COMPLETE AUTHOR LIST HYPERLINKED TO PAPERS



Abd Bari, M.A.ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHMICAS2018_0328
Abdalla, A.M.ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OFSUPERSONIC BUSINESS JETSICAS2018_0030
Abdalla, A.M.EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFTICAS2018_0199
Abdalla, A.M.DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATIONICAS2018_0814
Abdelmoula, F.LNAS - A PILOT ASSISTANCE SYSTEM FOR LOW-NOISE APPROACHES WITH MINIMAL FUEL CONSUMPTIONICAS2018_0096
Abramova, K.A.NUMERICAL OPTIMIZATION OF FLOW CONTROL BY TANGENTIAL JET BLOWING ON TRANSONIC AIRFOILICAS2018_0704
Abramovich, H.INVESTIGATION OF CRACK PROPAGATION PROPERTIES OF ADDITIVE MANUFACTURING PRODUCTSICAS2018_0012
Abreu, D.F.EFFECTS OF NUMERICAL MODELING CHOICES FOR HEATED JETS IN CROSS FLOWICAS2018_0369
Abreu, L.I.WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOILICAS2018_0388
Abulawi, J.A SYSML-BASED APPROACH TO EXPLORING INNOVATIVE SYSTEM IDEAS FOR AERONAUTICAL APPLICATIONSICAS2018_0821
Acevedo-Giraldo, D.EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCEICAS2018_0815
Afonin, A.I.APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADESICAS2018_0173
Ahn, J.M.ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTINGICAS2018_0159
Aigner, B.MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERINGICAS2018_0633
Aigner, B.DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORKICAS2018_0674
Aigner, B.COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTSICAS2018_0785
Akiyama, T.FLIGHT DEMONSTRATION OF A LONG RANGE ONBOARD DOPPLER LIDARICAS2018_0121
Akiyama, T.DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEMICAS2018_0284
Akman, T.USING SENSITIVITY PENALTIES TO ROBUSTIFY THE OPTIMAL REENTRY TRAJECTORY OF A HYPERSONIC VEHICLEICAS2018_0564
Akman, T.NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCINGICAS2018_0782
Akroyd, G.RECTANGULAR CAVITY FLOWFIELD EFFECTS ON STORES IN THE SHEAR LAYERICAS2018_0045
Akroyd, G.STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDSICAS2018_0367
Aksenov, A.A.CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLESICAS2018_0242
Alegre, G.S.P.PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMSICAS2018_0194
Aleksandrov, V.Y.GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORSICAS2018_0628
Aleksandrov, V.Y.INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELSICAS2018_0645
Aleksandrov, V.Y.COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODELICAS2018_0672
Alexandrov, S.V.NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTSICAS2018_0700
Alexandrova, E.A.EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOWICAS2018_0690
Alexandrova, E.A.NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTSICAS2018_0700
Alfredson, J.DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMSICAS2018_0305
Alfredson, J.A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTSICAS2018_0309
Algodoal, L.A.HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOTICAS2018_0337
Almeida, S.F.M.RESULTS AND COMPARISON OF NUMERICAL SIMULATION AND THE TESTING OF LUG MANUFACTURED BY COMPOSITE MATERIAL BY RTM PROCESSICAS2018_0007
Almeida, A.C.V.M.CFD INVESTIGATION OF AERODYNAMIC COEFFICIENTS AND STALL CHARACTERISTICS FOR HIGH LIFT CONFIGURATIONSICAS2018_0076
Almeida, S.F.M. A PASSIVE-ADAPTIVE WING FOR DRAG REDUCTIONICAS2018_0179
Almeida, A.N.A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTSICAS2018_0309
Almeida, A.EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONSICAS2018_0402
Almeida, S.F.M.MODIFIED WHITNEY-NUISMER CRITERIA FOR PREDICTION OF NOTCHED STRENGTH OF COMPOSITE LAMINATESICAS2018_0677
Almeida Jr, J.C. PREDICTIVE & DETECTIVE MAINTENANCE: EFFECTIVE TOOLS IN THE MANAGEMENT OF AERONAUTICAL PRODUCTSICAS2018_0336
Altenscheidt, L.PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALSICAS2018_0050
Altenscheidt, M.PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALSICAS2018_0050
Alves, D.S.MODELLING OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITES: A COMPARATIVE STUDYICAS2018_0519
Amadori, K.MULTIDISCIPLINARY OPTIMIZATION OF UNMANNED AIRCRAFT IN A SYSTEM OF SYSTEMS CONTEXTICAS2018_0047
Amadori, K.A HOLISTIC ENGINEERING APPROACH FOR AERONAUTICAL PRODUCT DEVELOPMENTICAS2018_0724
Amelyushkin, I.A.EXPERIMENTAL INVESTIGATION, MATHEMATICAL AND NUMERICAL SIMULATION OF AIRCRAFT ICING PHENOMENAICAS2018_0741
Amiryants, G.A.AEROELASTIC PROPERTIES OF ACTIVE WINGLETSICAS2018_0276
Ananyan, M.V.INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELSICAS2018_0645
Andersson, J.COMPARISON OF TWO DIFFERENT INDICATORS FOR HOT CRACKING IN WELDED STRUCTURESICAS2018_0142
Andrade, D.STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODSICAS2018_0579
Andrews, G.A HYBRID LENGTH SCALE SIMILARITY SOLUTION FOR SWIRLING TURBULENT JETSICAS2018_0872
Angélico, R.A.INFLUENCE OF AIRFRAME STIFFNESS ON THE AERODYNAMIC COEFFICIENTS OF A HIGH ASPECT RATIO WINGICAS2018_0776
Angelo, M.V.AN XFEM FRAMEWORK FOR ONSET AND CRACK PROPAGATION FOR COMPOSITES BASED ON ACTION PLANE THEORYICAS2018_0502
Anisimov, K.MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECTICAS2018_0783
Anisimov, K.S.PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECTICAS2018_0788
Ann, S.MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMITICAS2018_0080
Antunes, P.ARAMID-FIBER REINFORCED ELASTOMERS AS FUTURE AIRCRAFT ACTUATORS - A PROOF-OF-CONCEPT INVESTIGATIONICAS2018_0377
Arantes, J.S.SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVSICAS2018_0374
Arantes, M.S.SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVSICAS2018_0374
Archer, R.GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESSICAS2018_0182
Arefyev, K.Y.INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELSICAS2018_0645
Argolo Jesus, T.FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETSICAS2018_0396
Arjoni, D.H.A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTSICAS2018_0309
Arjoni, D.H.EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONSICAS2018_0402
Arnaldo, R.M.DETECTING HIGH-ALTITUDE ICE CRYSTAL (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATUREICAS2018_0611
Aso, S.PASSIVE VENTILATION FLOW CONTROL FOR AIRCRAFT GUST LOAD ALLEVIATIONICAS2018_0736
Atkin, C.DEVELOPMENT OF SECONDARY CROSSFLOW INSTABILITY NEAR BREAKDOWN INTO TURBULENCEICAS2018_0735
Atkin, C.LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLESICAS2018_0739
Atobe, T.DESTABILIZING EFFECT OF LONGITUDINAL WALL OSCILLATION ON OBLIQUE WAVES IN 2D CHANNEL FLOWICAS2018_0118
Avallone, F.AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMSICAS2018_0505
Avelar, A.C.TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCK OSCILATIONSICAS2018_0599
Avelino, W.O.DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONSICAS2018_0609
Awruch, A.M.LARGE EDDY SIMULATION OF A TRANSIENT SPOILER DEPLOYMENT IN A NACA0012 PROFILE IN SUBSONIC AND TRANSONIC SPEEDSICAS2018_0503
Azevedo, J.L.F.CFD INVESTIGATION OF AERODYNAMIC COEFFICIENTS AND STALL CHARACTERISTICS FOR HIGH LIFT CONFIGURATIONSICAS2018_0076
Bacciaglia, A.BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTINGICAS2018_0660
Baeva, S.I.NUMERICAL AND EXPERIMENTAL STUDY OF THE EFFECT OF CIRCUMFERENTIAL GROOVES ON HPC LAST STAGE PERFORMANCEICAS2018_0624
Bagassi, S.THE USE OF SYNTHETIC VISION TOOLS IN THE CONTROL TOWER ENVIRONMENT: THE RETINA CONCEPTICAS2018_0717
Bagassi, S.DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACHICAS2018_0774
Bagassi, S.PRELIMINARY DESIGN OF A LONG RANGE WINDOWLESS AIRCRAFT CONCEPTICAS2018_0777
Bai, Y.AEROELASTIC WIND TUNNEL EXPERIMENT OF A HIGH-ASPECT-RATIO WING MODEL AGAINST GEOMETRICAL NON-LINEARITYICAS2018_0720
Bai, Y.EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTSICAS2018_0784
Balachandran, S.AN EVALUATION OF VARIOUS GEOFENCE CONFLICT RESOLUTION ALGORITHMS AND THEIR IMPACT ON MISSION PERFORMANCEICAS2018_0393
Balunov, K.A.AEROELASTIC TAILORING OF COMPOSITE WING BY USING MULTIDISCIPLINARY DESIGN ENVIRONMENTICAS2018_0458
Balvedi, G.C.A METHOD FOR ESTIMATING THE PROBABILITY OF RARE ACCIDENTS IN COMPLEX SYSTEMSICAS2018_0849
Banfi , D.REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALSICAS2018_0437
Barbosa, G.C.ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFTICAS2018_0529
Barbosa, A.A.F.INFLUENCE OF GULL WING ON LONGITUDINAL AND LATERAL-DIRECTIONAL COEFFICIENTS OF AN AIRPLANEICAS2018_0670
Barbosa, R.C.M.G. CLOSED-LOOP SYSTEM IDENTIFICATION OF A LARGE FLEXIBLE AIRCRAFT USING SUBSPACE METHODSICAS2018_0813
Barrier, P.PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAVICAS2018_0233
Barros, J.STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWSICAS2018_0482
Batura, S.N.COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODELICAS2018_0672
Bauer, M.WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTINGICAS2018_0646
Bautin, A.A.DEVELOPMENT OF STRUCTURAL HEALTH MONITORING METHODS THROUGH THE ANALYSIS OF KINETICS OF LOCAL STRESS-STRAIN STATEICAS2018_0160
Bauzer Medeiros, E.UAV INITIAL PARAMETER ESTIMATIONICAS2018_0568
Bauzer Medeiros, E.HISTORY OF AVIATION IN MINAS GERAISICAS2018_0871
Bayandor, J.BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATIONICAS2018_0661
Bayandor, J.VERIFIED FUSELAGE SECTION WATER IMPACT MODELINGICAS2018_0732
Bayandor, J.PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFTICAS2018_0826
Bayma, A.HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENTICAS2018_0269
Beals, N.ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACHICAS2018_0851
Becker, G.G.HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOTICAS2018_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 ANALYSESICAS2018_0830
Belo, E.M.FLIGHT DYNAMICS MODELING AND TRIM CURVES OF A CONCEPTUAL SEMI-TANDEM WING VTOL UAVICAS2018_0171
Belo, E.M.PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMSICAS2018_0194
Belov, S.V.THE INFLUENCE OF THE SHAPE OF THE COOLING CHANNEL AND PRESSURE GRADIENT ON THE EFFICIENCY OF FILM COOLING OF GTE BLADESICAS2018_0629
Berlowitz, I.NARROW-BODY B737NG PASSENGER CONVERSION TO FREIGHTERICAS2018_0003
Bertolin, R.M.ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFTICAS2018_0529
Beyak, E.-S.IONIZATION AND DISSOCIATION EFFECTS ON HYPERSONIC BOUNDARY-LAYER STABILITYICAS2018_0837
Bi, S.APPLICATION RESEARCH OF LARGE-SCALED COMPLICATED FRAME-BEAM INTEGRAL COMPONENT BASED ON ELECTRON BEAM ADDITIVE MANUFACTURINGICAS2018_0319
Bi, S.AIRCRAFT STRUCTURE TECHNOLOGY OF ADDITIVE MANUFACTURINGICAS2018_0723
Bidinotto, J.H.PIO SUSCEPTIBILITY IN FLY-BY-WIRE SYSTEMSICAS2018_0194
Bier, N.WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTINGICAS2018_0646
Bijewitz, J.CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATIONICAS2018_0342
Bijewitz, J.DESIGN AND OFF-DESIGN PERFORMANCE OF ELECTRIC SYSTEM ARCHITECTURES FOR ELECTRIC POWERED AIRCRAFTICAS2018_0728
Bil, C.ADAPTIVE LANDING SEQUENCING USING BIPARTITE GRAPHS AND PERFECT MATCHINGICAS2018_0634
Bil, C.URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREAICAS2018_0635
Bil, C.BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTINGICAS2018_0660
Bile, Y.COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGNICAS2018_0134
Bizarro, A.F.MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UPICAS2018_0493
Bliznyukov, L.G.ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORSICAS2018_0639
Boggero, L.INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORKICAS2018_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 JETICAS2018_0655
Bonet, J.T.BLENDED WING BODY TRANSPORT AIRCRAFT RESEARCH & DEVELOPMENTICAS2018_0298
Boonjaipetch, P.ANALYSIS OF LOW-BOOM CHARACTERISTICS OF SUPERSONIC WAVERIDERICAS2018_0424
Boozer, C.M.COUPLED ADJOINT AEROSTRUCTURAL OPTIMIZATION FRAMEWORK FOR PRELIMINARY AIRCRAFT DESIGNICAS2018_0426
Borges Tôrres, L.A.FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETSICAS2018_0396
Borovoy, V.Y.EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOWICAS2018_0690
Botero-Bolivar, L.EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCEICAS2018_0815
Braschczok, M.PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALSICAS2018_0050
Braun, R.A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORTICAS2018_0203
Bravo-Mosquera, P.D.EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFTICAS2018_0199
