| Abd Bari, M.A. | ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHM | ICAS2018_0328 |
| Abdalla, A.M. | ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OFSUPERSONIC BUSINESS JETS | ICAS2018_0030 |
| Abdalla, A.M. | EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFT | ICAS2018_0199 |
| Abdalla, A.M. | DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION | ICAS2018_0814 |
| Abdelmoula, F. | LNAS - A PILOT ASSISTANCE SYSTEM FOR LOW-NOISE APPROACHES WITH MINIMAL FUEL CONSUMPTION | ICAS2018_0096 |
| Abramova, K.A. | NUMERICAL OPTIMIZATION OF FLOW CONTROL BY TANGENTIAL JET BLOWING ON TRANSONIC AIRFOIL | ICAS2018_0704 |
| Abramovich, H. | INVESTIGATION OF CRACK PROPAGATION PROPERTIES OF ADDITIVE MANUFACTURING PRODUCTS | ICAS2018_0012 |
| Abreu, D.F. | EFFECTS OF NUMERICAL MODELING CHOICES FOR HEATED JETS IN CROSS FLOW | ICAS2018_0369 |
| Abreu, L.I. | WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL | ICAS2018_0388 |
| Abulawi, J. | A SYSML-BASED APPROACH TO EXPLORING INNOVATIVE SYSTEM IDEAS FOR AERONAUTICAL APPLICATIONS | ICAS2018_0821 |
| Acevedo-Giraldo, D. | EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE | ICAS2018_0815 |
| Afonin, A.I. | APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADES | ICAS2018_0173 |
| Ahn, J.M. | ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTING | ICAS2018_0159 |
| Aigner, B. | MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERING | ICAS2018_0633 |
| Aigner, B. | DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK | ICAS2018_0674 |
| Aigner, B. | COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTS | ICAS2018_0785 |
| Akiyama, T. | FLIGHT DEMONSTRATION OF A LONG RANGE ONBOARD DOPPLER LIDAR | ICAS2018_0121 |
| Akiyama, T. | DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM | ICAS2018_0284 |
| Akman, T. | USING SENSITIVITY PENALTIES TO ROBUSTIFY THE OPTIMAL REENTRY TRAJECTORY OF A HYPERSONIC VEHICLE | ICAS2018_0564 |
| Akman, T. | NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING | ICAS2018_0782 |
| Akroyd, G. | RECTANGULAR CAVITY FLOWFIELD EFFECTS ON STORES IN THE SHEAR LAYER | ICAS2018_0045 |
| Akroyd, G. | STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDS | ICAS2018_0367 |
| Aksenov, A.A. | CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES | ICAS2018_0242 |
| Alegre, G.S.P. | PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMS | ICAS2018_0194 |
| Aleksandrov, V.Y. | GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORS | ICAS2018_0628 |
| Aleksandrov, V.Y. | INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELS | ICAS2018_0645 |
| Aleksandrov, V.Y. | COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL | ICAS2018_0672 |
| Alexandrov, S.V. | NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTS | ICAS2018_0700 |
| Alexandrova, E.A. | EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOW | ICAS2018_0690 |
| Alexandrova, E.A. | NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTS | ICAS2018_0700 |
| Alfredson, J. | DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMS | ICAS2018_0305 |
| Alfredson, J. | A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTS | ICAS2018_0309 |
| Algodoal, L.A. | HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOT | ICAS2018_0337 |
| Almeida, S.F.M. | RESULTS AND COMPARISON OF NUMERICAL SIMULATION AND THE TESTING OF LUG MANUFACTURED BY COMPOSITE MATERIAL BY RTM PROCESS | ICAS2018_0007 |
| Almeida, A.C.V.M. | CFD INVESTIGATION OF AERODYNAMIC COEFFICIENTS AND STALL CHARACTERISTICS FOR HIGH LIFT CONFIGURATIONS | ICAS2018_0076 |
| Almeida, S.F.M. | A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION | ICAS2018_0179 |
| Almeida, A.N. | A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTS | ICAS2018_0309 |
| Almeida, A. | EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS | ICAS2018_0402 |
| Almeida, S.F.M. | MODIFIED WHITNEY-NUISMER CRITERIA FOR PREDICTION OF NOTCHED STRENGTH OF COMPOSITE LAMINATES | ICAS2018_0677 |
| Almeida Jr, J.C. | PREDICTIVE & DETECTIVE MAINTENANCE: EFFECTIVE TOOLS IN THE MANAGEMENT OF AERONAUTICAL PRODUCTS | ICAS2018_0336 |
| Altenscheidt, L. | PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALS | ICAS2018_0050 |
| Altenscheidt, M. | PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALS | ICAS2018_0050 |
| Alves, D.S. | MODELLING OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITES: A COMPARATIVE STUDY | ICAS2018_0519 |
| Amadori, K. | MULTIDISCIPLINARY OPTIMIZATION OF UNMANNED AIRCRAFT IN A SYSTEM OF SYSTEMS CONTEXT | ICAS2018_0047 |
| Amadori, K. | A HOLISTIC ENGINEERING APPROACH FOR AERONAUTICAL PRODUCT DEVELOPMENT | ICAS2018_0724 |
| Amelyushkin, I.A. | EXPERIMENTAL INVESTIGATION, MATHEMATICAL AND NUMERICAL SIMULATION OF AIRCRAFT ICING PHENOMENA | ICAS2018_0741 |
| Amiryants, G.A. | AEROELASTIC PROPERTIES OF ACTIVE WINGLETS | ICAS2018_0276 |
| Ananyan, M.V. | INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELS | ICAS2018_0645 |
| Andersson, J. | COMPARISON OF TWO DIFFERENT INDICATORS FOR HOT CRACKING IN WELDED STRUCTURES | ICAS2018_0142 |
| Andrade, D. | STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODS | ICAS2018_0579 |
| Andrews, G. | A HYBRID LENGTH SCALE SIMILARITY SOLUTION FOR SWIRLING TURBULENT JETS | ICAS2018_0872 |
| Angélico, R.A. | INFLUENCE OF AIRFRAME STIFFNESS ON THE AERODYNAMIC COEFFICIENTS OF A HIGH ASPECT RATIO WING | ICAS2018_0776 |
| Angelo, M.V. | AN XFEM FRAMEWORK FOR ONSET AND CRACK PROPAGATION FOR COMPOSITES BASED ON ACTION PLANE THEORY | ICAS2018_0502 |
| Anisimov, K. | MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT | ICAS2018_0783 |
| Anisimov, K.S. | PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT | ICAS2018_0788 |
| Ann, S. | MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMIT | ICAS2018_0080 |
| Antunes, P. | ARAMID-FIBER REINFORCED ELASTOMERS AS FUTURE AIRCRAFT ACTUATORS - A PROOF-OF-CONCEPT INVESTIGATION | ICAS2018_0377 |
| Arantes, J.S. | SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVS | ICAS2018_0374 |
| Arantes, M.S. | SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVS | ICAS2018_0374 |
| Archer, R. | GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESS | ICAS2018_0182 |
| Arefyev, K.Y. | INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELS | ICAS2018_0645 |
| Argolo Jesus, T. | FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETS | ICAS2018_0396 |
| Arjoni, D.H. | A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTS | ICAS2018_0309 |
| Arjoni, D.H. | EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS | ICAS2018_0402 |
| Arnaldo, R.M. | DETECTING HIGH-ALTITUDE ICE CRYSTAL (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATURE | ICAS2018_0611 |
| Aso, S. | PASSIVE VENTILATION FLOW CONTROL FOR AIRCRAFT GUST LOAD ALLEVIATION | ICAS2018_0736 |
| Atkin, C. | DEVELOPMENT OF SECONDARY CROSSFLOW INSTABILITY NEAR BREAKDOWN INTO TURBULENCE | ICAS2018_0735 |
| Atkin, C. | LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLES | ICAS2018_0739 |
| Atobe, T. | DESTABILIZING EFFECT OF LONGITUDINAL WALL OSCILLATION ON OBLIQUE WAVES IN 2D CHANNEL FLOW | ICAS2018_0118 |
| Avallone, F. | AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMS | ICAS2018_0505 |
| Avelar, A.C. | TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCK OSCILATIONS | ICAS2018_0599 |
| Avelino, W.O. | DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS | ICAS2018_0609 |
| Awruch, A.M. | LARGE EDDY SIMULATION OF A TRANSIENT SPOILER DEPLOYMENT IN A NACA0012 PROFILE IN SUBSONIC AND TRANSONIC SPEEDS | ICAS2018_0503 |
| Azevedo, J.L.F. | CFD INVESTIGATION OF AERODYNAMIC COEFFICIENTS AND STALL CHARACTERISTICS FOR HIGH LIFT CONFIGURATIONS | ICAS2018_0076 |
| Bacciaglia, A. | BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTING | ICAS2018_0660 |
| Baeva, S.I. | NUMERICAL AND EXPERIMENTAL STUDY OF THE EFFECT OF CIRCUMFERENTIAL GROOVES ON HPC LAST STAGE PERFORMANCE | ICAS2018_0624 |
| Bagassi, S. | THE USE OF SYNTHETIC VISION TOOLS IN THE CONTROL TOWER ENVIRONMENT: THE RETINA CONCEPT | ICAS2018_0717 |
| Bagassi, S. | DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACH | ICAS2018_0774 |
| Bagassi, S. | PRELIMINARY DESIGN OF A LONG RANGE WINDOWLESS AIRCRAFT CONCEPT | ICAS2018_0777 |
| Bai, Y. | AEROELASTIC WIND TUNNEL EXPERIMENT OF A HIGH-ASPECT-RATIO WING MODEL AGAINST GEOMETRICAL NON-LINEARITY | ICAS2018_0720 |
| Bai, Y. | EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTS | ICAS2018_0784 |
| Balachandran, S. | AN EVALUATION OF VARIOUS GEOFENCE CONFLICT RESOLUTION ALGORITHMS AND THEIR IMPACT ON MISSION PERFORMANCE | ICAS2018_0393 |
| Balunov, K.A. | AEROELASTIC TAILORING OF COMPOSITE WING BY USING MULTIDISCIPLINARY DESIGN ENVIRONMENT | ICAS2018_0458 |
| Balvedi, G.C. | A METHOD FOR ESTIMATING THE PROBABILITY OF RARE ACCIDENTS IN COMPLEX SYSTEMS | ICAS2018_0849 |
| Banfi , D. | REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS | ICAS2018_0437 |
| Barbosa, G.C. | ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFT | ICAS2018_0529 |
| Barbosa, A.A.F. | INFLUENCE OF GULL WING ON LONGITUDINAL AND LATERAL-DIRECTIONAL COEFFICIENTS OF AN AIRPLANE | ICAS2018_0670 |
| Barbosa, R.C.M.G. | CLOSED-LOOP SYSTEM IDENTIFICATION OF A LARGE FLEXIBLE AIRCRAFT USING SUBSPACE METHODS | ICAS2018_0813 |
| Barrier, P. | PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAV | ICAS2018_0233 |
| Barros, J. | STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS | ICAS2018_0482 |
| Batura, S.N. | COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL | ICAS2018_0672 |
| Bauer, M. | WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING | ICAS2018_0646 |
| Bautin, A.A. | DEVELOPMENT OF STRUCTURAL HEALTH MONITORING METHODS THROUGH THE ANALYSIS OF KINETICS OF LOCAL STRESS-STRAIN STATE | ICAS2018_0160 |
| Bauzer Medeiros, E. | UAV INITIAL PARAMETER ESTIMATION | ICAS2018_0568 |
| Bauzer Medeiros, E. | HISTORY OF AVIATION IN MINAS GERAIS | ICAS2018_0871 |
| Bayandor, J. | BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION | ICAS2018_0661 |
| Bayandor, J. | VERIFIED FUSELAGE SECTION WATER IMPACT MODELING | ICAS2018_0732 |
| Bayandor, J. | PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFT | ICAS2018_0826 |
| Bayma, A. | HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENT | ICAS2018_0269 |
| Beals, N. | ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACH | ICAS2018_0851 |
| Becker, G.G. | HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOT | ICAS2018_0337 |
| Becker, G.G. | STATIC LOADS EVALUATION IN A FLEXIBLE AIRCRAFT USING HIGH FIDELITY FLUID-STRUCTURE ITERATION TOOL (E2-FSI) | ICAS2018_0702 |
| Becker, R.-G. | COUPLING OF PREDESIGN AND PERFORMANCE TOOLS FOR TRANSIENT AIRCRAFT ENGINE ANALYSES | ICAS2018_0830 |
| Belo, E.M. | FLIGHT DYNAMICS MODELING AND TRIM CURVES OF A CONCEPTUAL SEMI-TANDEM WING VTOL UAV | ICAS2018_0171 |
| Belo, E.M. | PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMS | ICAS2018_0194 |
| Belov, S.V. | THE INFLUENCE OF THE SHAPE OF THE COOLING CHANNEL AND PRESSURE GRADIENT ON THE EFFICIENCY OF FILM COOLING OF GTE BLADES | ICAS2018_0629 |
| Berlowitz, I. | NARROW-BODY B737NG PASSENGER CONVERSION TO FREIGHTER | ICAS2018_0003 |
| Bertolin, R.M. | ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFT | ICAS2018_0529 |
| Beyak, E.-S. | IONIZATION AND DISSOCIATION EFFECTS ON HYPERSONIC BOUNDARY-LAYER STABILITY | ICAS2018_0837 |
| Bi, S. | APPLICATION RESEARCH OF LARGE-SCALED COMPLICATED FRAME-BEAM INTEGRAL COMPONENT BASED ON ELECTRON BEAM ADDITIVE MANUFACTURING | ICAS2018_0319 |
| Bi, S. | AIRCRAFT STRUCTURE TECHNOLOGY OF ADDITIVE MANUFACTURING | ICAS2018_0723 |
| Bidinotto, J.H. | PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMS | ICAS2018_0194 |
| Bier, N. | WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING | ICAS2018_0646 |
| Bijewitz, J. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Bijewitz, J. | DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT | ICAS2018_0728 |
| Bil, C. | ADAPTIVE LANDING SEQUENCING USING BIPARTITE GRAPHS AND PERFECT MATCHING | ICAS2018_0634 |
| Bil, C. | URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREA | ICAS2018_0635 |
| Bil, C. | BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTING | ICAS2018_0660 |
| Bile, Y. | COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN | ICAS2018_0134 |
| Bizarro, A.F. | MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP | ICAS2018_0493 |
| Bliznyukov, L.G. | ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORS | ICAS2018_0639 |
| Boggero, L. | INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORK | ICAS2018_0412 |
| Boggero, L. | STUDIES ON PROPULSION AND ON-BOARD SYSTEMS MATCHING IN AGILE PROJECT DISTRIBUTED COLLABORATIVE MDO ENVIRONMENT APPLYING FOR ADVANCED REGIONAL AND MEDIUM HAUL JET | ICAS2018_0655 |
| Bonet, J.T. | BLENDED WING BODY TRANSPORT AIRCRAFT RESEARCH & DEVELOPMENT | ICAS2018_0298 |
| Boonjaipetch, P. | ANALYSIS OF LOW-BOOM CHARACTERISTICS OF SUPERSONIC WAVERIDER | ICAS2018_0424 |
| Boozer, C.M. | COUPLED ADJOINT AEROSTRUCTURAL OPTIMIZATION FRAMEWORK FOR PRELIMINARY AIRCRAFT DESIGN | ICAS2018_0426 |
| Borges Tôrres, L.A. | FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETS | ICAS2018_0396 |
| Borovoy, V.Y. | EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOW | ICAS2018_0690 |
| Botero-Bolivar, L. | EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE | ICAS2018_0815 |
| Braschczok, M. | PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALS | ICAS2018_0050 |
| Braun, R. | A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT | ICAS2018_0203 |
| Bravo-Mosquera, P.D. | EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFT | ICAS2018_0199 |
| Bravo-Mosquera, P.D. | DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION | ICAS2018_0814 |
| Bravo-Mosquera, P.D. | EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE | ICAS2018_0815 |
| Breard, C. | CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF "PARASITE" NOISE | ICAS2018_0116 |
| Breard, C. | IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED | ICAS2018_0119 |
| Breitsamter, C. | OUTBOARD SPLIT FLAP AERODYNAMICS OF A FLYING WING CONFIGURATION | ICAS2018_0069 |
| Breitsamter, C. | PERFORMANCE IMPROVEMENT OF A COMPOUND HELICOPTER ROTOR HEAD BY AERODYNAMIC SHAPE OPTIMIZATION | ICAS2018_0070 |
| Breitsamter, C. | TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTS | ICAS2018_0126 |
| Breymann, B. | COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN | ICAS2018_0167 |
| Bringhenti, C. | PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS | ICAS2018_0649 |
| Broekhuijsen, J.J. | NUMERICAL INVESTIGATION AERODYNAMICS NACELLE-STRAKE EFFECT | ICAS2018_0205 |
| Broitman, N. | INVESTIGATION OF CRACK PROPAGATION PROPERTIES OF ADDITIVE MANUFACTURING PRODUCTS | ICAS2018_0012 |
| Brügge, T. | A FRAMEWORK FOR UNCONVENTIONAL LANDING GEAR CONFIGURATION MODELLING | ICAS2018_0688 |
| Buch, J.-P. | IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS | ICAS2018_0249 |
| Buchwald, M. | STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACH | ICAS2018_0082 |
| Budinger, M. | A MORE INTEGRATED DESIGN APPROACH FOR EMBEDDED MECHATRONIC SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMS | ICAS2018_0170 |
| Bussamra, F.L.S. | STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS | ICAS2018_0482 |
| Bussamra, F.L.S. | MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP | ICAS2018_0493 |
| Bussamra, F.L.S. | STATIC LOADS EVALUATION IN A FLEXIBLE AIRCRAFT USING HIGH FIDELITY FLUID-STRUCTURE ITERATION TOOL (E2-FSI) | ICAS2018_0702 |
| Bussemaker, J. | DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK | ICAS2018_0674 |
| Caldas, L.C. | DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONES | ICAS2018_0591 |
| Calvo, M. | ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OFSUPERSONIC BUSINESS JETS | ICAS2018_0030 |
| Campobasso, M.S. | FEASIBILITY OF THE NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING AIRCRAFT UNSTEADY AERODYNAMICS | ICAS2018_0791 |
| Camponogara, A. | POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION | ICAS2018_0818 |
| Campos, R.M.V. | COMPARATIVE STUDY AND VALIDATION OF MATERIAL WITH BETTER PERFORMANCE IN TERMS OF THERMAL ABSORPTION INSIDE AN AIRCRAFT | ICAS2018_0017 |
| Campos, G.B. | PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS | ICAS2018_0649 |
| Canzian, L. | IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS | ICAS2018_0249 |
| Capristan, F. | A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIES | ICAS2018_0088 |
| Capuano, F. | NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMP | ICAS2018_0622 |
| Cardoso-Ribeiro, F.L. | APPLICABILITY OF GEOMETRICALLY-LINEAR STRUCTURAL-DYNAMIC MODELS FOR THE FLIGHT DYNAMICS OF ARBITRARILY-FLEXIBLE AIRCRAFT | ICAS2018_0523 |
| Carmona, L.C. | UAV INITIAL PARAMETER ESTIMATION | ICAS2018_0568 |
| Carrera, E. | GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGS | ICAS2018_0245 |
| Carvalho, L.M.M.O. | CFD INVESTIGATION OF AERODYNAMIC COEFFICIENTS AND STALL CHARACTERISTICS FOR HIGH LIFT CONFIGURATIONS | ICAS2018_0076 |
| Carvalho, F.I. | INCREASED FLUTTER VELOCITY WITH USE OF A PASSIVE CONTROL SYSTEM | ICAS2018_0800 |
| Carvalho, R.C. | DEVELOPMENT OF THE REGENERATIVE SOARER: THEORETICAL AND PRACTICAL ASPECTS | ICAS2018_0839 |
| Cary, A. | CFD VERIFICATION AND VALIDATION FOR INDUSTRIAL APPLICATIONS | ICAS2018_0857 |
| Casalino, D. | AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMS | ICAS2018_0505 |
| Castillo Pardo, A. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Castro, S.G.P | AN ACTIVE-PASSIVE NONLINEAR FINITE ELEMENT MODEL FOR ELECTROMECHANICAL COMPOSITE MORPHING BEAMS | ICAS2018_0207 |
| Catalano, P. | DE-ICING PHENOMENA MODELLED BY FINITE ELEMENT MODELS | ICAS2018_0180 |
| Catalano, F.M. | EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFT | ICAS2018_0199 |
| Catalano, P. | VALIDATION OF INTERMITTENCY MODEL FOR TRANSITION PREDICTION IN A RANS FLOW SOLVER | ICAS2018_0484 |
| Catalano, F.M. | MULTI-DISCIPLINARY DESIGN OPTIMIZATION OF A BLENDED WINGLET | ICAS2018_0598 |
| Catalano, F.M. | BRAZILIAN AVIATION HISTORY: THE UNIVERSITY OF SÃO PAULO CASE | ICAS2018_0601 |
| Catalano, P. | NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMP | ICAS2018_0622 |
| Catalano, F.M. | INFLUENCE OF GULL WING ON LONGITUDINAL AND LATERAL-DIRECTIONAL COEFFICIENTS OF AN AIRPLANE | ICAS2018_0670 |
| Catalano, F.M. | EVALUATION OF WIND TUNNEL WALL BOUNDARY-LAYER CONTROL FOR 2-D HIGH-LIFT AERODYNAMIC AND AEROACOUSTIC TESTING | ICAS2018_0780 |
| Catalano , F.M. | DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION | ICAS2018_0814 |
| Catalano, F.M. | EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE | ICAS2018_0815 |
| Cavalcanti, J. | A CASE OF SUCESS: MDO APPLIED ON THE DEVELOPMENT OF EMBRAER 175 ENHANCED WINGTIP | ICAS2018_0034 |
| Cavalieri, A.V.G. | STRUCTURAL DAMPING EFFECTS ON THE ACOUSTIC SCATTERING BY ELASTIC PLATES | ICAS2018_0108 |
| Cavalieri, A.V.G. | ON THE WAVE-CANCELLING NATURE OF BOUNDARY LAYER TRANSITION CONTROL | ICAS2018_0349 |
| Cavalieri, A.V.G. | WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL | ICAS2018_0388 |
| Cavalieri, A.V.G. | ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIES | ICAS2018_0438 |
| Cavalieri, A. | ACOUSTIC MODES AND GLOBAL INSTABILITIES IN WAKES AND JETS | ICAS2018_0450 |
| Cavalieri, A. | CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE | ICAS2018_0473 |
| Cavalieri, A.V.G. | RESOLVENT-BASED CONTROL OF STREAKS IN BOUNDARY LAYERS | ICAS2018_0477 |
| Cecrdle, J. | FLUTTER ANALYSIS OF TWIN TURBOPROP AIRCRAFT WITH TIP-TANKS | ICAS2018_0004 |
| Cecrdle, J. | EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPS | ICAS2018_0258 |
| Celso Jr., P. | PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIG | ICAS2018_0147 |
| Cen, F. | A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNEL | ICAS2018_0406 |
| Cen, F. | OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC | ICAS2018_0750 |
| Cenko, A. | RECTANGULAR CAVITY FLOWFIELD EFFECTS ON STORES IN THE SHEAR LAYER | ICAS2018_0045 |
| Cenko, A. | STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDS | ICAS2018_0367 |
| Cerino, G. | MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECT | ICAS2018_0648 |
| Cerón-Muñoz, H.D. | DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION | ICAS2018_0814 |
| Cerón-Muñoz, H.D. | EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE | ICAS2018_0815 |
| Ceruti, A. | BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTING | ICAS2018_0660 |
| Cesnik, C.E.S. | PROPELLER INFLUENCE ON THE STABILITY OF HALE AIRCRAFT | ICAS2018_0177 |
| Cesnik, C.E.S. | NONLINEAR AEROELASTIC REDUCED ORDER MODELS USING MODAL COORDINATES | ICAS2018_0262 |
| Cesnik, C.E.S. | STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS | ICAS2018_0482 |
| Cesnik, C.E.S. | MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP | ICAS2018_0493 |
| Cesnik , C.E.S. | IMPLEMENTATION AND FLIGHT TESTING OF AN ENHANCED STABILITY SYSTEM FOR A VERY FLEXIBLE AIRCRAFT | ICAS2018_0534 |
