE-WAKE METHOD EMBEDDED FOR ROTOR ICING ANALYSES | ICAS2020_0096 |
| Zhang, J. | A PERTURBATION ANALYSIS OF NONLINEARITY IN LANDING-GEAR SHIMMY OF A FLEET AIRCRAFT | ICAS2020_0097 |
| Zhang, S.H. | COMPUTATIONAL STUDY OF THREE-DIMENSIONAL OPEN CAVITY FLOWS | ICAS2020_0114 |
| Zhang, W. | FRACTURE CRITERION ANALYSIS AND CRACK GROWTH PROPERTY OF MIXED-MODE CRACK EXPERIMENTS | ICAS2020_0118 |
| Zhang, Z.-B. | MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSOR | ICAS2020_0138 |
| Zhang, Z.-B. | EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIV | ICAS2020_0140 |
| Zhang, W. | VIRTUAL PROTOTYPING OF ELECTRICAL THSA FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS | ICAS2020_0196 |
| Zhang, Q. | RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREAS | ICAS2020_0219 |
| Zhang, L. | A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDING | ICAS2020_0282 |
| Zhang, Y. | VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING | ICAS2020_0284 |
| Zhang, S. | VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING | ICAS2020_0284 |
| Zhang, R. | MECHANISM DESIGN AND AERODYNAMIC RESEARCH OF RETRACTABLE FOLDING FLAPPING WING | ICAS2020_0333 |
| Zhang, S. | AN ALTERNATIVE BUT EQUIVALENT REALIZATION OF FINITE-HORIZON SUBOPTIMAL CONTROL FOR VEHICLE LANDING | ICAS2020_0348 |
| Zhang, K.-S. | EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR THE “AEROSTRUCT” WING OPTIMIZATION PLATFORM | ICAS2020_0350 |
| Zhang, Y.Z. | FAILURE PROCESS IDENTIFICATION IN C/SIC SAMPLES WITH A RANGE OF TENSILE PERFORMANCE USING ACOUSTIC EMISSION | ICAS2020_0364 |
| Zhang, Y. | DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEM | ICAS2020_0386 |
| Zhang, Y.-F. | RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNING | ICAS2020_0388 |
| Zhang, W. | PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2020_0398 |
| Zhang, Y. | PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2020_0398 |
| Zhang, Z.B. | EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR | ICAS2020_0429 |
| Zhang, Y. | AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHING | ICAS2020_0476 |
| Zhang, L. | WIND-TUNNEL INVESTIGATION OF COMMERCIAL TRANSPORT AIRCRAFT STATIC AND DYNAMIC AERODYNAMIC CHARACTERISTICS AT EXTREME FLIGHT CONDITIONS | ICAS2020_0483 |
| Zhang, H. | EXPERIMENTAL INVESTIGATION OF THE CHN-T1 MODEL IN FL-13 WIND TUNNEL OF CARDC AND DNW-LLF FACILITY | ICAS2020_0492 |
| Zhang, S. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Zhang, Y.-J. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Zhang, Y.-Z. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Zhang, B.-Q. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Zhang, Y.F. | MULTIPOINT OPTIMIZATION OF TRANSONIC NATURAL LAMINAR FLOW NACELLES | ICAS2020_0501 |
| Zhang, M.H. | MULTIPOINT OPTIMIZATION OF TRANSONIC NATURAL LAMINAR FLOW NACELLES | ICAS2020_0501 |
| Zhang, M. | NUMERICAL INVESTIGATION OF NACELLE INTAKE FLOW DISTORTION AT CROSSWIND CONDITIONS | ICAS2020_0504 |
| Zhang, H. | RESEARCH ON THE ENVIRONMENTAL WORTHINESS OF THE CIVIL AIRCRAFT USING THE FUZZY THEORY | ICAS2020_0514 |
| Zhang, W. | AXIAL ASSEMBLAGE DEVIATION ON PERFORMANCE OF ONE TRANSONIC CENTRIFUGAL COMPRESSOR | ICAS2020_0538 |
| Zhang, X.-Y. | EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2020_0620 |
| Zhang, X.-B. | EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2020_0620 |
| Zhang, W. | EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DUAL-BODY DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT | ICAS2020_0620 |