Bravo-Mosquera, P.D.DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATIONICAS2018_0814
Bravo-Mosquera, P.D.EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCEICAS2018_0815
Breard, C.CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF "PARASITE" NOISEICAS2018_0116
Breard, C.IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BEDICAS2018_0119
Breitsamter, C.OUTBOARD SPLIT FLAP AERODYNAMICS OF A FLYING WING CONFIGURATIONICAS2018_0069
Breitsamter, C.PERFORMANCE IMPROVEMENT OF A COMPOUND HELICOPTER ROTOR HEAD BY AERODYNAMIC SHAPE OPTIMIZATIONICAS2018_0070
Breitsamter, C.TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTSICAS2018_0126
Breymann, B.COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMENICAS2018_0167
Bringhenti, C.PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERSICAS2018_0649
Broekhuijsen, J.J.NUMERICAL INVESTIGATION AERODYNAMICS NACELLE-STRAKE EFFECTICAS2018_0205
Broitman, N.INVESTIGATION OF CRACK PROPAGATION PROPERTIES OF ADDITIVE MANUFACTURING PRODUCTSICAS2018_0012
Brügge, T.A FRAMEWORK FOR UNCONVENTIONAL LANDING GEAR CONFIGURATION MODELLINGICAS2018_0688
Buch, J.-P.IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMSICAS2018_0249
Buchwald, M.STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACHICAS2018_0082
Budinger, M.A MORE INTEGRATED DESIGN APPROACH FOR EMBEDDED MECHATRONIC SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMSICAS2018_0170
Bussamra, F.L.S.STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWSICAS2018_0482
Bussamra, F.L.S.MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UPICAS2018_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 FRAMEWORKICAS2018_0674
Caldas, L.C.DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONESICAS2018_0591
Calvo, M.ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OFSUPERSONIC BUSINESS JETSICAS2018_0030
Campobasso, M.S.FEASIBILITY OF THE NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING AIRCRAFT UNSTEADY AERODYNAMICSICAS2018_0791
Camponogara, A.POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATIONICAS2018_0818
Campos, R.M.V.COMPARATIVE STUDY AND VALIDATION OF MATERIAL WITH BETTER PERFORMANCE IN TERMS OF THERMAL ABSORPTION INSIDE AN AIRCRAFTICAS2018_0017
Campos, G.B.PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERSICAS2018_0649
Canzian, L.IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMSICAS2018_0249
Capristan, F.A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIESICAS2018_0088
Capuano, F.NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMPICAS2018_0622
Cardoso-Ribeiro, F.L.APPLICABILITY OF GEOMETRICALLY-LINEAR STRUCTURAL-DYNAMIC MODELS FOR THE FLIGHT DYNAMICS OF ARBITRARILY-FLEXIBLE AIRCRAFTICAS2018_0523
Carmona, L.C.UAV INITIAL PARAMETER ESTIMATIONICAS2018_0568
Carrera, E.GLOBAL-LOCAL STRUCTURAL ANALYSIS OF COMPOSITE WINGSICAS2018_0245
Carvalho, L.M.M.O.CFD INVESTIGATION OF AERODYNAMIC COEFFICIENTS AND STALL CHARACTERISTICS FOR HIGH LIFT CONFIGURATIONSICAS2018_0076
Carvalho, F.I. INCREASED FLUTTER VELOCITY WITH USE OF A PASSIVE CONTROL SYSTEMICAS2018_0800
Carvalho, R.C.DEVELOPMENT OF THE REGENERATIVE SOARER: THEORETICAL AND PRACTICAL ASPECTSICAS2018_0839
Cary, A.CFD VERIFICATION AND VALIDATION FOR INDUSTRIAL APPLICATIONSICAS2018_0857
Casalino, D.AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMSICAS2018_0505
Castillo Pardo, A.CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATIONICAS2018_0342
Castro, S.G.PAN ACTIVE-PASSIVE NONLINEAR FINITE ELEMENT MODEL FOR ELECTROMECHANICAL COMPOSITE MORPHING BEAMSICAS2018_0207
Catalano, P.DE-ICING PHENOMENA MODELLED BY FINITE ELEMENT MODELSICAS2018_0180
Catalano, F.M.EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFTICAS2018_0199
Catalano, P.VALIDATION OF INTERMITTENCY MODEL FOR TRANSITION PREDICTION IN A RANS FLOW SOLVERICAS2018_0484
Catalano, F.M.MULTI-DISCIPLINARY DESIGN OPTIMIZATION OF A BLENDED WINGLETICAS2018_0598
Catalano, F.M.BRAZILIAN AVIATION HISTORY: THE UNIVERSITY OF SĂO PAULO CASEICAS2018_0601
Catalano, P.NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMPICAS2018_0622
Catalano, F.M.INFLUENCE OF GULL WING ON LONGITUDINAL AND LATERAL-DIRECTIONAL COEFFICIENTS OF AN AIRPLANEICAS2018_0670
Catalano, F.M.EVALUATION OF WIND TUNNEL WALL BOUNDARY-LAYER CONTROL FOR 2-D HIGH-LIFT AERODYNAMIC AND AEROACOUSTIC TESTINGICAS2018_0780
Catalano , F.M.DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATIONICAS2018_0814
Catalano, F.M.EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCEICAS2018_0815
Cavalcanti, J.A CASE OF SUCESS: MDO APPLIED ON THE DEVELOPMENT OF EMBRAER 175 ENHANCED WINGTIPICAS2018_0034
Cavalieri, A.V.G.STRUCTURAL DAMPING EFFECTS ON THE ACOUSTIC SCATTERING BY ELASTIC PLATESICAS2018_0108
Cavalieri, A.V.G.ON THE WAVE-CANCELLING NATURE OF BOUNDARY LAYER TRANSITION CONTROLICAS2018_0349
Cavalieri, A.V.G.WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOILICAS2018_0388
Cavalieri, A.V.G.ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIESICAS2018_0438
Cavalieri, A.ACOUSTIC MODES AND GLOBAL INSTABILITIES IN WAKES AND JETSICAS2018_0450
Cavalieri, A.CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATEICAS2018_0473
Cavalieri, A.V.G.RESOLVENT-BASED CONTROL OF STREAKS IN BOUNDARY LAYERSICAS2018_0477
Cecrdle, J.FLUTTER ANALYSIS OF TWIN TURBOPROP AIRCRAFT WITH TIP-TANKSICAS2018_0004
Cecrdle, J.EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPSICAS2018_0258
Celso Jr., P.PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIGICAS2018_0147
Cen, F.A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNELICAS2018_0406
Cen, F.OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDCICAS2018_0750
Cenko, A.RECTANGULAR CAVITY FLOWFIELD EFFECTS ON STORES IN THE SHEAR LAYERICAS2018_0045
Cenko, A.STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDSICAS2018_0367
Cerino, G.MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECTICAS2018_0648
Cerón-Muńoz, H.D.DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATIONICAS2018_0814
Cerón-Muńoz, H.D.EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCEICAS2018_0815
Ceruti, A.BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTINGICAS2018_0660
Cesnik, C.E.S.PROPELLER INFLUENCE ON THE STABILITY OF HALE AIRCRAFTICAS2018_0177
Cesnik, C.E.S.NONLINEAR AEROELASTIC REDUCED ORDER MODELS USING MODAL COORDINATESICAS2018_0262
Cesnik, C.E.S.STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWSICAS2018_0482
Cesnik, C.E.S.MULTIDISCIPLINARY METHODS FOR WING FLIGHT SHAPE ANALYSIS - EFFECT OF THE GEOMETRIC NONLINEAR STRUCTURE FOR STATIC PULL-UPICAS2018_0493
Cesnik , C.E.S.IMPLEMENTATION AND FLIGHT TESTING OF AN ENHANCED STABILITY SYSTEM FOR A VERY FLEXIBLE AIRCRAFTICAS2018_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 CONTROLICAS2018_0430
Cestino, E.REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALSICAS2018_0437
Cestino, E.NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODELICAS2018_0556
Chaitanya Munjulury, R.INTEGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONSICAS2018_0873
Chaitanya Munjulurynjulury, R.HURRICANE-CS: CONTROL SURFACES AND HIGH LIFT DEVICES MODELING AND SIZING PROGRAMICAS2018_0627
Chambers, J.DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPTICAS2018_0875
Chang, H.-C.HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILESICAS2018_0270
Charbonnier, D.DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORKICAS2018_0674
Charbonnier, D.MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECTICAS2018_0783
Chedrik, V.V.STRESS-BASED TOPOLOGY OPTIMIZATION WITH USING GLOBAL-LOCAL APPROACHICAS2018_0316
Chedrik, V.V.AEROELASTIC TAILORING OF COMPOSITE WING BY USING MULTIDISCIPLINARY DESIGN ENVIRONMENTICAS2018_0458
Chedrik, V.V.PROBABILISTIC METHOD OF DETERMINATION OF ALLOWABLE DESIGN PARAMETER SCATTERS ON FLUTTER AND STRENGTH CRITERIAICAS2018_0756
Chen, Z.W.STUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGNICAS2018_0041
Chen, Y.CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF "PARASITE" NOISEICAS2018_0116
Chen, H.X.MULTI-POINT AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WINGICAS2018_0154
Chen, B.Y.LONGITUDINAL STABILITY DESIGN CRITERIA FOR HYPERSONIC GLIDERSICAS2018_0166
Chen, Z.W.AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGEICAS2018_0210
Chen, Z.-K.STUDY ON EVALUATION METHODS OF UNDERGRADUATE AIRCRAFT OVERALL DESIGN COURSE BASED ON TEAM DESIGN COMPETITIONICAS2018_0250
Chen, Z.W.CFD-BASED STUDY OF DAMAGE LOCATION INFLUENCE ON AERODYNAMICS OF WINGS WITH SINGLE AND DOUBLE THROUGH HOLESICAS2018_0294
Chen, K.STUDY ON AIRCRAFT EVACUATION MODELING AND MODEL PARAMETERS BASED ON SOCIAL FORCEICAS2018_0320
Chen, Y.NUMERICAL ANALYSIS OF BLEND-WING-BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCEICAS2018_0326
Chen, Q.NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTORICAS2018_0334
Chen, C.PASSIVE CONTROL METHOD IN ATTENUATING SELF-INDUCED ROLL OSCILLATIONS OF LOW-ASPECT-RATIO WINGS USING OBLIQUE SLOT BLEEDICAS2018_0468
Chen, X.EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTSICAS2018_0784
Cheng, J.FAULT DIAGNOSIS METHOD STUDY FOR COMPLEX SYSTEM BASED ON KALMAN FILTERSICAS2018_0015
Chernousov, V.I.CONTAINERIZED AIR FREIGHT SYSTEM POWERED BY CRYOGENIC FUELICAS2018_0103
Chernov, A.V.INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURESICAS2018_0299
Chernyshev, S.L.APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTSICAS2018_0321
Chernyshov, V.I.ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORSICAS2018_0639
Choi, U.H.ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTINGICAS2018_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 CONCEPTICAS2018_0875
Churkina, T.OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCEICAS2018_0361
Chuvakhov, P.V.EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOWICAS2018_0690
Chuvakhov, P.V.NUMERICAL COMPARISON OF STEADY DISTURBANCES IN THE WAKE OF PERIODIC BLOW-SUCTION AND ROUGHNESS ELEMENTSICAS2018_0700
Chuvakhov, P.V.ENTROPY LAYER EFFECT ON ROUGHNESS-INDUCED LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLAT PLATE FLOWICAS2018_0701
Ciampa, P.D.INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORKICAS2018_0412
Ciampa, P.D.STREAMLINING CROSS-ORGANIZATIONAL AIRCRAFT DEVELOPMENT PROCESSES: AN OVERVIEW OF THE AGILE PROJECTICAS2018_0621
Ciampa, P.D.MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERINGICAS2018_0633
Ciampa, P.D.DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORKICAS2018_0674
Ciampa, P.D.AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORKICAS2018_0675
Ciampa, P.D.MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECTICAS2018_0783
Ciampa, P.D.COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTSICAS2018_0785
Ciliberti, D.NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODELICAS2018_0264
Ciliberti , D.MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECTICAS2018_0783
Ciloni, P.A CASE OF SUCESS: MDO APPLIED ON THE DEVELOPMENT OF EMBRAER 175 ENHANCED WINGTIPICAS2018_0034
Cimini Jr., C.A.FINITE ELEMENT MODEL DEVELOPMENT FOR SIMULTANEOUS CRACK PROPAGATION IN TWO COOPERATIVE LUGSICAS2018_0512
Cimini Jr., C.A.CRACK PROPAGATION STARTING AT HOLE’S EDGE GROWING TO PLATE’S MAJOR DIMENSION USING FEMICAS2018_0516
Cimini Jr., C.A.PLY THICKNESS INFLUENCE IN COMPRESSION AFTER IMPACT DAMAGE ON CARBON/EPOXY TEST SPECIMENSICAS2018_0707
Ciobaca, V.WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTINGICAS2018_0646
Coetzee, E.B.NONLINEAR AEROELASTIC REDUCED ORDER MODELS USING MODAL COORDINATESICAS2018_0262
Collier, F.PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFTICAS2018_0826
Consiglio, M.AN EVALUATION OF VARIOUS GEOFENCE CONFLICT RESOLUTION ALGORITHMS AND THEIR IMPACT ON MISSION PERFORMANCEICAS2018_0393
Cooper, J.E.AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATIONICAS2018_0133
Corbelli, W.STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODSICAS2018_0579
Corcione, S.AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATIONICAS2018_0191
Corcione, S.NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODELICAS2018_0264
Corman, J.A.AN APPROACH TO ASSESS AIRFRAME WEIGHT REDUCTION PERFORMANCE OF STITCHED COMPOSITE TECHNOLOGIESICAS2018_0793
