COMPLETE AUTHOR LIST HYPERLINKED TO PAPERS



Abdalla, A.M.KNOWLEDGE-BASED FUTURE COMBAT AIRCRAFT OPTIMIZATION2016_0538
Abedian, A.AIRLINES MAINTENANCE COST ANALYSIS USING SYSTEM DYNAMICS MODELING2016_0452
Abedian, A.OPTIMIZATION OF COMPOSITE PATCH REPAIR FOR INCLINED CRACK ON ALUMINUM PLATE USING GENETIC ALGORITHM2016_0500
Abedian, A.INSTANTANEOUS BASELINE MULTIPLE DAMAGE DETECTION AND LOCALIZATION IN AN ALUMINIUM PLATE USING LAMB WAVES2016_0640
Abu-Zurayk, M.COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT2016_0345
Abulawi, J.USING INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN PROJECTS TO ENHANCE UNDERGRADUATE DESIGN EDUCATION: LESSONS LEARNED2016_0650
Adden, S.DESIGN, MANUFACTURING AND VALIDATION OF A GUST GENERATOR FOR WIND TUNNEL TEST OF A LARGE SCALE AEROELASTIC MODEL2016_0676
Ahn, D.-M.HISTORY OF RAPID GROWTH IN KOREAN AERONAUTICAL INDUSTRY2016_0035
Ahn, J.HYPERPARAMETERS OPTIMIZATION FOR ADAPTIVE DESIGN OF EXPERIMENTS APPLIED TO WIND TUNNEL TESTING2016_0319
Ahn, J.M.PERCH LANDING ASSISTED BY THRUSTER (PLAT): SIX D.O.F. TRAJECTORY OPTIMIZATION2016_0334
Ahn, J.M.ADAPTIVE NEURAL NETWORK CONTROLLER DESIGN FOR BLENDED-WING UAV WITH COMPLEX DAMAGE2016_0516
Ahn, M.H.DEVELOPMENT OF HIGH-ORDER AND HIGH-RESOLUTION SCHEMES FOR EFFICIENT SHOCK CAPTURING IN HIGH-SPEED FLOWS2016_0705
Ai, B.PANEL VIBRO-ACOUSTIC RESPONSE PREDICTION BASED ON TURBULENT BOUNDARY LAYER MEASUREMENT2016_0040
Akhmedzyanov, D.A.KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES2016_0008
Akhmedzyanov, D.A.AUTOMATED SELECTION OF THE MATERIAL A FAN BLADE PS-90A2016_0068
Akroyd, G.STORE SEPARATION FROM WEAPON BAYS2016_0156
Aksenov, A.A. NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN2016_0550
Alam, M.I.MULTIDISCIPLINARY DESIGN OPTIMIZATION OF STRATOSPHERIC AIRSHIP2016_0703
Aleksandrov, V.V.THE FLYING QUALITIES IMPROVEMENT FOR THE VEHICLES WITH TIME DELAY IN THEIR DYNAMICS2016_0043
Aleksandrov, V.Y.NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE2016_0380
Alem, B.INSTANTANEOUS BASELINE MULTIPLE DAMAGE DETECTION AND LOCALIZATION IN AN ALUMINIUM PLATE USING LAMB WAVES2016_0640
Alfano, M.CHAOS THEORY APPLIED TO BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELL2016_0673
Alfredson, J.DETECT AND AVOID FOR REMOTELY PILOTED AIRCRAFT IN AIR TRAFFIC CONTROL SIMULATIONS2016_0176
Ali, A.IMPORTANCE OF TRANSIENT AERODYNAMIC DERIVATIVES FOR V-TAIL AIRCRAFT FLIGHT DYNAMIC DESIGN2016_0515
Almeida, S.F.M.NUMERICAL SIMULATION IN FINITE ELEMENT METHOD AND MANUFACTURING OF LUG MATERIAL COMPOSITE BY RTM PROCESS2016_0279
Amato, E.M.ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES2016_0467
Amelyushkin, I.A.MATHEMATICAL MODELS AND OPTICAL INVESTIGATION OF TWO PHASE FLOWS IN WIND TUNNELS2016_0656
Amiez, A.NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION2016_0370
Amiryants, G.A.THE ACTIVE AEROELASTICITY CONCEPT - THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT2016_0436
Andreeva-Mori, A.DESIGN AND PRELIMINARY EVALUATION OF AN INTEGRATED AIRCRAFT OPERATION SYSTEM FOR DISASTER RELIEF2016_0088
Andreeva-Mori, A.IMPACT OF WEATHER UNCERTAINTIES ON NOISE CONTOURS AND NOISE ABATEMENT DESCENT TRAJECTORIES2016_0331
Anisimov, K.EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL2016_0572
Anisimov, K.AERODYNAMIC OPTIMIZATION OF AIRPLANE PROPULSION SYSTEM WITHIN THE FRAMEWORK OF AGILE PROJECT2016_0583
Anton, F.HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES2016_0744
Anton Diez, A.ADVANCED REFUELING BOOM SYSTEM (ARBS) DEVELOPMENT AND HANDLING QUALITIES EVALUATION2016_0586
Antunes, A.P.EFFECTS OF THE BOUNDARY LAYER TRANSITION ON THE GLOBAL AERODYNAMIC COEFFICIENTS2016_0330
Arai, N.EVALUATION OF CONCEPTUAL DESIGN BASED ON MANUFACTURED ACTUAL UNMANNED SOLAR PLANE2016_0685
Ariola, M.MODEL PREDICTIVE CONTROL FOR A SWARM OF FIXED WING UAVS2016_0326
Ariyarit, A.DESIGN OPTIMIZATION OF HELICOPTER BLADE USING CLASS SHAPE FUNCTION BASED GEOMETRY REPRESENTATION2016_0479
Arkhipov, M.SMALL HEIGHT DUCT DESIGN FOR MULTICOPTER FAN2016_0611
Asai, K.NON-INTRUSIVE UNSTEADY PSP TECHNIQUE FOR INVESTIGATION OF TRANSONIC BUFFETING2016_0553
Asensio Nieto, F.ADVANCED REFUELING BOOM SYSTEM (ARBS) DEVELOPMENT AND HANDLING QUALITIES EVALUATION2016_0586
Atinault, O.AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS2016_0092
Atkin, C.J.STAGGERED THREE-DIMENSIONAL CAVITIES AS A POSSIBLE METHOD FOR SKIN FRICTION DRAG REDUCTION2016_0606
Atkin, C. AFLONEXT – ACTIVE FLOW_LOADS AND NOISE CONTROL ON NEXT GENERATION ACTIVE WING2016_0755
Avelar, A.C.EXPERIMENTAL STUDY OF GEOMETRIC VARIATIONS EFFECT ON THE FLOW PATTERNS ON A HAMMERHEAD SATELLITE LAUNCH VEHICLE2016_0683
Azevedo, J.L.F.NUMERICAL SIMULATIONS OF TURBULENT FLOWS OVER THE ONERA-M6 AND DLR-F6 CONFIGURATIONS2016_0050
Azevedo, J.L.F.EFFECTS OF THE BOUNDARY LAYER TRANSITION ON THE GLOBAL AERODYNAMIC COEFFICIENTS2016_0330
Babel, R.COMPARATIVE ANALYSIS OF AIR FLOW IN THE COMPRESSOR OF THE GTD-350 ENGINE2016_0417
Babiak, M.IS TO BE THE MICRODRONE2016_0646
Bach, T.NUMERICAL ASSESSSMENT OF DAMAGE TOLERANCE ALLOWABLES FOR NEW DESIGN CONCEPTS OF STIFFENED COMPOSITE PANELS2016_0277
Bae, S.MULTI-STEP TRAJECTORY OPTIMIZATION FOR ATM BASED ON APPROXIMATED OPTIMAL PATH2016_0723
Bagassi, S.AUGMENTED AND VIRTUAL REALITY IN THE AIRPORT CONTROL TOWER2016_0719
Bagassi, S.GENERATIVE DESIGN: ADVANCED DESIGN OPTIMIZATION PROCESSES FOR AERONAUTICAL APPLICATIONS2016_0720
Bai, Y.-G.DESIGN, MANUFACTURE AND FREQUENCY EXPERIMENT OF A NOVEL FLUTTER MODEL FOR AGARD WING 445.6 WITH STRUCTURE-SIMILARITY2016_0519
Bai, Y.-G.INFLUENCE OF THE RHOMBOID ZONE ON AEROELASTIC EXPERIMENTS OF SUPERSONIC AIRCRAFT2016_0564
Baklanov, V.DYNAMICS AND VIBRATION OF NEW GENERATION AVIATION ENGINES2016_0566
Balakrishnan, H.STATISTICAL MODELING OF AIRCRAFT ENGINE FUEL FLOW RATE2016_0619
Balasubramanian, P.DYNAMIC MODELING AND STABILITY ANALYSIS OF A HIGH ALTITUDE AIRSHIP2016_0700
Balunov, K.A.MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS2016_0226
Ban, N.LOW-DRAG / LOW-BOOM SHAPE OPTIMIZATION OF A BIPLANE WING / TWIN-BODY FUSELAGE SST CONFIGURATION2016_0283
Bang, H.C.OPERATION SCENARIOS OF UNMANNED AIRCRAFT SYSTEMS INTEGRATED INTO THE KOREAN NATIONAL AIRSPACE SYSTEM2016_0445
Barbosa, L.M.F.STUDY OF THE COMPROMISE OF AERODYNAMIC AND STRUCTURE STANDPOINTS IN A HIGH-ASPECT RATIO WING DESIGN2016_0615
Barrier, R.AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS2016_0092
Bartasevicius, J.ACTIVE VORTEX FLOW CONTROL ON A GENERIC DELTA WING2016_0257
Bartels, R.MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES2016_0596
Battaglia, F.A COMPUTATIONAL STUDY ON AVIAN FLAPPING FLIGHT AND THE INFLUENCE OF FEATHER SEPARATION2016_0657
Baumann, S.AN INTERFACE CONCEPT TO SUPPORT THE COCKPIT CREW DURING TRAJECTORY-BASED DISPATCH TOWING2016_0080