| Cesnik, C.E.S. | STATIC LOADS EVALUATION IN A FLEXIBLE AIRCRAFT USING HIGH FIDELITY FLUID-STRUCTURE ITERATION TOOL (E2-FSI) | ICAS2018_0702 |
| Cestino, E. | PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROL | ICAS2018_0430 |
| Cestino, E. | REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS | ICAS2018_0437 |
| Cestino, E. | NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODEL | ICAS2018_0556 |
| Chaitanya Munjulury, R. | INTEGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS | ICAS2018_0873 |
| Chaitanya Munjulurynjulury, R. | HURRICANE-CS: CONTROL SURFACES AND HIGH LIFT DEVICES MODELING AND SIZING PROGRAM | ICAS2018_0627 |
| Chambers, J. | DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT | ICAS2018_0875 |
| Chang, H.-C. | HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILES | ICAS2018_0270 |
| Charbonnier, D. | DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK | ICAS2018_0674 |
| Charbonnier, D. | MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT | ICAS2018_0783 |
| Chedrik, V.V. | STRESS-BASED TOPOLOGY OPTIMIZATION WITH USING GLOBAL-LOCAL APPROACH | ICAS2018_0316 |
| Chedrik, V.V. | AEROELASTIC TAILORING OF COMPOSITE WING BY USING MULTIDISCIPLINARY DESIGN ENVIRONMENT | ICAS2018_0458 |
| Chedrik, V.V. | PROBABILISTIC METHOD OF DETERMINATION OF ALLOWABLE DESIGN PARAMETER SCATTERS ON FLUTTER AND STRENGTH CRITERIA | ICAS2018_0756 |
| Chen, Z.W. | STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN | ICAS2018_0041 |
| Chen, Y. | CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF "PARASITE" NOISE | ICAS2018_0116 |
| Chen, H.X. | MULTI-POINT AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WING | ICAS2018_0154 |
| Chen, B.Y. | LONGITUDINAL STABILITY DESIGN CRITERIA FOR HYPERSONIC GLIDERS | ICAS2018_0166 |
| Chen, Z.W. | AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGE | ICAS2018_0210 |
| Chen, Z.-K. | STUDY ON EVALUATION METHODS OF UNDERGRADUATE AIRCRAFT OVERALL DESIGN COURSE BASED ON TEAM DESIGN COMPETITION | ICAS2018_0250 |
| Chen, Z.W. | CFD-BASED STUDY OF DAMAGE LOCATION INFLUENCE ON AERODYNAMICS OF WINGS WITH SINGLE AND DOUBLE THROUGH HOLES | ICAS2018_0294 |
| Chen, K. | STUDY ON AIRCRAFT EVACUATION MODELING AND MODEL PARAMETERS BASED ON SOCIAL FORCE | ICAS2018_0320 |
| Chen, Y. | NUMERICAL ANALYSIS OF BLEND-WING-BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCE | ICAS2018_0326 |
| Chen, Q. | NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTOR | ICAS2018_0334 |
| Chen, C. | PASSIVE CONTROL METHOD IN ATTENUATING SELF-INDUCED ROLL OSCILLATIONS OF LOW-ASPECT-RATIO WINGS USING OBLIQUE SLOT BLEED | ICAS2018_0468 |
| Chen, X. | EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTS | ICAS2018_0784 |
| Cheng, J. | FAULT DIAGNOSIS METHOD STUDY FOR COMPLEX SYSTEM BASED ON KALMAN FILTERS | ICAS2018_0015 |
| Chernousov, V.I. | CONTAINERIZED AIR FREIGHT SYSTEM POWERED BY CRYOGENIC FUEL | ICAS2018_0103 |
| Chernov, A.V. | INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURES | ICAS2018_0299 |
| Chernyshev, S.L. | APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTS | ICAS2018_0321 |
| Chernyshov, V.I. | ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORS | ICAS2018_0639 |
| Choi, U.H. | ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTING | ICAS2018_0159 |
| Chu, M.Q. | EVALUATION OF MECHANICAL PROPERTIES OF TI-6AL-4V FABRICATED BY SELECTIVE LASER MELTING (SLM) | ICAS2018_0866 |
| Church, C. | DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT | ICAS2018_0875 |
| Churkina, T. | OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE | ICAS2018_0361 |
| Chuvakhov, P.V. | EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOW | ICAS2018_0690 |
| Chuvakhov, P.V. | NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTS | ICAS2018_0700 |
| Chuvakhov, P.V. | ENTROPY LAYER EFFECT ON ROUGHNESS-INDUCED LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLAT PLATE FLOW | ICAS2018_0701 |
| Ciampa, P.D. | INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORK | ICAS2018_0412 |
| Ciampa, P.D. | STREAMLINING CROSS-ORGANIZATIONAL AIRCRAFT DEVELOPMENT PROCESSES: AN OVERVIEW OF THE AGILE PROJECT | ICAS2018_0621 |
| Ciampa, P.D. | MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERING | ICAS2018_0633 |
| Ciampa, P.D. | DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK | ICAS2018_0674 |
| Ciampa, P.D. | AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK | ICAS2018_0675 |
| Ciampa, P.D. | MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT | ICAS2018_0783 |
| Ciampa, P.D. | COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTS | ICAS2018_0785 |
| Ciliberti, D. | NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODEL | ICAS2018_0264 |
| Ciliberti , D. | MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT | ICAS2018_0783 |
| Ciloni, P. | A CASE OF SUCESS: MDO APPLIED ON THE DEVELOPMENT OF EMBRAER 175 ENHANCED WINGTIP | ICAS2018_0034 |
| Cimini Jr., C.A. | FINITE ELEMENT MODEL DEVELOPMENT FOR SIMULTANEOUS CRACK PROPAGATION IN TWO COOPERATIVE LUGS | ICAS2018_0512 |
| Cimini Jr., C.A. | CRACK PROPAGATION STARTING AT HOLE’S EDGE GROWING TO PLATE’S MAJOR DIMENSION USING FEM | ICAS2018_0516 |
| Cimini Jr., C.A. | PLY THICKNESS INFLUENCE IN COMPRESSION AFTER IMPACT DAMAGE ON CARBON/EPOXY TEST SPECIMENS | ICAS2018_0707 |
| Ciobaca, V. | WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING | ICAS2018_0646 |
| Coetzee, E.B. | NONLINEAR AEROELASTIC REDUCED ORDER MODELS USING MODAL COORDINATES | ICAS2018_0262 |
| Collier, F. | PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFT | ICAS2018_0826 |
| Consiglio, M. | AN EVALUATION OF VARIOUS GEOFENCE CONFLICT RESOLUTION ALGORITHMS AND THEIR IMPACT ON MISSION PERFORMANCE | ICAS2018_0393 |
| Cooper, J.E. | AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATION | ICAS2018_0133 |
| Corbelli, W. | STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODS | ICAS2018_0579 |
| Corcione, S. | AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATION | ICAS2018_0191 |
| Corcione, S. | NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODEL | ICAS2018_0264 |
| Corman, J.A. | AN APPROACH TO ASSESS AIRFRAME WEIGHT REDUCTION PERFORMANCE OF STITCHED COMPOSITE TECHNOLOGIES | ICAS2018_0793 |
| Costa, T.L. | MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATION | ICAS2018_0586 |
| Costa, F.P. | PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS | ICAS2018_0649 |
| Courtin, C. | DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT | ICAS2018_0875 |
| Cresto Aleina, S. | PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT | ICAS2018_0164 |
| Crockford, J. | AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACE | ICAS2018_0132 |
| Crovato, A. | HIGHER FIDELITY TRANSONIC AERODYNAMIC MODELING IN PRELIMINARY AIRCRAFT DESIGN | ICAS2018_0453 |
| Crowley, B. | LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLES | ICAS2018_0739 |
| Cuenca, R.G. | PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIG | ICAS2018_0147 |
| Cuenca, R.G. | DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONES | ICAS2018_0591 |
| Cui, B. | CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORK | ICAS2018_0268 |
| Cui, H. | APPLICATION RESEARCH OF LARGE-SCALED COMPLICATED FRAME-BEAM INTEGRAL COMPONENT BASED ON ELECTRON BEAM ADDITIVE MANUFACTURING | ICAS2018_0319 |
| Cui, D. | BUCKLING/POSTBUCKLING OPTIMIZATION OF STIFFENED COMPOSITE PANELS BASED ON SENSITIVITY ANALYSIS | ICAS2018_0714 |
| Cui, H. | AIRCRAFT STRUCTURE TECHNOLOGY OF ADDITIVE MANUFACTURING | ICAS2018_0723 |
| Cunha, R.R. | CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHM | ICAS2018_0355 |
| Cunha Jr., S.S. | A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOT | ICAS2018_0559 |
| Curran, R. | CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORK | ICAS2018_0268 |
| Cusati, V. | PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT | ICAS2018_0164 |
| Cusati, V. | NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODEL | ICAS2018_0264 |
| Cusati, V. | MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGN | ICAS2018_0504 |
| Czado, C. | INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS | ICAS2018_0043 |
| Czajkowski, L. | NEW TECHNOLOGY OF LAYERED STRUCTURES IMPLEMENTED IN SELECTED GYROPLANE COMPONENTS | ICAS2018_0356 |
| D'Assunção, D. | EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTION | ICAS2018_0391 |
| da Costa, J.P. | CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHM | ICAS2018_0355 |
| Da Ronch, A. | ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHM | ICAS2018_0328 |
| Da Ronch, A. | WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITY | ICAS2018_0440 |
| Da Ronch, A. | ON REAL–TIME SIMULATION OF FLEXIBLE AIRCRAFT WITH PHYSICS–DERIVED MODELS | ICAS2018_0501 |
| Da Ronch, A. | FEASIBILITY OF THE NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING AIRCRAFT UNSTEADY AERODYNAMICS | ICAS2018_0791 |
| da Silva, R.G. | CFD INVESTIGATION OF AERODYNAMIC COEFFICIENTS AND STALL CHARACTERISTICS FOR HIGH LIFT CONFIGURATIONS | ICAS2018_0076 |
| da Silva, G.A.L. | SHIP-HELICOPTER OPERATIONAL LIMITATION ENVELOPE DEFINITION WITH CFD RESULTS AND WIND TUNNEL DATA | ICAS2018_0345 |
| da Silva, P.A. | SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE | ICAS2018_0354 |
| da Silva, P.A. | CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHM | ICAS2018_0355 |
| da Silva, R.G.A. | EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATION | ICAS2018_0382 |
| Da Silva, E.R. | COMPARISON AND APPLICATION OF DIFFERENTS TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMIC WING DESIGN | ICAS2018_0527 |
| da Silva, R.G.A. | TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCK OSCILATIONS | ICAS2018_0599 |
| Dai, Z. | AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROL | ICAS2018_0129 |
| Dala, L. | PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAV | ICAS2018_0233 |
| Damodaran, M. | MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLE | ICAS2018_0230 |
| Danilkin, S.Y. | PERFORMANCES OF LPT AND LINEAR CASCADES AT LOW REYNOLDS NUMBERS | ICAS2018_0652 |
| Danzi, F. | NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODEL | ICAS2018_0556 |
| Daoud, F. | AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK | ICAS2018_0675 |
| Daud Filho, A.C. | FLIGHT DYNAMICS MODELING AND TRIM CURVES OF A CONCEPTUAL SEMI-TANDEM WING VTOL UAV | ICAS2018_0171 |
| Dautermann, T. | PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALS | ICAS2018_0050 |
| De Aguiar Quintanilha Jr., H.R. | ON THE EXISTENCE OF MULTIPLE SELF-EXCITATION FREQUENCIES IN THE INSTABILITY OF INTERACTING PLANAR MIXING LAYER AND WAKE | ICAS2018_0537 |
| de Almeida, O. | AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER PICKUP TRUCKS | ICAS2018_0201 |
| de Azevedo, B.A. | DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATS | ICAS2018_0807 |
| de Blécourt, A. | WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING | ICAS2018_0646 |
| De Breuker, R. | INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING | ICAS2018_0786 |
| de Bruin, A. | WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING | ICAS2018_0646 |
| de Campos, F.P.V. | POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION | ICAS2018_0818 |
| de Castro, E.S.B. | POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION | ICAS2018_0818 |
| De Crescenzio , F. | THE USE OF SYNTHETIC VISION TOOLS IN THE CONTROL TOWER ENVIRONMENT: THE RETINA CONCEPT | ICAS2018_0717 |
| De Crescenzio, F. | DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACH | ICAS2018_0774 |
| de Lima Monteiro, D.W. | DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS | ICAS2018_0609 |
| De Marco, A. | MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGN | ICAS2018_0504 |
| De Marco, A. | MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECT | ICAS2018_0648 |
| De Marqui Jr., C. | EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTION | ICAS2018_0391 |
| De Negri, V. | A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL | ICAS2018_0052 |
| De Negri, V.J. | DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE OF QUANTIZED CONTROL AND LMI APPROACH | ICAS2018_0521 |
| de Oliveira, W.R. | CHARACTERISTIC HELICOPTER FLIGHT MECHANICS AND MOTION CUEING INTEGRATION INTO THE SIVOR ROBOTIC FLIGHT SIMULATOR: AN OBJECTIVE APPROACH | ICAS2018_0506 |
| de Oliveira, L.A. | MODELLING OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITES: A COMPARATIVE STUDY | ICAS2018_0519 |
| de Pieri, E.R. | MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATION | ICAS2018_0586 |
| de Rosa, D. | VALIDATION OF INTERMITTENCY MODEL FOR TRANSITION PREDICTION IN A RANS FLOW SOLVER | ICAS2018_0484 |
| De Simone, V. | DE-ICING PHENOMENA MODELLED BY FINITE ELEMENT MODELS | ICAS2018_0180 |
| de Sousa, M.S. | STAMP METHOD APPLICATION ON INDUSTRIAL MANAGEMENT | ICAS2018_0553 |
| de Souza, C.E. | OPTIMAL SHAPE OF REPAIR PATCHES IN COMPOSITES | ICAS2018_0471 |
| Degtyar, V.G. | CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES | ICAS2018_0242 |
| Delbecq, S. | A MORE INTEGRATED DESIGN APPROACH FOR EMBEDDED MECHATRONIC SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMS | ICAS2018_0170 |
| Della Corte, B. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Della Vecchia, P. | AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATION | ICAS2018_0191 |
| Della Vecchia, P. | NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODEL | ICAS2018_0264 |
| Della Vecchia, P. | MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECT | ICAS2018_0648 |
| Della Vecchia , P. | MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT | ICAS2018_0783 |
| Della Vecchia, P. | COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTS | ICAS2018_0785 |
| Dell’Amico, A. | A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL | ICAS2018_0052 |
| Deng, Y.-P. | GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEM | ICAS2018_0057 |
| Deng, L. | ANALYSIS OF XH-59A ROTOR IN FORWARD FIGHT WITH HIGH EFFICIENCY TRIM METHOD | ICAS2018_0469 |
| Desvigne, D. | PERFORMANCE IMPROVEMENT OF A COMPOUND HELICOPTER ROTOR HEAD BY AERODYNAMIC SHAPE OPTIMIZATION | ICAS2018_0070 |
| Di Pasquale, D. | A RAPID AERODYNAMIC PREDICTION METHOD FOR UNCONVENTIONAL TRANSONIC AIRCRAFT CONFIGURATIONS | ICAS2018_0138 |
| Di Pasquale, D. | THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENT | ICAS2018_0297 |
| Di Rito, G. | MULTI-VARIABLE AIRCRAFT DIRECTIONAL CONTROL WITH ANTI-SKID DIFFERENTIAL BRAKES | ICAS2018_0607 |
| Di Rito, G. | SMART FAULT-TOLERANT AIR-DATA SENSOR FOR AIRCRAFT FLOW ANGLES MEASUREMENT | ICAS2018_0625 |
| Di Vito, V. | ALGORITHMS AND SYSTEM FOR CURVED AND CONTINUOUS DESCENT TRAJECTORIES IMPROVING FUEL EFFICIENCY IN TMA | ICAS2018_0063 |
| Diaz, M.A.R. | A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTS | ICAS2018_0309 |
| Díaz-Méndez, Y.A. | A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOT | ICAS2018_0559 |
| Diepolder, J. | USING SENSITIVITY PENALTIES TO ROBUSTIFY THE OPTIMAL REENTRY TRAJECTORY OF A HYPERSONIC VEHICLE | ICAS2018_0564 |
| Diepolder, J. | NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING | ICAS2018_0782 |
| Dietz, M. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Dikova, O.D. | INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELS | ICAS2018_0645 |
| Dillinger, E. | HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2018_0492 |
| Dimitriadis, G. | INVISCID AND VISCOUS FLOW MODELING FOR FAST TRANSONIC FLUTTER CALCULATIONS | ICAS2018_0436 |
| Dimitriadis, G. | HIGHER FIDELITY TRANSONIC AERODYNAMIC MODELING IN PRELIMINARY AIRCRAFT DESIGN | ICAS2018_0453 |
| Ding, K.H. | DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATE | ICAS2018_0691 |
| Djojodihardjo, H. | OVERVIEW ON THE INFLUENCE OF COANDA BLANKET CURVATURE ON COANDA DEVICE PERFORMANCE | ICAS2018_0738 |
| Djojodihardjo, H. | ASSESSMENT OF THE AERODYNAMICS AND AEROELASTICITY OF FLAPPING WING USING LINEARIZED COMPUTATIONAL METHOD | ICAS2018_0740 |
| Donadon, M.V. | STRUCTURAL DAMPING EFFECTS ON THE ACOUSTIC SCATTERING BY ELASTIC PLATES | ICAS2018_0108 |
| Donadon, M.V. | AN ACTIVE-PASSIVE NONLINEAR FINITE ELEMENT MODEL FOR ELECTROMECHANICAL COMPOSITE MORPHING BEAMS | ICAS2018_0207 |
| Donadon, M.V. | MODELLING OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITES: A COMPARATIVE STUDY | ICAS2018_0519 |
| Donadon, L.V. | GROUND VIBRATION TEST USING ACOUSTIC EXCITATION: APPLICATION ON A COMPOSITE WING | ICAS2018_0836 |
| Dong, W. | CALCULATION OF WATER FILM FLOW AND HEAT TRANSFER ON THE AIRCRAFT ANTI-ICING SURFACE | ICAS2018_0100 |
| Dong, L. | BUCKLING/POSTBUCKLING OPTIMIZATION OF STIFFENED COMPOSITE PANELS BASED ON SENSITIVITY ANALYSIS | ICAS2018_0714 |
| Dotta, F. | SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE | ICAS2018_0354 |
| Dotta, F. | CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHM | ICAS2018_0355 |
| Draxler, J. | COMPARISON OF TWO DIFFERENT INDICATORS FOR HOT CRACKING IN WELDED STRUCTURES | ICAS2018_0142 |
| Drewiacki, D. | THE INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIES | ICAS2018_0460 |
| Drofelnik, J. | ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHM | ICAS2018_0328 |
| Drofelnik, J. | WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITY | ICAS2018_0440 |
| Drofelnik, J. | FEASIBILITY OF THE NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING AIRCRAFT UNSTEADY AERODYNAMICS | ICAS2018_0791 |
| Droney, C.K. | SUBSONIC ULTRA-GREEN AIRCRAFT RESEARCH: TRANSONIC TRUSS-BRACED WING TECHNICAL MATURATION | ICAS2018_0597 |
| Duan, Z. | FEASIBILITY STUDY OF MODIFYING A BASELINE KEROSENE AIRCRAFT TO A LH2 POWERED VERSION | ICAS2018_0580 |
| Duarte, R.N.C. | EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORS | ICAS2018_0809 |
| Dubinskii, S. | STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATION | ICAS2018_0234 |
| Dubovikov, E.A. | INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURES | ICAS2018_0299 |
| Dubovikov, E. | NUMERICAL INVESTIGATION OF INFLUENCE OF INITIAL DAMAGES ON STRENGTH PARAMETERS OF CFRP | ICAS2018_0302 |
| Dugard, L. | A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNEL | ICAS2018_0406 |
| Döll, C. | HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2018_0492 |
| D´Ippolito, R. | MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECT | ICAS2018_0654 |
| Ebel, T. | MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENT | ICAS2018_0365 |
| Echer, L. | OPTIMAL SHAPE OF REPAIR PATCHES IN COMPOSITES | ICAS2018_0471 |
| Edberg, J. | COMPARISON OF TWO DIFFERENT INDICATORS FOR HOT CRACKING IN WELDED STRUCTURES | ICAS2018_0142 |
| Eek, M. | A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT | ICAS2018_0203 |
| Eek, M. | PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODEL | ICAS2018_0463 |
| Egorov, I.V. | DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATE | ICAS2018_0691 |
| Eitelberg, G. | AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMS | ICAS2018_0505 |
| Elham, A. | COUPLED ADJOINT AEROSTRUCTURAL OPTIMIZATION FRAMEWORK FOR PRELIMINARY AIRCRAFT DESIGN | ICAS2018_0426 |
| El´Youssef, E.S. | MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATION | ICAS2018_0586 |
| Enghardt, L. | NOVEL JET ENGINE ACOUSTIC LINER WITH IMPROVED BROADBAND NOISE ABSORPTION | ICAS2018_0333 |
| Entezari, M.M. | AN EFFICIENT FRAMEWORK FOR AERODYNAMIC CONFIGURATION EVOLUTION OF REENTRY VEHICELES | ICAS2018_0745 |
| Entzinger, J.O. | INDIVIDUALIZING FLIGHT SKILL TRAINING USING SIMULATOR DATA ANALYSIS AND BIOFEEDBACK | ICAS2018_0220 |
| Entzinger, J.O. | DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM | ICAS2018_0284 |
| Entzinger, J.O. | FAULT-TOLERANT FLIGHT CONTROL SYSTEM WITH SIMPLE ADAPTIVE CONTROL CONSIDERING PILOT INPUT | ICAS2018_0651 |
| Erhard, R. | A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIES | ICAS2018_0088 |
| Ernst, J.M. | 3D PERSPECTIVE VIEWS ON IMMERSIVE HEAD-WORN DISPLAYS - CAN EXOCENTRIC VIEWS INCREASE PILOT SITUATIONAL AWARENESS? | ICAS2018_0751 |
| Errico, A. | ALGORITHMS AND SYSTEM FOR CURVED AND CONTINUOUS DESCENT TRAJECTORIES IMPROVING FUEL EFFICIENCY IN TMA | ICAS2018_0063 |
| Eun, Y. | INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORT | ICAS2018_0059 |
| Eun, Y. | AIRPORT SURFACE TRAFFIC SCHEDULING WITH CONSIDERATION OF DE-ICING OPERATIONS | ICAS2018_0211 |
| Evangelista, L.M.C.S. | POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION | ICAS2018_0818 |
| Ezer, N. | HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONS | ICAS2018_0419 |
| Fan, Z. | APPLICATION OF HIGH-ROBUSTNESS BEMT FOR SIMULATION OF UAV-VTOL PROPELLER AT LOW/HIGH ADVANCE RATIO | ICAS2018_0131 |
| Fang, W. | ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLE | ICAS2018_0222 |
| Fang, F. | CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCH | ICAS2018_0405 |
| Fang, W. | STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WING | ICAS2018_0526 |
| Faraj, R. | HIGH PERFORMANCE PNEUMATIC SHOCK-ABSORBERS FOR AERONAUTICAL APPLICATIONS | ICAS2018_0344 |
| Fares, E. | LATTICE BOLTZMANN HIGH-LIFT SIMULATIONS - A STEP BEYOND CLASSICAL CFD | ICAS2018_0318 |