| Zhang, Z.-K. | AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE | ICAS2020_0631 |
| Zhang, J. | DESIGN AND TEST OF A HIGH SLOPE ANGLE INTERMEDIATE DUCT BETWEEN LOW-PRESSURE COMPRESSOR AND HIGH-PRESSURE COMPRESSOR | ICAS2020_0632 |
| Zhang, C. | A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT | ICAS2020_0650 |
| Zhang, Q.Q. | THE AERODYNAMIC OPTIMIZATION AND TRIM CHARACTERISTICS RESEARCH ON VARIABLE CAMBER WING OF WIDE-BODY CIVIL TRANSPORT | ICAS2020_0676 |
| Zhang, J. | STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESH | ICAS2020_0686 |
| Zhang, K.-S. | IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC MODELING PROBLEMS | ICAS2020_0787 |
| Zhang, R.Y. | RESEARCH ON TRAJECTORY OPTIMIZATION TECHNOLOGY CONSIDERING METEOROLOGICAL INFORMATION PREDICTION | ICAS2020_0823 |
| Zhang, W.W. | DATA FUSION UNSTEADY AERODYNAMIC MODELING BASED ON EXPERIMENTAL DATA | ICAS2020_0842 |
| Zhang, M.X. | INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINE | ICAS2020_0845 |
| Zhang, Q.B. | RESEARCH ON FSI DYNAMIC CHARACTERISTICS OF PARAFOIL TRAILING EDGE DEFLECTION | ICAS2020_0909 |
| Zhang, M. | SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION EXPERIMENT ON C919 FUSELAGE MODEL | ICAS2020_0928 |
| Zhang, Z.X. | AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS | ICAS2020_0939 |
| Zhang, L.X. | AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS | ICAS2020_0939 |
| Zhang, K.-W. | AN INTEGRATED METHOD FOR ACCURATE IDENTIFICATION AND DYNAMIC MONITORING OF BUILDINGS IN AERODROME OBSTACLE FREE SPACE | ICAS2020_1061 |
| Zhang, W. | RESEARCH ON FAULT DIAGNOSIS AND FAILURE RECONFIGURATION OF FLUSH AIR DATA SENSING | ICAS2020_1064 |
| Zhang, H.-Y. | GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOW | ICAS2020_1073 |
| Zhang, B. | TWISTOR BASED 6-DOF DISTRIBUTED ADAPTIVE LEADER-FOLLOWING CONTROL FOR MULTIPLE RIGID SPACECRAFT FORMATION | ICAS2020_1089 |
| Zhang, S.S. | TOPOLOGY OPTIMIZATION FOR WING STRUCTURE OF HYPERSONIC VEHICLE | ICAS2020_1110 |
| Zhang, H. | A DYNAMIC SELF-CONTROL ERR STRATEGY FOR BI-DIRECTIONAL EVOLUTIONARY STRUCTURAL OPTIMIZATION | ICAS2020_1153 |
| Zhang, Q. | A DYNAMIC SELF-CONTROL ERR STRATEGY FOR BI-DIRECTIONAL EVOLUTIONARY STRUCTURAL OPTIMIZATION | ICAS2020_1153 |
| Zhang, L. | TOTAL TEMPERATURE MEASUREMENTS IN WATER INJECTION AND PRE-COMPRESSOR COOLING TECHNOLOGY | ICAS2020_1170 |
| Zhang, H.P. | NUMERICAL SIMULATION OF RIDGE ICE AND AERODYNAMIC EFFECT UNDER THERMAL ANTI-ICE | ICAS2020_1179 |
| Zhang, R. | NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTS | ICAS2020_1183 |
| Zhang, Y.D. | NUMERICAL SIMULATION OF LOCAL LONG SHALLOW CAVITY EFFECT ON THE STABILITY OF A HYPERSONIC BOUNDARY LAYER | ICAS2020_1189 |
| Zhang, R. | NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WING | ICAS2020_1240 |
| Zhang, L. | METHODS OF DIRECTIONAL COARSENING FOR UNSTRUCTURED GRIDS AND APPLICATIONS | ICAS2020_1261 |
| Zhao, H. | STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TESTING | ICAS2020_0039 |
| Zhao, H. | SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHOD | ICAS2020_0094 |
| Zhao, Z. | DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEM | ICAS2020_0386 |
| Zhao, S. | DYNAMIC PERFORMANCE ANALYSIS AND WEIGHTED-BASED FAULT DIAGNOSIS SCHEME FOR AIRCRAFT ELECTRIC POWER SYSTEM | ICAS2020_0386 |
| Zhao, B.-D. | PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNEL | ICAS2020_0418 |
