| Abdalla, A.M. | KNOWLEDGE-BASED FUTURE COMBAT AIRCRAFT OPTIMIZATION | 2016_0538 |
| Abedian, A. | AIRLINES MAINTENANCE COST ANALYSIS USING SYSTEM DYNAMICS MODELING | 2016_0452 |
| Abedian, A. | OPTIMIZATION OF COMPOSITE PATCH REPAIR FOR INCLINED CRACK ON ALUMINUM PLATE USING GENETIC ALGORITHM | 2016_0500 |
| Abedian, A. | INSTANTANEOUS BASELINE MULTIPLE DAMAGE DETECTION AND LOCALIZATION IN AN ALUMINIUM PLATE USING LAMB WAVES | 2016_0640 |
| Abu-Zurayk, M. | COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT | 2016_0345 |
| Abulawi, J. | USING INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN PROJECTS TO ENHANCE UNDERGRADUATE DESIGN EDUCATION: LESSONS LEARNED | 2016_0650 |
| Adden, S. | DESIGN, MANUFACTURING AND VALIDATION OF A GUST GENERATOR FOR WIND TUNNEL TEST OF A LARGE SCALE AEROELASTIC MODEL | 2016_0676 |
| Ahn, D.-M. | HISTORY OF RAPID GROWTH IN KOREAN AERONAUTICAL INDUSTRY | 2016_0035 |
| Ahn, J. | HYPERPARAMETERS OPTIMIZATION FOR ADAPTIVE DESIGN OF EXPERIMENTS APPLIED TO WIND TUNNEL TESTING | 2016_0319 |
| Ahn, J.M. | PERCH LANDING ASSISTED BY THRUSTER (PLAT): SIX D.O.F. TRAJECTORY OPTIMIZATION | 2016_0334 |
| Ahn, J.M. | ADAPTIVE NEURAL NETWORK CONTROLLER DESIGN FOR BLENDED-WING UAV WITH COMPLEX DAMAGE | 2016_0516 |
| Ahn, M.H. | DEVELOPMENT OF HIGH-ORDER AND HIGH-RESOLUTION SCHEMES FOR EFFICIENT SHOCK CAPTURING IN HIGH-SPEED FLOWS | 2016_0705 |
| Ai, B. | PANEL VIBRO-ACOUSTIC RESPONSE PREDICTION BASED ON TURBULENT BOUNDARY LAYER MEASUREMENT | 2016_0040 |
| Akhmedzyanov, D.A. | KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES | 2016_0008 |
| Akhmedzyanov, D.A. | AUTOMATED SELECTION OF THE MATERIAL A FAN BLADE PS-90A | 2016_0068 |
| Akroyd, G. | STORE SEPARATION FROM WEAPON BAYS | 2016_0156 |
| Aksenov, A.A. | NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN | 2016_0550 |
| Alam, M.I. | MULTIDISCIPLINARY DESIGN OPTIMIZATION OF STRATOSPHERIC AIRSHIP | 2016_0703 |
| Aleksandrov, V.V. | THE FLYING QUALITIES IMPROVEMENT FOR THE VEHICLES WITH TIME DELAY IN THEIR DYNAMICS | 2016_0043 |
| Aleksandrov, V.Y. | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE | 2016_0380 |
| Alem, B. | INSTANTANEOUS BASELINE MULTIPLE DAMAGE DETECTION AND LOCALIZATION IN AN ALUMINIUM PLATE USING LAMB WAVES | 2016_0640 |
| Alfano, M. | CHAOS THEORY APPLIED TO BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELL | 2016_0673 |
| Alfredson, J. | DETECT AND AVOID FOR REMOTELY PILOTED AIRCRAFT IN AIR TRAFFIC CONTROL SIMULATIONS | 2016_0176 |
| Ali, A. | IMPORTANCE OF TRANSIENT AERODYNAMIC DERIVATIVES FOR V-TAIL AIRCRAFT FLIGHT DYNAMIC DESIGN | 2016_0515 |
| Almeida, S.F.M. | NUMERICAL SIMULATION IN FINITE ELEMENT METHOD AND MANUFACTURING OF LUG MATERIAL COMPOSITE BY RTM PROCESS | 2016_0279 |
| Amato, E.M. | ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES | 2016_0467 |
| Amelyushkin, I.A. | MATHEMATICAL MODELS AND OPTICAL INVESTIGATION OF TWO PHASE FLOWS IN WIND TUNNELS | 2016_0656 |
| Amiez, A. | NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION | 2016_0370 |
| Amiryants, G.A. | THE ACTIVE AEROELASTICITY CONCEPT - THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT | 2016_0436 |
| Andreeva-Mori, A. | DESIGN AND PRELIMINARY EVALUATION OF AN INTEGRATED AIRCRAFT OPERATION SYSTEM FOR DISASTER RELIEF | 2016_0088 |
| Andreeva-Mori, A. | IMPACT OF WEATHER UNCERTAINTIES ON NOISE CONTOURS AND NOISE ABATEMENT DESCENT TRAJECTORIES | 2016_0331 |
| Anisimov, K. | EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL | 2016_0572 |
| Anisimov, K. | AERODYNAMIC OPTIMIZATION OF AIRPLANE PROPULSION SYSTEM WITHIN THE FRAMEWORK OF AGILE PROJECT | 2016_0583 |
| Anton, F. | HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES | 2016_0744 |
| Anton Diez, A. | ADVANCED REFUELING BOOM SYSTEM (ARBS) DEVELOPMENT AND HANDLING QUALITIES EVALUATION | 2016_0586 |
| Antunes, A.P. | EFFECTS OF THE BOUNDARY LAYER TRANSITION ON THE GLOBAL AERODYNAMIC COEFFICIENTS | 2016_0330 |
| Arai, N. | EVALUATION OF CONCEPTUAL DESIGN BASED ON MANUFACTURED ACTUAL UNMANNED SOLAR PLANE | 2016_0685 |
| Ariola, M. | MODEL PREDICTIVE CONTROL FOR A SWARM OF FIXED WING UAVS | 2016_0326 |
| Ariyarit, A. | DESIGN OPTIMIZATION OF HELICOPTER BLADE USING CLASS SHAPE FUNCTION BASED GEOMETRY REPRESENTATION | 2016_0479 |
| Arkhipov, M. | SMALL HEIGHT DUCT DESIGN FOR MULTICOPTER FAN | 2016_0611 |
| Asai, K. | NON-INTRUSIVE UNSTEADY PSP TECHNIQUE FOR INVESTIGATION OF TRANSONIC BUFFETING | 2016_0553 |
| Asensio Nieto, F. | ADVANCED REFUELING BOOM SYSTEM (ARBS) DEVELOPMENT AND HANDLING QUALITIES EVALUATION | 2016_0586 |
| Atinault, O. | AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS | 2016_0092 |
| Atkin, C.J. | STAGGERED THREE-DIMENSIONAL CAVITIES AS A POSSIBLE METHOD FOR SKIN FRICTION DRAG REDUCTION | 2016_0606 |
| Atkin, C. | AFLONEXT – ACTIVE FLOW_LOADS AND NOISE CONTROL ON NEXT GENERATION ACTIVE WING | 2016_0755 |