| Fateev, V.A. | CERTAIN ASPECTS OF FAN MODEL STAGE DESIGNING FOR ADVANCED TURBOFANS | ICAS2018_0626 |
| Favalli, F. | REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE | ICAS2018_0432 |
| Feaster, J. | BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION | ICAS2018_0661 |
| Fedorov, A.V. | DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATE | ICAS2018_0691 |
| Fedotova, K.V. | INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELS | ICAS2018_0645 |
| FEI, Y. | APPLICATION RESEARCH OF ZIMMERMAN-WEISSENBURGER-YANG METHOD FOR PREDICTING FLUTTER BOUNDARY | ICAS2018_0078 |
| Felux, M. | FLIGHT TECHNICAL ERROR EVALUATIONS FOR GBAS NAVIGATION REQUIREMENT DEFINITION | ICAS2018_0722 |
| Fenelon, F.A. | STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARS | ICAS2018_0573 |
| Feng, Z. | ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION | ICAS2018_0389 |
| Fernandez Villace, V. | LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMS | ICAS2018_0425 |
| Fernandez Villace, V. | A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE | ICAS2018_0429 |
| Ferrara, M. | REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE | ICAS2018_0432 |
| Ferrari, F. | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFTS | ICAS2018_0162 |
| Ferrari, D.B. | PROBABILISTIC FORECASTING IN AIRCRAFT EMERGENCY EVACUATION SIMULATION | ICAS2018_0202 |
| Ferreira, L.P.S. | GROUND VIBRATION TEST USING ACOUSTIC EXCITATION: APPLICATION ON A COMPOSITE WING | ICAS2018_0836 |
| Ferretto, D. | PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT | ICAS2018_0164 |
| Ferretto, D. | LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMS | ICAS2018_0425 |
| Ferretto, D. | A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE | ICAS2018_0429 |
| Feygenbaum, Y. | STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATION | ICAS2018_0234 |
| Fichera, S. | DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIES | ICAS2018_0509 |
| Fichert, F. | ADAPTING CAPACITY OF AIR NAVIGATION SERVICE PROVISION IN EUROPE - BETWEEN SCYLLA AND CHARYBDIS | ICAS2018_0483 |
| Fields, T.D. | FLIGHT PERFORMANCE OF STEERABLE CRUCIFORM PARACHUTE SYSTEMS | ICAS2018_0614 |
| Figueira, N. | SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVS | ICAS2018_0374 |
| Filatyev, A.S. | NEW APPROACH FOR INVESTIGATION OF MAXIMUM-RANGE AIRCRAFT TRAJECTORIES | ICAS2018_0726 |
| Fioriti, M. | PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT | ICAS2018_0164 |
| Fioriti, M. | INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORK | ICAS2018_0412 |
| Fioriti, M. | STUDIES ON PROPULSION AND ON-BOARD SYSTEMS MATCHING IN AGILE PROJECT DISTRIBUTED COLLABORATIVE MDO ENVIRONMENT APPLYING FOR ADVANCED REGIONAL AND MEDIUM HAUL JET | ICAS2018_0655 |
| Fioriti, M. | DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK | ICAS2018_0674 |
| Fioriti, M. | MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT | ICAS2018_0783 |
| Fischer, C. | IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLE | ICAS2018_0764 |
| Fisk, N. | AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATION | ICAS2018_0664 |
| Fokin, D. | MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECT | ICAS2018_0654 |
| Fomin, V. | NUMERICAL INVESTIGATION OF INFLUENCE OF INITIAL DAMAGES ON STRENGTH PARAMETERS OF CFRP | ICAS2018_0302 |
| Fomin, D. | NUMERICAL INVESTIGATION OF INFLUENCE OF INITIAL DAMAGES ON STRENGTH PARAMETERS OF CFRP | ICAS2018_0302 |
| Fonseca, G.C. | RESULTS AND COMPARISON OF NUMERICAL SIMULATION AND THE TESTING OF LUG MANUFACTURED BY COMPOSITE MATERIAL BY RTM PROCESS | ICAS2018_0007 |
| Fonseca, D.A. | HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENT | ICAS2018_0269 |
| Freire, G.A. | ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIES | ICAS2018_0438 |
| Frulla, G. | PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROL | ICAS2018_0430 |
| Frulla, G. | REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS | ICAS2018_0437 |
| Frulla, G. | NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODEL | ICAS2018_0556 |
| Frömming, C. | COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNS | ICAS2018_0708 |
| Fu, S. | THEORETICAL STUDY OF RECEPTIVITY OF HIGH-SPEED BOUNDARY LAYER TO SURFACE PERTURBATIONS | ICAS2018_0524 |
| Fu, J. | POSITION SYNCHRONIZATION OF AEROSPACE ELECTROMECHANICAL ACTUATORS FOR DISTRIBUTED ELECTRICAL ACTUATION SYSTEM | ICAS2018_0653 |
| Fu, Y. | POSITION SYNCHRONIZATION OF AEROSPACE ELECTROMECHANICAL ACTUATORS FOR DISTRIBUTED ELECTRICAL ACTUATION SYSTEM | ICAS2018_0653 |
| Fujita, K. | MONTE-CARLO EVALUATION OF CONTROL LAW FOR HIGH ALTITUDE FLIGHT TEST OF MARS AIRPLANE | ICAS2018_0431 |
| Fusaro, R. | LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMS | ICAS2018_0425 |
| Fusaro, R. | A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE | ICAS2018_0429 |
| Gál, I. | DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM | ICAS2018_0697 |
| Galatolo, R. | MULTI-VARIABLE AIRCRAFT DIRECTIONAL CONTROL WITH ANTI-SKID DIFFERENTIAL BRAKES | ICAS2018_0607 |
| Gamba, G. | IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS | ICAS2018_0249 |
| Gang, L. | KNOWLEDGE ENGINEERING BASED FLIGHT TEST TECHNOLOGY FOR CIVIL AIRCRAFT AIRWORTHINESS CONFORMITY | ICAS2018_0009 |
| Gao, Z.H | STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN | ICAS2018_0041 |
| Gao, Z.-H. | GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEM | ICAS2018_0057 |
| Gao, H.-G. | GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEM | ICAS2018_0057 |
| Gao, Z. | MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSIS | ICAS2018_0226 |
| Gao, X. | HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADES | ICAS2018_0248 |
| Gao, X. | WIND SHEAR PARAMETER ESTIMATION FOR DYNAMIC SOARING WITH UNMANNED AERIAL VEHICLES | ICAS2018_0464 |
| Gao, B. | RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFT | ICAS2018_0623 |
| García-Fogeda , B. | FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONS | ICAS2018_0286 |
| Gardi, A. | HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONS | ICAS2018_0419 |
| Gardi, A. | A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFT | ICAS2018_0684 |
| Gardi, A. | EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORS | ICAS2018_0694 |
| Garry, K.P. | A RAPID AERODYNAMIC PREDICTION METHOD FOR UNCONVENTIONAL TRANSONIC AIRCRAFT CONFIGURATIONS | ICAS2018_0138 |
| Garry, K. | THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENT | ICAS2018_0297 |
| Gastaldi, A.A. | AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK | ICAS2018_0675 |
| Gastaldi, A.A. | IMPLEMENTATION OF A VORTEX LATTICE METHOD IN A HETEROGENEOUS PROGRAMMING LANGUAGE ENVIRONMENT | ICAS2018_0846 |
| Gater, B. | BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION | ICAS2018_0661 |
| Gatlin, G.M. | SUBSONIC ULTRA-GREEN AIRCRAFT RESEARCH: TRANSONIC TRUSS-BRACED WING TECHNICAL MATURATION | ICAS2018_0597 |
| Gauci, J. | GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESS | ICAS2018_0182 |
| Gautier, N. | COMPARISON AND APPLICATION OF DIFFERENTS TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMIC WING DESIGN | ICAS2018_0527 |
| Gehlen, M. | EDUCATING ENGINEERS FOR THE DEVELOPMENT OF PRODUCT SERVICE SYSTEMS (PSS) | ICAS2018_0522 |
| Geister, R. | PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALS | ICAS2018_0050 |
| Geister, R. | IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS | ICAS2018_0249 |
| Gennaro, E.M. | EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF LAMINAR SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCES | ICAS2018_0195 |
| Gesell, H. | SYSTEM ANALYSIS OF TURBO ELECTRIC AND HYBRID ELECTRIC PROPULSION SYSTEMS ON A REGIONAL AIRCRAFT | ICAS2018_0831 |
| Geuther, S. | A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIES | ICAS2018_0088 |
| Giarola, R. | PROBABILISTIC FORECASTING IN AIRCRAFT EMERGENCY EVACUATION SIMULATION | ICAS2018_0202 |
| Gibert, J.-M. | NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODEL | ICAS2018_0556 |
| Gillen, S. | EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORK | ICAS2018_0178 |
| Girardi, R.d.M. | EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATION | ICAS2018_0382 |
| Goes, L.C.S. | A BOND GRAPH-ORIENTED METHOD FOR ASSESSMENT OF FAILURES IN AN AIRCRAFT HYDRAULIC BRAKE SYSTEM | ICAS2018_0551 |
| Góes, L.C.S. | IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLE | ICAS2018_0764 |
| Góes, L.C.S. | DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATS | ICAS2018_0807 |
| Góes, L.C.S. | CLOSED-LOOP SYSTEM IDENTIFICATION OF A LARGE FLEXIBLE AIRCRAFT USING SUBSPACE METHODS | ICAS2018_0813 |
| Goetzendorf-Grabowski, T. | MORPHING WING WITH SURFACE DISCONTINUITY - COMPARATIVE TESTS | ICAS2018_0025 |
| Golberg, F.D. | APPLICATION OF "VIRTUAL" CONTROLLERS FOR INTEGRATED PROPULSION AND AIRCRAFT CONTROL | ICAS2018_0640 |
| Golberg, F.D. | IDENTIFICATION METHOD OF THE SIMULATION MODEL "VIRTUAL ENGINE" BUILT INTO THE DIGITAL ENGINE CONTROL SYSTEM | ICAS2018_0643 |
| Goliszek, B. | STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATION | ICAS2018_0752 |
| Gollnick, V. | IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WIND | ICAS2018_0619 |
| Gollnick, V. | IMPLEMENTATION OF ECO-EFFICIENT PROCEDURES TO MITIGATE THE CLIMATE IMPACT OF NON-CO2 EFFECTS | ICAS2018_0644 |
| Gollnick, V. | COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNS | ICAS2018_0708 |
| Gollnick, V. | QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNING | ICAS2018_0755 |
| Golovanov, V. | DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINES | ICAS2018_0820 |
| Golubev, V. | ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV | ICAS2018_0254 |
| Golyska, U. | DESIGN AND OPTIMIZATION OF A VERSATILE UAV FOR OBSERVATION AND RESEARCH USING THERMAL COLUMNS FOR EXTENDED ENDURANCE | ICAS2018_0272 |
| Gomes, G.F. | A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOT | ICAS2018_0559 |
| Gomes Olavo, J.L. | FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETS | ICAS2018_0396 |
| Gómez Comendador, F. | DETECTING HIGH-ALTITUDE ICE CRYSTAL (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATURE | ICAS2018_0611 |
| Gómez-Escalonilla, J. | FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONS | ICAS2018_0286 |
| Gong, A. | FLIGHT TEST OF A FUEL-CELL/BATTERY/SUPERCAPACITOR TRIPLE HYBRID UAV PROPULSION SYSTEM | ICAS2018_0864 |
| Gonzaga Trabasso, L. | EDUCATING ENGINEERS FOR THE DEVELOPMENT OF PRODUCT SERVICE SYSTEMS (PSS) | ICAS2018_0522 |
| Gonzalez, P. | A NUMERICAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTURE | ICAS2018_0206 |
| Gonzalez, P.J. | IMPLEMENTATION AND FLIGHT TESTING OF AN ENHANCED STABILITY SYSTEM FOR A VERY FLEXIBLE AIRCRAFT | ICAS2018_0534 |
| González Biedma, C. | "FAST" CFD METHODS IN AIRCRAFT SYSTEM DESIGN. APPLICATION TO C295W MODIFICATIONS. | ICAS2018_0112 |
| Goraj, Z. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Goraj, Z.-J. | STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATION | ICAS2018_0752 |
| Gordin, M.V. | CHARACTERISTICS OF SYSTEMS WITH ELECTRICALLY DRIVEN UNITS - EXPERIMENTAL STUDIES IN A GAS TURBINE ENGINE DEMONSTRATOR | ICAS2018_0637 |
| Gouskov, O.V. | COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL | ICAS2018_0672 |
| Granlund, R. | DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMS | ICAS2018_0305 |
| Granzoto, R.M. | HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOT | ICAS2018_0337 |
| Grech, R. | GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESS | ICAS2018_0182 |
| Greco Jr., P.C. | DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONES | ICAS2018_0591 |
| Grewe, V. | IMPLEMENTATION OF ECO-EFFICIENT PROCEDURES TO MITIGATE THE CLIMATE IMPACT OF NON-CO2 EFFECTS | ICAS2018_0644 |
| Grewe, V. | COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNS | ICAS2018_0708 |
| Grigoriev, A.V. | AEROELASTIC PROPERTIES OF ACTIVE WINGLETS | ICAS2018_0276 |
| Grillo, C. | RECURSIVE AERODYNAMIC PARAMETER IDENTIFICATION OF A FIGHTER JET FLYING IN TURBULENT AIR | ICAS2018_0279 |
| Gringinger, E. | SEMANTICS-BASED SUMMARIZATION OF ATM DATA TO MANAGE INFORMATION OVERLOAD IN PILOT BRIEFINGS | ICAS2018_0763 |
| Grüter, B. | USING SENSITIVITY PENALTIES TO ROBUSTIFY THE OPTIMAL REENTRY TRAJECTORY OF A HYPERSONIC VEHICLE | ICAS2018_0564 |
| Grüter, B. | NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING | ICAS2018_0782 |
| Grönstedt, T. | PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS | ICAS2018_0649 |
| Guan, J. | WIND TUNNEL VIRTUAL FLIGHT TEST FOR A TRANSPORT AIRCRAFT WITH SIMULATED ICE SHAPE | ICAS2018_0125 |
| Gubanov, A.A. | RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0256 |
| Gubanov, A.A. | INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0508 |
| Gubskiy, V.V. | ADAPTIVE WING HIGH-LIFT SYSTEM | ICAS2018_0371 |
| Guedes, M.J.M. | SHIP-HELICOPTER OPERATIONAL LIMITATION ENVELOPE DEFINITION WITH CFD RESULTS AND WIND TUNNEL DATA | ICAS2018_0345 |
| Guenov, M. | AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACE | ICAS2018_0132 |
| Guenov, M.D. | COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN | ICAS2018_0134 |
| Guimaraes, T.A.M. | DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIES | ICAS2018_0509 |
| Guimarães Neto, A.B. | THE INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIES | ICAS2018_0460 |
| Guimarães Neto, A.B. | STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS | ICAS2018_0482 |
| Guimarães Neto, A.B. | CONTROL OF A VERY FLEXIBLE WING WITH SIMULTANEOUS OPTIMIZATION OF THE GAIN MATRIX AND THE SPATIAL DISTRIBUTION OF THE SENSORS | ICAS2018_0500 |
| Guimarães Neto, A.B. | ON REAL–TIME SIMULATION OF FLEXIBLE AIRCRAFT WITH PHYSICS–DERIVED MODELS | ICAS2018_0501 |
| Guimarães Neto, A.B. | APPLICABILITY OF GEOMETRICALLY-LINEAR STRUCTURAL-DYNAMIC MODELS FOR THE FLIGHT DYNAMICS OF ARBITRARILY-FLEXIBLE AIRCRAFT | ICAS2018_0523 |
| Guimarães Neto, A.B. | ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFT | ICAS2018_0529 |
| Gulienko, A.I. | CHARACTERISTICS OF SYSTEMS WITH ELECTRICALLY DRIVEN UNITS - EXPERIMENTAL STUDIES IN A GAS TURBINE ENGINE DEMONSTRATOR | ICAS2018_0637 |
| Guo, Z. | CALCULATION OF WATER FILM FLOW AND HEAT TRANSFER ON THE AIRCRAFT ANTI-ICING SURFACE | ICAS2018_0100 |
| Guo, L. | WIND TUNNEL VIRTUAL FLIGHT TEST FOR A TRANSPORT AIRCRAFT WITH SIMULATED ICE SHAPE | ICAS2018_0125 |
| Guo, L.L. | A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNEL | ICAS2018_0406 |
| Guo, B. | RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFT | ICAS2018_0610 |
| Guo, D. | BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTING | ICAS2018_0660 |
| Guo, L. | OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC | ICAS2018_0750 |
| Gupta, P.K. | SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTION | ICAS2018_0066 |
| Gurevich, O.S. | CHARACTERISTICS OF SYSTEMS WITH ELECTRICALLY DRIVEN UNITS - EXPERIMENTAL STUDIES IN A GAS TURBINE ENGINE DEMONSTRATOR | ICAS2018_0637 |
| Gurevich, O.S. | APPLICATION OF "VIRTUAL" CONTROLLERS FOR INTEGRATED PROPULSION AND AIRCRAFT CONTROL | ICAS2018_0640 |
| Gurevich, O.S. | IDENTIFICATION METHOD OF THE SIMULATION MODEL "VIRTUAL ENGINE" BUILT INTO THE DIGITAL ENGINE CONTROL SYSTEM | ICAS2018_0643 |
| Gwon, H.R. | DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM | ICAS2018_0067 |
| Güner, H. | INVISCID AND VISCOUS FLOW MODELING FOR FAST TRANSONIC FLUTTER CALCULATIONS | ICAS2018_0436 |
| Gårdhagen, R. | A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT | ICAS2018_0203 |
| Gårdhagen, R. | DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMS | ICAS2018_0305 |
| Gårdhagen, R. | PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODEL | ICAS2018_0463 |
| Göttlicher, C. | DEVELOPMENT OF A GENERIC FLIGHT TEST MANEUVER INJECTION MODULE | ICAS2018_0434 |
| Ha, S.K. | PLY THICKNESS INFLUENCE IN COMPRESSION AFTER IMPACT DAMAGE ON CARBON/EPOXY TEST SPECIMENS | ICAS2018_0707 |
| Habermann, A. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Hackett, K. | FUEL-BURN PENALTIES CAUSED BY IRREGULARITIES IN AIRCRAFT SURFACES (ASTEROID PROJECT) | ICAS2018_0184 |
| Hackett, K. | PRACTICAL APPLICATIONS OF VISCOUS FULL-POTENTIAL CFD CODES | ICAS2018_0338 |
| Hall, C.A. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Hall, D. | DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT | ICAS2018_0875 |
| Halle, M. | LOCAL MODEL NETWORKS APPLIED TO FLIGHT LOADS ESTIMATION | ICAS2018_0650 |
| Han, D. | DESIGN PARAMETER STUDY OF DRONE BLADE CONSIDERING AEROACOUSTICS | ICAS2018_0216 |
| Han, J.S. | UNSTEADY AERODYNAMIC CHARACTERISTICS OF THE OSCILLATING AIRFOIL USING MSBS | ICAS2018_0253 |
| Han, J.H. | UNSTEADY AERODYNAMIC CHARACTERISTICS OF THE OSCILLATING AIRFOIL USING MSBS | ICAS2018_0253 |
| Han, J.-H. | LONGITUDINAL FLIGHT CONTROL OF BIOINSPIRED FLAPPING-WING MICRO AIR VEHICLE WITH EXTENDED UNSTEADY VORTEX-LATTICE METHOD. | ICAS2018_0260 |
| Han, Z.-H. | SURROGATE-BASED OPTIMIZATION METHOD APPLIED TO MULTIDISCIPLINARY DESIGN OPTIMIZATION ARCHITECTURES | ICAS2018_0496 |
| Han, Z.-H. | A COMPARISON STUDY ON TRANSITION CHARACTERISTICS OF NLF FORWARD-SWEPT-WING AND AFT-SWEPT-WING | ICAS2018_0497 |
| Han, D. | ANALYSIS OF CHEMICALLY REACTING HYPERSONIC FLOW USING A MESHLESS METHOD | ICAS2018_0525 |
| Han, Z.-H. | COMBINING ADJOINT-BASED AND SURROGATE-BASED OPTIMIZATIONS FOR BENCHMARK AERODYNAMIC DESIGN PROBLEMS | ICAS2018_0715 |
| Han, S.-Q. | COMBINING ADJOINT-BASED AND SURROGATE-BASED OPTIMIZATIONS FOR BENCHMARK AERODYNAMIC DESIGN PROBLEMS | ICAS2018_0715 |
| Hanifi, A. | ON THE WAVE-CANCELLING NATURE OF BOUNDARY LAYER TRANSITION CONTROL | ICAS2018_0349 |
| Hanifi, A. | CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE | ICAS2018_0473 |
| Hanifi, A. | RESOLVENT-BASED CONTROL OF STREAKS IN BOUNDARY LAYERS | ICAS2018_0477 |
| Hansen, R.M.O. | DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS | ICAS2018_0609 |
| Hare, A.C.R. | BEYOND BEDFORD - DEVELOPMENT OF A TWO-DIMENSIONAL PILOT WORKLOAD RATING SCALE | ICAS2018_0699 |
| Harrison, N.A. | SUBSONIC ULTRA-GREEN AIRCRAFT RESEARCH: TRANSONIC TRUSS-BRACED WING TECHNICAL MATURATION | ICAS2018_0597 |
| Hartmann, P. | SCALABLE DESIGN APPROACH TO ANALYZE FLIGHT MECHANICAL PERFORMANCE OF TILT-WING UAVS | ICAS2018_0161 |
| Hartmann, J. | COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN | ICAS2018_0167 |
| Harton, B. | VERIFIED FUSELAGE SECTION WATER IMPACT MODELING | ICAS2018_0732 |
| He, X. | STUDY ON RADRA CROSS SECTION FOR FLYING-WING UNMANNED AERIAL VEHICLE WITH CLOSE FORMATION FLIGHT | ICAS2018_0086 |
| Hektor, O. | LIFECYCLE COSTS AND FEASIBILITY ANALYSIS OF THE DESIGNS OF UAV'S FOR HUMANITARIAN RELIEF MISSIONS | ICAS2018_0498 |
| Henningson, D.S. | ON THE WAVE-CANCELLING NATURE OF BOUNDARY LAYER TRANSITION CONTROL | ICAS2018_0349 |
| Henningson, D. | WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL | ICAS2018_0388 |
| Henningson, D. | CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE | ICAS2018_0473 |
| Henningson, D.S. | RESOLVENT-BASED CONTROL OF STREAKS IN BOUNDARY LAYERS | ICAS2018_0477 |
| Hermanutz, A. | VIRTUAL AIRCRAFT MODEL FOR AEROELASTIC SIMULATION AND LOAD PREDICTION OF A HIGH ASPECT RATIO COMPOSITE SWEPT WING | ICAS2018_0296 |
| Hermetz, J. | HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2018_0492 |
| Herrington, S.M. | FLIGHT PERFORMANCE OF STEERABLE CRUCIFORM PARACHUTE SYSTEMS | ICAS2018_0614 |
| Hesse, H. | DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATION | ICAS2018_0569 |
| Hickson, M. | ADAPTIVE LANDING SEQUENCING USING BIPARTITE GRAPHS AND PERFECT MATCHING | ICAS2018_0634 |
| Hidalgo, D. | EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS | ICAS2018_0402 |
| Hidalgo, D.F. | CHARACTERISTIC HELICOPTER FLIGHT MECHANICS AND MOTION CUEING INTEGRATION INTO THE SIVOR ROBOTIC FLIGHT SIMULATOR: AN OBJECTIVE APPROACH | ICAS2018_0506 |
| Higashino, S. | VERTICAL LANDING OF A FIXED-WING UAV USING THE FLAT SPIN | ICAS2018_0415 |
| Hinchliffe, B. | FUEL-BURN PENALTIES CAUSED BY IRREGULARITIES IN AIRCRAFT SURFACES (ASTEROID PROJECT) | ICAS2018_0184 |
| Hirabayashi, H. | SIMULATION STUDY FOR VFR AIRCRAFT AND SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) MIXED OPERATIONS IN LOW LEVEL AIRSPACE | ICAS2018_0636 |
| Hiruma, M. | EVALUATION OF ALTITUDE CONTROL FOR AN AIRBREATHING HYPERSONIC AIRCRAFT MODEL | ICAS2018_0796 |
| Hlybov, V.I. | CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES | ICAS2018_0242 |
| Hobbins, R. | STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDS | ICAS2018_0367 |
| Hoeijmakers, H.W.M. | NUMERICAL INVESTIGATION AERODYNAMICS NACELLE-STRAKE EFFECT | ICAS2018_0205 |
| Hoeschler, K. | NOVEL JET ENGINE ACOUSTIC LINER WITH IMPROVED BROADBAND NOISE ABSORPTION | ICAS2018_0333 |
| Holmberg, G. | DIGITAL INNOVATION IN COMPLEX SYSTEMS-MANAGING CRITICAL APPLICATIONS AND GENERATIVITY | ICAS2018_0867 |
| Holzapfel, F. | INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS | ICAS2018_0043 |
| Holzapfel, F. | BI-LEVEL TRAJECTORY OPTIMIZATION BY STOCHASTIC COLLOCATION FOR UNCERTAINTY INTERVAL CALCULATION | ICAS2018_0221 |
| Holzapfel, F. | ROBUST TRAJECTORY OPTIMIZATION OF VTOL TRANSITION MANEUVER USING BI-LEVEL OPTIMAL CONTROL | ICAS2018_0224 |