Costa, T.L.MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATIONICAS2018_0586
Costa, F.P.PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERSICAS2018_0649
Courtin, C.DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPTICAS2018_0875
Cresto Aleina, S.PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFTICAS2018_0164
Crockford, J.AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACEICAS2018_0132
Crovato, A.HIGHER FIDELITY TRANSONIC AERODYNAMIC MODELING IN PRELIMINARY AIRCRAFT DESIGNICAS2018_0453
Crowley, B.LAMINAR-TURBULENT TRANSITION MECHANISMS OVER WIDELY-SPACED SUCTION HOLESICAS2018_0739
Cuenca, R.G.PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIGICAS2018_0147
Cuenca, R.G.DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONESICAS2018_0591
Cui, B.CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORKICAS2018_0268
Cui, H.APPLICATION RESEARCH OF LARGE-SCALED COMPLICATED FRAME-BEAM INTEGRAL COMPONENT BASED ON ELECTRON BEAM ADDITIVE MANUFACTURINGICAS2018_0319
Cui, D.BUCKLING/POSTBUCKLING OPTIMIZATION OF STIFFENED COMPOSITE PANELS BASED ON SENSITIVITY ANALYSISICAS2018_0714
Cui, H.AIRCRAFT STRUCTURE TECHNOLOGY OF ADDITIVE MANUFACTURINGICAS2018_0723
Cunha, R.R.CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHMICAS2018_0355
Cunha Jr., S.S.A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOTICAS2018_0559
Curran, R.CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORKICAS2018_0268
Cusati, V.PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFTICAS2018_0164
Cusati, V.NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODELICAS2018_0264
Cusati, V.MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGNICAS2018_0504
Czado, C.INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONSICAS2018_0043
Czajkowski, L.NEW TECHNOLOGY OF LAYERED STRUCTURES IMPLEMENTED IN SELECTED GYROPLANE COMPONENTSICAS2018_0356
D'Assunçăo, D.EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTIONICAS2018_0391
da Costa, J.P.CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHMICAS2018_0355
Da Ronch, A.ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHMICAS2018_0328
Da Ronch, A.WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITYICAS2018_0440
Da Ronch, A.ON REAL–TIME SIMULATION OF FLEXIBLE AIRCRAFT WITH PHYSICS–DERIVED MODELSICAS2018_0501
Da Ronch, A.FEASIBILITY OF THE NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING AIRCRAFT UNSTEADY AERODYNAMICSICAS2018_0791
da Silva, R.G.CFD INVESTIGATION OF AERODYNAMIC COEFFICIENTS AND STALL CHARACTERISTICS FOR HIGH LIFT CONFIGURATIONSICAS2018_0076
da Silva, G.A.L.SHIP-HELICOPTER OPERATIONAL LIMITATION ENVELOPE DEFINITION WITH CFD RESULTS AND WIND TUNNEL DATAICAS2018_0345
da Silva, P.A.SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCEICAS2018_0354
da Silva, P.A.CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHMICAS2018_0355
da Silva, R.G.A.EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATIONICAS2018_0382
Da Silva, E.R.COMPARISON AND APPLICATION OF DIFFERENTS TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMIC WING DESIGNICAS2018_0527
da Silva, R.G.A.TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCK OSCILATIONSICAS2018_0599
Dai, Z.AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROLICAS2018_0129
Dala, L.PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAVICAS2018_0233
Damodaran, M.MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLEICAS2018_0230
Danilkin, S.Y.PERFORMANCES OF LPT AND LINEAR CASCADES AT LOW REYNOLDS NUMBERSICAS2018_0652
Danzi, F.NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODELICAS2018_0556
Daoud, F.AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORKICAS2018_0675
Daud Filho, A.C.FLIGHT DYNAMICS MODELING AND TRIM CURVES OF A CONCEPTUAL SEMI-TANDEM WING VTOL UAVICAS2018_0171
Dautermann, T.PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALSICAS2018_0050
De Aguiar Quintanilha Jr., H.R.ON THE EXISTENCE OF MULTIPLE SELF-EXCITATION FREQUENCIES IN THE INSTABILITY OF INTERACTING PLANAR MIXING LAYER AND WAKEICAS2018_0537
de Almeida, O.AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER PICKUP TRUCKSICAS2018_0201
de Azevedo, B.A.DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATSICAS2018_0807
de Blécourt, A.WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTINGICAS2018_0646
De Breuker, R.INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WINGICAS2018_0786
de Bruin, A.WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTINGICAS2018_0646
de Campos, F.P.V.POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATIONICAS2018_0818
de Castro, E.S.B.POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATIONICAS2018_0818
De Crescenzio , F.THE USE OF SYNTHETIC VISION TOOLS IN THE CONTROL TOWER ENVIRONMENT: THE RETINA CONCEPTICAS2018_0717
De Crescenzio, F.DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACHICAS2018_0774
de Lima Monteiro, D.W.DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONSICAS2018_0609
De Marco, A.MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGNICAS2018_0504
De Marco, A.MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECTICAS2018_0648
De Marqui Jr., C.EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTIONICAS2018_0391
De Negri, V.A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROLICAS2018_0052
De Negri, V.J.DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE OF QUANTIZED CONTROL AND LMI APPROACHICAS2018_0521
de Oliveira, W.R.CHARACTERISTIC HELICOPTER FLIGHT MECHANICS AND MOTION CUEING INTEGRATION INTO THE SIVOR ROBOTIC FLIGHT SIMULATOR: AN OBJECTIVE APPROACHICAS2018_0506
de Oliveira, L.A.MODELLING OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITES: A COMPARATIVE STUDYICAS2018_0519
de Pieri, E.R.MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATIONICAS2018_0586
de Rosa, D.VALIDATION OF INTERMITTENCY MODEL FOR TRANSITION PREDICTION IN A RANS FLOW SOLVERICAS2018_0484
De Simone, V.DE-ICING PHENOMENA MODELLED BY FINITE ELEMENT MODELSICAS2018_0180
de Sousa, M.S.STAMP METHOD APPLICATION ON INDUSTRIAL MANAGEMENTICAS2018_0553
de Souza, C.E.OPTIMAL SHAPE OF REPAIR PATCHES IN COMPOSITESICAS2018_0471
Degtyar, V.G.CFD PACKAGE "FLOW VISION" FOR SIMULATIONS AND IMITATION MODELING OF HYPERSONIC VEHICLESICAS2018_0242
Delbecq, S.A MORE INTEGRATED DESIGN APPROACH FOR EMBEDDED MECHATRONIC SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMSICAS2018_0170
Della Corte, B.CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATIONICAS2018_0342
Della Vecchia, P.AERODYNAMIC DESIGN AND ANALYSIS OF AN INNOVATIVE REGIONAL TURBOPROP CONFIGURATIONICAS2018_0191
Della Vecchia, P.NUMERICAL HIGH LIFT PREDICTION ON THE JAXA STANDARD MODELICAS2018_0264
Della Vecchia, P.MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECTICAS2018_0648
Della Vecchia , P.MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECTICAS2018_0783
Della Vecchia, P.COLLABORATIVE OPEN SOURCE AIRCRAFT DESIGN FRAMEWORK FOR EDUCATION - AGILE ACADEMY INITIATIVES AND RESULTSICAS2018_0785
Dell’Amico, A.A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROLICAS2018_0052
Deng, Y.-P.GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEMICAS2018_0057
Deng, L.ANALYSIS OF XH-59A ROTOR IN FORWARD FIGHT WITH HIGH EFFICIENCY TRIM METHODICAS2018_0469
Desvigne, D.PERFORMANCE IMPROVEMENT OF A COMPOUND HELICOPTER ROTOR HEAD BY AERODYNAMIC SHAPE OPTIMIZATIONICAS2018_0070
Di Pasquale, D.A RAPID AERODYNAMIC PREDICTION METHOD FOR UNCONVENTIONAL TRANSONIC AIRCRAFT CONFIGURATIONSICAS2018_0138
Di Pasquale, D.THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENTICAS2018_0297
Di Rito, G.MULTI-VARIABLE AIRCRAFT DIRECTIONAL CONTROL WITH ANTI-SKID DIFFERENTIAL BRAKESICAS2018_0607
Di Rito, G.SMART FAULT-TOLERANT AIR-DATA SENSOR FOR AIRCRAFT FLOW ANGLES MEASUREMENTICAS2018_0625
Di Vito, V.ALGORITHMS AND SYSTEM FOR CURVED AND CONTINUOUS DESCENT TRAJECTORIES IMPROVING FUEL EFFICIENCY IN TMAICAS2018_0063
Diaz, M.A.R.A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTSICAS2018_0309
Díaz-Méndez, Y.A.A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOTICAS2018_0559
Diepolder, J.USING SENSITIVITY PENALTIES TO ROBUSTIFY THE OPTIMAL REENTRY TRAJECTORY OF A HYPERSONIC VEHICLEICAS2018_0564
Diepolder, J.NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCINGICAS2018_0782
Dietz, M.CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATIONICAS2018_0342
Dikova, O.D.INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELSICAS2018_0645
Dillinger, E.HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSIONICAS2018_0492
Dimitriadis, G.INVISCID AND VISCOUS FLOW MODELING FOR FAST TRANSONIC FLUTTER CALCULATIONSICAS2018_0436
Dimitriadis, G.HIGHER FIDELITY TRANSONIC AERODYNAMIC MODELING IN PRELIMINARY AIRCRAFT DESIGNICAS2018_0453
Ding, K.H.DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATEICAS2018_0691
Djojodihardjo, H.OVERVIEW ON THE INFLUENCE OF COANDA BLANKET CURVATURE ON COANDA DEVICE PERFORMANCEICAS2018_0738
Djojodihardjo, H.ASSESSMENT OF THE AERODYNAMICS AND AEROELASTICITY OF FLAPPING WING USING LINEARIZED COMPUTATIONAL METHODICAS2018_0740
Donadon, M.V.STRUCTURAL DAMPING EFFECTS ON THE ACOUSTIC SCATTERING BY ELASTIC PLATESICAS2018_0108
Donadon, M.V.AN ACTIVE-PASSIVE NONLINEAR FINITE ELEMENT MODEL FOR ELECTROMECHANICAL COMPOSITE MORPHING BEAMSICAS2018_0207
Donadon, M.V.MODELLING OF MIXED MODE FATIGUE-INDUCED DELAMINATION IN COMPOSITES: A COMPARATIVE STUDYICAS2018_0519
Donadon, L.V.GROUND VIBRATION TEST USING ACOUSTIC EXCITATION: APPLICATION ON A COMPOSITE WINGICAS2018_0836
Dong, W.CALCULATION OF WATER FILM FLOW AND HEAT TRANSFER ON THE AIRCRAFT ANTI-ICING SURFACEICAS2018_0100
Dong, L.BUCKLING/POSTBUCKLING OPTIMIZATION OF STIFFENED COMPOSITE PANELS BASED ON SENSITIVITY ANALYSISICAS2018_0714
Dotta, F.SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCEICAS2018_0354
Dotta, F.CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHMICAS2018_0355
Draxler, J.COMPARISON OF TWO DIFFERENT INDICATORS FOR HOT CRACKING IN WELDED STRUCTURESICAS2018_0142
Drewiacki, D.THE INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIESICAS2018_0460
Drofelnik, J.ON THE CALIBRATION OF THE INTERMITTENCY TRANSITION TURBULENCE MODEL FOR WIND TURBINE AIRFOIL BY MACHINE LEARNING ALGORITHMICAS2018_0328
Drofelnik, J.WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITYICAS2018_0440
Drofelnik, J.FEASIBILITY OF THE NAVIER-STOKES HARMONIC BALANCE METHOD FOR MODELLING AIRCRAFT UNSTEADY AERODYNAMICSICAS2018_0791
Droney, C.K.SUBSONIC ULTRA-GREEN AIRCRAFT RESEARCH: TRANSONIC TRUSS-BRACED WING TECHNICAL MATURATIONICAS2018_0597
Duan, Z.FEASIBILITY STUDY OF MODIFYING A BASELINE KEROSENE AIRCRAFT TO A LH2 POWERED VERSIONICAS2018_0580
Duarte, R.N.C.EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORSICAS2018_0809
Dubinskii, S.STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATIONICAS2018_0234
Dubovikov, E.A.INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURESICAS2018_0299
Dubovikov, E.NUMERICAL INVESTIGATION OF INFLUENCE OF INITIAL DAMAGES ON STRENGTH PARAMETERS OF CFRPICAS2018_0302
Dugard, L.A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNELICAS2018_0406
Döll, C.HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSIONICAS2018_0492
D´Ippolito, R.MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECTICAS2018_0654
Ebel, T.MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENTICAS2018_0365
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Edberg, J.COMPARISON OF TWO DIFFERENT INDICATORS FOR HOT CRACKING IN WELDED STRUCTURESICAS2018_0142
Eek, M.A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORTICAS2018_0203
Eek, M.PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODELICAS2018_0463
Egorov, I.V.DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATEICAS2018_0691
Eitelberg, G.AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMSICAS2018_0505
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El´Youssef, E.S.MODELLING AND CONTROL OF A BI-TILT-ROTOR UAV WITH DOUBLE GIMBAL AND CAMERA FOR SURVEILLANCE SYSTEMS APPLICATIONICAS2018_0586
Enghardt, L.NOVEL JET ENGINE ACOUSTIC LINER WITH IMPROVED BROADBAND NOISE ABSORPTIONICAS2018_0333
Entezari, M.M.AN EFFICIENT FRAMEWORK FOR AERODYNAMIC CONFIGURATION EVOLUTION OF REENTRY VEHICELESICAS2018_0745