| Avelar, A.C. | EXPERIMENTAL STUDY OF GEOMETRIC VARIATIONS EFFECT ON THE FLOW PATTERNS ON A HAMMERHEAD SATELLITE LAUNCH VEHICLE | 2016_0683 |
| Azevedo, J.L.F. | NUMERICAL SIMULATIONS OF TURBULENT FLOWS OVER THE ONERA-M6 AND DLR-F6 CONFIGURATIONS | 2016_0050 |
| Azevedo, J.L.F. | EFFECTS OF THE BOUNDARY LAYER TRANSITION ON THE GLOBAL AERODYNAMIC COEFFICIENTS | 2016_0330 |
| Babel, R. | COMPARATIVE ANALYSIS OF AIR FLOW IN THE COMPRESSOR OF THE GTD-350 ENGINE | 2016_0417 |
| Babiak, M. | IS TO BE THE MICRODRONE | 2016_0646 |
| Bach, T. | NUMERICAL ASSESSSMENT OF DAMAGE TOLERANCE ALLOWABLES FOR NEW DESIGN CONCEPTS OF STIFFENED COMPOSITE PANELS | 2016_0277 |
| Bae, S. | MULTI-STEP TRAJECTORY OPTIMIZATION FOR ATM BASED ON APPROXIMATED OPTIMAL PATH | 2016_0723 |
| Bagassi, S. | AUGMENTED AND VIRTUAL REALITY IN THE AIRPORT CONTROL TOWER | 2016_0719 |
| Bagassi, S. | GENERATIVE DESIGN: ADVANCED DESIGN OPTIMIZATION PROCESSES FOR AERONAUTICAL APPLICATIONS | 2016_0720 |
| Bai, Y.-G. | DESIGN, MANUFACTURE AND FREQUENCY EXPERIMENT OF A NOVEL FLUTTER MODEL FOR AGARD WING 445.6 WITH STRUCTURE-SIMILARITY | 2016_0519 |
| Bai, Y.-G. | INFLUENCE OF THE RHOMBOID ZONE ON AEROELASTIC EXPERIMENTS OF SUPERSONIC AIRCRAFT | 2016_0564 |
| Baklanov, V. | DYNAMICS AND VIBRATION OF NEW GENERATION AVIATION ENGINES | 2016_0566 |
| Balakrishnan, H. | STATISTICAL MODELING OF AIRCRAFT ENGINE FUEL FLOW RATE | 2016_0619 |
| Balasubramanian, P. | DYNAMIC MODELING AND STABILITY ANALYSIS OF A HIGH ALTITUDE AIRSHIP | 2016_0700 |
| Balunov, K.A. | MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS | 2016_0226 |
| Ban, N. | LOW-DRAG / LOW-BOOM SHAPE OPTIMIZATION OF A BIPLANE WING / TWIN-BODY FUSELAGE SST CONFIGURATION | 2016_0283 |
| Bang, H.C. | OPERATION SCENARIOS OF UNMANNED AIRCRAFT SYSTEMS INTEGRATED INTO THE KOREAN NATIONAL AIRSPACE SYSTEM | 2016_0445 |
| Barbosa, L.M.F. | STUDY OF THE COMPROMISE OF AERODYNAMIC AND STRUCTURE STANDPOINTS IN A HIGH-ASPECT RATIO WING DESIGN | 2016_0615 |
| Barrier, R. | AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS | 2016_0092 |
| Bartasevicius, J. | ACTIVE VORTEX FLOW CONTROL ON A GENERIC DELTA WING | 2016_0257 |
| Bartels, R. | MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES | 2016_0596 |
| Battaglia, F. | A COMPUTATIONAL STUDY ON AVIAN FLAPPING FLIGHT AND THE INFLUENCE OF FEATHER SEPARATION | 2016_0657 |
| Baumann, S. | AN INTERFACE CONCEPT TO SUPPORT THE COCKPIT CREW DURING TRAJECTORY-BASED DISPATCH TOWING | 2016_0080 |
| Baumann, S. | ACOUSTICAL COMPARISON OF CONVENTIONAL TAXIING AND DISPATCH TOWING - TAXIBOT´S CONTRIBUTION TO GROUND NOISE ABATEMENT | 2016_0454 |
| Bayandor, J. | A FOLDABLE FLAPPING WING DESIGN INSPIRED BY THE ELBOW-WRIST ANATOMY OF BATS | 2016_0609 |
| Bayandor, J. | CHARACTERIZATION OF DISTORTED FLUID FLOW ALONG ADVANCED HIGH-BYPASS PROPULSION SYSTEM | 2016_0628 |
| Bayandor, J. | ADVANCED PROPULSION COLLISION DAMAGE DUE TO UNMANNED AERIAL SYSTEM INGESTION | 2016_0629 |
| Bayandor, J. | LOW ORDER MODELING OF THE UNSTEADY AND 3D EFFECTS OF CONTINUOUS WAKE FLAPPING FLIGHT | 2016_0651 |
| Bayandor, J. | A COMPUTATIONAL STUDY ON AVIAN FLAPPING FLIGHT AND THE INFLUENCE OF FEATHER SEPARATION | 2016_0657 |
| Bayandor, J. | DYNAMICS MODELLING FOR CONTROL OF AN UNSTEADY HYDRODYNAMIC STINGRAY ROBOT | 2016_0658 |
| Bayandor, J. | NUMERICAL INVESTIGATION OF FAN-BLADE OUT USING MESO-SCALE COMPOSITE MODELING | 2016_0670 |
| Becker, R. | COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT | 2016_0345 |
| Bedouet, J. | MODELLING, GENERATING AND EVALUATING SECTOR CONFIGURATION PLANS - METHODOLOGY REPORT OF THE SESAR VP-755 EXERCISE | 2016_0063 |
| Bedouet, J. | TOWARDS A 4D TRAFFIC MANAGEMENT OF SMALL UAS OPERATING AT VERY LOW LEVEL | 2016_0064 |
| Been, Y.B. | A NEW SOLUTION METHOD FOR SIX DEGREE OF FREEDOM FLIGHT DYNAMICS SIMULATION OF A HIGH ASPECT RATIO WING VEHICLE | 2016_0158 |
| Beerhorst, M. | WEIGHT REDUCTION OF CYLINDRICAL GRID STRUCTURES USING AXIAL-HELICAL-DESIGN | 2016_0708 |
| Belo, E.M. | SYSTEM IDENTIFICATION OF A SCALE HELICOPTER IN HOVERING FLIGHT | 2016_0686 |
| Ben-Asher, J.Z. | FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS | 2016_0073 |
| Berk, T.A. | EXPERIMENTAL STUDY ON AERODYNAMIC LOAD CONTROL USING SYNTHETIC JET ACTUATORS | 2016_0389 |
| Berlowitz, I. | COMMERCIAL DERIVATIVE AIRCRAFT AND TURBINE ENGINE | 2016_0002 |
| Bernatzky, T. | AN INTERFACE CONCEPT TO SUPPORT THE COCKPIT CREW DURING TRAJECTORY-BASED DISPATCH TOWING | 2016_0080 |
| Berry, P. | KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD OPTIMIZATION | 2016_0375 |
| Bewick, C. | THE ROLLS-ROYCE PLC ULTRAFAN HEAT MANAGEMENT CHALLENGE | 2016_0344 |
| Bezzina, F. | CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION | 2016_0211 |
| Bigarella, E.D.V. | EFFECTS OF SOME NUMERICAL FORMULATION ASPECTS IN HIGH-LIFT CONFIGURATION SIMULATIONS | 2016_0713 |
| Bijewitz, J. | A REVIEW OF RECENT AIRCRAFT CONCEPTS EMPLOYING SYNERGISTIC PROPULSION-AIRFRAME INTEGRATION | 2016_0727 |