Baumann, S.ACOUSTICAL COMPARISON OF CONVENTIONAL TAXIING AND DISPATCH TOWING - TAXIBOT´S CONTRIBUTION TO GROUND NOISE ABATEMENT2016_0454
Bayandor, J.A FOLDABLE FLAPPING WING DESIGN INSPIRED BY THE ELBOW-WRIST ANATOMY OF BATS2016_0609
Bayandor, J.CHARACTERIZATION OF DISTORTED FLUID FLOW ALONG ADVANCED HIGH-BYPASS PROPULSION SYSTEM2016_0628
Bayandor, J.ADVANCED PROPULSION COLLISION DAMAGE DUE TO UNMANNED AERIAL SYSTEM INGESTION2016_0629
Bayandor, J.LOW ORDER MODELING OF THE UNSTEADY AND 3D EFFECTS OF CONTINUOUS WAKE FLAPPING FLIGHT2016_0651
Bayandor, J.A COMPUTATIONAL STUDY ON AVIAN FLAPPING FLIGHT AND THE INFLUENCE OF FEATHER SEPARATION2016_0657
Bayandor, J.DYNAMICS MODELLING FOR CONTROL OF AN UNSTEADY HYDRODYNAMIC STINGRAY ROBOT2016_0658
Bayandor, J.NUMERICAL INVESTIGATION OF FAN-BLADE OUT USING MESO-SCALE COMPOSITE MODELING2016_0670
Becker, R.COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT2016_0345
Bedouet, J.MODELLING, GENERATING AND EVALUATING SECTOR CONFIGURATION PLANS - METHODOLOGY REPORT OF THE SESAR VP-755 EXERCISE2016_0063
Bedouet, J.TOWARDS A 4D TRAFFIC MANAGEMENT OF SMALL UAS OPERATING AT VERY LOW LEVEL2016_0064
Been, Y.B.A NEW SOLUTION METHOD FOR SIX DEGREE OF FREEDOM FLIGHT DYNAMICS SIMULATION OF A HIGH ASPECT RATIO WING VEHICLE2016_0158
Beerhorst, M.WEIGHT REDUCTION OF CYLINDRICAL GRID STRUCTURES USING AXIAL-HELICAL-DESIGN2016_0708
Belo, E.M.SYSTEM IDENTIFICATION OF A SCALE HELICOPTER IN HOVERING FLIGHT2016_0686
Ben-Asher, J.Z.FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS2016_0073
Berk, T.A.EXPERIMENTAL STUDY ON AERODYNAMIC LOAD CONTROL USING SYNTHETIC JET ACTUATORS2016_0389
Berlowitz, I.COMMERCIAL DERIVATIVE AIRCRAFT AND TURBINE ENGINE2016_0002
Bernatzky, T.AN INTERFACE CONCEPT TO SUPPORT THE COCKPIT CREW DURING TRAJECTORY-BASED DISPATCH TOWING2016_0080
Berry, P.KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD OPTIMIZATION2016_0375
Bewick, C.THE ROLLS-ROYCE PLC ULTRAFAN HEAT MANAGEMENT CHALLENGE2016_0344
Bezzina, F.CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION2016_0211
Bigarella, E.D.V.EFFECTS OF SOME NUMERICAL FORMULATION ASPECTS IN HIGH-LIFT CONFIGURATION SIMULATIONS2016_0713
Bijewitz, J.A REVIEW OF RECENT AIRCRAFT CONCEPTS EMPLOYING SYNERGISTIC PROPULSION-AIRFRAME INTEGRATION2016_0727
Bil, C.THE DESIGN OF AN AUTOMATIC BEACON EJECTING SYSTEM FOR AIRCRAFT2016_0465
Bil, C.INFLUENCE OF ETHNICITY ON PASSENGER STANDARD WEIGHT2016_0466
Birukov, R.V.CONTROL OF CONDITION OF GAS TURBINE ENGINE ROTOR BEARINGS IN DIAGNOSTIC PARAMETERS IN A DIFFERENT PHYSICAL NATURE2016_0273
Bisagni, C.CHAOS THEORY APPLIED TO BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELL2016_0673
Bittner, M.OPTIMAL APPROACH TRAJECTORIES FOR MULTIPLE AIRCRAFT CONSIDERING DISTURBANCES AND CONFIGURATION CHANGES2016_0051
Bittner, M.FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS2016_0073
Bittner, M.OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH2016_0287
Blase, T.ADVANCED RNP TO ILS AUTOLAND APPROACHES FOR OPTIMAL BENEFITS FROM PBN: FLIGHT TESTING PROCEDURES WITH AN A3202016_0147
Blasi, L.NONLINEAR DYNAMIC INVERSION WITH NEURAL NETWORKS FOR THE FLIGHT CONTROL OF A LOW COST TILT ROTOR UAV2016_0637
Bo, J.-L.NUMERICAL INVESTIGATION OF UNSTEADY INTERACTION CHARACTERISTIC INDUCED BY IMPULSIVE JET2016_0362
Bode-Oke, A.T.STRATEGIES FOR ACHIEVING BACKWARD FLIGHT BY A DRAGONFLY2016_0754
Bogdanski, K.ANALYSES OF AIRFLOW AROUND DUCTED FAN PROPULSION SYSTEM IN PUSHER CONFIGURATION USING PIV METHOD2016_0659
Boggero, L.COLLABORATIVE SYSTEMS DRIVEN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION2016_0585
Bonet, J.T.UHB ENGINE INTEGRATION FOR HYBRID WING BODY AIRCRAFT2016_0741
Boniface, J.-C.AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS2016_0092
Bons, J. -P.AN AERODYNAMIC ANALYSIS OF THE 3D FLOW AROUND THE SSC-A09 AIRFOIL2016_0671
Booij, P.J.A.QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH2016_0555
Borener, S.ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS2016_0413
Bosnyakov, I.COMPUTATIONAL EFFICIENCY AND QUALITY OF DIFFERENT VERSIONS OF DISCONTINUOUS GALERKIN METHOD FOR LES/DES APPLICATIONS2016_0099
Bradley, M.K.HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES2016_0744
Braun, R.METHODS FOR AUTOMATING MODEL VALIDATION: STEADY-STATE IDENTIFICATION APPLIED ON GRIPEN FIGHTER ENVIRONMENTAL CONTROL SYSTEM MEASUREMENTS2016_0188
Bravo-Mosquera , P.D.EXPERIMENTAL ANALYSES OF DROOP, WINGTIPS AND FENCES ON A BWB MODEL2016_0262
Bravo-Mosquera, P.D.CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING2016_0397
Breitsamter, C.SENSITIVITY ANALYSIS OF UNSTEADY AERODYNAMIC REDUCED-ORDER MODELS ROBUST TO FREESTREAM PARAMETER VARIATIONS2016_0206
Breitsamter, C.ACTIVE VORTEX FLOW CONTROL ON A GENERIC DELTA WING2016_0257
Breitsamter, C.AERODYNAMIC TESTING OF HELICOPTER NOVEL AIR INTAKES2016_0508
Brown, M.VISUALIZATION OF AIRSPACE COMPLEXITY BASED ON AIR TRAFFIC CONTROL DIFFICULTY2016_0160
Brown, M.EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA2016_0682
Brutyan, M.A.NEW METHOD OF TRANSONIC BUFFET DECREASING ON SUPERCRITICAL AIRFOIL2016_0127
Brutyan, M.A.INFLUENCE OF SURFACE FRACTAL MICROSTRUCTURE ON THE CHARACTERISTICS OF A TURBULENT BOUNDARY LAYER2016_0138
Budaev, V.P.INFLUENCE OF SURFACE FRACTAL MICROSTRUCTURE ON THE CHARACTERISTICS OF A TURBULENT BOUNDARY LAYER2016_0138
Burgstaller, F.IN-FLIGHT PROVISIONING AND DISTRIBUTION OF ATM INFORMATION2016_0385
Buttsworth, D.NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT2016_0353
Buzica, A.ACTIVE VORTEX FLOW CONTROL ON A GENERIC DELTA WING2016_0257
Candon, M.CHARACTERIZATION OF THE NONLINEAR AEROELASTIC BEHAVIOR OF AN AIRFOIL WITH FREEPLAY AND AERODYNAMIC NONLINEARITY2016_0716
Cao, N.EXPERIMENTAL INVESTIGATION OF LATERAL PULSE JET INTERACTION FLOWFIELD IN HYPERSONIC FLOW2016_0391
Carossa, G.M.EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL2016_0572
Carrese, R.ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES2016_0467
Carrese, R.CHARACTERIZATION OF THE NONLINEAR AEROELASTIC BEHAVIOR OF AN AIRFOIL WITH FREEPLAY AND AERODYNAMIC NONLINEARITY2016_0716
Catalano, F.M.LOW REYNOLDS PROPELLER META-MODEL FOR MULTIDICIPLYNARY OPTIMIZATION2016_0003
Catalano, F.M.CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING2016_0397
Catalanode, F.M.EXPERIMENTAL ANALYSES OF DROOP, WINGTIPS AND FENCES ON A BWB MODEL2016_0262
Cen, F.WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS2016_0091
Cenko, A.STORE SEPARATION FROM WEAPON BAYS2016_0156
Cerón-Muñoz, H.D.EXPERIMENTAL ANALYSES OF DROOP, WINGTIPS AND FENCES ON A BWB MODEL2016_0262
Cerón-Muñoz, H.D.CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING2016_0397
Cervinka, J.EXPERIMENATAL AND COMPUTATIONAL STUDY OF GROUND EFFECT ON AIRFOIL SECTION2016_0122
Cervinka, J.SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL2016_0593