| Holzapfel, F. | EVALUATION OF AIRCRAFT BRAKING PERFORMANCE BASED ON OPERATIONAL FLIGHT DATA | ICAS2018_0232 |
| Holzapfel, F. | THRUST MODELS BASED ON OPERATIONAL FLIGHT DATA USED IN PARAMETER ESTIMATION FOR SAFETY ANALYSES | ICAS2018_0314 |
| Holzapfel, F. | DEVELOPMENT OF A GENERIC FLIGHT TEST MANEUVER INJECTION MODULE | ICAS2018_0434 |
| Holzapfel, F. | USING SENSITIVITY PENALTIES TO ROBUSTIFY THE OPTIMAL REENTRY TRAJECTORY OF A HYPERSONIC VEHICLE | ICAS2018_0564 |
| Holzapfel, F. | FLIGHT TECHNICAL ERROR EVALUATIONS FOR GBAS NAVIGATION REQUIREMENT DEFINITION | ICAS2018_0722 |
| Holzapfel, F. | NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING | ICAS2018_0782 |
| Holzapfel, F. | PLANNING, IMPLEMENTATION, AND EXECUTION OF AN AUTOMATIC FIRST FLIGHT OF A UAV | ICAS2018_0844 |
| Hong, Y. | DESIGN PARAMETER STUDY OF DRONE BLADE CONSIDERING AEROACOUSTICS | ICAS2018_0216 |
| Hong, S.-M. | MULTISTAGE MISSILE TRAJECTORY AND STAGE OPTIMIZATION VIA DELTA-V APPROACH | ICAS2018_0385 |
| Hoogreef, M.F.M. | SYSTEM-LEVEL ASSESSMENT OF TAIL-MOUNTED PROPELLERS FOR REGIONAL AIRCRAFT | ICAS2018_0065 |
| Horiuchi, R. | SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT | ICAS2018_0754 |
| Horn, M. | STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION | ICAS2018_0852 |
| Hornung, M. | DEVELOPMENT AND PERFORMANCE COMPARISON OF OPTIMIZED ELECTRIC FIXED-WING VTOL UAV CONFIGURATIONS | ICAS2018_0169 |
| Hornung, M. | EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORK | ICAS2018_0178 |
| Hornung, M. | A TECHNIQUE FOR CAPTURING STAKEHOLDER PREFERENCES AND KNOWLEDGE IN EARLY DESIGN STUDIES | ICAS2018_0208 |
| Hornung, M. | ELECTRIC VTOL UAV CONFIGURATION STUDIES AND OPTIMIZATION WITHIN AIRCRAFT DESIGN PRACTICAL COURSE AT TECHNICAL UNIVERSITY OF MUNICH | ICAS2018_0240 |
| Hornung, M. | A FRAMEWORK TO ASSESS FUTURE AIRPORT NOISE APPLIED TO A TWO-RUNWAY AIRPORT | ICAS2018_0277 |
| Hornung, M. | VIRTUAL AIRCRAFT MODEL FOR AEROELASTIC SIMULATION AND LOAD PREDICTION OF A HIGH ASPECT RATIO COMPOSITE SWEPT WING | ICAS2018_0296 |
| Hornung, M. | A FRAMEWORK FOR UNCONVENTIONAL LANDING GEAR CONFIGURATION MODELLING | ICAS2018_0688 |
| Hornung, M. | DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT | ICAS2018_0728 |
| Hornung, M. | A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR VEHICLE CONCEPTS FOR URBAN AIR MOBILITY | ICAS2018_0794 |
| Horton, B. | PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFT | ICAS2018_0826 |
| Hou, T. | PASSIVE CONTROL METHOD IN ATTENUATING SELF-INDUCED ROLL OSCILLATIONS OF LOW-ASPECT-RATIO WINGS USING OBLIQUE SLOT BLEED | ICAS2018_0468 |
| Howarth, D.K. | A 7D TRADE | ICAS2018_0062 |
| Hu, T. | PASSIVE CONTROL METHOD IN ATTENUATING SELF-INDUCED ROLL OSCILLATIONS OF LOW-ASPECT-RATIO WINGS USING OBLIQUE SLOT BLEED | ICAS2018_0468 |
| Huan, Z. | ROBUST DESIGN OPTIMIZATION OF BENCHMARK AERODYNAMIC CASE BASED ON POLYNOMIAL CHAOS EXPANSION | ICAS2018_0187 |
| Huang, M. | AERODYNAMIC DESIGN OF A RIGID COAXIAL ROTOR AIRFOIL IN UNSTEADY FLOW | ICAS2018_0172 |
| Huang, W.C. | HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADES | ICAS2018_0248 |
| Huang, N.-Z. | THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVER | ICAS2018_0470 |
| Huh, J.Y. | ANALYSIS OF CHEMICALLY REACTING HYPERSONIC FLOW USING A MESHLESS METHOD | ICAS2018_0525 |
| Huo, S. | THERMAL-MECHNICAL COUPLING ANALYSIS AND OPTIMIZATION DESIGN ON TPS WITH GAP | ICAS2018_0266 |
| Hällqvist, R. | A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT | ICAS2018_0203 |
| Hällqvist, R. | PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODEL | ICAS2018_0463 |
| Höhndorf, L. | INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS | ICAS2018_0043 |
| Iha, K. | MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENT | ICAS2018_0365 |
| Iijima, T. | DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM | ICAS2018_0284 |
| Iijima, T. | OPERATIONAL CONCEPT AND VALIDATION OF A NEW AIRPORT LOW-LEVEL WIND INFORMATION SYSTEM | ICAS2018_0452 |
| Ikeda, T. | MULTIFUNCTIONAL COMPOSITE PROCESSED USING EMBROIDERY TECHNOLOGY | ICAS2018_0475 |
| Inokuchi, H. | FLIGHT DEMONSTRATION OF A LONG RANGE ONBOARD DOPPLER LIDAR | ICAS2018_0121 |
| Inokuchi, H. | DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM | ICAS2018_0284 |
| Invigorito, M. | NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMP | ICAS2018_0622 |
| Iscold, P.H. | GROUND VIBRATION TEST USING ACOUSTIC EXCITATION: APPLICATION ON A COMPOSITE WING | ICAS2018_0836 |
| Ishigami, M. | MULTIFUNCTIONAL COMPOSITE PROCESSED USING EMBROIDERY TECHNOLOGY | ICAS2018_0475 |
| Ishmuratov, F.Z. | AEROELASTIC TAILORING OF COMPOSITE WING BY USING MULTIDISCIPLINARY DESIGN ENVIRONMENT | ICAS2018_0458 |
| Islam, T. | SCALABLE DESIGN APPROACH TO ANALYZE FLIGHT MECHANICAL PERFORMANCE OF TILT-WING UAVS | ICAS2018_0161 |
| Isyanov, A. | MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECT | ICAS2018_0654 |
| Isyanov, A. | STUDIES ON PROPULSION AND ON-BOARD SYSTEMS MATCHING IN AGILE PROJECT DISTRIBUTED COLLABORATIVE MDO ENVIRONMENT APPLYING FOR ADVANCED REGIONAL AND MEDIUM HAUL JET | ICAS2018_0655 |
| Itoh, E. | STUDY ON THE ARRIVAL MANAGER MAXIMIZING THE BENEFIT OF FOUR-DIMENSIONAL TRAJECTORY BASED OPERATIONS | ICAS2018_0315 |
| Ivanov, A.I. | APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTS | ICAS2018_0321 |
| Ivanyushkin, D.S. | RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0256 |
| Ivanyushkin, D.S. | INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0508 |
| Iwafuji, H. | EXHAUST PLUME EFFECT OF WINGED TWO-STAGE-TO-ORBIT SEPARATION AT ASCENT USING AERODYNAMIC-FLIGHT DYNAMICS TECHNIQUE | ICAS2018_0444 |
| Iwata, K. | SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT | ICAS2018_0754 |
| Izuka, J.H. | A NUMERICAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTURE | ICAS2018_0206 |
| Izuka, J. | KINEMATICS AND DYNAMICS OF A TENSEGRITY STRUCTURE IN EXPANSION | ICAS2018_0329 |
| Jamison, K.A. | GRID-MODE TRANSONIC STORE SEPARATION ANALYSES USING MODERN DESIGN OF EXPERIMENTS | ICAS2018_0552 |
| Jankovics, I. | LOAD MONITORING FOR OPERATORS’ LOAD MANAGEMENT | ICAS2018_0698 |
| Jankowski, A. | ENGINE TEST RESULTS OF FUEL-WATER MICROEMULSION | ICAS2018_0769 |
| Jankowski, A. | OPTIMIZATION OF THE FUEL INJECTOR TO AN INTERNAL COMBUSTION ENGINE BY MEANS OF LASER EQUIPMENT | ICAS2018_0825 |
| Janser, F. | SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY | ICAS2018_0727 |
| Jara, A. | AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR-SPACE EXPLORATION USING A HIGH ALTITUDE BALLOON | ICAS2018_0582 |
| Jegley, D. | PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFT | ICAS2018_0826 |
| Jehl, L. | BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION | ICAS2018_0661 |
| Jeon, D. | INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORT | ICAS2018_0059 |
| Jeon, D. | AIRPORT SURFACE TRAFFIC SCHEDULING WITH CONSIDERATION OF DE-ICING OPERATIONS | ICAS2018_0211 |
| Jeong, M. | INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORT | ICAS2018_0059 |
| Jiffri, S. | DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIES | ICAS2018_0509 |
| Jiménez Serrano, F. | DECISION-MAKING INFORMATION SYSTEM FOR MULTIMODAL DISRUPTION MANAGEMENT: SYSTEM ARCHITECTURE AND CONCEPT OF OPERATIONS | ICAS2018_0671 |
| Jin, X.H. | SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLE | ICAS2018_0306 |
| Johannesson, H. | MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENT | ICAS2018_0101 |
| Johansson, B.J.E. | DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMS | ICAS2018_0305 |
| Jokinen, J. | MULTI-SITE DELAMINATION ANALYSIS USING VIRTUAL CRACK CLOSURE TECHNIQUE FOR A COMPOSITE AIRCRAFT WING FLAP | ICAS2018_0343 |
| Jordan, P. | ACOUSTIC MODES AND GLOBAL INSTABILITIES IN WAKES AND JETS | ICAS2018_0450 |
| Jorge, C.T. | MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP | ICAS2018_0493 |
| Jouannet, C. | MULTIDISCIPLINARY OPTIMIZATION OF UNMANNED AIRCRAFT IN A SYSTEM OF SYSTEMS CONTEXT | ICAS2018_0047 |
| Jouannet, C. | METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT | ICAS2018_0663 |
| Jouannet, C. | A HOLISTIC ENGINEERING APPROACH FOR AERONAUTICAL PRODUCT DEVELOPMENT | ICAS2018_0724 |
| Joyodiharjo, A.K. | ASSESSMENT OF THE AERODYNAMICS AND AEROELASTICITY OF FLAPPING WING USING LINEARIZED COMPUTATIONAL METHOD | ICAS2018_0740 |
| Jungo, A. | AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK | ICAS2018_0675 |
| Jungo, A. | MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT | ICAS2018_0783 |
| Júnior, H.N.S. | MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP | ICAS2018_0493 |
| Justin, C. | ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACH | ICAS2018_0851 |
| Kadjardouzov, P. | THE STUDY OF TURBORAMJETS IN CIAM | ICAS2018_0848 |
| Kageyama, K. | A SIMULATION MODELING STUDY FOR FREE ROUTING AIRSPACE IN JAPAN | ICAS2018_0158 |
| Kaiser, S. | A COMPOSITE CYCLE ENGINE CONCEPT FOR YEAR 2050 | ICAS2018_0638 |
| Kaiser, J. | DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT | ICAS2018_0728 |
| Kajiwara, Y. | AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM | ICAS2018_0219 |
| Kalashnikov, S.T. | CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES | ICAS2018_0242 |
| Kale, U. | LOAD MONITORING FOR OPERATORS’ LOAD MANAGEMENT | ICAS2018_0698 |
| Kalinin, D.V. | APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADES | ICAS2018_0173 |
| Kalinin, D. | DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINES | ICAS2018_0820 |
| Kamimura, A. | SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT | ICAS2018_0754 |
| Kanazawa, F. | AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR-SPACE EXPLORATION USING A HIGH ALTITUDE BALLOON | ICAS2018_0582 |
| Kanerva, M. | MULTI-SITE DELAMINATION ANALYSIS USING VIRTUAL CRACK CLOSURE TECHNIQUE FOR A COMPOSITE AIRCRAFT WING FLAP | ICAS2018_0343 |
| Kanerva, M. | ARAMID-FIBER REINFORCED ELASTOMERS AS FUTURE AIRCRAFT ACTUATORS - A PROOF-OF-CONCEPT INVESTIGATION | ICAS2018_0377 |
| Kang, J.P. | COST-EFFECTIVE TELEMETRY, TRACKING AND COMMAND SYSTEM DEVELOPMENT FOR HIGH-ALTITUDE SCIENTIFIC BALLOON | ICAS2018_0214 |
| Kang, L. | IMPROVED DELAYED DETACHED EDDY SIMULATION OF THE FLOWS AROUND S809 AIRFOIL FOR ANGLES OF ATTACK FROM 0 TO 90 DEGREES | ICAS2018_0323 |
| Kartashev, A. | RESEARCH OF FLOW IN STAGE OF TURBINE AND OPTIMAL MODES OF MICRO GAS TURBINE POWER PLANT | ICAS2018_0075 |
| Kassapoglou, C. | MODIFIED WHITNEY-NUISMER CRITERIA FOR PREDICTION OF NOTCHED STRENGTH OF COMPOSITE LAMINATES | ICAS2018_0677 |
| Kazarin, P. | ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV | ICAS2018_0254 |
| Kellermann, H. | A COMPOSITE CYCLE ENGINE CONCEPT FOR YEAR 2050 | ICAS2018_0638 |
| Kesselman, M.G. | ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORS | ICAS2018_0639 |
| Kharkovsky, S.V. | THE INFLUENCE OF THE SHAPE OF THE COOLING CHANNEL AND PRESSURE GRADIENT ON THE EFFICIENCY OF FILM COOLING OF GTE BLADES | ICAS2018_0629 |
| Kharlamov, D. | WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITY | ICAS2018_0440 |
| Khoo, B.C. | MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLE | ICAS2018_0230 |
| Kii, K. | PRECISE MEASUREMENT OF PROPAGATING FLAME IN 2-STROKE GASOLINE ENGINE BY MULTIPLE ION-PROBES | ICAS2018_0149 |
| Kim, Y. | PERFORMANCE ANALYSIS OF UAV PERSISTENT SURVEILLANCE ALGORITHM | ICAS2018_0046 |
| Kim, H. | INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORT | ICAS2018_0059 |
| Kim, S. | INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORT | ICAS2018_0059 |
| Kim, W.B. | DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM | ICAS2018_0067 |
| Kim, D.W. | DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM | ICAS2018_0067 |
| Kim, Y. | MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMIT | ICAS2018_0080 |
| Kim, J.H. | ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTING | ICAS2018_0159 |
| Kim, Y. | QUASI-LPV MODELING AND PARAMETER-DEPENDENT OPTIMAL CONTROL OF MORPHING WING AIRCRAFT | ICAS2018_0218 |
| Kim, A.S. | INVESTIGATION OF BULGING EFFECTS ON PROPAGATION OF 1-BAY AND 2-BAY LONGITUDINAL CRACKS WITH BROKEN/INTACT STIFFENER | ICAS2018_0376 |
| Kim, K.H. | ANALYSIS OF CHEMICALLY REACTING HYPERSONIC FLOW USING A MESHLESS METHOD | ICAS2018_0525 |
| Kim, H. | DEVELOPMENT OF A COMPREHENSIVE ANALYSIS AND OPTIMIZED DESIGN FRAMEWORK FOR THE MULTIROTOR UAV | ICAS2018_0594 |
| Kirk, J. | A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIES | ICAS2018_0088 |
| Klein, C. | COUPLING OF PREDESIGN AND PERFORMANCE TOOLS FOR TRANSIENT AIRCRAFT ENGINE ANALYSES | ICAS2018_0830 |
| Kling, U. | A FRAMEWORK FOR UNCONVENTIONAL LANDING GEAR CONFIGURATION MODELLING | ICAS2018_0688 |
| Koenig, B. | LATTICE BOLTZMANN HIGH-LIFT SIMULATIONS - A STEP BEYOND CLASSICAL CFD | ICAS2018_0318 |
| Kohmura, A. | SIMULATION STUDY FOR VFR AIRCRAFT AND SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) MIXED OPERATIONS IN LOW LEVEL AIRSPACE | ICAS2018_0636 |
| Kondakov, I. | DEVELOPMENT OF STRUCTURE ELEMENTS BASED ON ARCHITECTURED MATERIALS FOR PERSPECTIVE CIVIL AIRCRAFTS | ICAS2018_0304 |
| Konovalov, V.V. | ON EQUIVALENCE OF POLYMER COMPOSITE MATERIALS STRUCTURES LOADING PROGRAMS UNDER FULL-SCALED SERVICE CYCLE TESTING | ICAS2018_0185 |
| Koppitz, P. | INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS | ICAS2018_0043 |
| Koppitz, P. | THRUST MODELS BASED ON OPERATIONAL FLIGHT DATA USED IN PARAMETER ESTIMATION FOR SAFETY ANALYSES | ICAS2018_0314 |
| Koslosky, L.B. | AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATION | ICAS2018_0664 |
| Koster, J.N. | EXPERIENCE WITH INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN EDUCATION: AREND UAV | ICAS2018_0217 |
| Kota, S. | FLEXFLOIL SHAPE ADAPTIVE CONTROL SURFACES-FLIGHT TEST AND NUMERICAL RESULTS | ICAS2018_0384 |
| Kotsur, O.S. | VISCOUS FLUID SIMULATION WITH THE VORTEX ELEMENT METHOD | ICAS2018_0718 |
| Kowalski, R. | FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORS | ICAS2018_0271 |
| Kowalski, M. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Kowalski, M. | STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATION | ICAS2018_0752 |
| Kowalski, M. | ENGINE TEST RESULTS OF FUEL-WATER MICROEMULSION | ICAS2018_0769 |
| Kowalski, M. | OPTIMIZATION OF THE FUEL INJECTOR TO AN INTERNAL COMBUSTION ENGINE BY MEANS OF LASER EQUIPMENT | ICAS2018_0825 |
| Kraemer, A.D. | DATA-DRIVEN FAILURE IDENTIFICATION USING A MOTION-BASED SIMULATOR | ICAS2018_0581 |
| Krause, C. | DEVELOPMENT OF A GENERIC FLIGHT TEST MANEUVER INJECTION MODULE | ICAS2018_0434 |
| Kreimeier, M. | SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY | ICAS2018_0727 |
| Krupa, G.P. | APPLICATION OF AGILE MODEL-BASED SYSTEMS ENGINEERING IN AIRCRAFT CONCEPTUAL DESIGN | ICAS2018_0570 |
| Krus, P. | A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL | ICAS2018_0052 |
| Krus, P. | EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROL | ICAS2018_0200 |
| Krus, P. | A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT | ICAS2018_0203 |
| Krus, P. | DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE OF QUANTIZED CONTROL AND LMI APPROACH | ICAS2018_0521 |
| Krus, P. | METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT | ICAS2018_0663 |
| Krus, P. | AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATION | ICAS2018_0664 |
| Krus, P. | INTEGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS | ICAS2018_0873 |
| Krutov, A.A. | CONTAINERIZED AIR FREIGHT SYSTEM POWERED BY CRYOGENIC FUEL | ICAS2018_0103 |
| Krzysiak, A. | EXPERIMENTAL INVESTIGATION OF WING LOAD CONTROL USING FLUIDIC DEVICES | ICAS2018_0095 |
| Kuerten, J. | THRUST MODELS BASED ON OPERATIONAL FLIGHT DATA USED IN PARAMETER ESTIMATION FOR SAFETY ANALYSES | ICAS2018_0314 |
| Kukshinov, N.V. | INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0508 |
| Kukshinov, N.V. | COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL | ICAS2018_0672 |
| Kulhánek, R. | EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPS | ICAS2018_0258 |
| Kurita, J. | AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR-SPACE EXPLORATION USING A HIGH ALTITUDE BALLOON | ICAS2018_0582 |
| Kurka, P. | A NUMERICAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTURE | ICAS2018_0206 |
| Kurka, P. | KINEMATICS AND DYNAMICS OF A TENSEGRITY STRUCTURE IN EXPANSION | ICAS2018_0329 |
| Kursakov, I.A. | PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT | ICAS2018_0788 |
| Kuzmin, P.V. | MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALL | ICAS2018_0016 |
| Kuzmin, Y.V. | THE NUMERICAL HISTORY OF AIRPLANE MANUFACTURING IN XX CENTURY | ICAS2018_0705 |
| Kwak, D. | PRELIMINARY STUDY OF THE AERODYNAMIC CHARACTERISTICS OF KRUEGER FLAP ON THE SST CONFIGURATION | ICAS2018_0098 |
| Kügler, M.E. | PLANNING, IMPLEMENTATION, AND EXECUTION OF AN AUTOMATIC FIRST FLIGHT OF A UAV | ICAS2018_0844 |
| Ladner, R. | FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORS | ICAS2018_0271 |
| Laguardia, J. | ERRORS FROM ENGINEERING IN FLIGHT SAFETY | ICAS2018_0307 |
| Lakemond, N. | DIGITAL INNOVATION IN COMPLEX SYSTEMS-MANAGING CRITICAL APPLICATIONS AND GENERATIVITY | ICAS2018_0867 |
| Lammen, W.F. | INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING | ICAS2018_0786 |
| Lammers, K.H. | RELEASE OF DYNAMICALLY SCALED OBJECTS FROM A HELICOPTER WIND TUNNEL MODEL | ICAS2018_0064 |
| Landahl, J. | MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENT | ICAS2018_0101 |
| Lanshin, A.I. | RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM | ICAS2018_0036 |
| Lantto, B. | A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL | ICAS2018_0052 |
| Lantto, B. | EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROL | ICAS2018_0200 |
| Lanzillotti, A. | PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROL | ICAS2018_0430 |
| Lapcevic, V. | DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCES | ICAS2018_0364 |
| Larsson, R. | METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT | ICAS2018_0663 |
| Lauterjung Q., R. | DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONES | ICAS2018_0591 |
| Lawson, N.J. | THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENT | ICAS2018_0297 |
| Le Blaye, P. | LOW LEVEL TRAFFIC MONITORING: RPAS CONCEPT OF OPERATION AND DEVELOPEMENT OF A GROUND BASED SYSTEM | ICAS2018_0193 |
| Le Tallec, C. | LOW LEVEL TRAFFIC MONITORING: RPAS CONCEPT OF OPERATION AND DEVELOPEMENT OF A GROUND BASED SYSTEM | ICAS2018_0193 |
| Lee, R. | SIMULATIONS OF UNSTEADY AIRWAKES BEHIND SHIPS IN MOTION | ICAS2018_0038 |
| Lee, S. | PERFORMANCE ANALYSIS OF UAV PERSISTENT SURVEILLANCE ALGORITHM | ICAS2018_0046 |
| Lee, K.W. | DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM | ICAS2018_0067 |
| Lee, H.S. | DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORM | ICAS2018_0067 |
| Lee, S. | MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMIT | ICAS2018_0080 |
| Lee, Y.B. | ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTING | ICAS2018_0159 |
| Lee, J. | QUASI-LPV MODELING AND PARAMETER-DEPENDENT OPTIMAL CONTROL OF MORPHING WING AIRCRAFT | ICAS2018_0218 |
| Lee, S. | MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLE | ICAS2018_0230 |
| Lee, J.-W. | LONGITUDINAL FLIGHT CONTROL OF BIOINSPIRED FLAPPING-WING MICRO AIR VEHICLE WITH EXTENDED UNSTEADY VORTEX-LATTICE METHOD. | ICAS2018_0260 |
| Lee, Y. | INVESTIGATION ON THE POSSIBILITY OF FLOW CONTROL AROUND CAVITY USING TANGENTIAL JET | ICAS2018_0311 |
| Lee, J. | FLIGHT TECHNICAL ERROR EVALUATIONS FOR GBAS NAVIGATION REQUIREMENT DEFINITION | ICAS2018_0722 |
| Leite, H.F. | TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCK OSCILATIONS | ICAS2018_0599 |
| Lemmens, Y. | AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATION | ICAS2018_0133 |
| Leng, Y. | ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLE | ICAS2018_0039 |
| Levin, V. | STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPY | ICAS2018_0308 |
| Li, X. | CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF "PARASITE" NOISE | ICAS2018_0116 |
| Li, X.P. | IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED | ICAS2018_0119 |
| Li, R.Z. | MULTI-POINT AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WING | ICAS2018_0154 |
| Li, P. | THE EFFECT OF STRUCTURAL PARAMETERS OF AIRCRAFT PANEL ON VIBRATION FATIGUE LIFE | ICAS2018_0281 |
| Li, Y.-H. | MULTI-CHANNEL HUMAN-MACHINE INTERACTIVE SYSTEM FOR MULTIPLE UAVS' CONTROL | ICAS2018_0348 |
| Li, Q. | AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMS | ICAS2018_0505 |
| Li, Z. | RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFT | ICAS2018_0610 |
| Li, Z. | RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFT | ICAS2018_0623 |
| Liaboeuf, R. | HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2018_0492 |
| Liang, X. | THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVER | ICAS2018_0470 |
| Lieu, W. | DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT | ICAS2018_0875 |
| Lim, Y. | HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONS | ICAS2018_0419 |