| Bil, C. | THE DESIGN OF AN AUTOMATIC BEACON EJECTING SYSTEM FOR AIRCRAFT | 2016_0465 |
| Bil, C. | INFLUENCE OF ETHNICITY ON PASSENGER STANDARD WEIGHT | 2016_0466 |
| Birukov, R.V. | CONTROL OF CONDITION OF GAS TURBINE ENGINE ROTOR BEARINGS IN DIAGNOSTIC PARAMETERS IN A DIFFERENT PHYSICAL NATURE | 2016_0273 |
| Bisagni, C. | CHAOS THEORY APPLIED TO BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELL | 2016_0673 |
| Bittner, M. | OPTIMAL APPROACH TRAJECTORIES FOR MULTIPLE AIRCRAFT CONSIDERING DISTURBANCES AND CONFIGURATION CHANGES | 2016_0051 |
| Bittner, M. | FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS | 2016_0073 |
| Bittner, M. | OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH | 2016_0287 |
| Blase, T. | ADVANCED RNP TO ILS AUTOLAND APPROACHES FOR OPTIMAL BENEFITS FROM PBN: FLIGHT TESTING PROCEDURES WITH AN A320 | 2016_0147 |
| Blasi, L. | NONLINEAR DYNAMIC INVERSION WITH NEURAL NETWORKS FOR THE FLIGHT CONTROL OF A LOW COST TILT ROTOR UAV | 2016_0637 |
| Bo, J.-L. | NUMERICAL INVESTIGATION OF UNSTEADY INTERACTION CHARACTERISTIC INDUCED BY IMPULSIVE JET | 2016_0362 |
| Bode-Oke, A.T. | STRATEGIES FOR ACHIEVING BACKWARD FLIGHT BY A DRAGONFLY | 2016_0754 |
| Bogdanski, K. | ANALYSES OF AIRFLOW AROUND DUCTED FAN PROPULSION SYSTEM IN PUSHER CONFIGURATION USING PIV METHOD | 2016_0659 |
| Boggero, L. | COLLABORATIVE SYSTEMS DRIVEN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION | 2016_0585 |
| Bonet, J.T. | UHB ENGINE INTEGRATION FOR HYBRID WING BODY AIRCRAFT | 2016_0741 |
| Boniface, J.-C. | AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS | 2016_0092 |
| Bons, J. -P. | AN AERODYNAMIC ANALYSIS OF THE 3D FLOW AROUND THE SSC-A09 AIRFOIL | 2016_0671 |
| Booij, P.J.A. | QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH | 2016_0555 |
| Borener, S. | ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS | 2016_0413 |
| Bosnyakov, I. | COMPUTATIONAL EFFICIENCY AND QUALITY OF DIFFERENT VERSIONS OF DISCONTINUOUS GALERKIN METHOD FOR LES/DES APPLICATIONS | 2016_0099 |
| Bradley, M.K. | HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES | 2016_0744 |
| Braun, R. | METHODS FOR AUTOMATING MODEL VALIDATION: STEADY-STATE IDENTIFICATION APPLIED ON GRIPEN FIGHTER ENVIRONMENTAL CONTROL SYSTEM MEASUREMENTS | 2016_0188 |
| Bravo-Mosquera , P.D. | EXPERIMENTAL ANALYSES OF DROOP, WINGTIPS AND FENCES ON A BWB MODEL | 2016_0262 |
| Bravo-Mosquera, P.D. | CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING | 2016_0397 |
| Breitsamter, C. | SENSITIVITY ANALYSIS OF UNSTEADY AERODYNAMIC REDUCED-ORDER MODELS ROBUST TO FREESTREAM PARAMETER VARIATIONS | 2016_0206 |
| Breitsamter, C. | ACTIVE VORTEX FLOW CONTROL ON A GENERIC DELTA WING | 2016_0257 |
| Breitsamter, C. | AERODYNAMIC TESTING OF HELICOPTER NOVEL AIR INTAKES | 2016_0508 |
| Brown, M. | VISUALIZATION OF AIRSPACE COMPLEXITY BASED ON AIR TRAFFIC CONTROL DIFFICULTY | 2016_0160 |
| Brown, M. | EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA | 2016_0682 |
| Brutyan, M.A. | NEW METHOD OF TRANSONIC BUFFET DECREASING ON SUPERCRITICAL AIRFOIL | 2016_0127 |
| Brutyan, M.A. | INFLUENCE OF SURFACE FRACTAL MICROSTRUCTURE ON THE CHARACTERISTICS OF A TURBULENT BOUNDARY LAYER | 2016_0138 |
| Budaev, V.P. | INFLUENCE OF SURFACE FRACTAL MICROSTRUCTURE ON THE CHARACTERISTICS OF A TURBULENT BOUNDARY LAYER | 2016_0138 |
| Burgstaller, F. | IN-FLIGHT PROVISIONING AND DISTRIBUTION OF ATM INFORMATION | 2016_0385 |
| Buttsworth, D. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Buzica, A. | ACTIVE VORTEX FLOW CONTROL ON A GENERIC DELTA WING | 2016_0257 |
| Candon, M. | CHARACTERIZATION OF THE NONLINEAR AEROELASTIC BEHAVIOR OF AN AIRFOIL WITH FREEPLAY AND AERODYNAMIC NONLINEARITY | 2016_0716 |
| Cao, N. | EXPERIMENTAL INVESTIGATION OF LATERAL PULSE JET INTERACTION FLOWFIELD IN HYPERSONIC FLOW | 2016_0391 |
| Carossa, G.M. | EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL | 2016_0572 |
| Carrese, R. | ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES | 2016_0467 |
| Carrese, R. | CHARACTERIZATION OF THE NONLINEAR AEROELASTIC BEHAVIOR OF AN AIRFOIL WITH FREEPLAY AND AERODYNAMIC NONLINEARITY | 2016_0716 |
| Catalano, F.M. | LOW REYNOLDS PROPELLER META-MODEL FOR MULTIDICIPLYNARY OPTIMIZATION | 2016_0003 |
| Catalano, F.M. | CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING | 2016_0397 |
| Catalanode, F.M. | EXPERIMENTAL ANALYSES OF DROOP, WINGTIPS AND FENCES ON A BWB MODEL | 2016_0262 |
| Cen, F. | WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS | 2016_0091 |
| Cenko, A. | STORE SEPARATION FROM WEAPON BAYS | 2016_0156 |
| Cerón-Muñoz, H.D. | EXPERIMENTAL ANALYSES OF DROOP, WINGTIPS AND FENCES ON A BWB MODEL | 2016_0262 |
| Cerón-Muñoz, H.D. | CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING | 2016_0397 |
| Cervinka, J. | EXPERIMENATAL AND COMPUTATIONAL STUDY OF GROUND EFFECT ON AIRFOIL SECTION | 2016_0122 |