Cestino, E.ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES2016_0467
Chae, S.EFFICIENT MULTI-RESOLUTION ANALYSIS FOR IMPLICIT TEMPORAL INTEGRATION2016_0427
Chakraborti, D.DYNAMIC MODELING AND STABILITY ANALYSIS OF A HIGH ALTITUDE AIRSHIP2016_0700
Chang, Y.H.SECURE ESTIMATION FOR UNMANNED AERIAL VEHICLES AGAINST ADVERSARIAL ATTACKS2016_0221
Chang, K.CFD OF BLENDED WING BODY UCAV WITH VORTEX GENERATOR2016_0246
Chapuis, D.THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION2016_0731
Chati, Y.S.STATISTICAL MODELING OF AIRCRAFT ENGINE FUEL FLOW RATE2016_0619
Chedrik, V.V.MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS2016_0226
Chen, H.3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION2016_0039
Chen, L.NUMERICAL SIMULATION OF RCS FOR A SPHERICAL CONVERGENT FLAP NOZZLE WITH A NON-RECTANGULAR DIVERGENT DUCT2016_0077
Chen, Z.H.UNCERTAINTY QUANTIFICATION AND GLOBAL SENSITIVITY ANALYSIS FOR HYPERSONIC AEROTHERMOELASTIC ANALYSIS2016_0135
Chen, L.-C.DETACHED EDDY SIMULATION OF AIRCRAFT MASSIVELY SEPARATED FLOWS2016_0140
Chen, C.W.W.A TEST METHOD BASED ON AIRCRAFT PLATFORM FOR ATMOSPHERIC LASER VISIBILITY2016_0167
Chen, J.RESEARCH ON LOAD SPECTRUM OF AERO HYDRAULIC PUMP BASED ON ACCELERATED DEGRADATION TESTING2016_0181
Chen, Z.PHYSICALLY-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION FRAMEWORK COUPLING AIRFRAME AND PROPULSION2016_0268
Chen, X.A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM2016_0321
Chen, Y.A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM2016_0321
Chen, J.A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM2016_0321
Chen, Q.DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL2016_0403
Chen, Z.A CONCEPTUAL DESIGN PLATFORM FOR BLENDED-WING-BODY TRANSPORTS2016_0510
Chen, H.A STUDY ON SAFETY ASSURANCE FOR INCREASINGLY AUTONOMOUS TRAFFIC FLOW MANAGEMENT SYSTEM2016_0672
Cheng, C.Y.A TEST METHOD BASED ON AIRCRAFT PLATFORM FOR ATMOSPHERIC LASER VISIBILITY2016_0167
Chernov, A.V. DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS2016_0620
Chernyshev, S.L.NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT2016_0353
Chevagin, A.EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL2016_0572
Chiba, T.INTEGRATED CONCEPTUAL DESIGN METHOD CONSIDERING ADVANCED AIRCRAFT SYSTEMS AND AIRCRAFT TRAJECTORY2016_0317
Chinchapatnam, P.IDENTIFYING THE BEST DESIGN FOR UNCERTAIN MARKETS2016_0626
Chircop, K.CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION2016_0211
Cho, A.LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV2016_0062
Cho, H.FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING2016_0123
Cho, N.APPROXIMATE THREE-DIMENSIONAL PATH GENERATION FOR UAV PATH-FOLLOWING2016_0128
Cho, I.AN INVESTIGATION OF EFFECTS OF FLIGHT MANEUVERS ON A SUPERSONIC AIRCRAFT WITH HORIZONTAL TAIL ACTUATOR FAILURE2016_0251
Cho, S.FLIGHT TESTS OF THE VISION-BASED TARGET SENSING AND APPROACHING2016_0373
Cho, M.-H.TRAJECTORY DESIGN WITH PATH PREDICTION FOR TERRAIN FOLLOWING2016_0379
Cho, S.GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV2016_0399
Cho, J.H.APPLICATION OF PROPER ORTHOGONAL DECOMPOSITION FOR AVIATION SAFETY2016_0576
Choi, S.ON MORE EFFECTIVE AERODYNAMIC DATA GENERATION FOR SIMULATION BASED AIRCRAFT CONCEPTUAL DESIGN2016_0151
Choi, H.-L.CLOSED-FORM COOPERATIVE GUIDANCE LAW FOR TWO MISSILES WITH COUPLED TERMINAL VELOCITY CONSTRAINTS2016_0387
Choi, S.GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV2016_0399
Choi, H.-L.MISSILE AUTOPILOT DESIGN USING CONTRACTION THEORY-BASED OUTPUT FEEDBACK CONTROL2016_0474
Choi, Y.-J.NUMERICAL INVESTIGATION OF SUBSONIC RAREFIED FLOWS USING DSMC-IP METHODS2016_0556
Choi, S.DEVELOPMENT OF A THREE-DIMENSIONAL TIGHTLY COUPLED EULER/POTENTIAL FLOW SOLVER FOR TRANSONIC FLOW2016_0712
Choroba, P.TOWARDS A MORE HARMONISED AND WIDER USE OF SHORT-TERM ATFCM MEASURES (STAM)2016_0055
Choung, J.Y.DETERMINATION OF DESIGN ALLOWABLES FOR AIRCRAFT COMPOSITE STRUCTURES2016_0522
Churkina, T.E.OPTIMIZATION OF THE TRAJECTORY AND ACCUMULATOR MASS FOR THE SOLAR-POWERED AIRPLANE2016_0388
Ciampa, P.D.TOWARDS THE 3RD GENERATION MDO COLLABORATIVE ENVIRONMENT2016_0563
Ciampa, P.D.COLLABORATIVE SYSTEMS DRIVEN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION2016_0585
Ciloni, P.A.G.EFFECTS OF SOME NUMERICAL FORMULATION ASPECTS IN HIGH-LIFT CONFIGURATION SIMULATIONS2016_0713
Cimini Jr., C.A.BEARING STRENGTH ASSESSMENT OF COMPOSITE MATERIAL THROUGH NUMERICAL MODELS2016_0633
Collier, F.ENVIRONMENTALLY RESPONSIBLE AVIATION PROJECT OVERVIEW2016_0738
Conway, S.R.AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS2016_0202
Craig, K.J.OPTIMISATION OF A WING-BODY-TAIL CONFIGURATION WITH AN ALTERNATIVE LOW DRAG FUSELAGE AND BODY TRAILING EDGE2016_0223
Cramer, K.E.RESEARCH DEVELOPMENTS IN NONDESTRUCTIVE EVALUATION AND STRUCTURAL HEALTH MONITORING FOR THE SUSTAINMENT OF COMPOSITE AEROSPACE STRUCTURES AT NASA2016_0733
Cresto Aleina, S.INVESTIGATIONS OF GROUND INFRASTRUCTURES FOR UAS FLIGHT MONITORING2016_0514
Cui, J.NUMERICAL SIMULATION OF RCS FOR A SPHERICAL CONVERGENT FLAP NOZZLE WITH A NON-RECTANGULAR DIVERGENT DUCT2016_0077
Cui, D.-G.FAIRING OPTIMIZATION DESIGN OF WING STRUCTURE2016_0282
Cui, D.-G.APPLICATION OF BUCKLING/POST-BUCKLING ANALYSIS FOR COMPOSITE STIFFENED PANELS2016_0337
Cui, A.FLEET DEVELOPMENT PLANNING OF AIRLINES: INCORPORATING THE AIRCRAFT OPERATING ECONOMICS FACTOR2016_0357
Czajkowski, L.MODERN MATERIALS IN AEROSPACE INDUSTRY - MAGNESIUM ALLOY CONTROL SYSTEM LEVER OF THE UNMANNED ILX - 27 HELICOPTER2016_0457
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Gopalakrishnan, P.EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL2016_0260
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Gorbushin, A.R.THE ORIGIN OF WIND TUNNELS IN RUSSIA2016_0069
Gorecki, T.THE SUPPORT PROCESS, SIMULATION RESEARCH DESIGN AND STRUCTURE OF THE NEW HELICOPTER'S CONSTRUCTION SCHEMATICS WITH SPECIAL EMPHASIS ON GROUND RESONANCE PHENOMENON2016_0354
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Grachev, A.V.AERODYNAMIC SHAPES DESIGN ON THE BASE OF DIRECT NEWTON TYPE OPTIMIZATION METHOD2016_0220
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Grigorev, A.V.THE ACTIVE AEROELASTICITY CONCEPT - THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT2016_0436
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Grishin, V.I.DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS2016_0620
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Guenov, M.D.ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN2016_0525
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Guo, Z.THE INVESTIGATION OF TIP CLEARANCE EFFECTS IN DUCTED ROTOR AERODYNAMIC CHARACTERISTICS USED IN UNMANNED AERIAL VEHICLES2016_0234
Gurevich, O.S.METHODS FOR IMPROVING THE RELIABILITY OF FUEL SUPPLY SYSTEM OF GAS TURBINE ENGINES WITH USING ELECTRICALLY DRIVEN PUMPS2016_0163