| Lim, D. | DEVELOPMENT OF A COMPREHENSIVE ANALYSIS AND OPTIMIZED DESIGN FRAMEWORK FOR THE MULTIROTOR UAV | ICAS2018_0594 |
| Lim, Y. | A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFT | ICAS2018_0684 |
| Lim, Y. | EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORS | ICAS2018_0694 |
| Lin, Y.-F. | ANALYSIS OF XH-59A ROTOR IN FORWARD FIGHT WITH HIGH EFFICIENCY TRIM METHOD | ICAS2018_0469 |
| Lin, Y.-F. | THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVER | ICAS2018_0470 |
| Linke, F. | THE GLOBAL FUEL SAVING POTENTIAL OF INTERMEDIATE STOP OPERATIONS CONSIDERING METEOROLOGICAL AND OPERATIONAL INFLUENCES | ICAS2018_0021 |
| Linn, R.V. | LARGE EDDY SIMULATION OF A TRANSIENT SPOILER DEPLOYMENT IN A NACA0012 PROFILE IN SUBSONIC AND TRANSONIC SPEEDS | ICAS2018_0503 |
| Liorbano, F.F. | INFLUENCE OF AIRFRAME STIFFNESS ON THE AERODYNAMIC COEFFICIENTS OF A HIGH ASPECT RATIO WING | ICAS2018_0776 |
| Litao, F. | RLG BASED REAL-TIME MODEL ATTITUDE DETERMINATION SYSTEM DEVELOPMENT FOR LARGE LOW SPEED FACILITY OF CARDC | ICAS2018_0317 |
| Liu, K. | NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON SUPERCRITICAL WING AERODYNAMIC LOADS | ICAS2018_0001 |
| Liu, N. | A ROBUST STABLE PI CONTROLLER DESIGN IN TIME-FREQUENCY DUAL DOMAINS FOR AIRCRAFT ENGINE | ICAS2018_0027 |
| Liu, Z. | ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLE | ICAS2018_0039 |
| Liu, H. | PREDICTING LOW-VELOCITY IMPACT DAMAGE IN COMPOSITE USING COHESIVE ELEMENT | ICAS2018_0049 |
| Liu, P. | IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED | ICAS2018_0119 |
| Liu, P.Q. | HIGH LIFT MECHANISM OF A 2D FLAPPING WING IN HOVERING FLIGHT | ICAS2018_0151 |
| Liu, X. | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFTS | ICAS2018_0162 |
| Liu, P. | MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSIS | ICAS2018_0226 |
| Liu, Z.B. | AERODYNAMIC DESIGN OF KEY COMPONENTS OF THE LARGE-DISCHARGE AXIAL FAN AT HIGH ALTITUDE | ICAS2018_0243 |
| Liu, H. | STUDY ON EVALUATION METHODS OF UNDERGRADUATE AIRCRAFT OVERALL DESIGN COURSE BASED ON TEAM DESIGN COMPETITION | ICAS2018_0250 |
| Liu, C.-M. | HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILES | ICAS2018_0270 |
| Liu, Z. | A RESEARCH OF MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM FOR FIGHT VEHICLE DESIGN | ICAS2018_0443 |
| Liu, D. | WIND SHEAR PARAMETER ESTIMATION FOR DYNAMIC SOARING WITH UNMANNED AERIAL VEHICLES | ICAS2018_0464 |
| Liu, Z. | OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC | ICAS2018_0750 |
| Lombardi, R. | MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECT | ICAS2018_0654 |
| London, P. | A CASE OF SUCESS: MDO APPLIED ON THE DEVELOPMENT OF EMBRAER 175 ENHANCED WINGTIP | ICAS2018_0034 |
| López Sánchez, C. | HURRICANE-CS: CONTROL SURFACES AND HIGH LIFT DEVICES MODELING AND SIZING PROGRAM | ICAS2018_0627 |
| Lozowski, E. | NUMERICAL SIMULATION OF ICE ACCRETION INFLUENCED BY AN ANTI-ICING HEATING SYSTEM | ICAS2018_0620 |
| Lu, G. | THE TECHNIQUE AND MODELLING FOR EQUIPMENT MAINTAINABILITY QUANTIFICATION IN 3D DIGITAL AIRCRAFT DESIGN CONDITION | ICAS2018_0055 |
| Lucchi, F. | DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACH | ICAS2018_0774 |
| Lucchi, F. | PRELIMINARY DESIGN OF A LONG RANGE WINDOWLESS AIRCRAFT CONCEPT | ICAS2018_0777 |
| Ludwig, T. | PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALS | ICAS2018_0050 |
| Lundbladh, A. | PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS | ICAS2018_0649 |
| Lundström, D. | METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT | ICAS2018_0663 |
| Lückhof, J. | SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY | ICAS2018_0727 |
| Lührs, B. | IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WIND | ICAS2018_0619 |
| Lührs, B. | IMPLEMENTATION OF ECO-EFFICIENT PROCEDURES TO MITIGATE THE CLIMATE IMPACT OF NON-CO2 EFFECTS | ICAS2018_0644 |
| Lührs, B. | COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNS | ICAS2018_0708 |
| Lührs, B. | QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNING | ICAS2018_0755 |
| Lysenkov, A.V. | PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT | ICAS2018_0788 |
| Lööf, J. | MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENT | ICAS2018_0101 |
| Ma, H. | AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGE | ICAS2018_0210 |
| Ma, H. | ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLE | ICAS2018_0222 |
| Ma, C. | NUMERICAL STUDY OF VARIABLE CAMBER WING EFFECT ON AERODYNAMIC PERFORMANCE FOR LONG RANGE CIVIL AIRCRAFT | ICAS2018_0231 |
| Ma, J. | THE EFFECT OF STRUCTURAL PARAMETERS OF AIRCRAFT PANEL ON VIBRATION FATIGUE LIFE | ICAS2018_0281 |
| Ma, H. | CFD-BASED STUDY OF DAMAGE LOCATION INFLUENCE ON AERODYNAMICS OF WINGS WITH SINGLE AND DOUBLE THROUGH HOLES | ICAS2018_0294 |
| Ma, B.H. | SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLE | ICAS2018_0306 |
| Ma, H. | STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WING | ICAS2018_0526 |
| Machini, F. | MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTOR | ICAS2018_0533 |
| MacKunis, W. | ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV | ICAS2018_0254 |
| MacNeill, R. | PROPELLER OPTIMISATION FOR AN ELECTRICAL-POWERED TACTICAL UAS | ICAS2018_0404 |
| Madrid, J. | MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENT | ICAS2018_0101 |
| Magerramova, L.A. | APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADES | ICAS2018_0173 |
| Magerramova, L. | DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINES | ICAS2018_0820 |
| Maia Neto, M. | A BOND GRAPH-ORIENTED METHOD FOR ASSESSMENT OF FAILURES IN AN AIRCRAFT HYDRAULIC BRAKE SYSTEM | ICAS2018_0551 |
| Maierl, R. | AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK | ICAS2018_0675 |
| Manfriani, L. | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFTS | ICAS2018_0162 |
| Mani, M. | CFD VERIFICATION AND VALIDATION FOR INDUSTRIAL APPLICATIONS | ICAS2018_0857 |
| Manzanares-Filho, N. | COMPARISON AND APPLICATION OF DIFFERENTS TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMIC WING DESIGN | ICAS2018_0527 |
| Marczak, R.J. | OPTIMAL SHAPE OF REPAIR PATCHES IN COMPOSITES | ICAS2018_0471 |
| Mare, J.-C. | POSITION SYNCHRONIZATION OF AEROSPACE ELECTROMECHANICAL ACTUATORS FOR DISTRIBUTED ELECTRICAL ACTUATION SYSTEM | ICAS2018_0653 |
| Mareskin, I.V. | INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURES | ICAS2018_0299 |
| Mareskin, I. | DEVELOPMENT OF STRUCTURE ELEMENTS BASED ON ARCHITECTURED MATERIALS FOR PERSPECTIVE CIVIL AIRCRAFTS | ICAS2018_0304 |
| Marinkovski, D. | DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCES | ICAS2018_0364 |
| Marks, T. | IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WIND | ICAS2018_0619 |
| Marks, T. | QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNING | ICAS2018_0755 |
| Martinez R. Jr., B. | DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONES | ICAS2018_0591 |
| Martini, E. | ACOUSTIC MODES AND GLOBAL INSTABILITIES IN WAKES AND JETS | ICAS2018_0450 |
| Martins, J.R.R.A. | FLEXFLOIL SHAPE ADAPTIVE CONTROL SURFACES-FLIGHT TEST AND NUMERICAL RESULTS | ICAS2018_0384 |
| Martins, J.S. | STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS | ICAS2018_0482 |
| Martins, R.S. | STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARS | ICAS2018_0573 |
| Martins, R. | STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODS | ICAS2018_0579 |
| Martins, R.S. | FASTENING ANALYSIS USING LOW FIDELITY FINITE ELEMENT MODELS | ICAS2018_0659 |
| Marzocca, P. | BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTING | ICAS2018_0660 |
| Mascia, E.-K. | AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER PICKUP TRUCKS | ICAS2018_0201 |
| Mastellone, A. | NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMP | ICAS2018_0622 |
| Matayoshi, N. | DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM | ICAS2018_0284 |
| Matayoshi, N. | OPERATIONAL CONCEPT AND VALIDATION OF A NEW AIRPORT LOW-LEVEL WIND INFORMATION SYSTEM | ICAS2018_0452 |
| Matheus, A.C. | A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTS | ICAS2018_0309 |
| Matheus, A. | EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS | ICAS2018_0402 |
| Mattei, A.-P. | SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVS | ICAS2018_0374 |
| Mavris, D.N. | UTILIZATION OF SCALING LAWS AND UNCERTAINTY QUANTIFICATION TO INFORM TECHNOLOGY DEVELOPMENT EXPERIMENTATION | ICAS2018_0183 |
| Mavris, D.N. | AN APPROACH TO ASSESS AIRFRAME WEIGHT REDUCTION PERFORMANCE OF STITCHED COMPOSITE TECHNOLOGIES | ICAS2018_0793 |
| Mavris, D. | ENABLING THE DIGITAL FACTORY THROUGH THE INTEGRATION OF DATA-DRIVEN AND SIMULATION MODELS | ICAS2018_0850 |
| Mavris, D. | ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACH | ICAS2018_0851 |
| Mavris, D.N. | FORMULATION AND IMPLEMENTATION OF A METHOD FOR TECHNOLOGY EVALUATION OF SYSTEM OF SYSTEMS | ICAS2018_0862 |
| Mašek, J. | THERMO-VACUUM TEST CHAMBER DEVELOPMENT FOR AIRBORNE AND SPACE EQUIPMENT TESTING IN SIMULATED EXTREME CONDITIONS | ICAS2018_0548 |
| Medeiros, R.R. | NONLINEAR AEROELASTIC REDUCED ORDER MODELS USING MODAL COORDINATES | ICAS2018_0262 |
| Mei, Y. | IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED | ICAS2018_0119 |
| Meilong, L. | CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORK | ICAS2018_0268 |
| Melin, T. | LIFECYCLE COSTS AND FEASIBILITY ANALYSIS OF THE DESIGNS OF UAV'S FOR HUMANITARIAN RELIEF MISSIONS | ICAS2018_0498 |
| Melin, T. | IMPLEMENTATION OF A VORTEX LATTICE METHOD IN A HETEROGENEOUS PROGRAMMING LANGUAGE ENVIRONMENT | ICAS2018_0846 |
| Meller, F. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Meller, F. | STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATION | ICAS2018_0752 |
| Melo, A.T.A. | FINITE ELEMENT MODEL DEVELOPMENT FOR SIMULTANEOUS CRACK PROPAGATION IN TWO COOPERATIVE LUGS | ICAS2018_0512 |
| Melo, A.T.A. | CRACK PROPAGATION STARTING AT HOLE’S EDGE GROWING TO PLATE’S MAJOR DIMENSION USING FEM | ICAS2018_0516 |
| Mendonça, W.R.P. | IMPORTANCE OF SECONDARY BENDING EVALUATION IN STRUCTURAL JOINT | ICAS2018_0583 |
| Meng, P. | NONLINEAR STATIC AEROELASTIC AND TRIM ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT | ICAS2018_0278 |
| Merkler, R. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Metelkin, E. | STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATION | ICAS2018_0234 |
| Meyer, M. | WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING | ICAS2018_0646 |
| Mieloszyk, J. | MORPHING WING WITH SURFACE DISCONTINUITY - COMPARATIVE TESTS | ICAS2018_0025 |
| Mileshin, V.I. | NUMERICAL AND EXPERIMENTAL STUDY OF THE EFFECT OF CIRCUMFERENTIAL GROOVES ON HPC LAST STAGE PERFORMANCE | ICAS2018_0624 |
| Mileshin, V.I. | CERTAIN ASPECTS OF FAN MODEL STAGE DESIGNING FOR ADVANCED TURBOFANS | ICAS2018_0626 |
| Mirgorodsky, Y. | DEVELOPMENT OF STRUCTURE ELEMENTS BASED ON ARCHITECTURED MATERIALS FOR PERSPECTIVE CIVIL AIRCRAFTS | ICAS2018_0304 |
| Miró Miró, F. | IONIZATION AND DISSOCIATION EFFECTS ON HYPERSONIC BOUNDARY-LAYER STABILITY | ICAS2018_0837 |
| Mirzoyan, A. | MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECT | ICAS2018_0654 |
| Mirzoyan, A. | STUDIES ON PROPULSION AND ON-BOARD SYSTEMS MATCHING IN AGILE PROJECT DISTRIBUTED COLLABORATIVE MDO ENVIRONMENT APPLYING FOR ADVANCED REGIONAL AND MEDIUM HAUL JET | ICAS2018_0655 |
| Mirzoyan, A. | MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT | ICAS2018_0783 |
| Mirzoyan, A.A. | PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT | ICAS2018_0788 |
| Modler, N. | NOVEL JET ENGINE ACOUSTIC LINER WITH IMPROVED BROADBAND NOISE ABSORPTION | ICAS2018_0333 |
| Moerland, E. | COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN | ICAS2018_0167 |
| Mohammadi-Amin, M. | AN EFFICIENT FRAMEWORK FOR AERODYNAMIC CONFIGURATION EVOLUTION OF REENTRY VEHICELES | ICAS2018_0745 |
| Moioli, M. | TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTS | ICAS2018_0126 |
| Molent, L. | USING THE LEAD CRACK CONCEPT TO REDUCE DURABILITY TEST DURATION | ICAS2018_0013 |
| Molina-Cristóbal, A. | AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACE | ICAS2018_0132 |
| Molina-Cristóbal, A. | COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN | ICAS2018_0134 |
| Monk, J.S. | THE AERONAUTICAL SOCIETY OF SOUTH AFRICA AEROSPACE CHALLENGE | ICAS2018_0859 |
| Monteiro, V. | MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENT | ICAS2018_0365 |
| Monteiro, T.P. | NUMERICAL DEVELOPMENT OF UNSTEADY VORTEX-LATTICE METHOD EXPANSION FOR LEADING-EDGE SHEDDING PREDICTION WITH EXPERIMENTAL VALIDATION | ICAS2018_0550 |
| Montel, M. | VALIDATION OF A HYBRID OBSERVER METHOD FOR FLIGHT LOADS ESTIMATION | ICAS2018_0605 |
| Moormann, D. | SCALABLE DESIGN APPROACH TO ANALYZE FLIGHT MECHANICAL PERFORMANCE OF TILT-WING UAVS | ICAS2018_0161 |
| Morais, K.C. | EFFECTS OF NUMERICAL MODELING CHOICES FOR HEATED JETS IN CROSS FLOW | ICAS2018_0369 |
| Morais, K.C. | STATIC LOADS EVALUATION IN A FLEXIBLE AIRCRAFT USING HIGH FIDELITY FLUID-STRUCTURE ITERATION TOOL (E2-FSI) | ICAS2018_0702 |
| Morales, M.A.V. | CONTROL OF A VERY FLEXIBLE WING WITH SIMULTANEOUS OPTIMIZATION OF THE GAIN MATRIX AND THE SPATIAL DISTRIBUTION OF THE SENSORS | ICAS2018_0500 |
| Morales, M.A.V. | ON REAL–TIME SIMULATION OF FLEXIBLE AIRCRAFT WITH PHYSICS–DERIVED MODELS | ICAS2018_0501 |
| Morales, M.A.V. | DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATION | ICAS2018_0569 |
| Moreira, F.J.O. | STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS | ICAS2018_0482 |
| Moreno, C. | ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAV | ICAS2018_0254 |
| Morokov, E. | STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPY | ICAS2018_0308 |
| Morra, P. | ON THE WAVE-CANCELLING NATURE OF BOUNDARY LAYER TRANSITION CONTROL | ICAS2018_0349 |
| Morra, P. | CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE | ICAS2018_0473 |
| Moruzzi, M.C. | PRELIMINARY DESIGN OF A LONG RANGE WINDOWLESS AIRCRAFT CONCEPT | ICAS2018_0777 |
| Mosharov, V.E. | PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENT | ICAS2018_0068 |
| Mottershead, J.E. | DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIES | ICAS2018_0509 |
| Moura, H.C. | PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMS | ICAS2018_0194 |
| Mourão, S.L. | THE PRIVATE MANAGEMENT OF BRAZILIAN AIRPORTS - A SHORT ANALYSIS | ICAS2018_0810 |
| Mullen, D. | IONIZATION AND DISSOCIATION EFFECTS ON HYPERSONIC BOUNDARY-LAYER STABILITY | ICAS2018_0837 |
| Munjulury, R.C. | ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OFSUPERSONIC BUSINESS JETS | ICAS2018_0030 |
| Munoz, C. | AN EVALUATION OF VARIOUS GEOFENCE CONFLICT RESOLUTION ALGORITHMS AND THEIR IMPACT ON MISSION PERFORMANCE | ICAS2018_0393 |
| Muravsky, D.V. | THE INFLUENCE OF THE SHAPE OF THE COOLING CHANNEL AND PRESSURE GRADIENT ON THE EFFICIENCY OF FILM COOLING OF GTE BLADES | ICAS2018_0629 |
| Murta, Y.B. | A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION | ICAS2018_0179 |
| Murton, A. | AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACE | ICAS2018_0132 |
| Musiak, J.D. | A METHOD FOR ESTIMATING THE PROBABILITY OF RARE ACCIDENTS IN COMPLEX SYSTEMS | ICAS2018_0849 |
| Na, Y. | GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEM | ICAS2018_0057 |
| Na, Y. | MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSIS | ICAS2018_0226 |
| Nagai, H. | MONTE-CARLO EVALUATION OF CONTROL LAW FOR HIGH ALTITUDE FLIGHT TEST OF MARS AIRPLANE | ICAS2018_0431 |
| Nagel, B. | COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN | ICAS2018_0167 |
| Nagel, B. | STREAMLINING CROSS-ORGANIZATIONAL AIRCRAFT DEVELOPMENT PROCESSES: AN OVERVIEW OF THE AGILE PROJECT | ICAS2018_0621 |
| Nakama, K. | VERTICAL LANDING OF A FIXED-WING UAV USING THE FLAT SPIN | ICAS2018_0415 |
| Nakamura, Y. | A SIMULATION MODELING STUDY FOR FREE ROUTING AIRSPACE IN JAPAN | ICAS2018_0158 |
| Naoto, M. | NEURAL NETWORK DRIVEN ADJOINT SOLVER BETWEEN FLIGHT-PATH OPTIMIZATION AND PANEL METHOD FOR AIRCRAFT DESIGN | ICAS2018_0746 |
| Narkawicz, A. | AN EVALUATION OF VARIOUS GEOFENCE CONFLICT RESOLUTION ALGORITHMS AND THEIR IMPACT ON MISSION PERFORMANCE | ICAS2018_0393 |
| Naruoka, M. | BAYESIAN APPROACH TO FLIGHT CHARACTERISTICS MODELING WITH REAL FLIGHT DATA | ICAS2018_0683 |
| Natori, H.O.H. | INFLUENCE OF AIRFRAME STIFFNESS ON THE AERODYNAMIC COEFFICIENTS OF A HIGH ASPECT RATIO WING | ICAS2018_0776 |
| Negulescu, C. | EXPLORATION OF THE AIRBUS "NAUTILIUS" ENGINE INTEGRATION CONCEPT | ICAS2018_0135 |
| Nepomnyashchiy, A.D. | PERFORMANCES OF LPT AND LINEAR CASCADES AT LOW REYNOLDS NUMBERS | ICAS2018_0652 |
| Nepomuceno, L.M. | IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLE | ICAS2018_0764 |
| Nepomuceno, L.M. | SYSTEM IDENTIFICATION OF A SUBSCALE FIGHTER AIRCRAFT | ICAS2018_0765 |
| Neto, R.M.F. | MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTOR | ICAS2018_0533 |
| Neumayr, B. | SEMANTICS-BASED SUMMARIZATION OF ATM DATA TO MANAGE INFORMATION OVERLOAD IN PILOT BRIEFINGS | ICAS2018_0763 |
| Neves, G.F.S. | STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARS | ICAS2018_0573 |
| Nguyen, A.T. | LONGITUDINAL FLIGHT CONTROL OF BIOINSPIRED FLAPPING-WING MICRO AIR VEHICLE WITH EXTENDED UNSTEADY VORTEX-LATTICE METHOD. | ICAS2018_0260 |
| Nickl, M. | A COMPOSITE CYCLE ENGINE CONCEPT FOR YEAR 2050 | ICAS2018_0638 |
| Nicolosi, F. | PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT | ICAS2018_0164 |
| Nicolosi, F. | AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATION | ICAS2018_0191 |
| Nicolosi, F. | NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODEL | ICAS2018_0264 |
| Nicolosi, F. | MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGN | ICAS2018_0504 |
| Nicolosi, F. | MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECT | ICAS2018_0648 |
| Nie, B. | WIND TUNNEL VIRTUAL FLIGHT TEST FOR A TRANSPORT AIRCRAFT WITH SIMULATED ICE SHAPE | ICAS2018_0125 |
| Nie, B.W. | A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNEL | ICAS2018_0406 |
| Nie, B. | OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC | ICAS2018_0750 |
| Niedermeier, D. | IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS | ICAS2018_0249 |
| Niermann, C.A. | 3D AUDIO SUPPORT FOR HELICOPTER PILOTS DURING CONFINED AREA LANDINGS | ICAS2018_0366 |
| Niklaß, M. | IMPLEMENTATION OF ECO-EFFICIENT PROCEDURES TO MITIGATE THE CLIMATE IMPACT OF NON-CO2 EFFECTS | ICAS2018_0644 |
| Niklaß, M. | COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNS | ICAS2018_0708 |
| Nilton, M.M. | STRUCTURAL DAMPING EFFECTS ON THE ACOUSTIC SCATTERING BY ELASTIC PLATES | ICAS2018_0108 |
| Nishihara, T. | MULTIFUNCTIONAL COMPOSITE PROCESSED USING EMBROIDERY TECHNOLOGY | ICAS2018_0475 |
| Niu, W. | FAULT DIAGNOSIS METHOD STUDY FOR COMPLEX SYSTEM BASED ON KALMAN FILTERS | ICAS2018_0015 |
| Niu, W. | FAULT DIAGNOSIS METHOD STUDY FOR COMPLEX SYSTEM BASED ON KALMAN FILTERS | ICAS2018_0015 |
| Nogueira, P.A.S. | RESOLVENT-BASED CONTROL OF STREAKS IN BOUNDARY LAYERS | ICAS2018_0477 |
| Noh, S. | ANALYSIS OF CHEMICALLY REACTING HYPERSONIC FLOW USING A MESHLESS METHOD | ICAS2018_0525 |
| Nolli, B.L. | FINITE ELEMENT MODEL DEVELOPMENT FOR SIMULTANEOUS CRACK PROPAGATION IN TWO COOPERATIVE LUGS | ICAS2018_0512 |
| Nolli, B.L. | CRACK PROPAGATION STARTING AT HOLE’S EDGE GROWING TO PLATE’S MAJOR DIMENSION USING FEM | ICAS2018_0516 |
| Notkin, V. | NUMERICAL INVESTIGATION OF INFLUENCE OF INITIAL DAMAGES ON STRENGTH PARAMETERS OF CFRP | ICAS2018_0302 |
| Nowowiejski, M. | DESIGN AND OPTIMIZATION OF A VERSATILE UAV FOR OBSERVATION AND RESEARCH USING THERMAL COLUMNS FOR EXTENDED ENDURANCE | ICAS2018_0272 |
| Nuzzo, C. | A RAPID AERODYNAMIC PREDICTION METHOD FOR UNCONVENTIONAL TRANSONIC AIRCRAFT CONFIGURATIONS | ICAS2018_0138 |
| Oh, E. | INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORT | ICAS2018_0059 |
| Ohira, K. | PRELIMINARY STUDY OF THE AERODYNAMIC CHARACTERISTICS OF KRUEGER FLAP ON THE SST CONFIGURATION | ICAS2018_0098 |
| Oliveira, C.O. | LOW-COST CERAMIC JET TURBINE | ICAS2018_0400 |
| Oliveira, M.L. | DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS | ICAS2018_0609 |
| Oliveira, C.F.R. | DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS | ICAS2018_0609 |
| Oliveira, K.A. | THE PRIVATE MANAGEMENT OF BRAZILIAN AIRPORTS - A SHORT ANALYSIS | ICAS2018_0810 |
| Olmos, S. | INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS | ICAS2018_0043 |
| Olympio, R.B. | AN ACTIVE-PASSIVE NONLINEAR FINITE ELEMENT MODEL FOR ELECTROMECHANICAL COMPOSITE MORPHING BEAMS | ICAS2018_0207 |
| Omagari, H. | POTENTIAL BENEFITS ASSESSMENT ON HOME DELIVERY SERVICE USING MULTIPLE DRONES | ICAS2018_0792 |
| Orekhov, I.K. | CERTAIN ASPECTS OF FAN MODEL STAGE DESIGNING FOR ADVANCED TURBOFANS | ICAS2018_0626 |
| Otsubo, G.M. | EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTION | ICAS2018_0391 |
| Oyama, A. | MONTE-CARLO EVALUATION OF CONTROL LAW FOR HIGH ALTITUDE FLIGHT TEST OF MARS AIRPLANE | ICAS2018_0431 |
| Pacuszka, P. | DESIGN AND OPTIMIZATION OF A VERSATILE UAV FOR OBSERVATION AND RESEARCH USING THERMAL COLUMNS FOR EXTENDED ENDURANCE | ICAS2018_0272 |
| Pagani, A. | GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGS | ICAS2018_0245 |