| Cervinka, J. | SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL | 2016_0593 |
| Cestino, E. | ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES | 2016_0467 |
| Chae, S. | EFFICIENT MULTI-RESOLUTION ANALYSIS FOR IMPLICIT TEMPORAL INTEGRATION | 2016_0427 |
| Chakraborti, D. | DYNAMIC MODELING AND STABILITY ANALYSIS OF A HIGH ALTITUDE AIRSHIP | 2016_0700 |
| Chang, Y.H. | SECURE ESTIMATION FOR UNMANNED AERIAL VEHICLES AGAINST ADVERSARIAL ATTACKS | 2016_0221 |
| Chang, K. | CFD OF BLENDED WING BODY UCAV WITH VORTEX GENERATOR | 2016_0246 |
| Chapuis, D. | THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION | 2016_0731 |
| Chati, Y.S. | STATISTICAL MODELING OF AIRCRAFT ENGINE FUEL FLOW RATE | 2016_0619 |
| Chedrik, V.V. | MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS | 2016_0226 |
| Chen, H. | 3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION | 2016_0039 |
| Chen, L. | NUMERICAL SIMULATION OF RCS FOR A SPHERICAL CONVERGENT FLAP NOZZLE WITH A NON-RECTANGULAR DIVERGENT DUCT | 2016_0077 |
| Chen, Z.H. | UNCERTAINTY QUANTIFICATION AND GLOBAL SENSITIVITY ANALYSIS FOR HYPERSONIC AEROTHERMOELASTIC ANALYSIS | 2016_0135 |
| Chen, L.-C. | DETACHED EDDY SIMULATION OF AIRCRAFT MASSIVELY SEPARATED FLOWS | 2016_0140 |
| Chen, C.W.W. | A TEST METHOD BASED ON AIRCRAFT PLATFORM FOR ATMOSPHERIC LASER VISIBILITY | 2016_0167 |
| Chen, J. | RESEARCH ON LOAD SPECTRUM OF AERO HYDRAULIC PUMP BASED ON ACCELERATED DEGRADATION TESTING | 2016_0181 |
| Chen, Z. | PHYSICALLY-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION FRAMEWORK COUPLING AIRFRAME AND PROPULSION | 2016_0268 |
| Chen, X. | A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM | 2016_0321 |
| Chen, Y. | A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM | 2016_0321 |
| Chen, J. | A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM | 2016_0321 |
| Chen, Q. | DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL | 2016_0403 |
| Chen, Z. | A CONCEPTUAL DESIGN PLATFORM FOR BLENDED-WING-BODY TRANSPORTS | 2016_0510 |
| Chen, H. | A STUDY ON SAFETY ASSURANCE FOR INCREASINGLY AUTONOMOUS TRAFFIC FLOW MANAGEMENT SYSTEM | 2016_0672 |
| Cheng, C.Y. | A TEST METHOD BASED ON AIRCRAFT PLATFORM FOR ATMOSPHERIC LASER VISIBILITY | 2016_0167 |
| Chernov, A.V. | DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS | 2016_0620 |
| Chernyshev, S.L. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Chevagin, A. | EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL | 2016_0572 |
| Chiba, T. | INTEGRATED CONCEPTUAL DESIGN METHOD CONSIDERING ADVANCED AIRCRAFT SYSTEMS AND AIRCRAFT TRAJECTORY | 2016_0317 |
| Chinchapatnam, P. | IDENTIFYING THE BEST DESIGN FOR UNCERTAIN MARKETS | 2016_0626 |
| Chircop, K. | CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION | 2016_0211 |
| Cho, A. | LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV | 2016_0062 |
| Cho, H. | FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING | 2016_0123 |
| Cho, N. | APPROXIMATE THREE-DIMENSIONAL PATH GENERATION FOR UAV PATH-FOLLOWING | 2016_0128 |
| Cho, I. | AN INVESTIGATION OF EFFECTS OF FLIGHT MANEUVERS ON A SUPERSONIC AIRCRAFT WITH HORIZONTAL TAIL ACTUATOR FAILURE | 2016_0251 |
| Cho, S. | FLIGHT TESTS OF THE VISION-BASED TARGET SENSING AND APPROACHING | 2016_0373 |
| Cho, M.-H. | TRAJECTORY DESIGN WITH PATH PREDICTION FOR TERRAIN FOLLOWING | 2016_0379 |
| Cho, S. | GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV | 2016_0399 |
| Cho, J.H. | APPLICATION OF PROPER ORTHOGONAL DECOMPOSITION FOR AVIATION SAFETY | 2016_0576 |
| Choi, S. | ON MORE EFFECTIVE AERODYNAMIC DATA GENERATION FOR SIMULATION BASED AIRCRAFT CONCEPTUAL DESIGN | 2016_0151 |
| Choi, H.-L. | CLOSED-FORM COOPERATIVE GUIDANCE LAW FOR TWO MISSILES WITH COUPLED TERMINAL VELOCITY CONSTRAINTS | 2016_0387 |
| Choi, S. | GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV | 2016_0399 |
| Choi, H.-L. | MISSILE AUTOPILOT DESIGN USING CONTRACTION THEORY-BASED OUTPUT FEEDBACK CONTROL | 2016_0474 |
| Choi, Y.-J. | NUMERICAL INVESTIGATION OF SUBSONIC RAREFIED FLOWS USING DSMC-IP METHODS | 2016_0556 |
| Choi, S. | DEVELOPMENT OF A THREE-DIMENSIONAL TIGHTLY COUPLED EULER/POTENTIAL FLOW SOLVER FOR TRANSONIC FLOW | 2016_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 STRUCTURES | 2016_0522 |
| Churkina, T.E. | OPTIMIZATION OF THE TRAJECTORY AND ACCUMULATOR MASS FOR THE SOLAR-POWERED AIRPLANE | 2016_0388 |
| Ciampa, P.D. | TOWARDS THE 3RD GENERATION MDO COLLABORATIVE ENVIRONMENT | 2016_0563 |
| Ciampa, P.D. | COLLABORATIVE SYSTEMS DRIVEN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION | 2016_0585 |
| Ciloni, P.A.G. | EFFECTS OF SOME NUMERICAL FORMULATION ASPECTS IN HIGH-LIFT CONFIGURATION SIMULATIONS | 2016_0713 |
| Cimini Jr., C.A. | BEARING STRENGTH ASSESSMENT OF COMPOSITE MATERIAL THROUGH NUMERICAL MODELS | 2016_0633 |
| Collier, F. | ENVIRONMENTALLY RESPONSIBLE AVIATION PROJECT OVERVIEW | 2016_0738 |