Entzinger, J.O.INDIVIDUALIZING FLIGHT SKILL TRAINING USING SIMULATOR DATA ANALYSIS AND BIOFEEDBACKICAS2018_0220
Entzinger, J.O.DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEMICAS2018_0284
Entzinger, J.O.FAULT-TOLERANT FLIGHT CONTROL SYSTEM WITH SIMPLE ADAPTIVE CONTROL CONSIDERING PILOT INPUTICAS2018_0651
Erhard, R.A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIESICAS2018_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 TMAICAS2018_0063
Eun, Y.INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORTICAS2018_0059
Eun, Y.AIRPORT SURFACE TRAFFIC SCHEDULING WITH CONSIDERATION OF DE-ICING OPERATIONSICAS2018_0211
Evangelista, L.M.C.S.POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATIONICAS2018_0818
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Fan, Z.APPLICATION OF HIGH-ROBUSTNESS BEMT FOR SIMULATION OF UAV-VTOL PROPELLER AT LOW/HIGH ADVANCE RATIOICAS2018_0131
Fang, W.ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLEICAS2018_0222
Fang, F.CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCHICAS2018_0405
Fang, W.STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WINGICAS2018_0526
Faraj, R.HIGH PERFORMANCE PNEUMATIC SHOCK-ABSORBERS FOR AERONAUTICAL APPLICATIONSICAS2018_0344
Fares, E.LATTICE BOLTZMANN HIGH-LIFT SIMULATIONS - A STEP BEYOND CLASSICAL CFDICAS2018_0318
Fateev, V.A.CERTAIN ASPECTS OF FAN MODEL STAGE DESIGNING FOR ADVANCED TURBOFANSICAS2018_0626
Favalli, F.REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANEICAS2018_0432
Feaster, J.BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATIONICAS2018_0661
Fedorov, A.V.DIRECT NUMERICAL SIMULATION OF MACH WAVE INFLUENCE ON LAMINAR-TURBULENT TRANSITION IN SUPERSONIC FLOW OVER A FLAT PLATEICAS2018_0691
Fedotova, K.V.INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELSICAS2018_0645
FEI, Y.APPLICATION RESEARCH OF ZIMMERMAN-WEISSENBURGER-YANG METHOD FOR PREDICTING FLUTTER BOUNDARYICAS2018_0078
Felux, M. FLIGHT TECHNICAL ERROR EVALUATIONS FOR GBAS NAVIGATION REQUIREMENT DEFINITIONICAS2018_0722
Fenelon, F.A.STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARSICAS2018_0573
Feng, Z.ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSIONICAS2018_0389
Fernandez Villace, V.LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMSICAS2018_0425
Fernandez Villace, V.A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLEICAS2018_0429
Ferrara, M.REPLICA 55 PROJECT: AERODYNAMIC AND FEM ANALYSIS OF A WOODEN SEAPLANEICAS2018_0432
Ferrari, F.NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFTSICAS2018_0162
Ferrari, D.B.PROBABILISTIC FORECASTING IN AIRCRAFT EMERGENCY EVACUATION SIMULATIONICAS2018_0202
Ferreira, L.P.S.GROUND VIBRATION TEST USING ACOUSTIC EXCITATION: APPLICATION ON A COMPOSITE WINGICAS2018_0836
Ferretto, D.PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFTICAS2018_0164
Ferretto, D.LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMSICAS2018_0425
Ferretto, D.A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLEICAS2018_0429
Feygenbaum, Y.STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATIONICAS2018_0234
Fichera, S.DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIESICAS2018_0509
Fichert, F.ADAPTING CAPACITY OF AIR NAVIGATION SERVICE PROVISION IN EUROPE - BETWEEN SCYLLA AND CHARYBDISICAS2018_0483
Fields, T.D.FLIGHT PERFORMANCE OF STEERABLE CRUCIFORM PARACHUTE SYSTEMSICAS2018_0614
Figueira, N.SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVSICAS2018_0374
Filatyev, A.S.NEW APPROACH FOR INVESTIGATION OF MAXIMUM-RANGE AIRCRAFT TRAJECTORIESICAS2018_0726
Fioriti, M.PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFTICAS2018_0164
Fioriti, M.INTEGRATION OF ON-BOARD SYSTEMS PRELIMINARY DESIGN DISCIPLINE WITHIN A COLLABORATIVE 3RD GENERATION MDO FRAMEWORKICAS2018_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 JETICAS2018_0655
Fioriti, M.DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORKICAS2018_0674
Fioriti, M.MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECTICAS2018_0783
Fischer, C.IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLEICAS2018_0764
Fisk, N.AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATIONICAS2018_0664
Fokin, D.MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECTICAS2018_0654
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Fonseca, G.C.RESULTS AND COMPARISON OF NUMERICAL SIMULATION AND THE TESTING OF LUG MANUFACTURED BY COMPOSITE MATERIAL BY RTM PROCESSICAS2018_0007
Fonseca, D.A.HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENTICAS2018_0269
Freire, G.A.ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIESICAS2018_0438
Frulla, G.PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROLICAS2018_0430
Frulla, G.REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALSICAS2018_0437
Frulla, G.NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODELICAS2018_0556
Frömming, C.COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNSICAS2018_0708
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Fu, J.POSITION SYNCHRONIZATION OF AEROSPACE ELECTROMECHANICAL ACTUATORS FOR DISTRIBUTED ELECTRICAL ACTUATION SYSTEMICAS2018_0653
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Fujita, K.MONTE-CARLO EVALUATION OF CONTROL LAW FOR HIGH ALTITUDE FLIGHT TEST OF MARS AIRPLANEICAS2018_0431
Fusaro, R.LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMSICAS2018_0425
Fusaro, R.A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLEICAS2018_0429
Gál, I.DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEMICAS2018_0697
Galatolo, R.MULTI-VARIABLE AIRCRAFT DIRECTIONAL CONTROL WITH ANTI-SKID DIFFERENTIAL BRAKESICAS2018_0607
Gamba, G.IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMSICAS2018_0249
Gang, L.KNOWLEDGE ENGINEERING BASED FLIGHT TEST TECHNOLOGY FOR CIVIL AIRCRAFT AIRWORTHINESS CONFORMITYICAS2018_0009
Gao, Z.HSTUDIES ON THE APPLICATION OF MOEA/D TO AERODYNAMIC OPTIMIZATION DESIGNICAS2018_0041
Gao, Z.-H.GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEMICAS2018_0057
Gao, H.-G.GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEMICAS2018_0057
Gao, Z.MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSISICAS2018_0226
Gao, X.HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADESICAS2018_0248
Gao, X.WIND SHEAR PARAMETER ESTIMATION FOR DYNAMIC SOARING WITH UNMANNED AERIAL VEHICLESICAS2018_0464
Gao, B.RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFTICAS2018_0623
García-Fogeda , B.FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONSICAS2018_0286
Gardi, A.HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONSICAS2018_0419
Gardi, A.A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFTICAS2018_0684
Gardi, A.EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORSICAS2018_0694
Garry, K.P.A RAPID AERODYNAMIC PREDICTION METHOD FOR UNCONVENTIONAL TRANSONIC AIRCRAFT CONFIGURATIONSICAS2018_0138
Garry, K.THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENTICAS2018_0297
Gastaldi, A.A.AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORKICAS2018_0675
Gastaldi, A.A.IMPLEMENTATION OF A VORTEX LATTICE METHOD IN A HETEROGENEOUS PROGRAMMING LANGUAGE ENVIRONMENTICAS2018_0846
Gater, B.BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATIONICAS2018_0661
Gatlin, G.M.SUBSONIC ULTRA-GREEN AIRCRAFT RESEARCH: TRANSONIC TRUSS-BRACED WING TECHNICAL MATURATIONICAS2018_0597
Gauci, J.GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESSICAS2018_0182
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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 ARRIVALSICAS2018_0050
Geister, R.IMPACT STUDY ON CYBER THREATS TO GNSS AND FMS SYSTEMSICAS2018_0249
Gennaro, E.M.EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF LAMINAR SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCESICAS2018_0195
Gesell, H.SYSTEM ANALYSIS OF TURBO ELECTRIC AND HYBRID ELECTRIC PROPULSION SYSTEMS ON A REGIONAL AIRCRAFTICAS2018_0831
Geuther, S.A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIESICAS2018_0088
Giarola, R.PROBABILISTIC FORECASTING IN AIRCRAFT EMERGENCY EVACUATION SIMULATIONICAS2018_0202
Gibert, J.-M.NUMERICAL AND EXPERIMENTAL VALIDATION OF UNITIZED BEAM MODELICAS2018_0556
Gillen, S.EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORKICAS2018_0178
Girardi, R.d.M.EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATIONICAS2018_0382
Goes, L.C.S.A BOND GRAPH-ORIENTED METHOD FOR ASSESSMENT OF FAILURES IN AN AIRCRAFT HYDRAULIC BRAKE SYSTEMICAS2018_0551
Góes, L.C.S.IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLEICAS2018_0764
Góes, L.C.S.DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATSICAS2018_0807
Góes, L.C.S.CLOSED-LOOP SYSTEM IDENTIFICATION OF A LARGE FLEXIBLE AIRCRAFT USING SUBSPACE METHODSICAS2018_0813
Goetzendorf-Grabowski, T.MORPHING WING WITH SURFACE DISCONTINUITY - COMPARATIVE TESTSICAS2018_0025
Golberg, F.D.APPLICATION OF "VIRTUAL" CONTROLLERS FOR INTEGRATED PROPULSION AND AIRCRAFT CONTROLICAS2018_0640
Golberg, F.D.IDENTIFICATION METHOD OF THE SIMULATION MODEL "VIRTUAL ENGINE" BUILT INTO THE DIGITAL ENGINE CONTROL SYSTEMICAS2018_0643
Goliszek, B.STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATIONICAS2018_0752
Gollnick, V.IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WINDICAS2018_0619
Gollnick, V.IMPLEMENTATION OF ECO-EFFICIENT PROCEDURES TO MITIGATE THE CLIMATE IMPACT OF NON-CO2 EFFECTSICAS2018_0644
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Gollnick, V.QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNINGICAS2018_0755
Golovanov, V.DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINESICAS2018_0820
Golubev, V.ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAVICAS2018_0254
Golyska, U.DESIGN AND OPTIMIZATION OF A VERSATILE UAV FOR OBSERVATION AND RESEARCH USING THERMAL COLUMNS FOR EXTENDED ENDURANCEICAS2018_0272
Gomes, G.F.A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOTICAS2018_0559
Gomes Olavo, J.L.FIXED-WING UAV ROBUST GUIDANCE STRATEGY BASED ON COMPOUND FLIGHT MISSION OF ON-GROUND TARGETSICAS2018_0396
Gómez Comendador, F.DETECTING HIGH-ALTITUDE ICE CRYSTAL (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATUREICAS2018_0611
Gómez-Escalonilla, J.FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONSICAS2018_0286
Gong, A.FLIGHT TEST OF A FUEL-CELL/BATTERY/SUPERCAPACITOR TRIPLE HYBRID UAV PROPULSION SYSTEMICAS2018_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 STRUCTUREICAS2018_0206
Gonzalez, P.J.IMPLEMENTATION AND FLIGHT TESTING OF AN ENHANCED STABILITY SYSTEM FOR A VERY FLEXIBLE AIRCRAFTICAS2018_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 INTEGRATIONICAS2018_0342
Goraj, Z.-J.STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATIONICAS2018_0752
Gordin, M.V.CHARACTERISTICS OF SYSTEMS WITH ELECTRICALLY DRIVEN UNITS - EXPERIMENTAL STUDIES IN A GAS TURBINE ENGINE DEMONSTRATORICAS2018_0637
Gouskov, O.V.COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODELICAS2018_0672
Granlund, R.DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMSICAS2018_0305
Granzoto, R.M.HORIZONTAL TAIL LOCAL ANGLE-OF-ATTACK AND TOTAL PRESSURE MEASUREMENTS THROUGH STATIC PRESSURE PORTS AND KIEL PITOTICAS2018_0337
Grech, R.GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESSICAS2018_0182
Greco Jr., P.C.DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONESICAS2018_0591
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Grewe, V.COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNSICAS2018_0708
Grigoriev, A.V.AEROELASTIC PROPERTIES OF ACTIVE WINGLETSICAS2018_0276
Grillo, C.RECURSIVE AERODYNAMIC PARAMETER IDENTIFICATION OF A FIGHTER JET FLYING IN TURBULENT AIRICAS2018_0279
Gringinger, E.SEMANTICS-BASED SUMMARIZATION OF ATM DATA TO MANAGE INFORMATION OVERLOAD IN PILOT BRIEFINGSICAS2018_0763
Grüter, B.USING SENSITIVITY PENALTIES TO ROBUSTIFY THE OPTIMAL REENTRY TRAJECTORY OF A HYPERSONIC VEHICLEICAS2018_0564
Grüter, B.NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCINGICAS2018_0782
Grönstedt, T.PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERSICAS2018_0649
Guan, J.WIND TUNNEL VIRTUAL FLIGHT TEST FOR A TRANSPORT AIRCRAFT WITH SIMULATED ICE SHAPEICAS2018_0125
Gubanov, A.A.RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECTICAS2018_0256