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Gusev, D.Y.BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE2016_0383
Gustafsson, P.A STUDY OF THE ACCURACY OF GROUND VIBRATION TEST DATA USING A REPLICA OF THE GARTEUR SM-AG19 TESTBED STRUCTURE2016_0095
Gårdhagen, R.KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD OPTIMIZATION2016_0375
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Göttlicher, C.FLIGHT PATH RECONSTRUCTION FOR AN UNMANNED AERIAL VEHICLE USING LOW-COST SENSORS2016_0414
Ha, O.-K.GENERAL MESSAGE RACES IN DATA DISTRIBUTION SERVICE PROGRAMS FOR AIRBORNE SOFTWARE2016_0535
Hagström, P.DETECT AND AVOID FOR REMOTELY PILOTED AIRCRAFT IN AIR TRAFFIC CONTROL SIMULATIONS2016_0176
Hajduk, J.OVERVIEW OF THE INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME2016_0313
Hakkaart, J.F.QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH2016_0555
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Han, S.ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME2016_0096
Han, J.-H.THE EFFECTS OF BODY AERODYNAMICS ON THE DYNAMIC STABILITY OF INSECT FLIGHT2016_0121
Han, Z.-H.SURROOPT: A GENERIC SURROGATE-BASED OPTIMIZATION CODE FOR AERODYNAMIC AND MULTIDISCIPLINARY DESIGN2016_0281
Han, S.Y.PERCH LANDING ASSISTED BY THRUSTER (PLAT): SIX D.O.F. TRAJECTORY OPTIMIZATION2016_0334
Han, D.A DEVELOPMENT OF MESHLESS POINT GENERATION TECHNIQUE FOR ANALYSIS OF THE UNSTEADY FLOW AROUND THE MULTI-BODY2016_0502
Han, J.-H.SELECTION OF PARAMETERS IN SPR CAMERA SYSTEM FOR STRUCTURAL HEALTH MONITORING OF UAV MAIN WING2016_0505
Handroos, H.HIL TEST BENCH FOR ENGINE'S FUEL CONTROL SYSTEMS INVESTIGATION2016_0215
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Hanlon, G.INFLUENCE OF ETHNICITY ON PASSENGER STANDARD WEIGHT2016_0466
Hanses, C.AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS2016_0202
Harada, A.AIR TRAFFIC EFFICIENCY EVALUATION BY TRAJECTORY OPTIMIZATION AND ADS-B DATA2016_0621
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Hashim, F.ROTORCRAFT SYSTEMS MODELLING FOR TWIN-ENGINE HEAVY HELICOPTER2016_0610
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Hirabayashi, H.VISUALIZATION OF AIRSPACE COMPLEXITY BASED ON AIR TRAFFIC CONTROL DIFFICULTY2016_0160
Hirabayashi, H.BENEFITS ASSESSMENT ON TIME-BASED OCEANIC ARRIVALS TO THE TOKYO METROPOLITAN AREA2016_0475
Hiraoka, K.EVALUATION OF CONCEPTUAL DESIGN BASED ON MANUFACTURED ACTUAL UNMANNED SOLAR PLANE2016_0685
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Hornung, M.A REVIEW OF RECENT AIRCRAFT CONCEPTS EMPLOYING SYNERGISTIC PROPULSION-AIRFRAME INTEGRATION2016_0727
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Hou, Y.-Y.SOLAR UAV GUST LOAD AMENDMENT2016_0266
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Hun, R.DYNAMIC MODELING AND STABILITY ANALYSIS OF A HIGH ALTITUDE AIRSHIP2016_0700
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Hwang, I.H.DETERMINATION OF DESIGN ALLOWABLES FOR AIRCRAFT COMPOSITE STRUCTURES2016_0522
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Ignatyev , D.I. WIND TUNNEL THREE-DEGREE-OF-FREEDOM DYNAMIC RIG FOR CONTROL VALIDATION2016_0325
Iijima, T.OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS2016_0338
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Isikveren, A.T.COMPARATIVE EFFICIENCY ANALYSIS OF DISTRIBUTED PROPULSION SYSTEMS FOR PROPULSIVE FUSELAGE AND HYBRID WING BODY CONCEPTS IN FP7 PROJECT "DISPURSAL"2016_0602
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Ivankin, M.A.INVESTIGATION OF THE HYDROGEN COMBUSTION CHAMBER PERFORMANCE WITHIN THE HEXAFLY-INT PROJECT2016_0458
Ivanyushkin, D.S.BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE2016_0383
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Jang, E.-Y.LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV2016_0062
Jang, J.E.MODEL FOLLOWING CONTROL FOR MD500 HELICOPTER2016_0498
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Jouannet, C.SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT2016_0390
Joubert, E.THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION2016_0731
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Judt, D.M.ROTORCRAFT SYSTEMS MODELLING FOR TWIN-ENGINE HEAVY HELICOPTER2016_0610
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Kaleta, R.EVALUATION METHODS OF AIRCRAFT FLIGHT SAFETY2016_0661
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Kang, W.-H.HISTORY OF RAPID GROWTH IN KOREAN AERONAUTICAL INDUSTRY2016_0035
Kang, Y.-S.LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV2016_0062
Kang, Y.J.A NEW SOLUTION METHOD FOR SIX DEGREE OF FREEDOM FLIGHT DYNAMICS SIMULATION OF A HIGH ASPECT RATIO WING VEHICLE2016_0158
Kang, H.EFFICIENT MULTI-RESOLUTION ANALYSIS FOR IMPLICIT TEMPORAL INTEGRATION2016_0427
Kang, W.G.DEVELOPMENT OF SMART TILT-ROTOR UAS AND THE BEGINNINGS OF KOREAN CIVILIAN DRONES2016_0526
Kang, W.R.PERIODICALLY OSCILLATING TWO TRAILING EDGE FLAPS ACTUATED BY SMA WIRES2016_0706
Karkle, P.G.ON APPLYING PISTON THEORY IN INTERFERENCE FLOWS2016_0225
Karkle, P.G.EXPERIMENTAL COMPARISON OF LIMIT CYCLE METHOD WITH PHASE RESONANCE AND PHASE SEPARATION METHODS FOR DETERMINING MODAL CHARACTERISTICS OF AIRCRAFT STRUCTURES2016_0507
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Kato, H.PRESSURE ANALYSIS BASED ON PIV MEASUREMENT IN AIRPLANE WAKES2016_0594
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Khatri, A.K.BIFURCATION ANALYSIS OF A GENERIC PUSHER TYPE TRANSPORT AIRCRAFT CONFIGURATION IN NEAR-STALL FLIGHT2016_0197
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Kim, Y.-S.LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV2016_0062
Kim, J.-K.THE EFFECTS OF BODY AERODYNAMICS ON THE DYNAMIC STABILITY OF INSECT FLIGHT2016_0121
Kim, S.Y.FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING2016_0123
Kim, Y.APPROXIMATE THREE-DIMENSIONAL PATH GENERATION FOR UAV PATH-FOLLOWING2016_0128
Kim, Y.CAPTURE REGION ANALYSIS FOR MISSILE GUIDANCE WITH FIELD-OF-VIEW CONSTRAINT AGAINST MOVING TARGET2016_0129
Kim, J.PREDICTION OF FRACTURE STRENGTH FOR NOTCHED LAMINATE SUBJECTED TO COMPRESSION LOADING2016_0146
Kim, J.AIRFRAME STRUCTURAL SURVIVABILITY STUDY THROUGH HYDRODYNAMIC RAM OF WELDED METALLIC WATER TANKS2016_0232
Kim, C.AIRFRAME STRUCTURAL SURVIVABILITY STUDY THROUGH HYDRODYNAMIC RAM OF WELDED METALLIC WATER TANKS2016_0232
Kim, H.I.SAMPLING-BASED MOTION PLANNING FOR COOPERATIVE AERIAL MANIPULATION2016_0237
Kim, H.J.SAMPLING-BASED MOTION PLANNING FOR COOPERATIVE AERIAL MANIPULATION2016_0237
Kim, H.J.OPTICAL FLOW ON A FLAPPING WING-MICRO AIR VEHICLE TO AVOID COLLISIONS AND STEER2016_0256
Kim, H.-G.IMPACT ANGLE CONTROL GUIDANCE CONSIDERING GRAVITY EFFECT2016_0269
Kim, H.-J.IMPACT ANGLE CONTROL GUIDANCE CONSIDERING GRAVITY EFFECT2016_0269