| Conway, S.R. | AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS | 2016_0202 |
| Craig, K.J. | OPTIMISATION OF A WING-BODY-TAIL CONFIGURATION WITH AN ALTERNATIVE LOW DRAG FUSELAGE AND BODY TRAILING EDGE | 2016_0223 |
| Cramer, K.E. | RESEARCH DEVELOPMENTS IN NONDESTRUCTIVE EVALUATION AND STRUCTURAL HEALTH MONITORING FOR THE SUSTAINMENT OF COMPOSITE AEROSPACE STRUCTURES AT NASA | 2016_0733 |
| Cresto Aleina, S. | INVESTIGATIONS OF GROUND INFRASTRUCTURES FOR UAS FLIGHT MONITORING | 2016_0514 |
| Cui, J. | NUMERICAL SIMULATION OF RCS FOR A SPHERICAL CONVERGENT FLAP NOZZLE WITH A NON-RECTANGULAR DIVERGENT DUCT | 2016_0077 |
| Cui, D.-G. | FAIRING OPTIMIZATION DESIGN OF WING STRUCTURE | 2016_0282 |
| Cui, D.-G. | APPLICATION OF BUCKLING/POST-BUCKLING ANALYSIS FOR COMPOSITE STIFFENED PANELS | 2016_0337 |
| Cui, A. | FLEET DEVELOPMENT PLANNING OF AIRLINES: INCORPORATING THE AIRCRAFT OPERATING ECONOMICS FACTOR | 2016_0357 |
| Czajkowski, L. | MODERN MATERIALS IN AEROSPACE INDUSTRY - MAGNESIUM ALLOY CONTROL SYSTEM LEVER OF THE UNMANNED ILX - 27 HELICOPTER | 2016_0457 |
| Czekalowski, P. | AN EXPERIMENTAL STUDY OF MICRO-ELECTROMECHANICAL FLYING INSECT FLAPPING WINGS AERODYNAMIC PERFORMANCE | 2016_0025 |
| D'Amato, E. | AERODYNAMIC ANALYSIS WITH SEPARATION DYNAMICS OF A LAUNCHER AT STAGING CONDITIONS | 2016_0570 |
| da Silva, R.G. | NUMERICAL SIMULATIONS OF TURBULENT FLOWS OVER THE ONERA-M6 AND DLR-F6 CONFIGURATIONS | 2016_0050 |
| da Silva, R.G. | EFFECTS OF THE BOUNDARY LAYER TRANSITION ON THE GLOBAL AERODYNAMIC COEFFICIENTS | 2016_0330 |
| da Silva, R.G.A. | SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT | 2016_0390 |
| Dala, L. | ON APPLYING PISTON THEORY IN INTERFERENCE FLOWS | 2016_0225 |
| Damljanovic, D. | A STUDY OF WALL-INTERFERENCE EFECTS IN WIND-TUNNEL TESTING OF A STANDARD MODEL AT TRANSONIC SPEEDS | 2016_0216 |
| Damljanovic, D. | A GENERALISATION OF THE MATHEMATICAL MODEL OF INTERNAL WIND TUNNEL BALANCES | 2016_0329 |
| Danilin, A.I. | DESIGNING OF AIRFRAMES HAVING MINIMUM MASS UNDER SEVERAL LOADINGS (NOT ONLY FULLY STRESSED) | 2016_0098 |
| Danilkin, S.Y. | EFFECT OF REYNOLDS NUMBER, OPERATING MODE, TURBULENCE PARAMETERS ON PROFILE AND SECONDARY LOSSES OF LPT | 2016_0276 |
| Danilov, M.K. | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE | 2016_0380 |
| Daoud, F. | COLLABORATIVE AIRCRAFT DESIGN USING AN INTEGRATED AND DISTRIBUTED MULTIDISCIPLINARY PRODUCT DEVELOPMENT PROCESS | 2016_0328 |
| Dautermann, T. | ADVANCED RNP TO ILS AUTOLAND APPROACHES FOR OPTIMAL BENEFITS FROM PBN: FLIGHT TESTING PROCEDURES WITH AN A320 | 2016_0147 |
| De Breuker, R. | DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM | 2016_0166 |
| de Bruin, A.C. | KAI SURION HELICOPTER FULL-SCALE AIR INTAKE TESTING AT CIRA ICING WIND TUNNEL | 2016_0496 |
| De Crescenzio, F. | AUGMENTED AND VIRTUAL REALITY IN THE AIRPORT CONTROL TOWER | 2016_0719 |
| De Crescenzio, F. | GENERATIVE DESIGN: ADVANCED DESIGN OPTIMIZATION PROCESSES FOR AERONAUTICAL APPLICATIONS | 2016_0720 |
| de Freitas Pinto, R.L.U. | STUDY OF THE COMPROMISE OF AERODYNAMIC AND STRUCTURE STANDPOINTS IN A HIGH-ASPECT RATIO WING DESIGN | 2016_0615 |
| de Moura Pinho, R. | A STRESS INTENSITY FACTOR SOLUTION INSPIRED BY SOAP BUBBLES FRAMEWORK | 2016_0288 |
| De Visscher, I. | WAKE TURBULENCE RE-CATEGORISATION ON APPROACH AND DEPARTURE FOR SAFE AND MORE EFFICIENT AIR TRAFFIC MANAGEMENT | 2016_0230 |
| Degenhardt, R. | NEW DESIGN SCENARIO FOR FUTURE COMPOSITE LAUNCHER STRUCTURES | 2016_0037 |
| Degiorgio, J. | CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION | 2016_0211 |
| Degrémont, S. | MODELLING, GENERATING AND EVALUATING SECTOR CONFIGURATION PLANS - METHODOLOGY REPORT OF THE SESAR VP-755 EXERCISE | 2016_0063 |
| Deinert, S. | COLLABORATIVE AIRCRAFT DESIGN USING AN INTEGRATED AND DISTRIBUTED MULTIDISCIPLINARY PRODUCT DEVELOPMENT PROCESS | 2016_0328 |
| Delbecq, S. | SURROGATE MODELING TECHNIQUE FOR THE CONCEPTUAL AND PRELIMINARY DESIGN OF EMBEDDED ACTUATION SYSTEMS AND COMPONENTS | 2016_0184 |
| Deng, X.Y. | MULTI-POINT DESIGN OPTIMIZATION OF A HIGH BYPASS RATIO FAN BLADE | 2016_0172 |
| Denti, E. | NONLINEAR MODEL IDENTIFICATION OF A SMALL-SCALE UNMANNED ROTORCRAFT | 2016_0076 |
| Desai, A.A. | IDENTIFYING THE BEST DESIGN FOR UNCERTAIN MARKETS | 2016_0626 |
| Di Rito, G. | EXPERIMENTAL AND SIMULATION STUDY OF THE DYNAMICS OF AN ELECTRO-MECHANICAL LANDING GEAR ACTUATOR | 2016_0049 |
| Di Rito, G. | NONLINEAR MODEL IDENTIFICATION OF A SMALL-SCALE UNMANNED ROTORCRAFT | 2016_0076 |
| Dias, E.S. | BEARING STRENGTH ASSESSMENT OF COMPOSITE MATERIAL THROUGH NUMERICAL MODELS | 2016_0633 |
| Diaz-Izquierdo, D.O. | EXPERIMENTAL ANALYSES OF DROOP, WINGTIPS AND FENCES ON A BWB MODEL | 2016_0262 |
| Diepolder, J. | FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS | 2016_0073 |
| Diepolder, J. | OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH | 2016_0287 |