Gubanov, A.A.INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECTICAS2018_0508
Gubskiy, V.V.ADAPTIVE WING HIGH-LIFT SYSTEMICAS2018_0371
Guedes, M.J.M.SHIP-HELICOPTER OPERATIONAL LIMITATION ENVELOPE DEFINITION WITH CFD RESULTS AND WIND TUNNEL DATAICAS2018_0345
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Guenov, M.D.COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGNICAS2018_0134
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Guo, B.RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFTICAS2018_0610
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Howarth, D.K.A 7D TRADEICAS2018_0062
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Iijima, T.OPERATIONAL CONCEPT AND VALIDATION OF A NEW AIRPORT LOW-LEVEL WIND INFORMATION SYSTEMICAS2018_0452
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Ivanyushkin, D.S.INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECTICAS2018_0508
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Izuka, J.H. A NUMERICAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTUREICAS2018_0206
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Jeon, D.AIRPORT SURFACE TRAFFIC SCHEDULING WITH CONSIDERATION OF DE-ICING OPERATIONSICAS2018_0211
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Kazarin, P.ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAVICAS2018_0254
Kellermann, H.A COMPOSITE CYCLE ENGINE CONCEPT FOR YEAR 2050ICAS2018_0638
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Khoo, B.C.MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLEICAS2018_0230
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Kim, Y.PERFORMANCE ANALYSIS OF UAV PERSISTENT SURVEILLANCE ALGORITHMICAS2018_0046
Kim, H.INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORTICAS2018_0059
Kim, S.INTEGRATED ARRIVAL AND DEPARTURE MANAGEMENT FOR JEJU INTERNATIONAL AIRPORTICAS2018_0059
Kim, W.B.DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORMICAS2018_0067
Kim, D.W.DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORMICAS2018_0067
Kim, Y.MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMITICAS2018_0080
Kim, J.H.ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTINGICAS2018_0159
Kim, Y.QUASI-LPV MODELING AND PARAMETER-DEPENDENT OPTIMAL CONTROL OF MORPHING WING AIRCRAFTICAS2018_0218
Kim, A.S.INVESTIGATION OF BULGING EFFECTS ON PROPAGATION OF 1-BAY AND 2-BAY LONGITUDINAL CRACKS WITH BROKEN/INTACT STIFFENERICAS2018_0376
Kim, K.H.ANALYSIS OF CHEMICALLY REACTING HYPERSONIC FLOW USING A MESHLESS METHODICAS2018_0525
Kim, H.DEVELOPMENT OF A COMPREHENSIVE ANALYSIS AND OPTIMIZED DESIGN FRAMEWORK FOR THE MULTIROTOR UAVICAS2018_0594
Kirk, J.A VTOL SMALL UNMANNED AIRCRAFT SYSTEM TO EXPAND PAYLOAD CAPABILITIESICAS2018_0088
Klein, C.COUPLING OF PREDESIGN AND PERFORMANCE TOOLS FOR TRANSIENT AIRCRAFT ENGINE ANALYSESICAS2018_0830
Kling, U.A FRAMEWORK FOR UNCONVENTIONAL LANDING GEAR CONFIGURATION MODELLINGICAS2018_0688
Koenig, B.LATTICE BOLTZMANN HIGH-LIFT SIMULATIONS - A STEP BEYOND CLASSICAL CFDICAS2018_0318
Kohmura, A.SIMULATION STUDY FOR VFR AIRCRAFT AND SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) MIXED OPERATIONS IN LOW LEVEL AIRSPACEICAS2018_0636
Kondakov, I.DEVELOPMENT OF STRUCTURE ELEMENTS BASED ON ARCHITECTURED MATERIALS FOR PERSPECTIVE CIVIL AIRCRAFTSICAS2018_0304
Konovalov, V.V.ON EQUIVALENCE OF POLYMER COMPOSITE MATERIALS STRUCTURES LOADING PROGRAMS UNDER FULL-SCALED SERVICE CYCLE TESTINGICAS2018_0185
Koppitz, P.INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONSICAS2018_0043
Koppitz, P.THRUST MODELS BASED ON OPERATIONAL FLIGHT DATA USED IN PARAMETER ESTIMATION FOR SAFETY ANALYSESICAS2018_0314
Koslosky, L.B.AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATIONICAS2018_0664
Koster, J.N.EXPERIENCE WITH INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN EDUCATION: AREND UAVICAS2018_0217
Kota, S.FLEXFLOIL SHAPE ADAPTIVE CONTROL SURFACES-FLIGHT TEST AND NUMERICAL RESULTSICAS2018_0384
Kotsur, O.S.VISCOUS FLUID SIMULATION WITH THE VORTEX ELEMENT METHODICAS2018_0718
Kowalski, R.FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORSICAS2018_0271
Kowalski, M.CONCEPT VALIDATION STUDY FOR FUSELAGE WAKE-FILLING PROPULSION INTEGRATIONICAS2018_0342
Kowalski, M.STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATIONICAS2018_0752
Kowalski, M.ENGINE TEST RESULTS OF FUEL-WATER MICROEMULSIONICAS2018_0769
Kowalski, M.OPTIMIZATION OF THE FUEL INJECTOR TO AN INTERNAL COMBUSTION ENGINE BY MEANS OF LASER EQUIPMENTICAS2018_0825
Kraemer, A.D.DATA-DRIVEN FAILURE IDENTIFICATION USING A MOTION-BASED SIMULATORICAS2018_0581
Krause, C.DEVELOPMENT OF A GENERIC FLIGHT TEST MANEUVER INJECTION MODULEICAS2018_0434
Kreimeier, M.SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITYICAS2018_0727
Krupa, G.P.APPLICATION OF AGILE MODEL-BASED SYSTEMS ENGINEERING IN AIRCRAFT CONCEPTUAL DESIGNICAS2018_0570
Krus, P.A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROLICAS2018_0052
Krus, P.EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROLICAS2018_0200
Krus, P.A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORTICAS2018_0203
Krus, P.DIGITAL HYDRAULICS IN AEROSPACE APPLICATIONS: SLIDING MODE OF QUANTIZED CONTROL AND LMI APPROACHICAS2018_0521
Krus, P.METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHTICAS2018_0663
Krus, P.AIRLINE MAINTENANCE: A PROPOSAL ENVISIONING DIGITAL TRANSFORMATIONICAS2018_0664
Krus, P.INTEGRATED SYSTEM FOR UNIFICATION OF AIRCRAFT CONCEPTUAL DESIGN APPLICATIONSICAS2018_0873
Krutov, A.A.CONTAINERIZED AIR FREIGHT SYSTEM POWERED BY CRYOGENIC FUELICAS2018_0103
Krzysiak, A.EXPERIMENTAL INVESTIGATION OF WING LOAD CONTROL USING FLUIDIC DEVICESICAS2018_0095
Kuerten, J.THRUST MODELS BASED ON OPERATIONAL FLIGHT DATA USED IN PARAMETER ESTIMATION FOR SAFETY ANALYSESICAS2018_0314
Kukshinov, N.V.INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECTICAS2018_0508
Kukshinov, N.V.COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODELICAS2018_0672
Kulhánek, R.EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPSICAS2018_0258
Kurita, J.AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR-SPACE EXPLORATION USING A HIGH ALTITUDE BALLOONICAS2018_0582
Kurka, P.A NUMERICAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTUREICAS2018_0206
Kurka, P.KINEMATICS AND DYNAMICS OF A TENSEGRITY STRUCTURE IN EXPANSIONICAS2018_0329
Kursakov, I.A.PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECTICAS2018_0788
Kuzmin, P.V.MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALLICAS2018_0016
Kuzmin, Y.V.THE NUMERICAL HISTORY OF AIRPLANE MANUFACTURING IN XX CENTURYICAS2018_0705
Kwak, D.PRELIMINARY STUDY OF THE AERODYNAMIC CHARACTERISTICS OF KRUEGER FLAP ON THE SST CONFIGURATIONICAS2018_0098
Kügler, M.E.PLANNING, IMPLEMENTATION, AND EXECUTION OF AN AUTOMATIC FIRST FLIGHT OF A UAVICAS2018_0844
Ladner, R.FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORSICAS2018_0271
Laguardia, J. ERRORS FROM ENGINEERING IN FLIGHT SAFETYICAS2018_0307
Lakemond, N.DIGITAL INNOVATION IN COMPLEX SYSTEMS-MANAGING CRITICAL APPLICATIONS AND GENERATIVITYICAS2018_0867
Lammen, W.F.INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WINGICAS2018_0786
Lammers, K.H.RELEASE OF DYNAMICALLY SCALED OBJECTS FROM A HELICOPTER WIND TUNNEL MODELICAS2018_0064
Landahl, J.MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENTICAS2018_0101
Lanshin, A.I.RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEMICAS2018_0036
Lantto, B.A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROLICAS2018_0052
Lantto, B.EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROLICAS2018_0200
Lanzillotti, A.PRELIMINARY ASSESSMENT OF A WARPING WING CONFIGURATION IN ROLLING CONTROLICAS2018_0430
Lapcevic, V.DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCESICAS2018_0364
Larsson, R.METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHTICAS2018_0663
Lauterjung Q., R.DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONESICAS2018_0591
Lawson, N.J.THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENTICAS2018_0297
Le Blaye, P.LOW LEVEL TRAFFIC MONITORING: RPAS CONCEPT OF OPERATION AND DEVELOPEMENT OF A GROUND BASED SYSTEMICAS2018_0193
Le Tallec, C.LOW LEVEL TRAFFIC MONITORING: RPAS CONCEPT OF OPERATION AND DEVELOPEMENT OF A GROUND BASED SYSTEMICAS2018_0193
Lee, R.SIMULATIONS OF UNSTEADY AIRWAKES BEHIND SHIPS IN MOTIONICAS2018_0038
Lee, S.PERFORMANCE ANALYSIS OF UAV PERSISTENT SURVEILLANCE ALGORITHMICAS2018_0046
Lee, K.W.DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORMICAS2018_0067
Lee, H.S.DEVELOPMENT OF HYBRID GASOLINE-BATTERY PROPULSION SYSTEM FOR MULTI-COPTER PLATFORMICAS2018_0067
Lee, S.MODIFIED COMPOSITE GUIDANCE LAW AGAINST MOVING TARGET CONSIDERING NARROW FIELD-OF-VIEW LIMITICAS2018_0080
Lee, Y.B.ADAPTIVE DESIGN OF EXPERIMENT BASED ON GAUSSIAN PROCESS MODELS WITH NONSTATIONARY KERNEL APPLIED TO WIND TUNNEL TESTINGICAS2018_0159
Lee, J.QUASI-LPV MODELING AND PARAMETER-DEPENDENT OPTIMAL CONTROL OF MORPHING WING AIRCRAFTICAS2018_0218
Lee, S.MODELLING OF FLUTTER CHARACTERISTICS OF AIRCRAFT WING WITH PYLON-MOUNTED ENGINE NACELLEICAS2018_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 JETICAS2018_0311
Lee, J. FLIGHT TECHNICAL ERROR EVALUATIONS FOR GBAS NAVIGATION REQUIREMENT DEFINITIONICAS2018_0722
Leite, H.F.TIME-RESOLVED PRESSURE MEASUREMENTS FOR AN AIRFOIL WITH SELF-SUSTAINED SHOCK OSCILATIONSICAS2018_0599
Lemmens, Y.AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATIONICAS2018_0133
Leng, Y.ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLEICAS2018_0039
Levin, V.STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPYICAS2018_0308
Li, X.CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF "PARASITE" NOISEICAS2018_0116
Li, X.P.IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BEDICAS2018_0119
Li, R.Z.MULTI-POINT AERODYNAMIC OPTIMIZATION DESIGN OF A DUAL-AISLE AIRPLANE WINGICAS2018_0154
Li, P.THE EFFECT OF STRUCTURAL PARAMETERS OF AIRCRAFT PANEL ON VIBRATION FATIGUE LIFEICAS2018_0281
Li, Y.-H.MULTI-CHANNEL HUMAN-MACHINE INTERACTIVE SYSTEM FOR MULTIPLE UAVS' CONTROLICAS2018_0348
Li, Q.AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF SWIRL RECOVERY VANES FOR PROPELLER PROPULSION SYSTEMSICAS2018_0505
Li, Z.RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFTICAS2018_0610
Li, Z.RESERCH ON KEY TECHNOLOGY OF INTELLIGENT CIVIL AIRCRAFTICAS2018_0623
Liaboeuf, R.HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSIONICAS2018_0492
Liang, X.THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVERICAS2018_0470
Lieu, W.DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPTICAS2018_0875
Lim, Y.HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONSICAS2018_0419
Lim, D.DEVELOPMENT OF A COMPREHENSIVE ANALYSIS AND OPTIMIZED DESIGN FRAMEWORK FOR THE MULTIROTOR UAVICAS2018_0594
Lim, Y.A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFTICAS2018_0684
Lim, Y.EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORSICAS2018_0694
Lin, Y.-F.ANALYSIS OF XH-59A ROTOR IN FORWARD FIGHT WITH HIGH EFFICIENCY TRIM METHODICAS2018_0469
Lin, Y.-F.THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVERICAS2018_0470
Linke, F.THE GLOBAL FUEL SAVING POTENTIAL OF INTERMEDIATE STOP OPERATIONS CONSIDERING METEOROLOGICAL AND OPERATIONAL INFLUENCESICAS2018_0021
Linn, R.V.LARGE EDDY SIMULATION OF A TRANSIENT SPOILER DEPLOYMENT IN A NACA0012 PROFILE IN SUBSONIC AND TRANSONIC SPEEDSICAS2018_0503
Liorbano, F.F.INFLUENCE OF AIRFRAME STIFFNESS ON THE AERODYNAMIC COEFFICIENTS OF A HIGH ASPECT RATIO WINGICAS2018_0776
Litao, F.RLG BASED REAL-TIME MODEL ATTITUDE DETERMINATION SYSTEM DEVELOPMENT FOR LARGE LOW SPEED FACILITY OF CARDCICAS2018_0317
Liu, K.NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON SUPERCRITICAL WING AERODYNAMIC LOADSICAS2018_0001
Liu, N.A ROBUST STABLE PI CONTROLLER DESIGN IN TIME-FREQUENCY DUAL DOMAINS FOR AIRCRAFT ENGINEICAS2018_0027
Liu, Z.ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLEICAS2018_0039
Liu, H.PREDICTING LOW-VELOCITY IMPACT DAMAGE IN COMPOSITE USING COHESIVE ELEMENTICAS2018_0049
Liu, P.IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BEDICAS2018_0119
Liu, P.Q.HIGH LIFT MECHANISM OF A 2D FLAPPING WING IN HOVERING FLIGHTICAS2018_0151