Kim, C.-J.FLIGHT TEST FOR TYPE CERTIFICATION ACQUISITION OF SMALL CIVIL AIRPLANE KC-1002016_0280
Kim, M.VERTICAL POSITION ERROR BOUNDING FOR INTEGRATED GPS/BAROMETER SENSORS TO SUPPORT UNMANNED AERIAL VEHICLE (UAV)2016_0295
Kim, M.K.TRAJECTORY DESIGN WITH PATH PREDICTION FOR TERRAIN FOLLOWING2016_0379
Kim, J.-H.CLOSED-FORM COOPERATIVE GUIDANCE LAW FOR TWO MISSILES WITH COUPLED TERMINAL VELOCITY CONSTRAINTS2016_0387
Kim, H.GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV2016_0399
Kim, S.ADAPTIVE SLIDING MODE CONTROLLER DESIGN FOR RECONFIGURATION OF ORGANIC FLIGHT ARRAY2016_0401
Kim, J.COMBUSTION INSTABILITY FREQUENCY MODE SHIFT OF H2/CH4 RATIO AND COMBUSTOR LENGTH IN A MODEL GAS TURBINE2016_0406
Kim, S.COMBUSTION INSTABILITY FREQUENCY MODE SHIFT OF H2/CH4 RATIO AND COMBUSTOR LENGTH IN A MODEL GAS TURBINE2016_0406
Kim, Y.ON STABILITY MARGIN OF A LQR-BASED VEHICLE NETWORK2016_0412
Kim, H.DESIGN THE GUIDANCE LAW FOR FORMATION FLIGHT OF MULTIPLE UAVS2016_0415
Kim, Y.J.OPERATION SCENARIOS OF UNMANNED AIRCRAFT SYSTEMS INTEGRATED INTO THE KOREAN NATIONAL AIRSPACE SYSTEM2016_0445
Kim, S.REDUCED ORDER MODELING OF AVIATION ENVIRONMENTAL DESIGN TOOL WITH PROPER ORTHOGONAL DECOMPOSITION AND KRIGING2016_0483
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Kim, K.J.ADAPTIVE NEURAL NETWORK CONTROLLER DESIGN FOR BLENDED-WING UAV WITH COMPLEX DAMAGE2016_0516
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Kim, J.W.DETERMINATION OF DESIGN ALLOWABLES FOR AIRCRAFT COMPOSITE STRUCTURES2016_0522
Kim, J.W.DEVELOPMENT OF SMART TILT-ROTOR UAS AND THE BEGINNINGS OF KOREAN CIVILIAN DRONES2016_0526
Kim, H.-J.GENERAL MESSAGE RACES IN DATA DISTRIBUTION SERVICE PROGRAMS FOR AIRBORNE SOFTWARE2016_0535
Kim, J.W.NUMERICAL SIMULATION OF MIXING IN AN INLET-FUELED HYPERSONIC AIR-BREATHING PROPULSION2016_0549
Kim, T.-U.NONLINEAR DAMAGE MODELING AND ANALYSIS OF VISCOPLASTIC COMPOSITE MATERIALS2016_0746
Kim, S.-H.NONLINEAR DAMAGE MODELING AND ANALYSIS OF VISCOPLASTIC COMPOSITE MATERIALS2016_0746
Kimura, J.STUDENT DESIGN PROCESSES IN INTERDISCIPLINARY COLLABORATION ACTIVITIES IN AERONAUTICS ENGINEERING EDUCATION2016_0252
Kiselev, D.Y.CONTROL OF CONDITION OF GAS TURBINE ENGINE ROTOR BEARINGS IN DIAGNOSTIC PARAMETERS IN A DIFFERENT PHYSICAL NATURE2016_0273
Kiselev, Y.V.CONTROL OF CONDITION OF GAS TURBINE ENGINE ROTOR BEARINGS IN DIAGNOSTIC PARAMETERS IN A DIFFERENT PHYSICAL NATURE2016_0273
Kishalov, A.E.KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES2016_0008
Kishalov, A.E.AUTOMATED SELECTION OF THE MATERIAL A FAN BLADE PS-90A2016_0068
Kistan, T.PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORIES IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS2016_0691
Kitazume, N.EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA2016_0682
Klingauf, U.AN INTERFACE CONCEPT TO SUPPORT THE COCKPIT CREW DURING TRAJECTORY-BASED DISPATCH TOWING2016_0080
Knoth, F.AERODYNAMIC TESTING OF HELICOPTER NOVEL AIR INTAKES2016_0508
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Kobayashi, K.DESIGN AND PRELIMINARY EVALUATION OF AN INTEGRATED AIRCRAFT OPERATION SYSTEM FOR DISASTER RELIEF2016_0088
Koenig, B.EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL2016_0260
Kolinko, K.A. WIND TUNNEL THREE-DEGREE-OF-FREEDOM DYNAMIC RIG FOR CONTROL VALIDATION2016_0325
Kondakov, I.NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES2016_0551
Konovalov, V.V.VERIFICATION OF CFRP COMPONENTS FATIGUE EVALUATION PROCEDURE UNDER IRREGULAR CYCLING LOADING2016_0303
Kontis, K.CHARACTERISATION OF NS-DBD PLASMA ACTUATORS FOR SUPERSONIC FLOW CONTROL2016_0170
Koo, S.-O.LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV2016_0062
Kovacic, I.IN-FLIGHT PROVISIONING AND DISTRIBUTION OF ATM INFORMATION2016_0385
Kowaleczko, G.THE SUPPORT PROCESS, SIMULATION RESEARCH DESIGN AND STRUCTURE OF THE NEW HELICOPTER'S CONSTRUCTION SCHEMATICS WITH SPECIAL EMPHASIS ON GROUND RESONANCE PHENOMENON2016_0354
Kowalski, M.RESTARTING OF A JET ENGINE DURING FLYING AND FLIGHT SAFETY2016_0655
Kowalski, M.RESEARCH OF ALTERNATIVE FUEL WATER-FUEL MICRO EMULSION FROM POINT OF VIEW REDUCTION OF EMISSIONS2016_0667
Kozuka, T.EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA2016_0682
Kraiko, A.N.AERODYNAMIC SHAPES DESIGN ON THE BASE OF DIRECT NEWTON TYPE OPTIMIZATION METHOD2016_0220
Kreerenko, O.D.SYNTHESIS OF CONTROL LAWS OF AEROSPACE SYSTEM BASED ON A SYNERGISTIC APPROACH2016_0183
Kreerenko, E.S.SYNTHESIS OF CONTROL LAWS OF AEROSPACE SYSTEM BASED ON A SYNERGISTIC APPROACH2016_0183
Krstic, B.THE ANALYSIS OF LAMINATE LAY-UP EFFECT ON THE FLUTTER SPEED OF COMPOSITE STABILIZERS2016_0271
Krus, P.METHODS FOR AUTOMATING MODEL VALIDATION: STEADY-STATE IDENTIFICATION APPLIED ON GRIPEN FIGHTER ENVIRONMENTAL CONTROL SYSTEM MEASUREMENTS2016_0188
Krus, P.KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD OPTIMIZATION2016_0375
Krus, P.SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT2016_0390
Krus, P.DESIGN AND TESTING OF A LOW-COST FLIGHT CONTROL AND DATA ACQUISITION SYSTEM FOR UNSTABLE SUBSCALE AIRCRAFT2016_0449
Krus, P.KNOWLEDGE-BASED FUTURE COMBAT AIRCRAFT OPTIMIZATION2016_0538
Krus, P.SYSTEMS ENGINEERING: AN INTERDISCIPLINARY CHALLENGE2016_0752
Kryuchkov, A.HIL TEST BENCH FOR ENGINE'S FUEL CONTROL SYSTEMS INVESTIGATION2016_0215
Kshitij, A.THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW2016_0244
Kukshinov, N.V.NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT2016_0353
Kukshinov, N.V.NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE2016_0380
Kulhánek, R.SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL2016_0593
Kumar, V.BIFURCATION ANALYSIS OF A GENERIC PUSHER TYPE TRANSPORT AIRCRAFT CONFIGURATION IN NEAR-STALL FLIGHT2016_0197
Kumar, V.SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL2016_0593
Kumbasar, S.A NOVEL FLIGHT CONTORL ALGORITHM FOR MULTICOPTERS2016_0231
Kursakov, I.EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL2016_0572
Kuruliuk, K.INVESTIGATION OF DEFORMATION FIELDS IN AIRCRAFT PANELS BY NON-CONTACT OPTICAL VIDEOGRAMMETRY METHOD2016_0368
Kuzmin, P.V.HEURISTIC MODEL OF NON-STEADY LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK2016_0019
Kweon, J.H.A STUDY ON FAILURE BEHAVIORS OF REPAIRED COMPOSITE STRUCTURES WITH SCARF BONDED PATCH2016_0335
Kwiatkowski, T.SOURCE TERM MODEL FOR STREAMWISE JET VORTEX GENERATOR MODELLING2016_0521
Kwon, H.-H.MISSILE AUTOPILOT DESIGN USING CONTRACTION THEORY-BASED OUTPUT FEEDBACK CONTROL2016_0474
Kwon, O.J.NUMERICAL SIMULATION OF MIXING IN AN INLET-FUELED HYPERSONIC AIR-BREATHING PROPULSION2016_0549
Kwon, O.-J.NUMERICAL INVESTIGATION OF SUBSONIC RAREFIED FLOWS USING DSMC-IP METHODS2016_0556
Kächele, T.STUDY ON EFFICIENT FULL ANNULUS URANS COMPUTATIONS OF AN INTAKE COMPRESSOR CONFIGURATION2016_0548
Ladyzynska-Kozdras, E.DEVELOPMENT OF THE SMALL-SCALE MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT SAFETY TAKE-OFF AND LANDING2016_0359