| Dimithe Aboumou, L. | A STRESS INTENSITY FACTOR SOLUTION INSPIRED BY SOAP BUBBLES FRAMEWORK | 2016_0288 |
| Ding, D. | ANALYSIS ON OFFLINE AND ONLINE IDENTIFICATION METHODS FOR AIRCRAFT STABILITY AND CONTROL DERIVATIVES | 2016_0203 |
| Dinulovic, M. | THE ANALYSIS OF LAMINATE LAY-UP EFFECT ON THE FLUTTER SPEED OF COMPOSITE STABILIZERS | 2016_0271 |
| Dong, M. | EXTENDED LOCAL SCATTERING THEORY AND THE ROLE OF A SCATTER ON BOUNDARY-LAYER INSTABILITY AND ACOUSTIC RADIATION | 2016_0333 |
| Dong, L.-J. | APPLICATION OF BUCKLING/POST-BUCKLING ANALYSIS FOR COMPOSITE STIFFENED PANELS | 2016_0337 |
| Dong, H. | STRATEGIES FOR ACHIEVING BACKWARD FLIGHT BY A DRAGONFLY | 2016_0754 |
| Donjat, D. | COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN "MORE ELECTRICAL AIRCRAFT" | 2016_0105 |
| Dornwald, J. | COLLABORATIVE AIRCRAFT DESIGN USING AN INTEGRATED AND DISTRIBUTED MULTIDISCIPLINARY PRODUCT DEVELOPMENT PROCESS | 2016_0328 |
| Drees, L. | FUEL STARVATION CAUSED BY HUB CLOSURE | 2016_0513 |
| Du, M. | 3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION | 2016_0039 |
| Duan, S.H. | PID TUNING FOR MULTI-CHANNEL STRUCTURAL FATIGUE TESTING SYSTEM | 2016_0159 |
| Dubot, T. | MODELLING, GENERATING AND EVALUATING SECTOR CONFIGURATION PLANS - METHODOLOGY REPORT OF THE SESAR VP-755 EXERCISE | 2016_0063 |
| Dubot, T. | TOWARDS A 4D TRAFFIC MANAGEMENT OF SMALL UAS OPERATING AT VERY LOW LEVEL | 2016_0064 |
| Dubovikov, E. | DAMAGE TOLERANCE AND REPAIR OF UD-RIBS OF LATTICE COMPOSITE FUSELAGE STRUCTURES | 2016_0443 |
| Dudarkov, Y.I. | EXPERIENCE OF USING NONLINEAR NUMERICAL ANALYSIS TO ESTIMATE AIRCRAFT PRIMARY STRUCTURE STRENGTH | 2016_0201 |
| Dutta, P. | FORMAL VERIFICATION OF AUTOPILOTS IN UMANNED AIRCRAFT SYSTEMS | 2016_0190 |
| Dyadkin , A.A. | NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN | 2016_0550 |
| Dzuba, A.S. | EXPERIENCE OF USING NONLINEAR NUMERICAL ANALYSIS TO ESTIMATE AIRCRAFT PRIMARY STRUCTURE STRENGTH | 2016_0201 |
| Dzuba, A. | NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES | 2016_0551 |
| D\'Amato, E. | NONLINEAR DYNAMIC INVERSION WITH NEURAL NETWORKS FOR THE FLIGHT CONTROL OF A LOW COST TILT ROTOR UAV | 2016_0637 |
| D\'Souza, S.N. | APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS | 2016_0185 |
| D\\\'Amato, E. | MODEL PREDICTIVE CONTROL FOR A SWARM OF FIXED WING UAVS | 2016_0326 |
| Döll, C. | DISTRIBUTED ELECTRIC PROPULSION FOR SMALL BUSINESS AIRCRAFT A CONCEPT-PLANE FOR KEY-TECHNOLOGIES INVESTIGATIONS | 2016_0461 |
| Ebrahimi, M. | AERODYNAMIC SHAPE OPTIMIZATION WITH A NEW PARALLEL EVOLUTIONARY ALGORITHM AND NUMERICAL FLOW MODELLING | 2016_0717 |
| Eek, M. | METHODS FOR AUTOMATING MODEL VALIDATION: STEADY-STATE IDENTIFICATION APPLIED ON GRIPEN FIGHTER ENVIRONMENTAL CONTROL SYSTEM MEASUREMENTS | 2016_0188 |
| Efimov, R. | EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL | 2016_0572 |
| Efremov , A.V. | THE FLYING QUALITIES IMPROVEMENT FOR THE VEHICLES WITH TIME DELAY IN THEIR DYNAMICS | 2016_0043 |
| Egorov, I. | NUMERICAL SIMULATION OF AEROTHERMODYNAMIC CHARACTERISTICS OF FLOW OVER SPACE VEHICLE MODEL | 2016_0381 |
| Egorov, I.V. | AEROTHERMODYNAMICS CHARACTERISTICS OF A SPACE PROBE IN THE MARTIAN ATMOSPHERE | 2016_0386 |
| Egorov, I.V. | DIRECT NUMERICAL SIMULATION OF DISTURBANCES IN A THREE-DIMENSIONAL HYPERSONIC NEAR-WALL FLOW OVER FLAT PLATE AND COMPRESSION CORNER | 2016_0536 |
| Eitelberg, G. | ANALYSIS OF SWIRL RECOVERY VANES FOR INCREASED PROPULSIVE EFFICIENCY IN TRACTOR PROPELLER AIRCRAFT | 2016_0060 |
| El Haddad, N.R. | DETAILED AERO-STRUCTURAL DESIGN OF WINGLET FOR BUSINESS JET | 2016_0052 |
| Engelmann, M. | BOARDING PROCESS ASSESSMENT OF NOVEL AIRCRAFT CABIN CONCEPTS | 2016_0218 |
| Enomoto, S. | FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS | 2016_0393 |
| Entezari, M.M. | CFD-BASED AERODYNAMIC SHAPE OPTIMIZATION OF A MANNED RE-ENTRY VEHICLE | 2016_0627 |
| Entzinger, J.O. | OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS | 2016_0338 |
| Episkopou, P. | GEOMETRIC ROUGHNESS EFFECTS ON THE AERODYNAMIC CHARACTERISTICS OF A SPINNING CYLINDER IN CROSSFLOW | 2016_0250 |
| Epstein, A. | FUEL-FLEXIBLE, COMBUSTOR AND FAN DEVELOPMENTS FOR UHB ENGINES | 2016_0740 |
| Epstein, A. | THE FUTURE OF SUSTAINABLE COMMERCIAL PROPULSION | 2016_0745 |
| Erlandsson, T. | PLANNING AIR TEAM MISSIONS WITH MULTIPLE OBJECTIVES | 2016_0059 |
| Esteyne, D. | THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION | 2016_0731 |
| Ezhov, V. | THE FOAMING PROPERTIES OF LUBRICATING OILS FOR AIRCRAFT GAS TURBINE ENGINES | 2016_0270 |
| Fakkowski, K. | DEVELOPMENT OF THE SMALL-SCALE MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT SAFETY TAKE-OFF AND LANDING | 2016_0359 |
| Falcão Filho, J.B.P. | EXPERIMENTAL STUDY OF GEOMETRIC VARIATIONS EFFECT ON THE FLOW PATTERNS ON A HAMMERHEAD SATELLITE LAUNCH VEHICLE | 2016_0683 |