| Page, M.A. | SINGLE-AISLE AIRLINER DISRUPTION WITH A SINGLE-DECK BLENDED-WING-BODY | ICAS2018_0390 |
| Paiva, V. | KINEMATICS AND DYNAMICS OF A TENSEGRITY STRUCTURE IN EXPANSION | ICAS2018_0329 |
| Palkin, V. | THE STUDY OF TURBORAMJETS IN CIAM | ICAS2018_0848 |
| Palma, E.S. | FASTENING ANALYSIS USING LOW FIDELITY FINITE ELEMENT MODELS | ICAS2018_0659 |
| Palmer, J.L. | FLIGHT TEST OF A FUEL-CELL/BATTERY/SUPERCAPACITOR TRIPLE HYBRID UAV PROPULSION SYSTEM | ICAS2018_0864 |
| Pan, L. | PRELIMINARY DESIGN FOR A LOW REYNOLDS NUMBER BWB UAV DEMONSTRATOR | ICAS2018_0874 |
| Pang, M.B. | IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED | ICAS2018_0119 |
| Pang, E. | A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFT | ICAS2018_0684 |
| Pankov, A.V. | ON EQUIVALENCE OF POLYMER COMPOSITE MATERIALS STRUCTURES LOADING PROGRAMS UNDER FULL-SCALED SERVICE CYCLE TESTING | ICAS2018_0185 |
| Pankov, S.V. | CERTAIN ASPECTS OF FAN MODEL STAGE DESIGNING FOR ADVANCED TURBOFANS | ICAS2018_0626 |
| Pant, R.S. | DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATS | ICAS2018_0807 |
| Panzeri, M. | ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHM | ICAS2018_0328 |
| Papa, R. | EFFECTS OF NUMERICAL MODELING CHOICES FOR HEATED JETS IN CROSS FLOW | ICAS2018_0369 |
| Papageorgiou, A. | MULTIDISCIPLINARY OPTIMIZATION OF UNMANNED AIRCRAFT IN A SYSTEM OF SYSTEMS CONTEXT | ICAS2018_0047 |
| Parra, R.B. | LEONARDO DA VINCI INTERDISCIPLINARITY | ICAS2018_0301 |
| Parra, R.B. | ERRORS FROM ENGINEERING IN FLIGHT SAFETY | ICAS2018_0307 |
| Parra, R.B. | PREDICTIVE & DETECTIVE MAINTENANCE: EFFECTIVE TOOLS IN THE MANAGEMENT OF AERONAUTICAL PRODUCTS | ICAS2018_0336 |
| Paryshev, S.E. | AEROELASTIC PROPERTIES OF ACTIVE WINGLETS | ICAS2018_0276 |
| Pátek, Z. | EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPS | ICAS2018_0258 |
| Patrao, A.C. | PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS | ICAS2018_0649 |
| Patuelli, C. | REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE | ICAS2018_0432 |
| Paulino, J.A. | ON REAL–TIME SIMULATION OF FLEXIBLE AIRCRAFT WITH PHYSICS–DERIVED MODELS | ICAS2018_0501 |
| Pavlenko, O. | CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANE | ICAS2018_0104 |
| Pazini Brandão, M. | THE SANTOS-DUMONT LEGACY TO AERONAUTICS | ICAS2018_0089 |
| Pei, Y. | AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGE | ICAS2018_0210 |
| Pei, Y. | CFD-BASED STUDY OF DAMAGE LOCATION INFLUENCE ON AERODYNAMICS OF WINGS WITH SINGLE AND DOUBLE THROUGH HOLES | ICAS2018_0294 |
| Pei, Y. | BALLISTIC RESISTANT ANALYSIS FOR AIRCRAFT WING STRUCTURE | ICAS2018_0418 |
| Pelegrineli, L.A.V. | INFLUENCE OF AIRFRAME STIFFNESS ON THE AERODYNAMIC COEFFICIENTS OF A HIGH ASPECT RATIO WING | ICAS2018_0776 |
| Penna, S.D. | POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION | ICAS2018_0818 |
| Perchits, N. | NUMERICAL INVESTIGATION OF INFLUENCE OF INITIAL DAMAGES ON STRENGTH PARAMETERS OF CFRP | ICAS2018_0302 |
| Pereira, K.L.O. | SHM WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCE | ICAS2018_0357 |
| Pereira, L. | AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATION | ICAS2018_0664 |
| Pereira, L.T.L. | EVALUATION OF WIND TUNNEL WALL BOUNDARY-LAYER CONTROL FOR 2-D HIGH-LIFT AERODYNAMIC AND AEROACOUSTIC TESTING | ICAS2018_0780 |
| Peter, F. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Peter, F. | A FRAMEWORK FOR UNCONVENTIONAL LANDING GEAR CONFIGURATION MODELLING | ICAS2018_0688 |
| Peter, F. | STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATION | ICAS2018_0752 |
| Petit, O. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Petit, O. | PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS | ICAS2018_0649 |
| Petronyuk, Y. | STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPY | ICAS2018_0308 |
| Petrov, A. | CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANE | ICAS2018_0104 |
| Petrov, A.V. | ADAPTIVE WING HIGH-LIFT SYSTEM | ICAS2018_0371 |
| Petrovic, L. | DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCES | ICAS2018_0364 |
| Petrovichev, A.M. | NUMERICAL AND EXPERIMENTAL STUDY OF THE EFFECT OF CIRCUMFERENTIAL GROOVES ON HPC LAST STAGE PERFORMANCE | ICAS2018_0624 |
| Petukhov, A.A. | IDENTIFICATION METHOD OF THE SIMULATION MODEL "VIRTUAL ENGINE" BUILT INTO THE DIGITAL ENGINE CONTROL SYSTEM | ICAS2018_0643 |
| Pezzella, G. | LAUNCHER AERODYNAMIC ANALYSIS WITH PLUME EFFECTS | ICAS2018_0130 |
| Pfeiffer, T. | COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN | ICAS2018_0167 |
| Pfnür, S. | OUTBOARD SPLIT FLAP AERODYNAMICS OF A FLYING WING CONFIGURATION | ICAS2018_0069 |
| Pham, H. | A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFT | ICAS2018_0684 |
| Philipsen, I. | RELEASE OF DYNAMICALLY SCALED OBJECTS FROM A HELICOPTER WIND TUNNEL MODEL | ICAS2018_0064 |
| Philpott, D. | FUEL-BURN PENALTIES CAUSED BY IRREGULARITIES IN AIRCRAFT SURFACES (ASTEROID PROJECT) | ICAS2018_0184 |
| Philpott, D. | PRACTICAL APPLICATIONS OF VISCOUS FULL-POTENTIAL CFD CODES | ICAS2018_0338 |
| Piastra, S. | THE USE OF SYNTHETIC VISION TOOLS IN THE CONTROL TOWER ENVIRONMENT: THE RETINA CONCEPT | ICAS2018_0717 |
| Piastra, S. | DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACH | ICAS2018_0774 |
| Piaton, J. | A MORE INTEGRATED DESIGN APPROACH FOR EMBEDDED MECHATRONIC SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMS | ICAS2018_0170 |
| Pigusov, E.A. | CONTAINERIZED AIR FREIGHT SYSTEM POWERED BY CRYOGENIC FUEL | ICAS2018_0103 |
| Pigusov, E. | CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANE | ICAS2018_0104 |
| Pinna, F. | IONIZATION AND DISSOCIATION EFFECTS ON HYPERSONIC BOUNDARY-LAYER STABILITY | ICAS2018_0837 |
| Pinon, O.L. | ENABLING THE DIGITAL FACTORY THROUGH THE INTEGRATION OF DATA-DRIVEN AND SIMULATION MODELS | ICAS2018_0850 |
| Pinto, L.P.G. | A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL | ICAS2018_0052 |
| Pinto, P. | REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS | ICAS2018_0437 |
| Pinto, L.P.G. | DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE OF QUANTIZED CONTROL AND LMI APPROACH | ICAS2018_0521 |
| Pinto, T.H.L. | PLY THICKNESS INFLUENCE IN COMPRESSION AFTER IMPACT DAMAGE ON CARBON/EPOXY TEST SPECIMENS | ICAS2018_0707 |
| Piprek, P. | BI-LEVEL TRAJECTORY OPTIMIZATION BY STOCHASTIC COLLOCATION FOR UNCERTAINTY INTERVAL CALCULATION | ICAS2018_0221 |
| Piprek, P. | ROBUST TRAJECTORY OPTIMIZATION OF VTOL TRANSITION MANEUVER USING BI-LEVEL OPTIMAL CONTROL | ICAS2018_0224 |
| Piprek, P. | NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCING | ICAS2018_0782 |
| Plohr, M. | SYSTEM ANALYSIS OF TURBO ELECTRIC AND HYBRID ELECTRIC PROPULSION SYSTEMS ON A REGIONAL AIRCRAFT | ICAS2018_0831 |
| Podosinnikov, A.O. | RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0256 |
| Pogorzelski, G. | A STRATEGY FOR UAV PERFORMANCE ENHANCEMENT THROUGH ATMOSPHERIC ENERGY EXTRACTION USING MPC TECHNIQUES | ICAS2018_0840 |
| Poikelispää, M. | ARAMID-FIBER REINFORCED ELASTOMERS AS FUTURE AIRCRAFT ACTUATORS - A PROOF-OF-CONCEPT INVESTIGATION | ICAS2018_0377 |
| Poirel, D. | GLOBAL SENSITIVITY ANALYSIS OF TRANSONIC FLUTTER USING A COUPLED CFD-CSD SOLVER | ICAS2018_0037 |
| Polivanov, P.A. | EFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AIROFOIL | ICAS2018_0152 |
| Polla, A. | REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE | ICAS2018_0432 |
| Potapchik, A.V. | ADAPTIVE WING HIGH-LIFT SYSTEM | ICAS2018_0371 |
| Pozzobon, O. | IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMS | ICAS2018_0249 |
| Prado, G.O.C. | SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE | ICAS2018_0354 |
| Prado, G.O.C | CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHM | ICAS2018_0355 |
| Prado, G.O.C. | SHM WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCE | ICAS2018_0357 |
| Prakasha, P.S. | MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERING | ICAS2018_0633 |
| Prakasha, P.S. | MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT | ICAS2018_0783 |
| Prakasha, P.S. | COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTS | ICAS2018_0785 |
| Prakasha, P.S. | PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT | ICAS2018_0788 |
| Premlal, N. | EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORS | ICAS2018_0694 |
| Prince, S.A. | A RAPID AERODYNAMIC PREDICTION METHOD FOR UNCONVENTIONAL TRANSONIC AIRCRAFT CONFIGURATIONS | ICAS2018_0138 |
| Prince, S. | THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENT | ICAS2018_0297 |
| Prokhorov, A.N. | INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0508 |
| Prokhorov, A.N. | GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORS | ICAS2018_0628 |
| Prokhorov, A.N. | INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELS | ICAS2018_0645 |
| Prokhorov, A.N. | COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL | ICAS2018_0672 |
| Pushchin, N.A. | THE STUDIES ON LOW-NOISE LAMINAR WING REGIONAL AIRCRAFT | ICAS2018_0747 |
| Pölzlbauer, P. | PERFORMANCE IMPROVEMENT OF A COMPOUND HELICOPTER ROTOR HEAD BY AERODYNAMIC SHAPE OPTIMIZATION | ICAS2018_0070 |
| Qi, S.-J. | HUMAN FACTOR IN UNMANNED AIRCRAFT SYSTEM FLIGHT TEST | ICAS2018_0072 |
| Qian, G. | NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON SUPERCRITICAL WING AERODYNAMIC LOADS | ICAS2018_0001 |
| Qian, Z. | ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLE | ICAS2018_0039 |
| Qian, G. | NUMERICAL STUDY OF VARIABLE CAMBER WING EFFECT ON AERODYNAMIC PERFORMANCE FOR LONG RANGE CIVIL AIRCRAFT | ICAS2018_0231 |
| Qian, W. | AEROELASTIC WIND TUNNEL EXPERIMENT OF A HIGH-ASPECT-RATIO WING MODEL AGAINST GEOMETRICAL NON-LINEARITY | ICAS2018_0720 |
| Qian, W. | EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTS | ICAS2018_0784 |
| Qin, J. | HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADES | ICAS2018_0248 |
| Qiu, Z. | AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROL | ICAS2018_0129 |
| Qiu, T. | SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLE | ICAS2018_0306 |
| Qiu, X. | CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCH | ICAS2018_0405 |
| Qu, Q.L. | HIGH LIFT MECHANISM OF A 2D FLAPPING WING IN HOVERING FLIGHT | ICAS2018_0151 |
| Queiroz, R. | STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODS | ICAS2018_0579 |
| Quirino, M.U. | ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OFSUPERSONIC BUSINESS JETS | ICAS2018_0030 |
| Raabe, C.T. | AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM | ICAS2018_0219 |
| Radchenko, V.N. | PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENT | ICAS2018_0068 |
| Radchenko, V.N. | EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOW | ICAS2018_0690 |
| Rade, D.A. | DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIES | ICAS2018_0509 |
| Rafael, C.F. | SHIP-HELICOPTER OPERATIONAL LIMITATION ENVELOPE DEFINITION WITH CFD RESULTS AND WIND TUNNEL DATA | ICAS2018_0345 |
| Rajpal, D. | DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK | ICAS2018_0674 |
| Rajpal, D. | INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING | ICAS2018_0786 |
| Ramamurthy, A. | ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACH | ICAS2018_0851 |
| Ramesh, K. | NUMERICAL DEVELOPMENT OF UNSTEADY VORTEX-LATTICE METHOD EXPANSION FOR LEADING-EDGE SHEDDING PREDICTION WITH EXPERIMENTAL VALIDATION | ICAS2018_0550 |
| Ramos, A.C.B. | SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTION | ICAS2018_0066 |
| Ranasinghe, K. | HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONS | ICAS2018_0419 |
| Razaboni, P.M. | UNIVERSAL DESIGN FOR AIRCRAFT SAFETY | ICAS2018_0378 |
| Razaboni, P.M. | CREW TRAINING USING ANIMATION | ICAS2018_0380 |
| Reed, H.L. | IONIZATION AND DISSOCIATION EFFECTS ON HYPERSONIC BOUNDARY-LAYER STABILITY | ICAS2018_0837 |
| Reiser, C. | HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENT | ICAS2018_0269 |
| Reitenbach, S. | COUPLING OF PREDESIGN AND PERFORMANCE TOOLS FOR TRANSIENT AIRCRAFT ENGINE ANALYSES | ICAS2018_0830 |
| Ren, J. | VISUAL FLIGHT PROCEDURE DESIGN IN CHINA | ICAS2018_0282 |
| Riaz, A. | AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACE | ICAS2018_0132 |
| Riaz, A. | COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN | ICAS2018_0134 |
| Ribeiro, M.L. | AN XFEM FRAMEWORK FOR ONSET AND CRACK PROPAGATION FOR COMPOSITES BASED ON ACTION PLANE THEORY | ICAS2018_0502 |
| Ribeiro, L.J. | STAMP METHOD APPLICATION ON INDUSTRIAL MANAGEMENT | ICAS2018_0553 |
| Ribeiro, L.C. | DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS | ICAS2018_0609 |
| Ribeiro, M.V. | POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION | ICAS2018_0818 |
| Rice, T. | ADDRESSING TECHNICAL AND REGULATORY REQUIREMENTS TO DEPLOY STRUCTURAL HEALTH MONITORING SYSTEMS ON COMMERCIAL AIRCRAFT | ICAS2018_0109 |
| Rice, T. | SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE | ICAS2018_0354 |
| Ridel, M. | HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2018_0492 |
| Ridgway, G.R. | BEYOND BEDFORD - DEVELOPMENT OF A TWO-DIMENSIONAL PILOT WORKLOAD RATING SCALE | ICAS2018_0699 |
| Riedel, T. | A NOVEL CONTROL APPROACH TO IMPROVE SPEED COMMANDS AND PILOT WORKLOAD FOR FLIGHT-DECK BASED INTERVAL MANAGEMENT | ICAS2018_0174 |
| Ritt, S. | STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION | ICAS2018_0852 |
| Rivero, I. | FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONS | ICAS2018_0286 |
| Rizzi, F. | REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS | ICAS2018_0437 |
| Roach, D. | ADDRESSING TECHNICAL AND REGULATORY REQUIREMENTS TO DEPLOY STRUCTURAL HEALTH MONITORING SYSTEMS ON COMMERCIAL AIRCRAFT | ICAS2018_0109 |
| Roach, D. | SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE | ICAS2018_0354 |
| Roberts, T. | DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT | ICAS2018_0875 |
| Rocamora, B.M. | PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIG | ICAS2018_0147 |
| Rocha, G.C. | A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTS | ICAS2018_0309 |
| Rocha, G. | EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS | ICAS2018_0402 |
| Rodamilans, G.B. | CHARACTERISTIC HELICOPTER FLIGHT MECHANICS AND MOTION CUEING INTEGRATION INTO THE SIVOR ROBOTIC FLIGHT SIMULATOR: AN OBJECTIVE APPROACH | ICAS2018_0506 |
| Rodriguez, D. | EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF LAMINAR SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCES | ICAS2018_0195 |
| Rodriguez, M.A. | EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROL | ICAS2018_0200 |
| Rodríguez, M. | EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS | ICAS2018_0402 |
| Rodríguez-Sanz, A. | DETECTING HIGH-ALTITUDE ICE CRYSTAL (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATURE | ICAS2018_0611 |
| Rogalski, T. | APPLICATION OF THE DISTURBANCE VALUE MEASURED DURING THE REAL FLIGHT TO THE FLIGHT CONTROL SYSTEM SYNTHESIS | ICAS2018_0613 |
| Rohács, D. | DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM | ICAS2018_0697 |
| Rohács, J. | DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEM | ICAS2018_0697 |
| Rohacs, J. | LOAD MONITORING FOR OPERATORS’ LOAD MANAGEMENT | ICAS2018_0698 |
| Rohacs, D. | LOAD MONITORING FOR OPERATORS’ LOAD MANAGEMENT | ICAS2018_0698 |
| Romanenko, N.E. | APPLICATION OF "VIRTUAL" CONTROLLERS FOR INTEGRATED PROPULSION AND AIRCRAFT CONTROL | ICAS2018_0640 |
| Romani de Oliveira, I. | A METHOD FOR ESTIMATING THE PROBABILITY OF RARE ACCIDENTS IN COMPLEX SYSTEMS | ICAS2018_0849 |
| Rothfeld, R. | EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORK | ICAS2018_0178 |
| Rothfeld, R. | A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR VEHICLE CONCEPTS FOR URBAN AIR MOBILITY | ICAS2018_0794 |
| Rottach, M. | FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORS | ICAS2018_0271 |
| Rudinsky, A.V. | COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL | ICAS2018_0672 |
| Rulli, R.P. | SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE | ICAS2018_0354 |
| Rulli, R.P. | CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHM | ICAS2018_0355 |
| Ruocco, M. | AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATION | ICAS2018_0191 |
| Ruocco, M. | MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGN | ICAS2018_0504 |
| Ryu, M.H. | RELEASE OF DYNAMICALLY SCALED OBJECTS FROM A HELICOPTER WIND TUNNEL MODEL | ICAS2018_0064 |
| Ryzhova, T. | STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPY | ICAS2018_0308 |
| Rößler, C. | DEVELOPMENT AND PERFORMANCE COMPARISON OF OPTIMIZED ELECTRIC FIXED-WING VTOL UAV CONFIGURATIONS | ICAS2018_0169 |
| Rößler, C. | ELECTRIC VTOL UAV CONFIGURATION STUDIES AND OPTIMIZATION WITHIN AIRCRAFT DESIGN PRACTICAL COURSE AT TECHNICAL UNIVERSITY OF MUNICH | ICAS2018_0240 |
| Saarela, O. | MULTI-SITE DELAMINATION ANALYSIS USING VIRTUAL CRACK CLOSURE TECHNIQUE FOR A COMPOSITE AIRCRAFT WING FLAP | ICAS2018_0343 |
| Sabatini, R. | HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONS | ICAS2018_0419 |
| Sabatini, R. | A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFT | ICAS2018_0684 |
| Sabatini, R. | EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORS | ICAS2018_0694 |
| Sagalakov, A.E. | NEW APPROACH FOR INVESTIGATION OF MAXIMUM-RANGE AIRCRAFT TRAJECTORIES | ICAS2018_0726 |
| Samardzic, M. | DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCES | ICAS2018_0364 |
| Samuelsson, S. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Sanches, L. | MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTOR | ICAS2018_0533 |
| Sanches, A.C. | DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATION | ICAS2018_0569 |
| Sánchez Ayra, E. | DETECTING HIGH-ALTITUDE ICE CRYSTAL (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATURE | ICAS2018_0611 |
| Sánchez Franco, D. | HURRICANE-CS: CONTROL SURFACES AND HIGH LIFT DEVICES MODELING AND SIZING PROGRAM | ICAS2018_0627 |
| Sandhu, R. | GLOBAL SENSITIVITY ANALYSIS OF TRANSONIC FLUTTER USING A COUPLED CFD-CSD SOLVER | ICAS2018_0037 |
| Sano, H.H. | MODEL-BASED CONTROL LOGICS DEVELOPMENT OF AIRCRAFT SYSTEMS | ICAS2018_0479 |
| Santiago, M.S. | SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTION | ICAS2018_0066 |
| Santos, L.C.de C. | PROBABILISTIC FORECASTING IN AIRCRAFT EMERGENCY EVACUATION SIMULATION | ICAS2018_0202 |
| Santos, L.C.C. | EFFECTS OF NUMERICAL MODELING CHOICES FOR HEATED JETS IN CROSS FLOW | ICAS2018_0369 |
| Santos, M.T. | FASTENING ANALYSIS USING LOW FIDELITY FINITE ELEMENT MODELS | ICAS2018_0659 |
| Santos, J.S. | DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATS | ICAS2018_0807 |
| Santos de Brito Alves, L. | ON THE EXISTENCE OF MULTIPLE SELF-EXCITATION FREQUENCIES IN THE INSTABILITY OF INTERACTING PLANAR MIXING LAYER AND WAKE | ICAS2018_0537 |
| Sapienza, V. | REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS | ICAS2018_0437 |
| Saqui-Sannes, P. | SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVS | ICAS2018_0374 |
| Sarradj, E. | NOVEL JET ENGINE ACOUSTIC LINER WITH IMPROVED BROADBAND NOISE ABSORPTION | ICAS2018_0333 |
| Sartorius, S. | A TECHNIQUE FOR CAPTURING STAKEHOLDER PREFERENCES AND KNOWLEDGE IN EARLY DESIGN STUDIES | ICAS2018_0208 |
| Sasaki, K. | FLIGHT DEMONSTRATION OF A LONG RANGE ONBOARD DOPPLER LIDAR | ICAS2018_0121 |
| Sasaki, K. | ON THE WAVE-CANCELLING NATURE OF BOUNDARY LAYER TRANSITION CONTROL | ICAS2018_0349 |
| Sasaki, K. | CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATE | ICAS2018_0473 |
| Sato, M. | MANEUVERABILITY ASSESSMENT FOR FAULTY AIRPLANE BY IFS WITH SIMULTANEOUS MODEL-MATCHING FOR GUST AND HANDLING RESPONSES | ICAS2018_0241 |
| Savelyev, A. | DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK | ICAS2018_0674 |
| Savelyev, A.A. | PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT | ICAS2018_0788 |
| Scarso, S. | REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE | ICAS2018_0432 |
| Scherbakov, V. | STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPY | ICAS2018_0308 |
| Schettini, F. | MULTI-VARIABLE AIRCRAFT DIRECTIONAL CONTROL WITH ANTI-SKID DIFFERENTIAL BRAKES | ICAS2018_0607 |
| Schettini, F. | SMART FAULT-TOLERANT AIR-DATA SENSOR FOR AIRCRAFT FLOW ANGLES MEASUREMENT | ICAS2018_0625 |
| Schlatter, P. | WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL | ICAS2018_0388 |
| Schlösser, P. | WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING | ICAS2018_0646 |
| Schmid, M. | STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACH | ICAS2018_0082 |
| Schminder, J. | A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT | ICAS2018_0203 |
| Schminder, J. | DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMS | ICAS2018_0305 |
| Schminder, J. | PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODEL | ICAS2018_0463 |
| Schneider, J. | EXPERIENCE WITH INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN EDUCATION: AREND UAV | ICAS2018_0217 |
| Schneider, M. | STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION | ICAS2018_0852 |
| Scholz, M. | LNAS - A PILOT ASSISTANCE SYSTEM FOR LOW-NOISE APPROACHES WITH MINIMAL FUEL CONSUMPTION | ICAS2018_0096 |
| Schrefl, M. | SEMANTICS-BASED SUMMARIZATION OF ATM DATA TO MANAGE INFORMATION OVERLOAD IN PILOT BRIEFINGS | ICAS2018_0763 |