Lambert, J.-C.THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION2016_0731
Lambert, P.-A.HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES2016_0744
Lanshin, A.DEVELOPMENT OF TECHNOLOGY ADVANCE FOR FUTURE PROPULSION SYSTEMS OF HAUL AIRCRAFT2016_0542
Lapis, M.B.AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS2016_0202
Laskaridis, P.HYBRID TURBO-ELECTRIC DISTRIBUTED PROPULSION APPLIED TO SHORT RANGE AIRCRAFT2016_0748
Lauderdale, T.A.A STUDY ON SAFETY ASSURANCE FOR INCREASINGLY AUTONOMOUS TRAFFIC FLOW MANAGEMENT SYSTEM2016_0672
Lawson, C.P.ROTORCRAFT SYSTEMS MODELLING FOR TWIN-ENGINE HEAVY HELICOPTER2016_0610
Lee, S.-Y.LCC ESTIMATION AND CASE STUDY USING RELIABILITY AND MAINTAINABILITY ANALYSIS2016_0031
Lee, K.J.NONLINEAR OPTIMAL CONFLICT RESOLUTION SOLVED WITH PARTICLE SWARM OPTIMIZATION2016_0033
Lee, S.-Y.HISTORY OF RAPID GROWTH IN KOREAN AERONAUTICAL INDUSTRY2016_0035
Lee, R.SIMULATION OF UNSTEADY SHIP AIRWAKES USING OPENFOAM2016_0094
Lee, B.-Y.ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME2016_0096
Lee, N.FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING2016_0123
Lee, S.FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING2016_0123
Lee, S.CAPTURE REGION ANALYSIS FOR MISSILE GUIDANCE WITH FIELD-OF-VIEW CONSTRAINT AGAINST MOVING TARGET2016_0129
Lee, M.PREDICTION OF FRACTURE STRENGTH FOR NOTCHED LAMINATE SUBJECTED TO COMPRESSION LOADING2016_0146
Lee, H.B.SAMPLING-BASED MOTION PLANNING FOR COOPERATIVE AERIAL MANIPULATION2016_0237
Lee, J.G.OPTICAL FLOW ON A FLAPPING WING-MICRO AIR VEHICLE TO AVOID COLLISIONS AND STEER2016_0256
Lee, J.VERTICAL POSITION ERROR BOUNDING FOR INTEGRATED GPS/BAROMETER SENSORS TO SUPPORT UNMANNED AERIAL VEHICLE (UAV)2016_0295
Lee, J.VERTICAL POSITION ERROR BOUNDING FOR INTEGRATED GPS/BAROMETER SENSORS TO SUPPORT UNMANNED AERIAL VEHICLE (UAV)2016_0295
Lee, D.HYPERPARAMETERS OPTIMIZATION FOR ADAPTIVE DESIGN OF EXPERIMENTS APPLIED TO WIND TUNNEL TESTING2016_0319
Lee, J.HYPERPARAMETERS OPTIMIZATION FOR ADAPTIVE DESIGN OF EXPERIMENTS APPLIED TO WIND TUNNEL TESTING2016_0319
Lee, B.Y.PERCH LANDING ASSISTED BY THRUSTER (PLAT): SIX D.O.F. TRAJECTORY OPTIMIZATION2016_0334
Lee, D.CLOSED-FORM COOPERATIVE GUIDANCE LAW FOR TWO MISSILES WITH COUPLED TERMINAL VELOCITY CONSTRAINTS2016_0387
Lee, J.DESIGN THE GUIDANCE LAW FOR FORMATION FLIGHT OF MULTIPLE UAVS2016_0415
Lee, K.REDUCED ORDER MODELING OF AVIATION ENVIRONMENTAL DESIGN TOOL WITH PROPER ORTHOGONAL DECOMPOSITION AND KRIGING2016_0483
Lee, S.COMPUTATIONS OF SUPERSONIC LATERAL JET2016_0484
Lee, T.I.QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH2016_0555
Lee, J.STUDY ON THE SYSTEM INTEGRATION FOR MULTI-ELEMENT AIRFOIL AERODYNAMIC ANALYSIS2016_0598
Lee, K.-J.FIGHTER AIRCRAFT HIGH AOA DIRECTIONAL STABILITY IMPROVEMENT DESIGN2016_0600
Lee, C.MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR FIGHTER AIRCRAFT CONFIGURATION2016_0607
Lee, D.J.DEVELOPMENT OF HIGH-ORDER AND HIGH-RESOLUTION SCHEMES FOR EFFICIENT SHOCK CAPTURING IN HIGH-SPEED FLOWS2016_0705
Lee, D.J.PERIODICALLY OSCILLATING TWO TRAILING EDGE FLAPS ACTUATED BY SMA WIRES2016_0706
Lee, D.J.DEVELOPMENT OF A THREE-DIMENSIONAL TIGHTLY COUPLED EULER/POTENTIAL FLOW SOLVER FOR TRANSONIC FLOW2016_0712
Lee, H.-I.EVOLUTIONARY GAME BASED MULTI-OBJECTIVE OPTIMIZATION FOR MULTI-AGENT NETWORK RESILIENCE2016_0722
Lei, D.DEVELOPMENT OF HALF-MODEL TEST CAPABILITY AT THE NF-3 WIND TUNNEL2016_0034
Lengyel-Kampmann, T.MISSION BASED COMPARISON OF SINGLE- AND COUNTER-ROTATING FAN DESIGNS2016_0259
Lesire, C.NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION2016_0370
Levchenko, E.A.EXPERIENCE OF USING NONLINEAR NUMERICAL ANALYSIS TO ESTIMATE AIRCRAFT PRIMARY STRUCTURE STRENGTH2016_0201
Level, C.HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS2016_0438
Lewe, J.-H.AN EXPLORATION OF EVOLUTION PATHS FOR AIR TRANSPORTATION NETWORKS2016_0674
Lewe, J.-H.A REVIEW AND A CLASSIFICATION SCHEME FOR AIR TRANSPORTATION NETWORK RESEARCH2016_0688
Li, M.3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION2016_0039
Li, X.ENGINEERING APPLICATION OF GAO-YONG RATIONAL TURBULENCE MODEL TO AN INTER-COOLED DUCT2016_0065
Li, Q.WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS2016_0091
Li, Y.STUDY ON THE SAFETY RISK AND CAPACITY OF THE ONE-WAY CIRCULATION AIR ROUTE IN CHINA2016_0115
Li, J.RESEARCH ON LOAD SPECTRUM OF AERO HYDRAULIC PUMP BASED ON ACCELERATED DEGRADATION TESTING2016_0181
Li, X.THE INVESTIGATION OF TIP CLEARANCE EFFECTS IN DUCTED ROTOR AERODYNAMIC CHARACTERISTICS USED IN UNMANNED AERIAL VEHICLES2016_0234
Li, K.SEMI-A VIBRATION SUPPRESSION OF AIRCRAFT PANEL USING PIEZOELECTRIC ACTUATOR WITH SYNCHRONIZED SWITCH DAMPING TECHNIQUE2016_0248
Li, Y.EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL2016_0260
Li, C.LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER CORROSION ENVIRONMENT2016_0308
Li, X.LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER CORROSION ENVIRONMENT2016_0308
Li, F.-M.MAKING HEALTH MANAGEMENT MORE CONCISE AND EFFICIENT: AIRCRAFT CONDITION MONITORING BASED ON COMPRESSED SENSING2016_0400
Li, X.UNSTEADY AERODYNAMICS MODELLING AND ITS APPLICATION IN AEROELASTIC STABILITY ANALYSIS2016_0407
Li, J.RESEARCH ON THE IMPACT OF SHOCK WAVE TO EXTENSIONALITY OF POD METHOD2016_0409
Li, X.-T.RESEARCH ON THE IMPACT OF SHOCK WAVE TO EXTENSIONALITY OF POD METHOD2016_0409
Li, L.THE RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION FIELDMEASUREMENT BASED ON FLUORESCENT OIL FILM2016_0710
Liao, D.DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL2016_0403
Liao, M.RESEARCH ADVANCES ON AIRCRAFT STRUCTURAL INTEGRITY AND SUSTAINMENT AT NRC2016_0726
Liepelt, R.COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT2016_0345
Lim, Y.AUTOMATED SEPARATION ASSURANCE AND COLLISION AVOIDANCE FUNCTIONS IN THE CNS+A CONTEXT2016_0027
Lim, C.H.DEVELOPMENT OF SMART TILT-ROTOR UAS AND THE BEGINNINGS OF KOREAN CIVILIAN DRONES2016_0526
Lim, Y.PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORIES IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS2016_0691
Limonin, M.V.EXPERIENCE OF USING NONLINEAR NUMERICAL ANALYSIS TO ESTIMATE AIRCRAFT PRIMARY STRUCTURE STRENGTH2016_0201
Linderholt, A.A STUDY OF THE ACCURACY OF GROUND VIBRATION TEST DATA USING A REPLICA OF THE GARTEUR SM-AG19 TESTBED STRUCTURE2016_0095
Lipatov, V.D.KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES2016_0008
Lis, M.OVERVIEW OF THE INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME2016_0313
Liseykin, G.V.EXPERIMENTAL COMPARISON OF LIMIT CYCLE METHOD WITH PHASE RESONANCE AND PHASE SEPARATION METHODS FOR DETERMINING MODAL CHARACTERISTICS OF AIRCRAFT STRUCTURES2016_0507
Liu, J.3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION2016_0039