Liu, X.NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFTSICAS2018_0162
Liu, P.MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSISICAS2018_0226
Liu, Z.B.AERODYNAMIC DESIGN OF KEY COMPONENTS OF THE LARGE-DISCHARGE AXIAL FAN AT HIGH ALTITUDEICAS2018_0243
Liu, H.STUDY ON EVALUATION METHODS OF UNDERGRADUATE AIRCRAFT OVERALL DESIGN COURSE BASED ON TEAM DESIGN COMPETITIONICAS2018_0250
Liu, C.-M.HIGH SPEED DRAG REDUCTION OPTIMIZATION FOR PROJECTILESICAS2018_0270
Liu, Z.A RESEARCH OF MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM FOR FIGHT VEHICLE DESIGNICAS2018_0443
Liu, D.WIND SHEAR PARAMETER ESTIMATION FOR DYNAMIC SOARING WITH UNMANNED AERIAL VEHICLESICAS2018_0464
Liu, Z.OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDCICAS2018_0750
Lombardi, R.MULTIOBJECTIVE MULTIPARAMETRIC OPTIMIZATION OF PROPULSION SYSTEM FOR ADVANCED CIVIL AIRCRAFT IN DISTRIBUTED ENVIRONMENT OF COLLABORATIVE MDO SYSTEM DEVELOPED IN AGILE PROJECTICAS2018_0654
London, P.A CASE OF SUCESS: MDO APPLIED ON THE DEVELOPMENT OF EMBRAER 175 ENHANCED WINGTIPICAS2018_0034
López Sánchez, C.HURRICANE-CS: CONTROL SURFACES AND HIGH LIFT DEVICES MODELING AND SIZING PROGRAMICAS2018_0627
Lozowski, E.NUMERICAL SIMULATION OF ICE ACCRETION INFLUENCED BY AN ANTI-ICING HEATING SYSTEMICAS2018_0620
Lu, G.THE TECHNIQUE AND MODELLING FOR EQUIPMENT MAINTAINABILITY QUANTIFICATION IN 3D DIGITAL AIRCRAFT DESIGN CONDITIONICAS2018_0055
Lucchi, F.DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACHICAS2018_0774
Lucchi, F.PRELIMINARY DESIGN OF A LONG RANGE WINDOWLESS AIRCRAFT CONCEPTICAS2018_0777
Ludwig, T.PERFORMANCE COMPARISON OF A320 AND 737NG REGARDING THE VERTICAL AND AND SPEED PROFILES IN ADVANCED RNP TO XLS ARRIVALSICAS2018_0050
Lundbladh, A.PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERSICAS2018_0649
Lundström, D.METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHTICAS2018_0663
Lückhof, J.SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITYICAS2018_0727
Lührs, B.IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WINDICAS2018_0619
Lührs, B.IMPLEMENTATION OF ECO-EFFICIENT PROCEDURES TO MITIGATE THE CLIMATE IMPACT OF NON-CO2 EFFECTSICAS2018_0644
Lührs, B.COST-BENEFIT ASSESSMENT OF CLIMATE AND WEATHER OPTIMIZED TRAJECTORIES FOR DIFFERENT NORTH ATLANTIC WEATHER PATTERNSICAS2018_0708
Lührs, B.QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNINGICAS2018_0755
Lysenkov, A.V.PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECTICAS2018_0788
Lööf, J.MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENTICAS2018_0101
Ma, H.AERODYNAMIC ANALYSIS AND CONTROL ALLOCATION FOR ASYMMETRIC VARIABLE SWEEP AIRCRAFT WITH FLEXIBLE TRAILING EDGEICAS2018_0210
Ma, H.ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLEICAS2018_0222
Ma, C.NUMERICAL STUDY OF VARIABLE CAMBER WING EFFECT ON AERODYNAMIC PERFORMANCE FOR LONG RANGE CIVIL AIRCRAFTICAS2018_0231
Ma, J.THE EFFECT OF STRUCTURAL PARAMETERS OF AIRCRAFT PANEL ON VIBRATION FATIGUE LIFEICAS2018_0281
Ma, H.CFD-BASED STUDY OF DAMAGE LOCATION INFLUENCE ON AERODYNAMICS OF WINGS WITH SINGLE AND DOUBLE THROUGH HOLESICAS2018_0294
Ma, B.H.SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLEICAS2018_0306
Ma, H.STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WINGICAS2018_0526
Machini, F.MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTORICAS2018_0533
MacKunis, W.ON WAKE VORTEX SAFETY ANALYSIS AND CONTROL FOR UAVICAS2018_0254
MacNeill, R.PROPELLER OPTIMISATION FOR AN ELECTRICAL-POWERED TACTICAL UASICAS2018_0404
Madrid, J.MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENTICAS2018_0101
Magerramova, L.A.APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADESICAS2018_0173
Magerramova, L.DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINESICAS2018_0820
Maia Neto, M.A BOND GRAPH-ORIENTED METHOD FOR ASSESSMENT OF FAILURES IN AN AIRCRAFT HYDRAULIC BRAKE SYSTEMICAS2018_0551
Maierl, R.AERO-STRUCTURAL OPTIMIZATION OF A MALE CONFIGURATION IN THE AGILE MDO FRAMEWORKICAS2018_0675
Manfriani, L.NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFTSICAS2018_0162
Mani, M.CFD VERIFICATION AND VALIDATION FOR INDUSTRIAL APPLICATIONSICAS2018_0857
Manzanares-Filho, N.COMPARISON AND APPLICATION OF DIFFERENTS TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMIC WING DESIGNICAS2018_0527
Marczak, R.J.OPTIMAL SHAPE OF REPAIR PATCHES IN COMPOSITESICAS2018_0471
Mare, J.-C.POSITION SYNCHRONIZATION OF AEROSPACE ELECTROMECHANICAL ACTUATORS FOR DISTRIBUTED ELECTRICAL ACTUATION SYSTEMICAS2018_0653
Mareskin, I.V.INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURESICAS2018_0299
Mareskin, I.DEVELOPMENT OF STRUCTURE ELEMENTS BASED ON ARCHITECTURED MATERIALS FOR PERSPECTIVE CIVIL AIRCRAFTSICAS2018_0304
Marinkovski, D.DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCESICAS2018_0364
Marks, T.IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WINDICAS2018_0619
Marks, T.QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNINGICAS2018_0755
Martinez R. Jr., B.DESIGN OF AN INSTRUMENTED STATOR VANE FOR UNSTEADY PRESSURE MEASUREMENTS USING MEMS MICROPHONESICAS2018_0591
Martini, E.ACOUSTIC MODES AND GLOBAL INSTABILITIES IN WAKES AND JETSICAS2018_0450
Martins, J.R.R.A.FLEXFLOIL SHAPE ADAPTIVE CONTROL SURFACES-FLIGHT TEST AND NUMERICAL RESULTSICAS2018_0384
Martins, J.S.STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWSICAS2018_0482
Martins, R.S.STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARSICAS2018_0573
Martins, R.STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODSICAS2018_0579
Martins, R.S.FASTENING ANALYSIS USING LOW FIDELITY FINITE ELEMENT MODELSICAS2018_0659
Marzocca, P.BIMODAL UNMANNED VEHICLE: PROPULSION SYSTEM INTEGRATION AND WATER/AIR INTERFACE TESTINGICAS2018_0660
Mascia, E.-K.AERODYNAMIC EVALUATION OF THE EXTERNAL FLOW OVER PICKUP TRUCKSICAS2018_0201
Mastellone, A.NUMERICAL ANALYSIS OF THE FLOW AROUND A BACKWARD-FACING RAMPICAS2018_0622
Matayoshi, N.DEVELOPMENT AND FLIGHT DEMONSTRATION OF A NEW LIDAR-BASED ONBOARD TURBULENCE INFORMATION SYSTEMICAS2018_0284
Matayoshi, N.OPERATIONAL CONCEPT AND VALIDATION OF A NEW AIRPORT LOW-LEVEL WIND INFORMATION SYSTEMICAS2018_0452
Matheus, A.C.A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTSICAS2018_0309
Matheus, A.EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONSICAS2018_0402
Mattei, A.-P.SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVSICAS2018_0374
Mavris, D.N.UTILIZATION OF SCALING LAWS AND UNCERTAINTY QUANTIFICATION TO INFORM TECHNOLOGY DEVELOPMENT EXPERIMENTATIONICAS2018_0183
Mavris, D.N.AN APPROACH TO ASSESS AIRFRAME WEIGHT REDUCTION PERFORMANCE OF STITCHED COMPOSITE TECHNOLOGIESICAS2018_0793
Mavris, D.ENABLING THE DIGITAL FACTORY THROUGH THE INTEGRATION OF DATA-DRIVEN AND SIMULATION MODELSICAS2018_0850
Mavris, D.ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACHICAS2018_0851
Mavris, D.N.FORMULATION AND IMPLEMENTATION OF A METHOD FOR TECHNOLOGY EVALUATION OF SYSTEM OF SYSTEMSICAS2018_0862
Mašek, J.THERMO-VACUUM TEST CHAMBER DEVELOPMENT FOR AIRBORNE AND SPACE EQUIPMENT TESTING IN SIMULATED EXTREME CONDITIONSICAS2018_0548
Medeiros, R.R.NONLINEAR AEROELASTIC REDUCED ORDER MODELS USING MODAL COORDINATESICAS2018_0262
Mei, Y.IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BEDICAS2018_0119
Meilong, L.CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORKICAS2018_0268
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Pigusov, E.CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANEICAS2018_0104
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Piprek, P.BI-LEVEL TRAJECTORY OPTIMIZATION BY STOCHASTIC COLLOCATION FOR UNCERTAINTY INTERVAL CALCULATIONICAS2018_0221
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Piprek, P.NONLINEAR MODEL PREDICTIVE CONTROL FOR OPTIMAL AIRCRAFT SEQUENCINGICAS2018_0782
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Polivanov, P.A.EFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AIROFOILICAS2018_0152
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Potapchik, A.V.ADAPTIVE WING HIGH-LIFT SYSTEMICAS2018_0371
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Prado, G.O.C.SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCEICAS2018_0354
Prado, G.O.CCORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHMICAS2018_0355
Prado, G.O.C.SHM WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCEICAS2018_0357
Prakasha, P.S.MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERINGICAS2018_0633
Prakasha, P.S.MULTIDISCIPLINARY DESIGN ANALYSIS OF BLENDED WING BODY THROUGH COLLABORATIVE DESIGN APPROACH: AGILE EU PROJECTICAS2018_0783
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Prakasha, P.S.PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECTICAS2018_0788
Premlal, N.EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORSICAS2018_0694
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Prince, S.THE INFLUENCE OF HIGH-SPEED SPIV DATA PROCESSING PARAMETERS ON AIRCRAFT WING VORTEX WAKE ASSESSMENTICAS2018_0297
Prokhorov, A.N.INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECTICAS2018_0508
Prokhorov, A.N.GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORSICAS2018_0628
Prokhorov, A.N.INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELSICAS2018_0645
Prokhorov, A.N.COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODELICAS2018_0672
Pushchin, N.A.THE STUDIES ON LOW-NOISE LAMINAR WING REGIONAL AIRCRAFTICAS2018_0747
Pölzlbauer, P.PERFORMANCE IMPROVEMENT OF A COMPOUND HELICOPTER ROTOR HEAD BY AERODYNAMIC SHAPE OPTIMIZATIONICAS2018_0070
Qi, S.-J.HUMAN FACTOR IN UNMANNED AIRCRAFT SYSTEM FLIGHT TESTICAS2018_0072
Qian, G.NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON SUPERCRITICAL WING AERODYNAMIC LOADSICAS2018_0001
Qian, Z.ENGINE EXHAUST NOZZLE PLUME EFFECTS ON THE SONIC BOOM FOR A TYPE OF HYPERSONIC LONG-RANGE CIVIL VEHICLEICAS2018_0039
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Qian, W.AEROELASTIC WIND TUNNEL EXPERIMENT OF A HIGH-ASPECT-RATIO WING MODEL AGAINST GEOMETRICAL NON-LINEARITYICAS2018_0720
Qian, W.EXPERIMENTAL AND NUMERICAL STUDIES OF FLUTTER CHARACTERISTICS OF AN ALL-MOVING CONTROL SURFACE AGAINST GAP EFFECTSICAS2018_0784
Qin, J.HIGH FREQUENCY MODAL TEST AND DYNAMIC PERFORMANCE EVALUATION OF TURBINE ROTOR BLADESICAS2018_0248
Qiu, Z.AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROLICAS2018_0129
Qiu, T.SIMULTANEOUS MEASUREMENTS OF TEMPERATURE AND HEAT FLUX IN SUPERSONIC COMBUSTOR BY ITO THIN FILM THERMOCOUPLEICAS2018_0306
Qiu, X.CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCHICAS2018_0405
Qu, Q.L.HIGH LIFT MECHANISM OF A 2D FLAPPING WING IN HOVERING FLIGHTICAS2018_0151
Queiroz, R.STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODSICAS2018_0579
Quirino, M.U.ANALYSIS OF THE INFLUENCE OF THE EXTERNAL CONFIGURATION ON THE WAVE DRAG OFSUPERSONIC BUSINESS JETSICAS2018_0030
Raabe, C.T.AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEMICAS2018_0219
Radchenko, V.N.PARTICLE IMAGE SURFACE FLOW VISUALIZATION AND SKIN-FRICTION MEASUREMENTICAS2018_0068
Radchenko, V.N.EFFECT OF CONTROLLED PERIODIC ROUGHNESS ON GOERTLER VORTICES IN HYPERSONIC COMPRESSION RAMP FLOWICAS2018_0690
Rade, D.A.DESIGN OF A RECEPTANCE-BASED ACTIVE AEROELASTIC CONTROLLER IN THE PRESENCE OF PARAMETRIC UNCERTAINTIESICAS2018_0509
Rafael, C.F.SHIP-HELICOPTER OPERATIONAL LIMITATION ENVELOPE DEFINITION WITH CFD RESULTS AND WIND TUNNEL DATAICAS2018_0345
Rajpal, D.DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORKICAS2018_0674
Rajpal, D.INCLUDING AEROELASTIC TAILORING IN THE CONCEPTUAL DESIGN PROCESS OF A COMPOSITE STRUT BASED WINGICAS2018_0786
Ramamurthy, A.ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACHICAS2018_0851
Ramesh, K.NUMERICAL DEVELOPMENT OF UNSTEADY VORTEX-LATTICE METHOD EXPANSION FOR LEADING-EDGE SHEDDING PREDICTION WITH EXPERIMENTAL VALIDATIONICAS2018_0550
Ramos, A.C.B.SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTIONICAS2018_0066
Ranasinghe, K.HUMAN-MACHINE INTERFACES AND INTERACTIONS FOR MULTI UAS OPERATIONSICAS2018_0419
Razaboni, P.M.UNIVERSAL DESIGN FOR AIRCRAFT SAFETYICAS2018_0378
Razaboni, P.M.CREW TRAINING USING ANIMATIONICAS2018_0380
Reed, H.L.IONIZATION AND DISSOCIATION EFFECTS ON HYPERSONIC BOUNDARY-LAYER STABILITYICAS2018_0837