| Schröder, K.-U. | SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY | ICAS2018_0727 |
| Schuetz, C.G. | SEMANTICS-BASED SUMMARIZATION OF ATM DATA TO MANAGE INFORMATION OVERLOAD IN PILOT BRIEFINGS | ICAS2018_0763 |
| Schultz, M. | AIRCRAFT BOARDING AS PART OF AN EFFICIENT 4D TRAJECTORY | ICAS2018_0487 |
| Schwartz, K.G. | UTILIZATION OF SCALING LAWS AND UNCERTAINTY QUANTIFICATION TO INFORM TECHNOLOGY DEVELOPMENT EXPERIMENTATION | ICAS2018_0183 |
| Schwinn, D.B. | STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACH | ICAS2018_0082 |
| Schütt, M. | SCALABLE DESIGN APPROACH TO ANALYZE FLIGHT MECHANICAL PERFORMANCE OF TILT-WING UAVS | ICAS2018_0161 |
| Scigliano, R. | DE-ICING PHENOMENA MODELLED BY FINITE ELEMENT MODELS | ICAS2018_0180 |
| Seitz, A. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Seitz, A. | A COMPOSITE CYCLE ENGINE CONCEPT FOR YEAR 2050 | ICAS2018_0638 |
| Seitz, A. | STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATION | ICAS2018_0752 |
| Seitz, A. | STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATION | ICAS2018_0852 |
| Seki, S. | PASSIVE VENTILATION FLOW CONTROL FOR AIRCRAFT GUST LOAD ALLEVIATION | ICAS2018_0736 |
| Semenev, P.A. | NUMERICAL SIMULATION OF OPERATING PROCESS ELEMENTS FOR COMBUSTION CHAMBERS OF PERSPECTIVE GTE | ICAS2018_0737 |
| Semenov, V.L. | GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORS | ICAS2018_0628 |
| Sename, O. | A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNEL | ICAS2018_0406 |
| Senik, V. | STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATION | ICAS2018_0234 |
| Seren, T. | DEVELOPMENT AND PERFORMANCE COMPARISON OF OPTIMIZED ELECTRIC FIXED-WING VTOL UAV CONFIGURATIONS | ICAS2018_0169 |
| Serokhvostov, S. | SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTION | ICAS2018_0066 |
| Serokhvostov, S. | OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE | ICAS2018_0361 |
| Seung, T. | SELF-INDUCED FAULT OF A HYDRAULIC SERVO VALVE | ICAS2018_0853 |
| Shamiyeh, M. | A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR VEHICLE CONCEPTS FOR URBAN AIR MOBILITY | ICAS2018_0794 |
| Shanygin, A.N. | INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURES | ICAS2018_0299 |
| Shanygin, A. | STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPY | ICAS2018_0308 |
| Sharma, S. | AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACE | ICAS2018_0132 |
| Shattock, H.R. | BEYOND BEDFORD - DEVELOPMENT OF A TWO-DIMENSIONAL PILOT WORKLOAD RATING SCALE | ICAS2018_0699 |
| Shcheglov, G.A. | VISCOUS FLUID SIMULATION WITH THE VORTEX ELEMENT METHOD | ICAS2018_0718 |
| Shcherbakova, E.V. | THE INFLUENCE OF THE SHAPE OF THE COOLING CHANNEL AND PRESSURE GRADIENT ON THE EFFICIENCY OF FILM COOLING OF GTE BLADES | ICAS2018_0629 |
| Shelyukhin, Y.F. | MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALL | ICAS2018_0016 |
| Shi, L. | AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROL | ICAS2018_0129 |
| Shiguemori, E.H. | SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTION | ICAS2018_0066 |
| Shikhman, Y.M. | RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM | ICAS2018_0036 |
| Shim, G.J. | COST-EFFECTIVE TELEMETRY, TRACKING AND COMMAND SYSTEM DEVELOPMENT FOR HIGH-ALTITUDE SCIENTIFIC BALLOON | ICAS2018_0214 |
| Shires, A. | FUEL-BURN PENALTIES CAUSED BY IRREGULARITIES IN AIRCRAFT SURFACES (ASTEROID PROJECT) | ICAS2018_0184 |
| Shirizly, A. | INVESTIGATION OF CRACK PROPAGATION PROPERTIES OF ADDITIVE MANUFACTURING PRODUCTS | ICAS2018_0012 |
| Shlyakotin, V.E. | RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM | ICAS2018_0036 |
| Si, J. | NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON SUPERCRITICAL WING AERODYNAMIC LOADS | ICAS2018_0001 |
| Si, J. | NUMERICAL ANALYSIS OF BLEND-WING-BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCE | ICAS2018_0326 |
| Sidorenko, A.A. | EFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AIROFOIL | ICAS2018_0152 |
| Siedlak, D.J.L. | ENABLING THE DIGITAL FACTORY THROUGH THE INTEGRATION OF DATA-DRIVEN AND SIMULATION MODELS | ICAS2018_0850 |
| Silberhorn, D. | COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN | ICAS2018_0167 |
| Silva, G.H.C. | GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGS | ICAS2018_0245 |
| Silva, P.A. | SHM WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCE | ICAS2018_0357 |
| Silva, O.F.R. | MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENT | ICAS2018_0365 |
| Silva, T.M.P. | EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTION | ICAS2018_0391 |
| Silva, G.G. | UAV INITIAL PARAMETER ESTIMATION | ICAS2018_0568 |
| Silva, C.R.I. | PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS | ICAS2018_0649 |
| Silva, R.G.A. | IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLE | ICAS2018_0764 |
| Silva, R.G. | INCREASED FLUTTER VELOCITY WITH USE OF A PASSIVE CONTROL SYSTEM | ICAS2018_0800 |
| Silva, R.G.A. | EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORS | ICAS2018_0809 |
| Silva Neto, O.T. | EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORS | ICAS2018_0809 |
| Silvestre, F.J. | ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIES | ICAS2018_0438 |
| Silvestre, F.J. | THE INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIES | ICAS2018_0460 |
| Silvestre, F.J. | STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS | ICAS2018_0482 |
| Silvestre, F.J. | CONTROL OF A VERY FLEXIBLE WING WITH SIMULTANEOUS OPTIMIZATION OF THE GAIN MATRIX AND THE SPATIAL DISTRIBUTION OF THE SENSORS | ICAS2018_0500 |
| Silvestre, F.J. | ON REAL–TIME SIMULATION OF FLEXIBLE AIRCRAFT WITH PHYSICS–DERIVED MODELS | ICAS2018_0501 |
| Silvestre, F.J. | APPLICABILITY OF GEOMETRICALLY-LINEAR STRUCTURAL-DYNAMIC MODELS FOR THE FLIGHT DYNAMICS OF ARBITRARILY-FLEXIBLE AIRCRAFT | ICAS2018_0523 |
| Silvestre, F.J. | ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFT | ICAS2018_0529 |
| Silvestre, F.J. | IMPLEMENTATION AND FLIGHT TESTING OF AN ENHANCED STABILITY SYSTEM FOR A VERY FLEXIBLE AIRCRAFT | ICAS2018_0534 |
| Silvestre, F. | NUMERICAL DEVELOPMENT OF UNSTEADY VORTEX-LATTICE METHOD EXPANSION FOR LEADING-EDGE SHEDDING PREDICTION WITH EXPERIMENTAL VALIDATION | ICAS2018_0550 |
| Silvestre, F.J. | DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATION | ICAS2018_0569 |
| Silvestre, F.J. | A STRATEGY FOR UAV PERFORMANCE ENHANCEMENT THROUGH ATMOSPHERIC ENERGY EXTRACTION USING MPC TECHNIQUES | ICAS2018_0840 |
| Simomura, F.M. | SHM WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCE | ICAS2018_0357 |
| Simon, D. | A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL | ICAS2018_0052 |
| Singh, D. | LATTICE BOLTZMANN HIGH-LIFT SIMULATIONS - A STEP BEYOND CLASSICAL CFD | ICAS2018_0318 |
| Smetak, E.J. | SINGLE-AISLE AIRLINER DISRUPTION WITH A SINGLE-DECK BLENDED-WING-BODY | ICAS2018_0390 |
| Smetanin, S.A. | ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORS | ICAS2018_0639 |
| Smetanin, S.A. | APPLICATION OF "VIRTUAL" CONTROLLERS FOR INTEGRATED PROPULSION AND AIRCRAFT CONTROL | ICAS2018_0640 |
| Smith, L. | EXPERIENCE WITH INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN EDUCATION: AREND UAV | ICAS2018_0217 |
| Smith, H. | FEASIBILITY STUDY OF MODIFYING A BASELINE KEROSENE AIRCRAFT TO A LH2 POWERED VERSION | ICAS2018_0580 |
| Sobron, A. | METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHT | ICAS2018_0663 |
| Sokolova, O.V. | RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM | ICAS2018_0036 |
| Solonin, V. | THE STUDY OF TURBORAMJETS IN CIAM | ICAS2018_0848 |
| Son, K.E. | MULTIPHASE TURBULENCE MODELS FOR SCRAMJETS AND ABLATING WALLS | ICAS2018_0227 |
| Son, E.E. | CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES | ICAS2018_0242 |
| Son, K.E. | CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES | ICAS2018_0242 |
| Song, C. | STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS | ICAS2018_0128 |
| Song, B.F. | AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGE | ICAS2018_0210 |
| Song, B.F. | ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLE | ICAS2018_0222 |
| Song, C. | AERODYNAMIC DESIGN OF KEY COMPONENTS OF THE LARGE-DISCHARGE AXIAL FAN AT HIGH ALTITUDE | ICAS2018_0243 |
| Song, S. | ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION | ICAS2018_0389 |
| Song, D. | ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION | ICAS2018_0389 |
| Song, W.-P. | THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVER | ICAS2018_0470 |
| Song, W.-P. | SURROGATE-BASED OPTIMIZATION METHOD APPLIED TO MULTIDISCIPLINARY DESIGN OPTIMIZATION ARCHITECTURES | ICAS2018_0496 |
| Song, W.-P. | A COMPARISON STUDY ON TRANSITION CHARACTERISTICS OF NLF FORWARD-SWEPT-WING AND AFT-SWEPT-WING | ICAS2018_0497 |
| Song, W.-P. | COMBINING ADJOINT-BASED AND SURROGATE-BASED OPTIMIZATIONS FOR BENCHMARK AERODYNAMIC DESIGN PROBLEMS | ICAS2018_0715 |
| Song, Y. | VERIFIED FUSELAGE SECTION WATER IMPACT MODELING | ICAS2018_0732 |
| Song, Y. | PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFT | ICAS2018_0826 |
| Soudakov, V.G. | NUMERICAL OPTIMIZATION OF FLOW CONTROL BY TANGENTIAL JET BLOWING ON TRANSONIC AIRFOIL | ICAS2018_0704 |
| Sousa, R.S. | EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATION | ICAS2018_0382 |
| Sousa, M.S. | A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOT | ICAS2018_0559 |
| Souza, J.M. | MULTI-DISCIPLINARY DESIGN OPTIMIZATION OF A BLENDED WINGLET | ICAS2018_0598 |
| Souza, R.A. | DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS | ICAS2018_0609 |
| Souza, S.A. | POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION | ICAS2018_0818 |
| Spero, E. | ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACH | ICAS2018_0851 |
| Spieck, M. | MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERING | ICAS2018_0633 |
| Spiteri, A. | AN ATC ORIENTED INTERFACE FOR MULTI-AIRCRAFT OPTIMISATION FOR CLIMBS AND DESCENTS | ICAS2018_0433 |
| Staack, I. | A HOLISTIC ENGINEERING APPROACH FOR AERONAUTICAL PRODUCT DEVELOPMENT | ICAS2018_0724 |
| Stahl, P. | DEVELOPMENT AND PERFORMANCE COMPARISON OF OPTIMIZED ELECTRIC FIXED-WING VTOL UAV CONFIGURATIONS | ICAS2018_0169 |
| Stalewski, W. | CONTROL OF STRONG SEPARATION OF FLOW VIA SIMULTANEOUS-BLOWING-SUCTION TECHNIQUE | ICAS2018_0196 |
| Standfuss, T. | ADAPTING CAPACITY OF AIR NAVIGATION SERVICE PROVISION IN EUROPE - BETWEEN SCYLLA AND CHARYBDIS | ICAS2018_0483 |
| Stasenko, A.L. | EXPERIMENTAL INVESTIGATION, MATHEMATICAL AND NUMERICAL SIMULATION OF AIRCRAFT ICING PHENOMENA | ICAS2018_0741 |
| Stathopoulos, N. | STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDS | ICAS2018_0367 |
| Steelant, J. | LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMS | ICAS2018_0425 |
| Steelant , J. | A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE | ICAS2018_0429 |
| Stefes, B. | WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING | ICAS2018_0646 |
| Stepanov, J.G. | ADAPTIVE WING HIGH-LIFT SYSTEM | ICAS2018_0371 |
| Stingo, L. | MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECT | ICAS2018_0648 |
| Straker, L. | BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATION | ICAS2018_0661 |
| Strathoff, P. | SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY | ICAS2018_0727 |
| Streltsov, E.V. | APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTS | ICAS2018_0321 |
| Stumpf, E. | SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITY | ICAS2018_0727 |
| Sudol, A. | FORMULATION AND IMPLEMENTATION OF A METHOD FOR TECHNOLOGY EVALUATION OF SYSTEM OF SYSTEMS | ICAS2018_0862 |
| Sui, J.-F. | THRUST REVERSER INADVERTENT DEPLOYMENT IMPACT STUDY ON AIRPLANE CONTROLLABILITY | ICAS2018_0058 |
| Sun, Y. | CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF "PARASITE" NOISE | ICAS2018_0116 |
| Sun, Y. | IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED | ICAS2018_0119 |
| Sun, H. | OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDC | ICAS2018_0750 |
| Sun, X.F. | EVALUATION OF MECHANICAL PROPERTIES OF TI-6AL-4V FABRICATED BY SELECTIVE LASER MELTING (SLM) | ICAS2018_0866 |
| Sung, Y.H. | UNSTEADY AERODYNAMIC CHARACTERISTICS OF THE OSCILLATING AIRFOIL USING MSBS | ICAS2018_0253 |
| Suntsov, S.V. | PERFORMANCES OF LPT AND LINEAR CASCADES AT LOW REYNOLDS NUMBERS | ICAS2018_0652 |
| Surkov, N.A. | MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALL | ICAS2018_0016 |
| Suzuki, S. | AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM | ICAS2018_0219 |
| Suzuki, S. | INDIVIDUALIZING FLIGHT SKILL TRAINING USING SIMULATOR DATA ANALYSIS AND BIOFEEDBACK | ICAS2018_0220 |
| Suzuki, S. | FAULT-TOLERANT FLIGHT CONTROL SYSTEM WITH SIMPLE ADAPTIVE CONTROL CONSIDERING PILOT INPUT | ICAS2018_0651 |
| Svinareva, M.S. | APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADES | ICAS2018_0173 |
| Svirskiy, Y.A. | DEVELOPMENT OF STRUCTURAL HEALTH MONITORING METHODS THROUGH THE ANALYSIS OF KINETICS OF LOCAL STRESS-STRAIN STATE | ICAS2018_0160 |
| Swadesir, L. | URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREA | ICAS2018_0635 |
| Swaid, M. | IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WIND | ICAS2018_0619 |
| Swaid, M. | QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNING | ICAS2018_0755 |
| Szczepanik, T. | NEW TECHNOLOGY OF LAYERED STRUCTURES IMPLEMENTED IN SELECTED GYROPLANE COMPONENTS | ICAS2018_0356 |
| Szczepanik, R. | OPTIMIZATION OF THE FUEL INJECTOR TO AN INTERNAL COMBUSTION ENGINE BY MEANS OF LASER EQUIPMENT | ICAS2018_0825 |
| Szilder, K. | NUMERICAL SIMULATION OF ICE ACCRETION INFLUENCED BY AN ANTI-ICING HEATING SYSTEM | ICAS2018_0620 |
| Söderberg, R. | MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENT | ICAS2018_0101 |
| Sørensen, K.A. | TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTS | ICAS2018_0126 |
| Tadeu de Mello Lourencao, P. | EDUCATING ENGINEERS FOR THE DEVELOPMENT OF PRODUCT SERVICE SYSTEMS (PSS) | ICAS2018_0522 |
| Tahk, M.-J. | MULTISTAGE MISSILE TRAJECTORY AND STAGE OPTIMIZATION VIA DELTA-V APPROACH | ICAS2018_0385 |
| Takase, V.L. | MODEL-BASED CONTROL LOGICS DEVELOPMENT OF AIRCRAFT SYSTEMS | ICAS2018_0479 |
| Takase, R. | FAULT-TOLERANT FLIGHT CONTROL SYSTEM WITH SIMPLE ADAPTIVE CONTROL CONSIDERING PILOT INPUT | ICAS2018_0651 |
| Takatani, K. | PRECISE MEASUREMENT OF PROPAGATING FLAME IN 2-STROKE GASOLINE ENGINE BY MULTIPLE ION-PROBES | ICAS2018_0149 |
| Talyzin, V.A. | RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0256 |
| Talyzin, V.A. | INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0508 |
| Tamba, A.K.F. | SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE | ICAS2018_0354 |
| Tamba, A.K.F. | CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHM | ICAS2018_0355 |
| Tan, S. | PREDICTING LOW-VELOCITY IMPACT DAMAGE IN COMPOSITE USING COHESIVE ELEMENT | ICAS2018_0049 |
| Tan, Z. | NUMERICAL ANALYSIS OF BLEND-WING-BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCE | ICAS2018_0326 |
| Tani, Y. | PASSIVE VENTILATION FLOW CONTROL FOR AIRCRAFT GUST LOAD ALLEVIATION | ICAS2018_0736 |
| Tarifa, I.O. | MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTOR | ICAS2018_0533 |
| Tarnowski, A. | MORPHING WING WITH SURFACE DISCONTINUITY - COMPARATIVE TESTS | ICAS2018_0025 |
| Tay, G. | EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORK | ICAS2018_0178 |
| Teixeira, P.C. | PROPELLER INFLUENCE ON THE STABILITY OF HALE AIRCRAFT | ICAS2018_0177 |
| Teixeira, L.H. | A NUMERICAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTURE | ICAS2018_0206 |
| Temis, J. | DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINES | ICAS2018_0820 |
| Terrapon, V.E. | INVISCID AND VISCOUS FLOW MODELING FOR FAST TRANSONIC FLUTTER CALCULATIONS | ICAS2018_0436 |
| Terrapon, V.E. | HIGHER FIDELITY TRANSONIC AERODYNAMIC MODELING IN PRELIMINARY AIRCRAFT DESIGN | ICAS2018_0453 |
| Theron, J.-P. | PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAV | ICAS2018_0233 |
| Theuma, K. | GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESS | ICAS2018_0182 |
| Thielecke, F. | VALIDATION OF A HYBRID OBSERVER METHOD FOR FLIGHT LOADS ESTIMATION | ICAS2018_0605 |
| Thielecke, F. | LOCAL MODEL NETWORKS APPLIED TO FLIGHT LOADS ESTIMATION | ICAS2018_0650 |
| Tian, L. | GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEM | ICAS2018_0057 |
| Tian, J. | EFFECT OF DIELECTRIC PROPERTIES DUE TO THE CHANGE OF DIELECTRIC AS A RESULT OF ELEVATORY TEMPERATURE | ICAS2018_0293 |
| Timmermans, H. | DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK | ICAS2018_0674 |
| Timmermans, H. | INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING | ICAS2018_0786 |
| Tissot, G. | CONTROL OF A VERY FLEXIBLE WING WITH SIMULTANEOUS OPTIMIZATION OF THE GAIN MATRIX AND THE SPATIAL DISTRIBUTION OF THE SENSORS | ICAS2018_0500 |
| Tita, V. | AN XFEM FRAMEWORK FOR ONSET AND CRACK PROPAGATION FOR COMPOSITES BASED ON ACTION PLANE THEORY | ICAS2018_0502 |
| Titchener, N. | DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT | ICAS2018_0875 |
| Tobaldini Neto, L. | EFFECTS OF NUMERICAL MODELING CHOICES FOR HEATED JETS IN CROSS FLOW | ICAS2018_0369 |
| Toktaliev, P.D. | COMMUNICATION BETWEEN PS AND AIRCRAFT SYSTEMS IN COLLECTIVE MDO SYSTEM IN AGILE PROJECT | ICAS2018_0742 |
| Tokutake, H. | MONTE-CARLO EVALUATION OF CONTROL LAW FOR HIGH ALTITUDE FLIGHT TEST OF MARS AIRPLANE | ICAS2018_0431 |
| Toledo, C.F.M. | SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVS | ICAS2018_0374 |
| Tomasella, F. | INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORK | ICAS2018_0412 |
| Tomasella, F. | DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK | ICAS2018_0674 |
| Tomasello, D. | REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANE | ICAS2018_0432 |
| Tomczyk, A. | APPLICATION OF THE DISTURBANCE VALUE MEASURED DURING THE REAL FLIGHT TO THE FLIGHT CONTROL SYSTEM SYNTHESIS | ICAS2018_0613 |
| Tomita, J.T. | PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS | ICAS2018_0649 |
| Toratani, D. | STUDY ON THE ARRIVAL MANAGER MAXIMIZING THE BENEFIT OF FOUR-DIMENSIONAL TRAJECTORY BASED OPERATIONS | ICAS2018_0315 |
| Toratani, D. | SIMULATION STUDY FOR VFR AIRCRAFT AND SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) MIXED OPERATIONS IN LOW LEVEL AIRSPACE | ICAS2018_0636 |
| Torres, F.S. | DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS | ICAS2018_0609 |
| Torrigiani, F. | DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK | ICAS2018_0674 |
| Torrigiani, F. | INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WING | ICAS2018_0786 |
| Toussaint, C. | HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2018_0492 |
| Trabasso, L.G. | DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMS | ICAS2018_0305 |
| Trabasso, L.G. | A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTS | ICAS2018_0309 |
| Trabasso, L.G. | EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS | ICAS2018_0402 |
| Trapp, G. | PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS | ICAS2018_0649 |
| Trifari, V. | AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATION | ICAS2018_0191 |
| Trifari, V. | MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGN | ICAS2018_0504 |
| Trindade J., O. | SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVS | ICAS2018_0374 |
| Troeltsch, F. | DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT | ICAS2018_0728 |
| Tsipilev, N.S. | PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENT | ICAS2018_0068 |
| Tskhovrebov, M. | THE STUDY OF TURBORAMJETS IN CIAM | ICAS2018_0848 |
| Tsuchiya, T. | AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM | ICAS2018_0219 |
| Tsuchiya, T. | ALL JAPAN STUDENT'S INDOOR FLYING ROBOT CONTEST | ICAS2018_0858 |
| Tsvetkov, I.V. | PERFORMANCES OF LPT AND LINEAR CASCADES AT LOW REYNOLDS NUMBERS | ICAS2018_0652 |
| Tuktarov, S.A. | STRESS-BASED TOPOLOGY OPTIMIZATION WITH USING GLOBAL-LOCAL APPROACH | ICAS2018_0316 |
| Turetta, F.M.S. | A PRACTICAL ANALYSIS ON THE COMPLEXITY OF AIRCRAFT SYSTEMS ARCHITECTURE AND REQUIREMENTS DEVELOPMENT | ICAS2018_0514 |
| Tylko, J. | DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT | ICAS2018_0875 |
| Ueda, S. | OPERATIONAL CONCEPT AND VALIDATION OF A NEW AIRPORT LOW-LEVEL WIND INFORMATION SYSTEM | ICAS2018_0452 |
| Uemura, T. | INDIVIDUALIZING FLIGHT SKILL TRAINING USING SIMULATOR DATA ANALYSIS AND BIOFEEDBACK | ICAS2018_0220 |
| Uemura, T. | DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM | ICAS2018_0284 |
| Ulma, D. | INVESTIGATION OF ‘JUMP TAKEOFF’ POSSIBILITY FOR THE NEW CONCEPT OF MODERN AUTOGYRO | ICAS2018_0630 |
| van Bokhorst, E. | DEVELOPMENT OF SECONDARY CROSSFLOW INSTABILITY NEAR BREAKDOWN INTO TURBULENCE | ICAS2018_0735 |
| van den Ende, L.E. | AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMS | ICAS2018_0505 |
| van der Burg, J.W. | NUMERICAL INVESTIGATION AERODYNAMICS NACELLE-STRAKE EFFECT | ICAS2018_0205 |
| van Gent , I. | COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTS | ICAS2018_0785 |
| van Heerden, A.S.J. | COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN | ICAS2018_0134 |