| Zhao, S.-W. | PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECHNICAL UNIVERSITY | ICAS2020_0495 |
| Zhao, Y.Q. | DEFORMATION ANALYSIS OF C-SPAR COMPOSITE STRUCTURE DURING THE PREFORMING PROCESSING | ICAS2020_0599 |
| Zhao, H.J. | RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DIS | ICAS2020_0865 |
| Zhao, L.F. | ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION | ICAS2020_1074 |
| Zhao, L.F. | MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOW | ICAS2020_1078 |
| Zhao, X. | AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESS | ICAS2020_1118 |
| Zhao, S.-Z. | AERODYNAMIC MODELING AND FLIGHT PERFORMANCE RESEARCH OF THE COAXIAL RIGID HELICOPTER IN POP-UP PROCESS | ICAS2020_1118 |
| Zhao, S.-Z. | HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILS | ICAS2020_1125 |
| Zhao, X. | HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILS | ICAS2020_1125 |
| Zhao, S.-Z. | FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATION | ICAS2020_1127 |
| Zhao, X. | FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATION | ICAS2020_1127 |
| Zhao, L.F. | ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGS | ICAS2020_1171 |
| Zhao, Z.H. | RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGE | ICAS2020_1203 |
| Zhao, Y.X. | THE FLOW AND HEAT TRANSFER OF ANALYSIS TO ANNULAR CAVITY IN ENGINE CASE | ICAS2020_1251 |
| Zhao, Y. | ESTIMATION OF STATIC AND DYNAMIC FLOATATION CHARACTERISTICS DURING AIRCRAFT DITCHING | ICAS2020_1255 |
| Zharenov, I. | STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION | ICAS2020_0106 |
| Zhbanov, V.A. | EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE | ICAS2020_0894 |
| Zhen, H. | AIRCRAFT CRUISE PERFORMANCE DESIGN INTEGRATION BASED ON SYSTEM ENGINEERING | ICAS2020_0053 |
| Zheng, G. | ADVANCED WEAK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING | ICAS2020_0037 |
| Zheng, S. | AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION | ICAS2020_0071 |
| Zheng, W.P. | EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACK | ICAS2020_0182 |
| Zheng, C. | VIRTUAL PROTOTYPING OF ELECTRICAL THSA FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS | ICAS2020_0196 |
| Zheng, J.-J. | RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTER | ICAS2020_0304 |
| Zheng, L. | APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROL | ICAS2020_0978 |
| Zheng, X. | MULTI-UAV TRAJECTORY PLANNING BASED ON COORDINATION VARIABLES | ICAS2020_1139 |
| Zhong, M. | AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM WITH FLEXIBLE DROOP-NOSE FOR A LONG HAUL BUSINESS JET CONFIGURATION | ICAS2020_0071 |
| Zhong, S.-D. | STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEM | ICAS2020_0366 |
| Zhong, H.T. | SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TEST | ICAS2020_0744 |
| Zhou, Q. | ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META-MODEL | ICAS2020_0200 |
| Zhou, Z. | RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREAS | ICAS2020_0219 |
| Zhou, Y. | A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES | ICAS2020_0272 |
| Zhou, Z. | STUDY ON ADJOINT OPTIMIZATION OF BWB CONFIGURATION CONSIDERING THE INFLUENCE OF INTAKE AND EXHAUST SYSTEM | ICAS2020_0366 |
| Zhou, D. | PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTS | ICAS2020_0392 |
| Zhou, L. | STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION | ICAS2020_0416 |
| Zhou, H. | ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM FOR COMPLICATED PRODUCTS ENGINEERING | ICAS2020_0433 |