Reiser, C.HUMAN RELIABILITY ANALYSIS IN AN AIRCRAFT DECOMPRESSION EVENTICAS2018_0269
Reitenbach, S.COUPLING OF PREDESIGN AND PERFORMANCE TOOLS FOR TRANSIENT AIRCRAFT ENGINE ANALYSESICAS2018_0830
Ren, J.VISUAL FLIGHT PROCEDURE DESIGN IN CHINAICAS2018_0282
Riaz, A.AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACEICAS2018_0132
Riaz, A.COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGNICAS2018_0134
Ribeiro, M.L.AN XFEM FRAMEWORK FOR ONSET AND CRACK PROPAGATION FOR COMPOSITES BASED ON ACTION PLANE THEORYICAS2018_0502
Ribeiro, L.J.STAMP METHOD APPLICATION ON INDUSTRIAL MANAGEMENTICAS2018_0553
Ribeiro, L.C.DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONSICAS2018_0609
Ribeiro, M.V.POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATIONICAS2018_0818
Rice, T.ADDRESSING TECHNICAL AND REGULATORY REQUIREMENTS TO DEPLOY STRUCTURAL HEALTH MONITORING SYSTEMS ON COMMERCIAL AIRCRAFTICAS2018_0109
Rice, T.SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCEICAS2018_0354
Ridel, M.HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSIONICAS2018_0492
Ridgway, G.R.BEYOND BEDFORD - DEVELOPMENT OF A TWO-DIMENSIONAL PILOT WORKLOAD RATING SCALEICAS2018_0699
Riedel, T.A NOVEL CONTROL APPROACH TO IMPROVE SPEED COMMANDS AND PILOT WORKLOAD FOR FLIGHT-DECK BASED INTERVAL MANAGEMENTICAS2018_0174
Ritt, S.STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATIONICAS2018_0852
Rivero, I.FATIGUE AND CRACK PROPAGATION LIFE IMPROVEMENT QUANTIFICATION FOR COLD-WORKED HOLES OUTSIDE NOMINAL CONDITIONSICAS2018_0286
Rizzi, F.REPLICA 55 PROJECT: A WOOD SEAPLANE IN THE ERA OF COMPOSITE MATERIALSICAS2018_0437
Roach, D.ADDRESSING TECHNICAL AND REGULATORY REQUIREMENTS TO DEPLOY STRUCTURAL HEALTH MONITORING SYSTEMS ON COMMERCIAL AIRCRAFTICAS2018_0109
Roach, D.SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCEICAS2018_0354
Roberts, T.DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPTICAS2018_0875
Rocamora, B.M. PARAMETRIC INVESTIGATION OF EESC-USP AEROACOUSTIC FAN RIGICAS2018_0147
Rocha, G.C.A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTSICAS2018_0309
Rocha, G.EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONSICAS2018_0402
Rodamilans, G.B.CHARACTERISTIC HELICOPTER FLIGHT MECHANICS AND MOTION CUEING INTEGRATION INTO THE SIVOR ROBOTIC FLIGHT SIMULATOR: AN OBJECTIVE APPROACHICAS2018_0506
Rodriguez, D.EFFECTS OF THE INTRINSIC THREE-DIMENSIONALIZATION OF LAMINAR SEPARATION BUBBLES ON THE AMPLIFICATION OF EXTERNAL DISTURBANCESICAS2018_0195
Rodriguez, M.A.EFFECTS OF TAILORED CONTROL SURFACE COMPLIANCE ON AIRCRAFT STABILITY AND CONTROLICAS2018_0200
Rodríguez, M.EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONSICAS2018_0402
Rodríguez-Sanz, A.DETECTING HIGH-ALTITUDE ICE CRYSTAL (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATUREICAS2018_0611
Rogalski, T.APPLICATION OF THE DISTURBANCE VALUE MEASURED DURING THE REAL FLIGHT TO THE FLIGHT CONTROL SYSTEM SYNTHESISICAS2018_0613
Rohács, D.DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEMICAS2018_0697
Rohács, J.DEVELOPING THE UNMANNED UNCONVENTIONAL CARGO AIRPLANES WITH HYBRID PROPULSION SYSTEMICAS2018_0697
Rohacs, J.LOAD MONITORING FOR OPERATORS’ LOAD MANAGEMENTICAS2018_0698
Rohacs, D.LOAD MONITORING FOR OPERATORS’ LOAD MANAGEMENTICAS2018_0698
Romanenko, N.E.APPLICATION OF "VIRTUAL" CONTROLLERS FOR INTEGRATED PROPULSION AND AIRCRAFT CONTROLICAS2018_0640
Romani de Oliveira, I.A METHOD FOR ESTIMATING THE PROBABILITY OF RARE ACCIDENTS IN COMPLEX SYSTEMSICAS2018_0849
Rothfeld, R.EVALUATION OF THE POTENTIAL IMPACTS OF HYBRID-ELECTRIC AIRCRAFT ON THE GLOBAL AIR TRANSPORTATION NETWORKICAS2018_0178
Rothfeld, R.A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR VEHICLE CONCEPTS FOR URBAN AIR MOBILITYICAS2018_0794
Rottach, M.FORCE FIGHT COMPENSATION FOR REDUNDANT ELECTRO-MECHANICAL FLIGHT CONTROL ACTUATORSICAS2018_0271
Rudinsky, A.V.COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODELICAS2018_0672
Rulli, R.P.SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCEICAS2018_0354
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Rößler, C.DEVELOPMENT AND PERFORMANCE COMPARISON OF OPTIMIZED ELECTRIC FIXED-WING VTOL UAV CONFIGURATIONSICAS2018_0169
Rößler, C.ELECTRIC VTOL UAV CONFIGURATION STUDIES AND OPTIMIZATION WITHIN AIRCRAFT DESIGN PRACTICAL COURSE AT TECHNICAL UNIVERSITY OF MUNICHICAS2018_0240
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Sabatini, R.A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFTICAS2018_0684
Sabatini, R.EULERIAN OPTIMAL CONTROL FORMULATION FOR DYNAMIC MORPHING OF AIRSPACE SECTORSICAS2018_0694
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Sanches, A.C.DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATIONICAS2018_0569
Sánchez Ayra, E.DETECTING HIGH-ALTITUDE ICE CRYSTAL (HAIC) ICING EVENTS FROM TOTAL AIR TEMPERATUREICAS2018_0611
Sánchez Franco, D.HURRICANE-CS: CONTROL SURFACES AND HIGH LIFT DEVICES MODELING AND SIZING PROGRAMICAS2018_0627
Sandhu, R.GLOBAL SENSITIVITY ANALYSIS OF TRANSONIC FLUTTER USING A COUPLED CFD-CSD SOLVERICAS2018_0037
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Santiago, M.S.SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTIONICAS2018_0066
Santos, L.C.de C.PROBABILISTIC FORECASTING IN AIRCRAFT EMERGENCY EVACUATION SIMULATIONICAS2018_0202
Santos, L.C.C.EFFECTS OF NUMERICAL MODELING CHOICES FOR HEATED JETS IN CROSS FLOWICAS2018_0369
Santos, M.T.FASTENING ANALYSIS USING LOW FIDELITY FINITE ELEMENT MODELSICAS2018_0659
Santos, J.S.DEVELOPMENT OF A NOVEL AERIAL PLATFORM WHICH MERGES THE CONCEPT OF AIRSHIPS AND TETHERED AEROSTATSICAS2018_0807
Santos de Brito Alves, L.ON THE EXISTENCE OF MULTIPLE SELF-EXCITATION FREQUENCIES IN THE INSTABILITY OF INTERACTING PLANAR MIXING LAYER AND WAKEICAS2018_0537
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Saqui-Sannes, P.SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVSICAS2018_0374
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Sartorius, S.A TECHNIQUE FOR CAPTURING STAKEHOLDER PREFERENCES AND KNOWLEDGE IN EARLY DESIGN STUDIESICAS2018_0208
Sasaki, K.FLIGHT DEMONSTRATION OF A LONG RANGE ONBOARD DOPPLER LIDARICAS2018_0121
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Sasaki, K.CONTROL OF STREAKY DISTURBANCES IN THE BOUNDARY LAYER OVER A FLAT PLATEICAS2018_0473
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Schlatter, P.WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOILICAS2018_0388
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Schminder, J.PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODELICAS2018_0463
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Schneider, M.STRUCTURAL DESIGN AND TESTING OF A TAILORED SKIN SINGLE DUCT (TSSD) FIN APPLICATIONICAS2018_0852
Scholz, M.LNAS - A PILOT ASSISTANCE SYSTEM FOR LOW-NOISE APPROACHES WITH MINIMAL FUEL CONSUMPTIONICAS2018_0096
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Schultz, M.AIRCRAFT BOARDING AS PART OF AN EFFICIENT 4D TRAJECTORYICAS2018_0487
Schwartz, K.G.UTILIZATION OF SCALING LAWS AND UNCERTAINTY QUANTIFICATION TO INFORM TECHNOLOGY DEVELOPMENT EXPERIMENTATIONICAS2018_0183
Schwinn, D.B.STRUCTURAL SIZING OF A ROTORCRAFT FUSELAGE USING AN INTEGRATED DESIGN APPROACHICAS2018_0082
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Seitz, A.A COMPOSITE CYCLE ENGINE CONCEPT FOR YEAR 2050ICAS2018_0638
Seitz, A.STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATIONICAS2018_0752
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Seki, S.PASSIVE VENTILATION FLOW CONTROL FOR AIRCRAFT GUST LOAD ALLEVIATIONICAS2018_0736
Semenev, P.A.NUMERICAL SIMULATION OF OPERATING PROCESS ELEMENTS FOR COMBUSTION CHAMBERS OF PERSPECTIVE GTEICAS2018_0737
Semenov, V.L.GROUND FACILITY TESTS OF HIGH SPEED RAMJET DEMONSTRATORSICAS2018_0628
Sename, O.A LOW COST MODEL AIRCRAFT FLIGHT RESEARCH FACILITY IN WIND TUNNELICAS2018_0406
Senik, V.STUDY OF ACCIDENTAL IMPACT SCENARIOS FOR COMPOSITE WING DAMAGE TOLERANCE EVALUATIONICAS2018_0234
Seren, T.DEVELOPMENT AND PERFORMANCE COMPARISON OF OPTIMIZED ELECTRIC FIXED-WING VTOL UAV CONFIGURATIONSICAS2018_0169
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Shanygin, A.N.INVESTIGATION OF SYNERGETIC EFFECT INFLUENCE ON STRENGTH CHARACTERISTICS AND WEIGHT EFFICIENCY OF LOAD-BEARING AVIATION STRUCTURESICAS2018_0299
Shanygin, A.STUDY OF EXTERNAL FACTOR COMBINATIONS EFFECT ON CFRP STRUCTURE UTILYZING ULTRASONIC MICROSCOPYICAS2018_0308
Sharma, S.AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACEICAS2018_0132
Shattock, H.R.BEYOND BEDFORD - DEVELOPMENT OF A TWO-DIMENSIONAL PILOT WORKLOAD RATING SCALEICAS2018_0699
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Shcherbakova, E.V.THE INFLUENCE OF THE SHAPE OF THE COOLING CHANNEL AND PRESSURE GRADIENT ON THE EFFICIENCY OF FILM COOLING OF GTE BLADESICAS2018_0629
Shelyukhin, Y.F.MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALLICAS2018_0016
Shi, L.AN AIRBORNE DATA BUS NETWORK SYSTEM OF INTERFACE ADAPTIVE AND FLEXIBLE CONTROLICAS2018_0129
Shiguemori, E.H.SOLAR-POWERED UAV PLATFORM SYSTEM: A CASE STUDY FOR GROUND CHANGE DETECTIONICAS2018_0066
Shikhman, Y.M.RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEMICAS2018_0036
Shim, G.J.COST-EFFECTIVE TELEMETRY, TRACKING AND COMMAND SYSTEM DEVELOPMENT FOR HIGH-ALTITUDE SCIENTIFIC BALLOONICAS2018_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 PRODUCTSICAS2018_0012
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Si, J.NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON SUPERCRITICAL WING AERODYNAMIC LOADSICAS2018_0001
Si, J.NUMERICAL ANALYSIS OF BLEND-WING-BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCEICAS2018_0326
Sidorenko, A.A.EFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AIROFOILICAS2018_0152
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Silberhorn, D.COLLABORATIVE CONCEPTUAL DESIGN OF A MID-RANGE AIRCRAFT UNDER CONSIDERATION OF ADVANCED METHODS FOR TECHNOLOGY ASSESSMENICAS2018_0167
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Silva, P.A.SHM WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCEICAS2018_0357
Silva, O.F.R.MATCHING BETWEEN METAMODEL AND OPTIMIZATION TOOL APPLIED IN A MULTISTAGE AXIAL-FLOW COMPRESSOR AIMING DESIGN IMPROVEMENTICAS2018_0365
Silva, T.M.P.EFFECTS OF NONLINEAR ENERGY SINK ON THE AEROELASTIC BEHAVIOR OF AN ELECTROMECHANICALLY COUPLED TYPICAL SECTIONICAS2018_0391
Silva, G.G.UAV INITIAL PARAMETER ESTIMATIONICAS2018_0568
Silva, C.R.I.PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERSICAS2018_0649
Silva, R.G.A.IDENTIFICATION OF THE LATERAL-DIRECTIONAL MODEL OF THE VECTOR-P, UNMANNED AERIAL VEHICLEICAS2018_0764
Silva, R.G.INCREASED FLUTTER VELOCITY WITH USE OF A PASSIVE CONTROL SYSTEMICAS2018_0800
Silva, R.G.A.EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORSICAS2018_0809
Silva Neto, O.T.EXPERIMENTAL STUDY OF AEROELASTIC RESPONSE OF A FLEXIBLE HIGH ASPECT RATIO WING WITH PASSIVE SMA ACTUATORSICAS2018_0809
Silvestre, F.J.ACTUATOR AND SENSOR PLACEMENT FOR CLOSED-LOOP CONTROL OF CONVECTIVE INSTABILITIESICAS2018_0438
Silvestre, F.J.THE INFLUENCE OF BIODYNAMIC FEEDTHROUGH ON HANDLING QUALITIESICAS2018_0460
Silvestre, F.J.STRAIN GAGES FULL BRIDGE INSIDE COMPOSITE LAYERS TARGETING WING SHAPE FEEDBACK FOR FLIGHT CONTROL LAWSICAS2018_0482
Silvestre, F.J.CONTROL OF A VERY FLEXIBLE WING WITH SIMULTANEOUS OPTIMIZATION OF THE GAIN MATRIX AND THE SPATIAL DISTRIBUTION OF THE SENSORSICAS2018_0500
Silvestre, F.J.ON REAL–TIME SIMULATION OF FLEXIBLE AIRCRAFT WITH PHYSICS–DERIVED MODELSICAS2018_0501
Silvestre, F.J.APPLICABILITY OF GEOMETRICALLY-LINEAR STRUCTURAL-DYNAMIC MODELS FOR THE FLIGHT DYNAMICS OF ARBITRARILY-FLEXIBLE AIRCRAFTICAS2018_0523
Silvestre, F.J.ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFTICAS2018_0529
Silvestre, F.J.IMPLEMENTATION AND FLIGHT TESTING OF AN ENHANCED STABILITY SYSTEM FOR A VERY FLEXIBLE AIRCRAFTICAS2018_0534
Silvestre, F.NUMERICAL DEVELOPMENT OF UNSTEADY VORTEX-LATTICE METHOD EXPANSION FOR LEADING-EDGE SHEDDING PREDICTION WITH EXPERIMENTAL VALIDATIONICAS2018_0550
Silvestre, F.J.DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATIONICAS2018_0569