| Falzon, K. | CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION | 2016_0211 |
| Fares, E. | EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL | 2016_0260 |
| Farkhondeh, F. | AIRLINES MAINTENANCE COST ANALYSIS USING SYSTEM DYNAMICS MODELING | 2016_0452 |
| Fateev, V.A. | DEVELOPMENT OF THE FAN STAGE WITH ULTRA-LOW ROTATIONAL SPEED | 2016_0261 |
| Fatigati, G. | KAI SURION HELICOPTER FULL-SCALE AIR INTAKE TESTING AT CIRA ICING WIND TUNNEL | 2016_0496 |
| Feaster, J. | A COMPUTATIONAL STUDY ON AVIAN FLAPPING FLIGHT AND THE INFLUENCE OF FEATHER SEPARATION | 2016_0657 |
| Fefermann, Y. | HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS | 2016_0438 |
| Feng, J.M. | PID TUNING FOR MULTI-CHANNEL STRUCTURAL FATIGUE TESTING SYSTEM | 2016_0159 |
| Feng, G. | LABYRINTH SEALS DYNAMIC COEFFICIENTS AND CRITICAL SPEED RESEARCH BASE OF CHILDS´ MODEL | 2016_0212 |
| Fenoglio, F. | CABIN ESCAPE SYSTEM: A WAY TO ENSURE CREW SAFETY DURING SUBORBITAL FLIGHTS | 2016_0506 |
| Ferretto, D. | CABIN ESCAPE SYSTEM: A WAY TO ENSURE CREW SAFETY DURING SUBORBITAL FLIGHTS | 2016_0506 |
| Fioriti, M. | COLLABORATIVE SYSTEMS DRIVEN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION | 2016_0585 |
| Firooz, S. | OPTIMIZATION OF COMPOSITE PATCH REPAIR FOR INCLINED CRACK ON ALUMINUM PLATE USING GENETIC ALGORITHM | 2016_0500 |
| Flaszynski, P. | SOURCE TERM MODEL FOR STREAMWISE JET VORTEX GENERATOR MODELLING | 2016_0521 |
| Florjancic, D. | IMPROVED DESIGN OF A HIGH LIFT SYSTEM FOR GENERAL AVIATION AIRCRAFT | 2016_0347 |
| Fomin, V. | DAMAGE TOLERANCE AND REPAIR OF UD-RIBS OF LATTICE COMPOSITE FUSELAGE STRUCTURES | 2016_0443 |
| Fomin, D.Y. | DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS | 2016_0620 |
| Fonseca, G.C. | NUMERICAL SIMULATION IN FINITE ELEMENT METHOD AND MANUFACTURING OF LUG MATERIAL COMPOSITE BY RTM PROCESS | 2016_0279 |
| Fonte, F. | DESIGN, MANUFACTURING AND VALIDATION OF A GUST GENERATOR FOR WIND TUNNEL TEST OF A LARGE SCALE AEROELASTIC MODEL | 2016_0676 |
| Fouladi, E. | AIRLINES MAINTENANCE COST ANALYSIS USING SYSTEM DYNAMICS MODELING | 2016_0452 |
| Frank, S. | SENSOR CONCEPT OF HIGHLY-AUTOMATED AIRPORT TUGS FOR REDUCED EMISSION TAXI OPERATIONS | 2016_0530 |
| Fricke, T. | STRATEGIES FOR MANUAL LANDING OF REMOTELY PILOTED AIRPLANES WITH LARGE TIME DELAY | 2016_0444 |
| Frulla, G. | ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES | 2016_0467 |
| Fu, J. | SPECIAL CONSIDERATIONS TO THERMAL BEHAVIOR MODELING AND SIMULATION OF AN AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEM | 2016_0554 |
| Fu, Y. | SPECIAL CONSIDERATIONS TO THERMAL BEHAVIOR MODELING AND SIMULATION OF AN AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEM | 2016_0554 |
| Fujita, K. | EFFECT OF YAW-TILTED HINGE AXIS ON DEPLOYMENT ROBUSTNESS OF MARS AIRPLANE | 2016_0477 |
| Fukumoto, H. | MINIMUM-TIME FORMATION USING OPTIMAL SOLUTIONS OF SINGLE FIXED-WING AIRCRAFT | 2016_0195 |
| Fukushima, S. | BENEFITS ASSESSMENT ON TIME-BASED OCEANIC ARRIVALS TO THE TOKYO METROPOLITAN AREA | 2016_0475 |
| Fumarola, I. | AN EXPERIMENTAL INVESTIGATION ON THE FREESTREAM TURBULENCE UPSTREAM OF A SWEPT WING | 2016_0582 |
| Fusaro, R. | SELECTION OF AN UAV CONFIGURATION LAYOUT FOR OPTIMISATION OF TELEDETECTION MISSION USING HYPERSPECTRAL SENSORS | 2016_0318 |
| Fusaro, R. | CABIN ESCAPE SYSTEM: A WAY TO ENSURE CREW SAFETY DURING SUBORBITAL FLIGHTS | 2016_0506 |
| Fusaro, R. | INVESTIGATIONS OF GROUND INFRASTRUCTURES FOR UAS FLIGHT MONITORING | 2016_0514 |
| Führer, T. | COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT | 2016_0345 |
| Gabrys, A. | FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS | 2016_0073 |
| Gafurov, S. | HIL TEST BENCH FOR ENGINE'S FUEL CONTROL SYSTEMS INVESTIGATION | 2016_0215 |
| Galatolo, R. | EXPERIMENTAL AND SIMULATION STUDY OF THE DYNAMICS OF AN ELECTRO-MECHANICAL LANDING GEAR ACTUATOR | 2016_0049 |
| Galatolo, R. | NONLINEAR MODEL IDENTIFICATION OF A SMALL-SCALE UNMANNED ROTORCRAFT | 2016_0076 |
| Galinski, C. | OVERVIEW OF THE INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME | 2016_0313 |
| Gao, C.Q. | NUMERICAL STUDY ON TRANSONIC BUFFET ACTIVE CONTROL BY OPEN AND CLOSED-LOOP STRATEGIES | 2016_0346 |
| Garcia Martinez-Pardo, A. | XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES | 2016_0193 |
| Gardi, A. | AUTOMATED SEPARATION ASSURANCE AND COLLISION AVOIDANCE FUNCTIONS IN THE CNS+A CONTEXT | 2016_0027 |
| Gardi, A. | PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORIES IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS | 2016_0691 |
| Gareyev, A.M. | IMPROVING THE EFFICIENCY AND RELIABILITY ASSESSMENT TECHNICAL STATE LIQUID SYSTEMS AIRCRAFT DURING ACCEPTANCE TESTS | 2016_0192 |
| Garijo Hernandez, D. | XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES | 2016_0193 |
| Garry, K. | THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW | 2016_0244 |