| Zhou, Z. | PARETO FRONT EXPLORATION USING MANIFOLD RECONSTRUCTION APPROACH FOR ROTORCRAFT AIRFOILS DESIGN | ICAS2020_0463 |
| Zhou, Z. | A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT | ICAS2020_0650 |
| Zhou, N.-C. | STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESH | ICAS2020_0686 |
| Zhou, Z. | BIONIC LIGHT-WEIGHT GRID SURFACE WING STRUCTURE DESIGN FOR A SOLAR-POWERED UAV | ICAS2020_0731 |
| Zhou, Y. | A METHOD FOR EVALUATING THE APPLICABILITY OF MAINTENANCE TASKS BASED ON HELICOPTER HEALTH AND USAGE MONITORING SYSTEM | ICAS2020_0764 |
| Zhou, Q. | CO-SIMULATION OF SYSML AND SIMULINK/MODELICA USING FMI | ICAS2020_0803 |
| Zhou, Y.M. | RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DIS | ICAS2020_0865 |
| Zhou, Z. | APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROL | ICAS2020_0978 |
| Zhou, W.Y. | ADRC BASED HIGH MANEUVERING FLIGHT CONTROL LAW DESIGN FOR UAV | ICAS2020_1088 |
| Zhou, W.J. | NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH-SPEED VEHICLES | ICAS2020_1157 |
| Zhou, L.C. | RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGE | ICAS2020_1203 |
| Zhu, G. | CERTIFICATION CONSIDERATIONS FOR EVTOL AIRCRAFT | ICAS2020_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 BARYCENTER | ICAS2020_0304 |
| Zhu, R. | STRATEGIES TO ENHANCE CONFIGURATIONS FOR HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION | ICAS2020_0416 |
| Zhu, X. | ASSEMBLY QUALITY OPTIMIZATION APPROACH FOR LARGE-SCALE ACTIVE COMPONENTS BASED ON REVERSE ENGINEERING | ICAS2020_0542 |
| Zhu, J.Q. | SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATION | ICAS2020_0549 |
| Zhu, Q. | RESEARCH ON CERTIFICATION MANAGEMENT OF AIRCRAFT ENGINE BASED ON RISK ANALYSIS | ICAS2020_0715 |
| Zhu, A.-Y. | RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLES | ICAS2020_0851 |
| Zhu, Y. | BASED ON SYSTEMS ENGINEERING PROCESS THE CIVIL AIRCRAFT PROJECT PRODUCT BREAKDOWN STRUCTURE DEVELOPMENT RESEARCH | ICAS2020_1018 |
| Zhu, Y.-H. | GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOW | ICAS2020_1073 |
| Zhu, C.L. | EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACE | ICAS2020_1138 |
| Zhu, C.X. | EXPERIMENTAL STUDY OF THE DYNAMICS CHARACTERISTICS OF AN IMPACT WATER DROPLET ON SUPERHYDROPHOBIC SURFACE | ICAS2020_1138 |
| Zhu, C.-L. | ULTRASONIC DE-ICING SYSTEM DESIGN METHODS BASED ON RESONANCE AND IMPEDANCE MATCHING | ICAS2020_1148 |
| Zhu, Y. | NUMERICAL INVESTIGATION OF THE EFFECT OF WALL TEMPERATURE ON THERMAL ENVIRONMENT OF TWO-DIMENSIONAL TRANSVERSE GAP | ICAS2020_1149 |
| Zhu, Z.C. | NUMERICAL SIMULATION OF SWEEPING MOTION EFFECTS ON THE HOVERING DRAGONFLIES | ICAS2020_1167 |
| Zhu, S.F. | MODEL-BASED VIRTUAL INTEGRATED TEST METHOD FOR AVIONICS SYSTEM | ICAS2020_1212 |
| Ziverts, U. | ERAS- EVALUATION OF REALISTIC APPROACH SCENARIOS FOR MINIMAL NOISE - PRELIMINARY FINDINGS | ICAS2020_0409 |
| Zong, W.-G. | GEOMETRICAL PARAMETER STUDY OF A HYPERSONIC VERTICAL GAP FLOW | ICAS2020_1073 |
| Zou, C.H. | A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDING | ICAS2020_0282 |
| Zou, L. | TURBINE STRUCTURE ANALYSIS AND IMPROVEMENT OF A HIGH-SPEED ROTOR WITH MULTI-DISK AND MULTI-SUPPORT | ICAS2020_0391 |
| Zou, X.-Q. | APPLICATION OF A SKEWED-SLOT CASING TREATMENT IN A HIGH-LOADING AXIAL-CENTRIFUGAL COMPRESSOR | ICAS2020_0543 |
| Zou, C.H. | AUTONOMOUS FLIGHT CONTROL BASED ON NEURAL NETWORKS AND FUZZY DECISION | ICAS2020_0591 |
| Zuo, Y.T. | AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE | ICAS2020_1144 |