Liu, Z.-T.WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS2016_0091
Liu, G.TOTAL TEMPERATURE RECOVERY CHARACTERISTICS TEST TECHNIQUE BASED ON TOTAL PRESSURE CALIBRATION WIND TUNNEL2016_0112
Liu, F.INVESTIGATION ON OBLIQUE SHOCK WAVE CONTROL BY SURFACE ARC DISCHARGE PLASMA2016_0124
Liu, J.HANDLING QUALITIES PREDICTION BASED ON ADAPTIVE OPTIMAL CONTROL PILOT MODEL2016_0143
Liu, Z.-Q.SOLAR UAV GUST LOAD AMENDMENT2016_0266
Liu, X.-W.NUMERICAL INVESTIGATION OF INLET STARTING CHARACTERISTICS2016_0296
Liu, Y.-F.NUMERICAL INVESTIGATION OF UNSTEADY INTERACTION CHARACTERISTIC INDUCED BY IMPULSIVE JET2016_0362
Liu, Y.-W.NUMERICAL INVESTIGATION OF UNSTEADY INTERACTION CHARACTERISTIC INDUCED BY IMPULSIVE JET2016_0362
Liu, N.LINEAR MODELING BASED ON INSTRUMENTAL MODEL ESTIMATION AND PID PARAMETERS TUNING IN FREQUENCY-DOMAIN OF AIRCRAFT ENGINE2016_0702
Liu, H.STRATEGIES TO ENHANCE A CONFIGURATION FOR HIGH-PRECISION MULTI DISCIPLINARY OPTIMIZATION2016_0707
Liying, S.CONCEPTUAL STUDY OF AN INNOVATIVE HIGH ALTITUDE SOLAR POWERED FLIGHT VEHICLE2016_0015
Lobanova, M.A.LARGE-SCALE VORTEX STRUCTURE OF FLOW IN THE NEAR WAKE BEHIND AN AIRLINER DURING TAKEOFF AND LANDING2016_0666
Lu, C.MAKING HEALTH MANAGEMENT MORE CONCISE AND EFFICIENT: AIRCRAFT CONDITION MONITORING BASED ON COMPRESSED SENSING2016_0400
Lu, C.AIRCRAFT SECURITY ENHANCEMENT: ROTATING MACHINERY FAULT DIAGNOSIS AND HEALTH ASSESSMENT USING MANIFOLD LEARNING AND DYNAMIC TIME WARPING2016_0435
Lucchi, F.AUGMENTED AND VIRTUAL REALITY IN THE AIRPORT CONTROL TOWER2016_0719
Lucchi, F.GENERATIVE DESIGN: ADVANCED DESIGN OPTIMIZATION PROCESSES FOR AERONAUTICAL APPLICATIONS2016_0720
Ludwig, T.ADVANCED RNP TO ILS AUTOLAND APPROACHES FOR OPTIMAL BENEFITS FROM PBN: FLIGHT TESTING PROCEDURES WITH AN A3202016_0147
Lundström, D.SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT2016_0390
Lundström, D.DESIGN AND TESTING OF A LOW-COST FLIGHT CONTROL AND DATA ACQUISITION SYSTEM FOR UNSTABLE SUBSCALE AIRCRAFT2016_0449
Lung, S.-F.APPLICATIONS OF DISPLACEMENT TRANSFER FUNCTIONS TO DEFORMED SHAPE PREDICTIONS OF THE G-III SWEPT-WING STRUCTURE2016_0209
Lunin, V.Y.BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE2016_0383
Luo, X.L.TAXIING ROUTE PLANNING BASED ON AIRPORT HOTSPOTS2016_0402
Lysenkov, A.EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL2016_0572
Ma, C.SYNTHESIZED ANALYSIS FROM DESIGN RANGE TO THE CONCETUAL DESIGN OF WIDEBODY AIRLINER2016_0058
Ma, W.LABYRINTH SEALS DYNAMIC COEFFICIENTS AND CRITICAL SPEED RESEARCH BASE OF CHILDS´ MODEL2016_0212
Ma, C.A CONCEPTUAL ANALYSIS OF AN AIRCRAFT WITH REAR-MOUNTED OPEN ROTOR ENGINES2016_0253
MacKunis, W.ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS2016_0413
Mahiddini, F.COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN "MORE ELECTRICAL AIRCRAFT"2016_0105
Mainz, H.MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES2016_0596
Malenko, V.EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL2016_0572
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Mansor, S.IMPORTANCE OF TRANSIENT AERODYNAMIC DERIVATIVES FOR V-TAIL AIRCRAFT FLIGHT DYNAMIC DESIGN2016_0515
Mare, J.-C.SPECIAL CONSIDERATIONS TO THERMAL BEHAVIOR MODELING AND SIMULATION OF AN AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEM2016_0554
Mareskin, I.MULTIDISCIPLINARY OPTIMIZATION OF PRO-COMPOSITE STRUCTURAL LAYOUTS OF HIGH LOADED AIRCRAFT CONSTRUCTIONS2016_0622
Marini, M.NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT2016_0353
Markina, K.V.KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES2016_0008
Markina, K.V.AUTOMATED SELECTION OF THE MATERIAL A FAN BLADE PS-90A2016_0068
Marks, T.INFLUENCE OF AIRCRAFT TYPE AND ORDER ON FUEL SAVINGS GAINED BY TWO-AIRCRAFT FORMATIONS2016_0592
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Martins-Abdalla, A.CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING2016_0397
Marzocca, P.ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES2016_0467
Marzocca, P.CHARACTERIZATION OF THE NONLINEAR AEROELASTIC BEHAVIOR OF AN AIRFOIL WITH FREEPLAY AND AERODYNAMIC NONLINEARITY2016_0716
Maslov, V.P.EFFECT OF REYNOLDS NUMBER, OPERATING MODE, TURBULENCE PARAMETERS ON PROFILE AND SECONDARY LOSSES OF LPT2016_0276
Maslov, A.A.STUDY OF THE UNSTEADY STRUCTURES EVOLUTION IN SHOCK WAVE / BOUNDARY LAYER INTERACTION FOR VARIOUS UPSTREAM CONDITIONS2016_0560
Masotti, N.AUGMENTED AND VIRTUAL REALITY IN THE AIRPORT CONTROL TOWER2016_0719
Mat, S.EFFECTS OF PROPELLER LOCATIONS ON THE VORTEX SYSTEM ABOVE DELTA-SHAPED UAV MODEL2016_0162
Mat, S.EFFECTS OF REYNOLDS NUMBER ON THE ONSET OF LEADING EDGE VORTEX SEPARATION ABOVE BLUNT-EDGE DELTA WING VFE-2 CONFIGURATIONS2016_0608
Matayoshi, N.OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS2016_0338
Matsuda, T.FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS2016_0393
Matsushima, K.PRESSURE ANALYSIS BASED ON PIV MEASUREMENT IN AIRPLANE WAKES2016_0594
Matta, A.LOW ORDER MODELING OF THE UNSTEADY AND 3D EFFECTS OF CONTINUOUS WAKE FLAPPING FLIGHT2016_0651
Mattei, M.MODEL PREDICTIVE CONTROL FOR A SWARM OF FIXED WING UAVS2016_0326
Mattei, M.NONLINEAR DYNAMIC INVERSION WITH NEURAL NETWORKS FOR THE FLIGHT CONTROL OF A LOW COST TILT ROTOR UAV2016_0637
Maury, C.HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS2016_0438
Mavris, D.LINKING TECHNOLOGY READINESS TO UNCERTAINTY REDUCTION2016_0632
Mavris, D.N.UNCERTAINTY QUANTIFICATION OF AIRFOIL DESIGN FOR ADVANCED PROPELLER MODELS2016_0665
Mavris, D.N.AN EXPLORATION OF EVOLUTION PATHS FOR AIR TRANSPORTATION NETWORKS2016_0674
Mavris, D.N.A REVIEW AND A CLASSIFICATION SCHEME FOR AIR TRANSPORTATION NETWORK RESEARCH2016_0688
Mavris, D.N.UNMANNED VEHICLE COLLABORATION RESEARCH ENVIRONMENT FOR MARITIME SEARCH AND RESCUE2016_0728
Mavris, D.N.VIRTUAL EXPERIMENTATION AND VISUAL ANALYTICS IN SUPPORT OF SYSTEMS ENGINEERING AND SYSTEMS OF SYSTEMS ENGINEERING EFFORTS2016_0729
Mavris, D.N.TECHNOLOGY INTEGRATION AND SYSTEM ASSESSMENTS WITH UNCERTAINTY MODELLING2016_0742
Mazur, M.IS TO BE THE MICRODRONE2016_0646
McCartney, B.THE EFFECT OF LEADING EDGE ROUNDING ON A CARET WAVERIDER CONFIGURATION AT MACH 8.22016_0242
McLaughlin, C.AN INVESTIGATION OF EFFECTS OF FLIGHT MANEUVERS ON A SUPERSONIC AIRCRAFT WITH HORIZONTAL TAIL ACTUATOR FAILURE2016_0251
Medeiros, J.G.EXPERIMENTAL STUDY OF GEOMETRIC VARIATIONS EFFECT ON THE FLOW PATTERNS ON A HAMMERHEAD SATELLITE LAUNCH VEHICLE2016_0683
Meijer, M.-C.ON APPLYING PISTON THEORY IN INTERFERENCE FLOWS2016_0225
Meleshin, B.A.HEURISTIC MODEL OF NON-STEADY LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK2016_0019
Meshennikov, P.A.BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE2016_0383
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Mieloszyk, J.UNCONVENTIONAL CONFIGURATIONS - DESIGN AND OPTIMIZATION2016_0067
Mikhailova , M.K. NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN2016_0550