Silvestre, F.J.A STRATEGY FOR UAV PERFORMANCE ENHANCEMENT THROUGH ATMOSPHERIC ENERGY EXTRACTION USING MPC TECHNIQUESICAS2018_0840
Simomura, F.M.SHM WITH AUGMENTED REALITY FOR AIRCRAFT MAINTENANCEICAS2018_0357
Simon, D.A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROLICAS2018_0052
Singh, D.LATTICE BOLTZMANN HIGH-LIFT SIMULATIONS - A STEP BEYOND CLASSICAL CFDICAS2018_0318
Smetak, E.J.SINGLE-AISLE AIRLINER DISRUPTION WITH A SINGLE-DECK BLENDED-WING-BODYICAS2018_0390
Smetanin, S.A.ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORSICAS2018_0639
Smetanin, S.A.APPLICATION OF "VIRTUAL" CONTROLLERS FOR INTEGRATED PROPULSION AND AIRCRAFT CONTROLICAS2018_0640
Smith, L.EXPERIENCE WITH INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN EDUCATION: AREND UAVICAS2018_0217
Smith, H.FEASIBILITY STUDY OF MODIFYING A BASELINE KEROSENE AIRCRAFT TO A LH2 POWERED VERSIONICAS2018_0580
Sobron, A.METHODS FOR EFFICIENT FLIGHT TESTING AND MODELLING OF REMOTELY PILOTED AIRCRAFT WITHIN VISUAL LINE-OF-SIGHTICAS2018_0663
Sokolova, O.V.RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEMICAS2018_0036
Solonin, V.THE STUDY OF TURBORAMJETS IN CIAMICAS2018_0848
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Song, C.STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETSICAS2018_0128
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Song, C.AERODYNAMIC DESIGN OF KEY COMPONENTS OF THE LARGE-DISCHARGE AXIAL FAN AT HIGH ALTITUDEICAS2018_0243
Song, S.ENERGY-ABSORBING CHARACTERISTICS ANALYSIS OF COMPOSITE THIN-WALLED C-CHANNELS UNDER LOW SPEED AXIAL COMPRESSIONICAS2018_0389
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Song, W.-P.THE AERODYNAMIC PERFORMANCE MEASUREMENT OF COAXIAL ROTOR IN HOVERICAS2018_0470
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Song, W.-P.A COMPARISON STUDY ON TRANSITION CHARACTERISTICS OF NLF FORWARD-SWEPT-WING AND AFT-SWEPT-WINGICAS2018_0497
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Song, Y.VERIFIED FUSELAGE SECTION WATER IMPACT MODELINGICAS2018_0732
Song, Y.PREDICTIVE ANALYSIS OF STITCHED AEROSPACE STRUCTURES FOR ADVANCED AIRCRAFTICAS2018_0826
Soudakov, V.G.NUMERICAL OPTIMIZATION OF FLOW CONTROL BY TANGENTIAL JET BLOWING ON TRANSONIC AIRFOILICAS2018_0704
Sousa, R.S.EVALUATION OF TRANSONIC BUFFETING ONSET BOUNDARY ESTIMATED BY TRAILING EDGE PRESSURE DIVERGENCE AND RMS DATA OF WING VIBRATIONICAS2018_0382
Sousa, M.S.A COMPARISON BETWEEN UNIVERSAL INTEGRAL REGULATOR AND LINEAR QUADRATIC TECHNIQUE FOR AN AIRCRAFT AUTOPILOTICAS2018_0559
Souza, J.M.MULTI-DISCIPLINARY DESIGN OPTIMIZATION OF A BLENDED WINGLETICAS2018_0598
Souza, R.A.DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONSICAS2018_0609
Souza, S.A.POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATIONICAS2018_0818
Spero, E.ON-DEMAND SMALL UAS ARCHITECTURE SELECTION AND RAPID MANUFACTURING USING A MODEL-BASED SYSTEMS ENGINEERING APPROACHICAS2018_0851
Spieck, M.MDO AS A SOCIO-TECHNICAL SYSTEM - A SMALL CONTRIBUTION TO COLLABORATIVE ENGINEERINGICAS2018_0633
Spiteri, A.AN ATC ORIENTED INTERFACE FOR MULTI-AIRCRAFT OPTIMISATION FOR CLIMBS AND DESCENTSICAS2018_0433
Staack, I.A HOLISTIC ENGINEERING APPROACH FOR AERONAUTICAL PRODUCT DEVELOPMENTICAS2018_0724
Stahl, P.DEVELOPMENT AND PERFORMANCE COMPARISON OF OPTIMIZED ELECTRIC FIXED-WING VTOL UAV CONFIGURATIONSICAS2018_0169
Stalewski, W.CONTROL OF STRONG SEPARATION OF FLOW VIA SIMULTANEOUS-BLOWING-SUCTION TECHNIQUEICAS2018_0196
Standfuss, T.ADAPTING CAPACITY OF AIR NAVIGATION SERVICE PROVISION IN EUROPE - BETWEEN SCYLLA AND CHARYBDISICAS2018_0483
Stasenko, A.L.EXPERIMENTAL INVESTIGATION, MATHEMATICAL AND NUMERICAL SIMULATION OF AIRCRAFT ICING PHENOMENAICAS2018_0741
Stathopoulos, N.STORE SEPARATION TRAJECTORY PREDICTIONS AT LOW SPEEDSICAS2018_0367
Steelant, J.LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMSICAS2018_0425
Steelant , J.A METHODOLOGY FOR PRELIMINARY SIZING OF A THERMAL AND ENERGY MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLEICAS2018_0429
Stefes, B.WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTINGICAS2018_0646
Stepanov, J.G.ADAPTIVE WING HIGH-LIFT SYSTEMICAS2018_0371
Stingo, L.MDO APPLICATIONS TO CONVENTIONAL AND NOVEL TURBOPROP AIRCRAFT WITHIN AGILE EUROPEAN PROJECTICAS2018_0648
Straker, L.BIO-DYNAMIC STABILITY ANALYSIS OF A GREBE DURING MIGRATIONICAS2018_0661
Strathoff, P.SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITYICAS2018_0727
Streltsov, E.V.APPLICATION OF THE COMBINED BOUNDARIES TO REDUCE WALL INTERFERENCE FOR NACA 0012 AIRFOIL TESTSICAS2018_0321
Stumpf, E.SMALL AIRCRAFT CONCEPT FOR REGIONAL ON-DEMAND AIR MOBILITYICAS2018_0727
Sudol, A.FORMULATION AND IMPLEMENTATION OF A METHOD FOR TECHNOLOGY EVALUATION OF SYSTEM OF SYSTEMSICAS2018_0862
Sui, J.-F.THRUST REVERSER INADVERTENT DEPLOYMENT IMPACT STUDY ON AIRPLANE CONTROLLABILITYICAS2018_0058
Sun, Y.CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF "PARASITE" NOISEICAS2018_0116
Sun, Y.IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BEDICAS2018_0119
Sun, H.OVERVIEW OF DYNAMIC TEST TECHNIQUES AT LOW SPEED AERODYNAMICS INSTITUTE, CARDCICAS2018_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 MSBSICAS2018_0253
Suntsov, S.V.PERFORMANCES OF LPT AND LINEAR CASCADES AT LOW REYNOLDS NUMBERSICAS2018_0652
Surkov, N.A.MATHEMATICAL MODEL OF COMMERCIAL AIRPLANE DYNAMICS AT STALLICAS2018_0016
Suzuki, S.AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEMICAS2018_0219
Suzuki, S.INDIVIDUALIZING FLIGHT SKILL TRAINING USING SIMULATOR DATA ANALYSIS AND BIOFEEDBACKICAS2018_0220
Suzuki, S.FAULT-TOLERANT FLIGHT CONTROL SYSTEM WITH SIMPLE ADAPTIVE CONTROL CONSIDERING PILOT INPUTICAS2018_0651
Svinareva, M.S.APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADESICAS2018_0173
Svirskiy, Y.A.DEVELOPMENT OF STRUCTURAL HEALTH MONITORING METHODS THROUGH THE ANALYSIS OF KINETICS OF LOCAL STRESS-STRAIN STATEICAS2018_0160
Swadesir, L.URBAN AIR TRANSPORTATION JOURNEY TIME COMPARISON FOR MELBOURNE METROPOLITAN AREAICAS2018_0635
Swaid, M.IDENTIFICATION OF OPTIMAL RENDEZVOUS AND SEPARATION AREAS FOR FORMATION FLIGHT UNDER CONSIDERATION OF WINDICAS2018_0619
Swaid, M.QUANTIFICATION OF FORMATION FLIGHT BENEFITS UNDER CONSIDERATION OF UNCERTAINTIES ON FUEL PLANNINGICAS2018_0755
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Szczepanik, R.OPTIMIZATION OF THE FUEL INJECTOR TO AN INTERNAL COMBUSTION ENGINE BY MEANS OF LASER EQUIPMENTICAS2018_0825
Szilder, K.NUMERICAL SIMULATION OF ICE ACCRETION INFLUENCED BY AN ANTI-ICING HEATING SYSTEMICAS2018_0620
Söderberg, R.MITIGATING RISK OF PRODUCIBILITY FAILURES IN PLATFORM CONCEPT DEVELOPMENTICAS2018_0101
Sřrensen, K.A.TURBULENCE MODEL CONDITIONING FOR VORTEX DOMINATED FLOWS BASED ON EXPERIMENTAL RESULTSICAS2018_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 APPROACHICAS2018_0385
Takase, V.L.MODEL-BASED CONTROL LOGICS DEVELOPMENT OF AIRCRAFT SYSTEMSICAS2018_0479
Takase, R.FAULT-TOLERANT FLIGHT CONTROL SYSTEM WITH SIMPLE ADAPTIVE CONTROL CONSIDERING PILOT INPUTICAS2018_0651
Takatani, K.PRECISE MEASUREMENT OF PROPAGATING FLAME IN 2-STROKE GASOLINE ENGINE BY MULTIPLE ION-PROBESICAS2018_0149
Talyzin, V.A.RESEARCH ON EXTERNAL AERODYNAMICS OF THE HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECTICAS2018_0256
Talyzin, V.A.INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECTICAS2018_0508
Tamba, A.K.F.SHM QUALIFICATION PROCESS AND THE FUTURE OF AIRCRAFT MAINTENANCEICAS2018_0354
Tamba, A.K.F.CORROSION DETECTION IN AERONAUTICAL STRUCTURES USING LAMB WAVES SYSTEM FOR SHMICAS2018_0355
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Tarifa, I.O.MODELING, CONTROL AND HARDWARE-IN-THE-LOOP SIMULATION OF A GENERIC TILTING MULTI-ROTORICAS2018_0533
Tarnowski, A.MORPHING WING WITH SURFACE DISCONTINUITY - COMPARATIVE TESTSICAS2018_0025
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Teixeira, P.C.PROPELLER INFLUENCE ON THE STABILITY OF HALE AIRCRAFTICAS2018_0177
Teixeira, L.H.A NUMERICAL ANALYSIS OF THE DYNAMICS OF A TENSEGRITY-MEMBRANE STRUCTUREICAS2018_0206
Temis, J.DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINESICAS2018_0820
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Terrapon, V.E.HIGHER FIDELITY TRANSONIC AERODYNAMIC MODELING IN PRELIMINARY AIRCRAFT DESIGNICAS2018_0453
Theron, J.-P.PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAVICAS2018_0233
Theuma, K.GROUND AND FLIGHT TESTING OF A MULTI-SENSOR OBSTACLE DETECTION AND TRACKING SYSTEM FOR RPAS SITUATION AWARENESSICAS2018_0182
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Thielecke, F.LOCAL MODEL NETWORKS APPLIED TO FLIGHT LOADS ESTIMATIONICAS2018_0650
Tian, L.GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEMICAS2018_0057
Tian, J.EFFECT OF DIELECTRIC PROPERTIES DUE TO THE CHANGE OF DIELECTRIC AS A RESULT OF ELEVATORY TEMPERATUREICAS2018_0293
Timmermans, H.DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORKICAS2018_0674
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Tissot, G.CONTROL OF A VERY FLEXIBLE WING WITH SIMULTANEOUS OPTIMIZATION OF THE GAIN MATRIX AND THE SPATIAL DISTRIBUTION OF THE SENSORSICAS2018_0500
Tita, V.AN XFEM FRAMEWORK FOR ONSET AND CRACK PROPAGATION FOR COMPOSITES BASED ON ACTION PLANE THEORYICAS2018_0502
Titchener, N.DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPTICAS2018_0875
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Toktaliev, P.D.COMMUNICATION BETWEEN PS AND AIRCRAFT SYSTEMS IN COLLECTIVE MDO SYSTEM IN AGILE PROJECTICAS2018_0742
Tokutake, H.MONTE-CARLO EVALUATION OF CONTROL LAW FOR HIGH ALTITUDE FLIGHT TEST OF MARS AIRPLANEICAS2018_0431
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Tomita, J.T.PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERSICAS2018_0649
Toratani, D.STUDY ON THE ARRIVAL MANAGER MAXIMIZING THE BENEFIT OF FOUR-DIMENSIONAL TRAJECTORY BASED OPERATIONSICAS2018_0315
Toratani, D.SIMULATION STUDY FOR VFR AIRCRAFT AND SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) MIXED OPERATIONS IN LOW LEVEL AIRSPACEICAS2018_0636
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Toussaint, C.HANDLING QUALITIES OF ONERA’S SMALL BUSINESS CONCEPT PLANE WITH DISTRIBUTED ELECTRIC PROPULSIONICAS2018_0492
Trabasso, L.G.DESIGN OF A DISTRIBUTED HUMAN FACTORS LABORATORY FOR FUTURE AIR SYSTEMSICAS2018_0305
Trabasso, L.G.A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTSICAS2018_0309
Trabasso, L.G.EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONSICAS2018_0402
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Trifari, V.MULTI-DISCIPLINARY ANALYSIS AND OPTIMIZATION JAVA TOOL FOR AIRCRAFT DESIGNICAS2018_0504
Trindade J., O.SERVICE-ORIENTED ARCHITECTURE TO INTEGRATE FLIGHT SAFETY AND MISSION MANAGEMENT SUBSYSTEMS INTO UAVSICAS2018_0374
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Tskhovrebov, M.THE STUDY OF TURBORAMJETS IN CIAMICAS2018_0848
Tsuchiya, T.AUTONOMOUS FLIGHT OF UNMANNED MULTICOPTER USING SUPER WIDE-ANGLE STEREO VISION SYSTEMICAS2018_0219
Tsuchiya, T.ALL JAPAN STUDENT'S INDOOR FLYING ROBOT CONTESTICAS2018_0858
Tsvetkov, I.V.PERFORMANCES OF LPT AND LINEAR CASCADES AT LOW REYNOLDS NUMBERSICAS2018_0652
Tuktarov, S.A.STRESS-BASED TOPOLOGY OPTIMIZATION WITH USING GLOBAL-LOCAL APPROACHICAS2018_0316
Turetta, F.M.S.A PRACTICAL ANALYSIS ON THE COMPLEXITY OF AIRCRAFT SYSTEMS ARCHITECTURE AND REQUIREMENTS DEVELOPMENTICAS2018_0514
Tylko, J.DESIGN AND DEVELOPMENT OF THE D8 COMMERCIAL TRANSPORT CONCEPTICAS2018_0875
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Vich, O.FLUTTER ANALYSIS OF TWIN TURBOPROP AIRCRAFT WITH TIP-TANKSICAS2018_0004
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Vielman, L.AN OVERVIEW OF THE FIRST PARAGUAYAN NEAR-SPACE EXPLORATION USING A HIGH ALTITUDE BALLOONICAS2018_0582
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Villani, E.DATA-DRIVEN FAILURE IDENTIFICATION USING A MOTION-BASED SIMULATORICAS2018_0581
Vinuesa, R.WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOILICAS2018_0388
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Viola, N.LIFE CYCLE COST ESTIMATION METHODOLOGY FOR HYPERSONIC TRANSPORTATION SYSTEMSICAS2018_0425
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Viviani, A.LAUNCHER AERODYNAMIC ANALYSIS WITH PLUME EFFECTSICAS2018_0130
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