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 |