Mileshin, V.I.DEVELOPMENT OF THE FAN STAGE WITH ULTRA-LOW ROTATIONAL SPEED2016_0261
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Miller, M.THE ROUGHNESS POSITION INFLUENCE ON LAMINAR AEROFOIL AERODYNAMIC CHARACTERISTIC IN TRANSONIC FLOW REGIME2016_0561
Min, J.K.THE ROLLS-ROYCE PLC ULTRAFAN HEAT MANAGEMENT CHALLENGE2016_0344
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Mirzoyan, A.COMPARATIVE EFFICIENCY ANALYSIS OF DISTRIBUTED PROPULSION SYSTEMS FOR PROPULSIVE FUSELAGE AND HYBRID WING BODY CONCEPTS IN FP7 PROJECT "DISPURSAL"2016_0602
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Miyazawa, Y.EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA2016_0682
Mizutani, K.FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS2016_0393
Modi, H.C.APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS2016_0185
Moerland, E.EXPLORING PROPAGATED UNCERTAINTIES IN A MULTI-DISCIPLINARY AIRCRAFT DESIGN FRAMEWORK2016_0145
Moerland, E.COLLABORATIVE AIRCRAFT DESIGN USING AN INTEGRATED AND DISTRIBUTED MULTIDISCIPLINARY PRODUCT DEVELOPMENT PROCESS2016_0328
Moerland, E.THE COLLABORATIVE ENGINEER: HOW EDUCATION SHOULD BRING FORTH THE NEW GENERATION OF ENGINEERS2016_0750
Mohammadi-Amin, M.CFD-BASED AERODYNAMIC SHAPE OPTIMIZATION OF A MANNED RE-ENTRY VEHICLE2016_0627
Molina-Cristobal, A.ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN2016_0525
Molokanov, A.THE FOAMING PROPERTIES OF LUBRICATING OILS FOR AIRCRAFT GAS TURBINE ENGINES2016_0270
Monner, H.P.DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM2016_0166
Moon, G.-H.AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY CONSTRAINTS2016_0355
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Moon, J.H.MODEL FOLLOWING CONTROL FOR MD500 HELICOPTER2016_0498
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Qin, J.RESEARCH ON VIBRATION CHARACTERISTIC FOR VARIABLE ROTATING VELOCITY BLADES2016_0189
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Raj, P.USING INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN PROJECTS TO ENHANCE UNDERGRADUATE DESIGN EDUCATION: LESSONS LEARNED2016_0650
Rajchel, J.RESTARTING OF A JET ENGINE DURING FLYING AND FLIGHT SAFETY2016_0655
Rajchel, J.EVALUATION METHODS OF AIRCRAFT FLIGHT SAFETY2016_0661
Ramasamy, S.AUTOMATED SEPARATION ASSURANCE AND COLLISION AVOIDANCE FUNCTIONS IN THE CNS+A CONTEXT2016_0027
Ramirez Gonzalez, V.XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES2016_0193
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Rangel, R.K.DEVELOPMENT OF PEST\'S BIOLOGICAL CONTROL TOOL USING VTOL UAV SYSTEMS2016_0207
Rasuo, B.A STUDY OF WALL-INTERFERENCE EFECTS IN WIND-TUNNEL TESTING OF A STANDARD MODEL AT TRANSONIC SPEEDS2016_0216
Rasuo, B.GENERAL APPROACH TO THE ANALYSIS OF THE ASYMMETRICALLY LOADED AIRPLANE FLIGHT LIMITATIONS2016_0227
Rasuo, B.THE ANALYSIS OF LAMINATE LAY-UP EFFECT ON THE FLUTTER SPEED OF COMPOSITE STABILIZERS2016_0271
Razin, A.NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES2016_0551
Reimann, B.NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT2016_0353
Rein-Weston, K.AN IN-FLIGHT AID TO NEGOTIATE A MORE EFFICIENT FLIGHT PATH2016_0463
Reis, F.C. SYSTEM IDENTIFICATION OF A SCALE HELICOPTER IN HOVERING FLIGHT2016_0686
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Revanth Reddy, A.IMPROVEMENT OF THE DESIGN AND METHODS OF DESIGNING TUBULER AIR-TO-AIR HEAT EXHANGERS COOLING SYSTEMS OF GAS TURBINES2016_0433
Rhee, J.S.A MESHLESS METHOD FOR SIMULATION OF HYPERSONIC VISCOUS FLOWS2016_0499
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Riaz, A.ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN2016_0525
Ribeiro, A.F.P.EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL2016_0260
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Ridel, M.DISTRIBUTED ELECTRIC PROPULSION FOR SMALL BUSINESS AIRCRAFT A CONCEPT-PLANE FOR KEY-TECHNOLOGIES INVESTIGATIONS2016_0461
Rieck, M.OPTIMAL APPROACH TRAJECTORIES FOR MULTIPLE AIRCRAFT CONSIDERING DISTURBANCES AND CONFIGURATION CHANGES2016_0051
Rieck, M.FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS2016_0073
Rieck, M.OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH2016_0287
Riemenschneider, J.DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM2016_0166
Riemenschneider, J.MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES2016_0596
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Rinoie, K.AIRCRAFT DESIGN EDUCATION FOR UNDERGRADUATE AND GRADUATE STUDENTS AT THE UNIVERSITY OF TOKYO2016_0749
Rivero Arevalo, I.XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES2016_0193
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Rodionov, L.HIL TEST BENCH FOR ENGINE'S FUEL CONTROL SYSTEMS INVESTIGATION2016_0215
Rodríguez Robles, R.ELASTIC MODES ADAPTIVE CANCELLATION ALGORITHM FOR THE A330 MRTT FLYING BOOM CONTROL LAWS2016_0528
Rohacs, D.DEVELOPMENT OF AN ADVANCED ATCO WORKSTATION2016_0662
Rohacs, J.DEVELOPMENT OF AN ADVANCED ATCO WORKSTATION2016_0662
Rooseleer, F.WAKE TURBULENCE RE-CATEGORISATION ON APPROACH AND DEPARTURE FOR SAFE AND MORE EFFICIENT AIR TRAFFIC MANAGEMENT2016_0230
Rothfeld, R.BOARDING PROCESS ASSESSMENT OF NOVEL AIRCRAFT CABIN CONCEPTS2016_0218
Roussel, A.THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW2016_0244
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Ruchala, P.ANALYSES OF AIRFLOW AROUND DUCTED FAN PROPULSION SYSTEM IN PUSHER CONFIGURATION USING PIV METHOD2016_0659
Russell, A.CHARACTERISATION OF NS-DBD PLASMA ACTUATORS FOR SUPERSONIC FLOW CONTROL2016_0170
Ryemill, M.THE ROLLS-ROYCE PLC ULTRAFAN HEAT MANAGEMENT CHALLENGE2016_0344
Ryoo, C.-K.REAL-TIME GENERATION OF WAYPOINTS ENHANCING UAV SURVIVABILITY2016_0485
Ryu, S.W.OPTICAL FLOW ON A FLAPPING WING-MICRO AIR VEHICLE TO AVOID COLLISIONS AND STEER2016_0256
Sabatini, R.AUTOMATED SEPARATION ASSURANCE AND COLLISION AVOIDANCE FUNCTIONS IN THE CNS+A CONTEXT2016_0027
Sabatini, R.PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORIES IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS2016_0691
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Said, M.EFFECTS OF REYNOLDS NUMBER ON THE ONSET OF LEADING EDGE VORTEX SEPARATION ABOVE BLUNT-EDGE DELTA WING VFE-2 CONFIGURATIONS2016_0608
Salanne, J.-P.HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS2016_0438
Sanchez, F.SURROGATE MODELING TECHNIQUE FOR THE CONCEPTUAL AND PRELIMINARY DESIGN OF EMBEDDED ACTUATION SYSTEMS AND COMPONENTS2016_0184
Santana, L.D.EXPERIMENTAL ANALYSES OF DROOP, WINGTIPS AND FENCES ON A BWB MODEL2016_0262
Santoro, F.CABIN ESCAPE SYSTEM: A WAY TO ENSURE CREW SAFETY DURING SUBORBITAL FLIGHTS2016_0506
Sanz de Blas, A.ELASTIC MODES ADAPTIVE CANCELLATION ALGORITHM FOR THE A330 MRTT FLYING BOOM CONTROL LAWS2016_0528
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