| van Sluis, M. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Vannini, V. | SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVS | ICAS2018_0374 |
| Vedernikov, D. | DEVELOPMENT OF STRUCTURE ELEMENTS BASED ON ARCHITECTURED MATERIALS FOR PERSPECTIVE CIVIL AIRCRAFTS | ICAS2018_0304 |
| Veldhuis, L.L.M. | AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMS | ICAS2018_0505 |
| Velicki, A. | DESIGNING PRIMARY STRUCTURES WITH STITCHED COMPOSITES | ICAS2018_0060 |
| Vendrichoski, J.C. | MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATION | ICAS2018_0586 |
| Verbeke, C. | HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSION | ICAS2018_0492 |
| Vercella, V. | PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT | ICAS2018_0164 |
| Vercella, V. | LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMS | ICAS2018_0425 |
| Vercella, V. | A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE | ICAS2018_0429 |
| Verri, A.A. | STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWS | ICAS2018_0482 |
| Verri, A.A. | MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UP | ICAS2018_0493 |
| Verri, A.A. | STATIC LOADS EVALUATION IN A FLEXIBLE AIRCRAFT USING HIGH FIDELITY FLUID-STRUCTURE ITERATION TOOL (E2-FSI) | ICAS2018_0702 |
| Verstraete, D. | MULTI-DISCIPLINARY OPTIMISATION OF MEDIUM ALTITUDE LONG ENDURANCE UAVS | ICAS2018_0416 |
| Verstraete, D. | FLIGHT TEST OF A FUEL-CELL/BATTERY/SUPERCAPACITOR TRIPLE HYBRID UAV PROPULSION SYSTEM | ICAS2018_0864 |
| Vich, O. | FLUTTER ANALYSIS OF TWIN TURBOPROP AIRCRAFT WITH TIP-TANKS | ICAS2018_0004 |
| Vidjaja, G. | NUMERICAL INVESTIGATION AERODYNAMICS NACELLE-STRAKE EFFECT | ICAS2018_0205 |
| Vieira, L.C. | SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCE | ICAS2018_0354 |
| Vieira, L.C. | CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHM | ICAS2018_0355 |
| Vieira, S.P.L. | DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS | ICAS2018_0609 |
| Vielman, L. | AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR-SPACE EXPLORATION USING A HIGH ALTITUDE BALLOON | ICAS2018_0582 |
| Vieweg, M. | COUPLING OF PREDESIGN AND PERFORMANCE TOOLS FOR TRANSIENT AIRCRAFT ENGINE ANALYSES | ICAS2018_0830 |
| Villani, E. | EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROL | ICAS2018_0200 |
| Villani, E. | EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS | ICAS2018_0402 |
| Villani, E. | DATA-DRIVEN FAILURE IDENTIFICATION USING A MOTION-BASED SIMULATOR | ICAS2018_0581 |
| Vinuesa, R. | WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL | ICAS2018_0388 |
| Viola, N. | PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT | ICAS2018_0164 |
| Viola, N. | LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMS | ICAS2018_0425 |
| Viola, N. | A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE | ICAS2018_0429 |
| Viviani, A. | LAUNCHER AERODYNAMIC ANALYSIS WITH PLUME EFFECTS | ICAS2018_0130 |
| Vodovozov, G. | NUMERICAL INVESTIGATION OF INFLUENCE OF INITIAL DAMAGES ON STRENGTH PARAMETERS OF CFRP | ICAS2018_0302 |
| Voevodenko, N.V. | RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0256 |
| Voevodenko, N.V. | INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0508 |
| Vogiatzis, E. | INTEGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONS | ICAS2018_0873 |
| Volkov, M.E. | APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADES | ICAS2018_0173 |
| Volkova, A.O. | APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTS | ICAS2018_0321 |
| Vos, R. | SYSTEM-LEVEL ASSESSMENT OF TAIL-MOUNTED PROPELLERS FOR REGIONAL AIRCRAFT | ICAS2018_0065 |
| Voskuijl , M. | MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECT | ICAS2018_0783 |
| Vratny, P.C. | DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFT | ICAS2018_0728 |
| Vrchota, P. | EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPS | ICAS2018_0258 |
| Vukovic, D. | DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCES | ICAS2018_0364 |
| Wall, A. | SIMULATIONS OF UNSTEADY AIRWAKES BEHIND SHIPS IN MOTION | ICAS2018_0038 |
| Wallach, R. | A CASE OF SUCESS: MDO APPLIED ON THE DEVELOPMENT OF EMBRAER 175 ENHANCED WINGTIP | ICAS2018_0034 |
| Wallner, C. | MODIFIED WHITNEY-NUISMER CRITERIA FOR PREDICTION OF NOTCHED STRENGTH OF COMPOSITE LAMINATES | ICAS2018_0677 |
| Walther, J.N. | AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK | ICAS2018_0675 |
| Wan, T. | HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILES | ICAS2018_0270 |
| Wang, C. | INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS | ICAS2018_0043 |
| Wang, F. | HUMAN FACTOR IN UNMANNED AIRCRAFT SYSTEM FLIGHT TEST | ICAS2018_0072 |
| Wang, Q. | CONTINUOUS MODELING IN AIRCRAFT TOP-LEVEL DEMONSTRATION | ICAS2018_0085 |
| Wang, B. | STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS | ICAS2018_0128 |
| Wang, H.-B. | INVESTIGATION ON APPROACH TO CONTROL LIFT DISTRIBUTION OF WING BY DISTRIBUTED PROPELLERS | ICAS2018_0189 |
| Wang, C. | MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSIS | ICAS2018_0226 |
| Wang, C. | EVALUATION OF AIRCRAFT BRAKING PERFORMANCE BASED ON OPERATIONAL FLIGHT DATA | ICAS2018_0232 |
| Wang, L. | VISUAL FLIGHT PROCEDURE DESIGN IN CHINA | ICAS2018_0282 |
| Wang, Q. | EFFECT OF DIELECTRIC PROPERTIES DUE TO THE CHANGE OF DIELECTRIC AS A RESULT OF ELEVATORY TEMPERATURE | ICAS2018_0293 |
| Wang, X. | APPLICATION RESEARCH OF LARGE-SCALED COMPLICATED FRAME-BEAM INTEGRAL COMPONENT BASED ON ELECTRON BEAM ADDITIVE MANUFACTURING | ICAS2018_0319 |
| Wang, J. | STUDY ON LARGE-SCALE FLIGHT DELAY RECOVERY | ICAS2018_0457 |
| Wang, H. | COMBINING ADJOINT-BASED AND SURROGATE-BASED OPTIMIZATIONS FOR BENCHMARK AERODYNAMIC DESIGN PROBLEMS | ICAS2018_0715 |
| Wang, X. | AIRCRAFT STRUCTURE TECHNOLOGY OF ADDITIVE MANUFACTURING | ICAS2018_0723 |
| Wang, Z.J. | TOWARDS INDUSTRIAL LARGE EDDY SIMULATION AND AERO-ACOUSTIC NOISE COMPUTATION WITH THE HIGH-ORDER FR/CPR METHOD | ICAS2018_0856 |
| Wang, L. | EVALUATION OF MECHANICAL PROPERTIES OF TI-6AL-4V FABRICATED BY SELECTIVE LASER MELTING (SLM) | ICAS2018_0866 |
| Ward, S. | A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL | ICAS2018_0052 |
| Weiand, P. | STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACH | ICAS2018_0082 |
| Weiss, M. | COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMEN | ICAS2018_0167 |
| Weiß, S. | INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS | ICAS2018_0043 |
| Wen, P.-C. | MULTI-CHANNEL HUMAN-MACHINE INTERACTIVE SYSTEM FOR MULTIPLE UAVS' CONTROL | ICAS2018_0348 |
| Weng, Y. | NUMERICAL SIMULATION OF THE AERIAL DROP OF WATER FOR FIXED-WING AIRTANKERS | ICAS2018_0474 |
| Wenping, S. | IMPROVED DELAYED DETACHED EDDY SIMULATION OF THE FLOWS AROUND S809 AIRFOIL FOR ANGLES OF ATTACK FROM 0 TO 90 DEGREES | ICAS2018_0323 |
| Whittome, M. | ADAPTING CAPACITY OF AIR NAVIGATION SERVICE PROVISION IN EUROPE - BETWEEN SCYLLA AND CHARYBDIS | ICAS2018_0483 |
| Wiart, L. | EXPLORATION OF THE AIRBUS "NAUTILIUS" ENGINE INTEGRATION CONCEPT | ICAS2018_0135 |
| Wickramasinghe, N.K. | STUDY ON THE ARRIVAL MANAGER MAXIMIZING THE BENEFIT OF FOUR-DIMENSIONAL TRAJECTORY BASED OPERATIONS | ICAS2018_0315 |
| Wild, J. | WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING | ICAS2018_0646 |
| Wilke, D.N. | PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAV | ICAS2018_0233 |
| Will, F. | A FRAMEWORK TO ASSESS FUTURE AIRPORT NOISE APPLIED TO A TWO-RUNWAY AIRPORT | ICAS2018_0277 |
| Wilson, T. | AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATION | ICAS2018_0133 |
| Wilson, S. | SEMANTICS-BASED SUMMARIZATION OF ATM DATA TO MANAGE INFORMATION OVERLOAD IN PILOT BRIEFINGS | ICAS2018_0763 |
| Windelberg, J. | FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORS | ICAS2018_0271 |
| Wirsing, L. | DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT | ICAS2018_0875 |
| Wojtas, M. | NEW TECHNOLOGY OF LAYERED STRUCTURES IMPLEMENTED IN SELECTED GYROPLANE COMPONENTS | ICAS2018_0356 |
| Wolf, W.R. | STRUCTURAL DAMPING EFFECTS ON THE ACOUSTIC SCATTERING BY ELASTIC PLATES | ICAS2018_0108 |
| Wolters, F. | COUPLING OF PREDESIGN AND PERFORMANCE TOOLS FOR TRANSIENT AIRCRAFT ENGINE ANALYSES | ICAS2018_0830 |
| Wolters, F. | SYSTEM ANALYSIS OF TURBO ELECTRIC AND HYBRID ELECTRIC PROPULSION SYSTEMS ON A REGIONAL AIRCRAFT | ICAS2018_0831 |
| Wortmann, G. | CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATION | ICAS2018_0342 |
| Wu, T.X. | THE TECHNIQUE AND MODELLING FOR EQUIPMENT MAINTAINABILITY QUANTIFICATION IN 3D DIGITAL AIRCRAFT DESIGN CONDITION | ICAS2018_0055 |
| Wu, X.-L. | HUMAN FACTOR IN UNMANNED AIRCRAFT SYSTEM FLIGHT TEST | ICAS2018_0072 |
| Wu, T. | CALCULATION OF WATER FILM FLOW AND HEAT TRANSFER ON THE AIRCRAFT ANTI-ICING SURFACE | ICAS2018_0100 |
| Wu, D. | NUMERICAL STUDY OF VARIABLE CAMBER WING EFFECT ON AERODYNAMIC PERFORMANCE FOR LONG RANGE CIVIL AIRCRAFT | ICAS2018_0231 |
| Wu, Y. | STUDY ON AIRCRAFT EVACUATION MODELING AND MODEL PARAMETERS BASED ON SOCIAL FORCE | ICAS2018_0320 |
| Wu, B. | CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCH | ICAS2018_0405 |
| Xi, Y. | THEORETICAL STUDY OF RECEPTIVITY OF HIGH-SPEED BOUNDARY LAYER TO SURFACE PERTURBATIONS | ICAS2018_0524 |
| Xie, W. | THERMAL-MECHNICAL COUPLING ANALYSIS AND OPTIMIZATION DESIGN ON TPS WITH GAP | ICAS2018_0266 |
| Xie, J. | ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION | ICAS2018_0389 |
| Xie, W. | FEASIBILITY STUDY OF MODIFYING A BASELINE KEROSENE AIRCRAFT TO A LH2 POWERED VERSION | ICAS2018_0580 |
| Xie, D. | RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFT | ICAS2018_0610 |
| Xie, D. | RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFT | ICAS2018_0623 |
| Xu, J. | STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS | ICAS2018_0128 |
| Xu, P. | APPLICATION RESEARCH OF LARGE-SCALED COMPLICATED FRAME-BEAM INTEGRAL COMPONENT BASED ON ELECTRON BEAM ADDITIVE MANUFACTURING | ICAS2018_0319 |
| Xu, C.-Z. | SURROGATE-BASED OPTIMIZATION METHOD APPLIED TO MULTIDISCIPLINARY DESIGN OPTIMIZATION ARCHITECTURES | ICAS2018_0496 |
| Xu, J.-H. | A COMPARISON STUDY ON TRANSITION CHARACTERISTICS OF NLF FORWARD-SWEPT-WING AND AFT-SWEPT-WING | ICAS2018_0497 |
| Xu, C.-Z. | COMBINING ADJOINT-BASED AND SURROGATE-BASED OPTIMIZATIONS FOR BENCHMARK AERODYNAMIC DESIGN PROBLEMS | ICAS2018_0715 |
| Xu, P. | AIRCRAFT STRUCTURE TECHNOLOGY OF ADDITIVE MANUFACTURING | ICAS2018_0723 |
| Xue, C. | INVESTIGATION ON APPROACH TO CONTROL LIFT DISTRIBUTION OF WING BY DISTRIBUTED PROPELLERS | ICAS2018_0189 |
| Yakimenko, O.A. | FLIGHT PERFORMANCE OF STEERABLE CRUCIFORM PARACHUTE SYSTEMS | ICAS2018_0614 |
| Yakovleva, V.A. | RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT | ICAS2018_0256 |
| Yamada, K. | SAFETY FLIGHT TESTING FOR CARGO UAV DEVELOPMENT | ICAS2018_0754 |
| Yamashita, T. | AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEM | ICAS2018_0219 |
| Yamashita, R. | ADVANCED SONIC BOOM ANALYSIS USING FULL-FIELD SIMULATION | ICAS2018_0870 |
| Yan, Q. | THERMAL-MECHNICAL COUPLING ANALYSIS AND OPTIMIZATION DESIGN ON TPS WITH GAP | ICAS2018_0266 |
| Yan, X. | A RESEARCH OF MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM FOR FIGHT VEHICLE DESIGN | ICAS2018_0443 |
| Yan, X. | NUMERICAL SIMULATION OF THE AERIAL DROP OF WATER FOR FIXED-WING AIRTANKERS | ICAS2018_0474 |
| Yang, X. | STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS | ICAS2018_0128 |
| Yang, X.-D. | AERODYNAMIC DESIGN OF A RIGID COAXIAL ROTOR AIRFOIL IN UNSTEADY FLOW | ICAS2018_0172 |
| Yang, X.D. | AERODYNAMIC DESIGN OF KEY COMPONENTS OF THE LARGE-DISCHARGE AXIAL FAN AT HIGH ALTITUDE | ICAS2018_0243 |
| Yang, C.-G. | STUDY ON EVALUATION METHODS OF UNDERGRADUATE AIRCRAFT OVERALL DESIGN COURSE BASED ON TEAM DESIGN COMPETITION | ICAS2018_0250 |
| Yang, X.W. | CFD-BASED STUDY OF DAMAGE LOCATION INFLUENCE ON AERODYNAMICS OF WINGS WITH SINGLE AND DOUBLE THROUGH HOLES | ICAS2018_0294 |
| Yang, S.L. | SINGLE-AISLE AIRLINER DISRUPTION WITH A SINGLE-DECK BLENDED-WING-BODY | ICAS2018_0390 |
| Yang, X.W. | BALLISTIC RESISTANT ANALYSIS FOR AIRCRAFT WING STRUCTURE | ICAS2018_0418 |
| Yang, G. | WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITY | ICAS2018_0440 |
| Yang, Y. | A RESEARCH OF MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM FOR FIGHT VEHICLE DESIGN | ICAS2018_0443 |
| Yang, X.-L. | NUMERICAL SIMULATION OF THE AERIAL DROP OF WATER FOR FIXED-WING AIRTANKERS | ICAS2018_0474 |
| Yang, R. | AEROELASTIC WIND TUNNEL EXPERIMENT OF A HIGH-ASPECT-RATIO WING MODEL AGAINST GEOMETRICAL NON-LINEARITY | ICAS2018_0720 |
| Yanovskiy, L.S. | INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELS | ICAS2018_0645 |
| Yao, Z.X. | RESEARCH ON DESIGN METHOD OF PETROL-ELECTRIC HYBRID DRIVE SYSTEM BASED ON MDO FOR A NOVEL VTOVL UAV | ICAS2018_0136 |
| Yao, G. | HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADES | ICAS2018_0248 |
| Yao, Z. | CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCH | ICAS2018_0405 |
| Yao, Z. | RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFT | ICAS2018_0610 |
| Yao, Z. | RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFT | ICAS2018_0623 |
| Yatsufusa, T. | PRECISE MEASUREMENT OF PROPAGATING FLAME IN 2-STROKE GASOLINE ENGINE BY MULTIPLE ION-PROBES | ICAS2018_0149 |
| Yee, K.J. | COST-EFFECTIVE TELEMETRY, TRACKING AND COMMAND SYSTEM DEVELOPMENT FOR HIGH-ALTITUDE SCIENTIFIC BALLOON | ICAS2018_0214 |
| Yee, K. | DESIGN PARAMETER STUDY OF DRONE BLADE CONSIDERING AEROACOUSTICS | ICAS2018_0216 |
| Yee, K. | DEVELOPMENT OF A COMPREHENSIVE ANALYSIS AND OPTIMIZED DESIGN FRAMEWORK FOR THE MULTIROTOR UAV | ICAS2018_0594 |
| Yee, K. | DESIGN OPTIMIZATION OF AIRFOIL FOR WIND TURBINE WITH RESPECT TO ICE ACCRETION | ICAS2018_0685 |
| Yoon, T. | DESIGN OPTIMIZATION OF AIRFOIL FOR WIND TURBINE WITH RESPECT TO ICE ACCRETION | ICAS2018_0685 |
| York, C.B. | A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTION | ICAS2018_0179 |
| Yoshikawa, E. | DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEM | ICAS2018_0284 |
| Yoshikawa, N. | FAULT TOLERANT CONTROL SYSTEM OF AIRCRAFT BY FEEDBACK ERROR LEARNING WITH SYSTEM ESTIMATION | ICAS2018_0665 |
| Yu, Q. | MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLE | ICAS2018_0230 |
| Yu, Y.S. | NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTOR | ICAS2018_0334 |
| Yuan, W.X. | GLOBAL SENSITIVITY ANALYSIS OF TRANSONIC FLUTTER USING A COUPLED CFD-CSD SOLVER | ICAS2018_0037 |
| Yuan, W.X. | SIMULATIONS OF UNSTEADY AIRWAKES BEHIND SHIPS IN MOTION | ICAS2018_0038 |
| Yue, W. | IMPROVED DELAYED DETACHED EDDY SIMULATION OF THE FLOWS AROUND S809 AIRFOIL FOR ANGLES OF ATTACK FROM 0 TO 90 DEGREES | ICAS2018_0323 |
| Yutko, B. | DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPT | ICAS2018_0875 |
| Zambrano, G.J. | HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOT | ICAS2018_0337 |
| Zammit-Mangion, D. | GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESS | ICAS2018_0182 |
| Zang, J. | CONTINUOUS MODELING IN AIRCRAFT TOP-LEVEL DEMONSTRATION | ICAS2018_0085 |
| Zaplana , L. | FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONS | ICAS2018_0286 |
| Zaramella , F. | REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALS | ICAS2018_0437 |
| Zeng, H. | AEROELASTIC WIND TUNNEL EXPERIMENT OF A HIGH-ASPECT-RATIO WING MODEL AGAINST GEOMETRICAL NON-LINEARITY | ICAS2018_0720 |
| Zhai, J. | WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING | ICAS2018_0646 |
| Zhang, S. | STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS | ICAS2018_0128 |
| Zhang, M. | MULTI-POINT AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WING | ICAS2018_0154 |
| Zhang, M.H. | MULTI-POINT AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WING | ICAS2018_0154 |
| Zhang, Y.F. | MULTI-POINT AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WING | ICAS2018_0154 |
| Zhang, H. | ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLE | ICAS2018_0222 |
| Zhang, S.L. | AERODYNAMIC DESIGN OF KEY COMPONENTS OF THE LARGE-DISCHARGE AXIAL FAN AT HIGH ALTITUDE | ICAS2018_0243 |
| Zhang, C. | NONLINEAR STATIC AEROELASTIC AND TRIM ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT | ICAS2018_0278 |
| Zhang, H.Y. | NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTOR | ICAS2018_0334 |
| Zhang, Y.-D. | MULTI-CHANNEL HUMAN-MACHINE INTERACTIVE SYSTEM FOR MULTIPLE UAVS' CONTROL | ICAS2018_0348 |
| Zhang, X. | ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSION | ICAS2018_0389 |
| Zhang, Z. | STUDY ON LARGE-SCALE FLIGHT DELAY RECOVERY | ICAS2018_0457 |
| Zhang, K.-S. | SURROGATE-BASED OPTIMIZATION METHOD APPLIED TO MULTIDISCIPLINARY DESIGN OPTIMIZATION ARCHITECTURES | ICAS2018_0496 |
| Zhang, H. | STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WING | ICAS2018_0526 |
| Zhang, M. | AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORK | ICAS2018_0675 |
| Zhang, R. | BUCKLING/POSTBUCKLING OPTIMIZATION OF STIFFENED COMPOSITE PANELS BASED ON SENSITIVITY ANALYSIS | ICAS2018_0714 |
| Zhang, Y. | COMBINING ADJOINT-BASED AND SURROGATE-BASED OPTIMIZATIONS FOR BENCHMARK AERODYNAMIC DESIGN PROBLEMS | ICAS2018_0715 |
| Zhang, M. | IMPLEMENTATION OF A VORTEX LATTICE METHOD IN A HETEROGENEOUS PROGRAMMING LANGUAGE ENVIRONMENT | ICAS2018_0846 |
| Zhao, X. | ANALYSIS OF XH-59A ROTOR IN FORWARD FIGHT WITH HIGH EFFICIENCY TRIM METHOD | ICAS2018_0469 |
| Zhao, X. | THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVER | ICAS2018_0470 |
| Zhao, X. | NUMERICAL SIMULATION OF THE AERIAL DROP OF WATER FOR FIXED-WING AIRTANKERS | ICAS2018_0474 |
| Zhaohui, L. | KNOWLEDGE ENGINEERING BASED FLIGHT TEST TECHNOLOGY FOR CIVIL AIRCRAFT AIRWORTHINESS CONFORMITY | ICAS2018_0009 |
| Zhbanov, V.A. | EXPERIMENTAL INVESTIGATION, MATHEMATICAL AND NUMERICAL SIMULATION OF AIRCRAFT ICING PHENOMENA | ICAS2018_0741 |
| Zhdanov, V.V. | NUMERICAL AND EXPERIMENTAL STUDY OF THE EFFECT OF CIRCUMFERENTIAL GROOVES ON HPC LAST STAGE PERFORMANCE | ICAS2018_0624 |
| Zheng, M. | CALCULATION OF WATER FILM FLOW AND HEAT TRANSFER ON THE AIRCRAFT ANTI-ICING SURFACE | ICAS2018_0100 |
| Zheng, Y.L. | HIGH LIFT MECHANISM OF A 2D FLAPPING WING IN HOVERING FLIGHT | ICAS2018_0151 |
| Zhenghong, G. | ROBUST DESIGN OPTIMIZATION OF BENCHMARK AERODYNAMIC CASE BASED ON POLYNOMIAL CHAOS EXPANSION | ICAS2018_0187 |
| Zhestkov, G.B. | THE INFLUENCE OF THE SHAPE OF THE COOLING CHANNEL AND PRESSURE GRADIENT ON THE EFFICIENCY OF FILM COOLING OF GTE BLADES | ICAS2018_0629 |
| Zhigang, W. | RLG BASED REAL-TIME MODEL ATTITUDE DETERMINATION SYSTEM DEVELOPMENT FOR LARGE LOW SPEED FACILITY OF CARDC | ICAS2018_0317 |
| Zhiyuan, H. | RLG BASED REAL-TIME MODEL ATTITUDE DETERMINATION SYSTEM DEVELOPMENT FOR LARGE LOW SPEED FACILITY OF CARDC | ICAS2018_0317 |
| Zhluktov, S.V. | CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLES | ICAS2018_0242 |
| Zhong, L. | SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTION | ICAS2018_0066 |
| Zhong, Y. | NUMERICAL ANALYSIS OF BLEND-WING-BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCE | ICAS2018_0326 |
| Zhonghua, H. | IMPROVED DELAYED DETACHED EDDY SIMULATION OF THE FLOWS AROUND S809 AIRFOIL FOR ANGLES OF ATTACK FROM 0 TO 90 DEGREES | ICAS2018_0323 |
| Zhou, Z. | APPLICATION OF HIGH-ROBUSTNESS BEMT FOR SIMULATION OF UAV-VTOL PROPELLER AT LOW/HIGH ADVANCE RATIO | ICAS2018_0131 |
| Zhou, Z. | INVESTIGATION ON APPROACH TO CONTROL LIFT DISTRIBUTION OF WING BY DISTRIBUTED PROPELLERS | ICAS2018_0189 |
| Zhou, Z. | NONLINEAR STATIC AEROELASTIC AND TRIM ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT | ICAS2018_0278 |
| Zhou, P. | ANALYSIS OF XH-59A ROTOR IN FORWARD FIGHT WITH HIGH EFFICIENCY TRIM METHOD | ICAS2018_0469 |
| Zhou, P. | THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVER | ICAS2018_0470 |
| Zhou, P. | NUMERICAL SIMULATION OF THE AERIAL DROP OF WATER FOR FIXED-WING AIRTANKERS | ICAS2018_0474 |
| Zhou, X.W. | EVALUATION OF MECHANICAL PROPERTIES OF TI-6AL-4V FABRICATED BY SELECTIVE LASER MELTING (SLM) | ICAS2018_0866 |
| Zhu, X.Q. | STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGN | ICAS2018_0041 |
| Zhu, J.-Q | CONTINUOUS MODELING IN AIRCRAFT TOP-LEVEL DEMONSTRATION | ICAS2018_0085 |
| Zhu, M. | WIND TUNNEL VIRTUAL FLIGHT TEST FOR A TRANSPORT AIRCRAFT WITH SIMULATED ICE SHAPE | ICAS2018_0125 |
| Zhu, X. | APPLICATION OF HIGH-ROBUSTNESS BEMT FOR SIMULATION OF UAV-VTOL PROPELLER AT LOW/HIGH ADVANCE RATIO | ICAS2018_0131 |
| Zhu, X. | MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSIS | ICAS2018_0226 |
| Zhu, Z. | A COMPARISON STUDY ON TRANSITION CHARACTERISTICS OF NLF FORWARD-SWEPT-WING AND AFT-SWEPT-WING | ICAS2018_0497 |
| Zichenkov, M.C. | INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURES | ICAS2018_0299 |
| Zou, T. | STUDY ON AIRCRAFT EVACUATION MODELING AND MODEL PARAMETERS BASED ON SOCIAL FORCE | ICAS2018_0320 |
| Zu, G.R. | BALLISTIC RESISTANT ANALYSIS FOR AIRCRAFT WING STRUCTURE | ICAS2018_0418 |
| Zurawski, R. | INVESTIGATION OF ‘JUMP TAKEOFF’ POSSIBILITY FOR THE NEW CONCEPT OF MODERN AUTOGYRO | ICAS2018_0630 |
| Ölvander, J. | MULTIDISCIPLINARY OPTIMIZATION OF UNMANNED AIRCRAFT IN A SYSTEM OF SYSTEMS CONTEXT | ICAS2018_0047 |
| Žižkovský, N. | EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPS | ICAS2018_0258 |