| Garry, K.P. | THE INFLUENCE OF A LOCAL CHANGE IN WING DIHEDRAL ON THE LOW SPEED FLOW CHARACTERISTICS OF RECTANGULAR PLANFORM WINGS | 2016_0459 |
| Garstka, A. | IS TO BE THE MICRODRONE | 2016_0646 |
| Gater, B. | DYNAMICS MODELLING FOR CONTROL OF AN UNSTEADY HYDRODYNAMIC STINGRAY ROBOT | 2016_0658 |
| Gati, B. | MOBILE LAUNCHING TREBUCHET FOR UAVS | 2016_0613 |
| Geister, R. | ADVANCED RNP TO ILS AUTOLAND APPROACHES FOR OPTIMAL BENEFITS FROM PBN: FLIGHT TESTING PROCEDURES WITH AN A320 | 2016_0147 |
| Gibbs, J. | EXPLORING PROPAGATED UNCERTAINTIES IN A MULTI-DISCIPLINARY AIRCRAFT DESIGN FRAMEWORK | 2016_0145 |
| Glebova, M. | DAMAGE TOLERANCE AND REPAIR OF UD-RIBS OF LATTICE COMPOSITE FUSELAGE STRUCTURES | 2016_0443 |
| Glowacki, P. | QUANTITATIVE EMISSIONS OF NOX, CO AND CO2 DURING AIRCRAFT OPERATIONS | 2016_0097 |
| Goetzendorf-Grabowski, T. | UNCONVENTIONAL CONFIGURATIONS - DESIGN AND OPTIMIZATION | 2016_0067 |
| Gollnick, V. | INFLUENCE OF AIRCRAFT TYPE AND ORDER ON FUEL SAVINGS GAINED BY TWO-AIRCRAFT FORMATIONS | 2016_0592 |
| Golubev, V. | ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS | 2016_0413 |
| Gomez-Escalonilla Martin, J. | XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES | 2016_0193 |
| Gong, A.-L. | NUMERICAL INVESTIGATION OF INLET STARTING CHARACTERISTICS | 2016_0296 |
| Gonzalez, L. | DETAILED AERO-STRUCTURAL DESIGN OF WINGLET FOR BUSINESS JET | 2016_0052 |
| Gonzalez, L. | SUPERSONIC BUSINESS JET TECHNOLOGY AND MISSION TRADE STUDIES | 2016_0053 |
| Goodwin, A. | TRANSFORMING MILITARY AEROSPACE SUSTAINMENT | 2016_0734 |
| Gopalakrishnan, P. | EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL | 2016_0260 |
| Goraj, Z. | INFLUENCE OF POWER UNIT CONFIGURATION LAYOUT OF A REGIONAL JET ON PERFORMANCE AND DIRECT OPERATING COST | 2016_0150 |
| Goraj, Z. | SELECTION OF AN UAV CONFIGURATION LAYOUT FOR OPTIMISATION OF TELEDETECTION MISSION USING HYPERSPECTRAL SENSORS | 2016_0318 |
| Gorbushin, A.R. | THE ORIGIN OF WIND TUNNELS IN RUSSIA | 2016_0069 |
| Gorecki, T. | THE SUPPORT PROCESS, SIMULATION RESEARCH DESIGN AND STRUCTURE OF THE NEW HELICOPTER'S CONSTRUCTION SCHEMATICS WITH SPECIAL EMPHASIS ON GROUND RESONANCE PHENOMENON | 2016_0354 |
| Gori, L. | STUDY OF THE COMPROMISE OF AERODYNAMIC AND STRUCTURE STANDPOINTS IN A HIGH-ASPECT RATIO WING DESIGN | 2016_0615 |
| Gouskov, O.V. | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE | 2016_0380 |
| Gowree, E.R. | EFFECT OF A 3D INDENTATION ON BOUNDARY LAYER INSTABILITY | 2016_0578 |
| Gowree, E.R. | STAGGERED THREE-DIMENSIONAL CAVITIES AS A POSSIBLE METHOD FOR SKIN FRICTION DRAG REDUCTION | 2016_0606 |
| Grachev, A.V. | AERODYNAMIC SHAPES DESIGN ON THE BASE OF DIRECT NEWTON TYPE OPTIMIZATION METHOD | 2016_0220 |
| Graham, R. | WAKE TURBULENCE RE-CATEGORISATION ON APPROACH AND DEPARTURE FOR SAFE AND MORE EFFICIENT AIR TRAFFIC MANAGEMENT | 2016_0230 |
| Grand, C. | NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION | 2016_0370 |
| Gray, A. | UNMANNED VEHICLE COLLABORATION RESEARCH ENVIRONMENT FOR MARITIME SEARCH AND RESCUE | 2016_0728 |
| Griendling, K. | UNMANNED VEHICLE COLLABORATION RESEARCH ENVIRONMENT FOR MARITIME SEARCH AND RESCUE | 2016_0728 |
| Griendling, K. | VIRTUAL EXPERIMENTATION AND VISUAL ANALYTICS IN SUPPORT OF SYSTEMS ENGINEERING AND SYSTEMS OF SYSTEMS ENGINEERING EFFORTS | 2016_0729 |
| Grigorev, A.V. | THE ACTIVE AEROELASTICITY CONCEPT - THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT | 2016_0436 |
| Grinev, K. | EFFECT OF FEEL SYSTEM CHARACTERISTICS ON PILOT MODEL PARAMETERS | 2016_0258 |
| Gringinger, E. | IN-FLIGHT PROVISIONING AND DISTRIBUTION OF ATM INFORMATION | 2016_0385 |
| Grishin, V.I. | DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS | 2016_0620 |
| Grüter, B. | OPTIMAL APPROACH TRAJECTORIES FOR MULTIPLE AIRCRAFT CONSIDERING DISTURBANCES AND CONFIGURATION CHANGES | 2016_0051 |
| Grüter, B. | FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS | 2016_0073 |
| Grüter, B. | OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH | 2016_0287 |
| Gu, Y.S. | THE INFLUENCE OF MORPHING PROCESS ON THE AEROELASTIC CHARACTERISTICS OF A FOLDING WING | 2016_0198 |
| Gu, W. | PHYSICALLY-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION FRAMEWORK COUPLING AIRFRAME AND PROPULSION | 2016_0268 |
| Gubanov, A.A. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Gubanov, A.A. | BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE | 2016_0383 |
| Guenov, M.D. | ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN | 2016_0525 |
| Gulienko, A.I. | METHODS FOR IMPROVING THE RELIABILITY OF FUEL SUPPLY SYSTEM OF GAS TURBINE ENGINES WITH USING ELECTRICALLY DRIVEN PUMPS | 2016_0163 |
| Guo, Z. | THE INVESTIGATION OF TIP CLEARANCE EFFECTS IN DUCTED ROTOR AERODYNAMIC CHARACTERISTICS USED IN UNMANNED AERIAL VEHICLES | 2016_0234 |
| Gurevich, O.S. | METHODS FOR IMPROVING THE RELIABILITY OF FUEL SUPPLY SYSTEM OF GAS TURBINE ENGINES WITH USING ELECTRICALLY DRIVEN PUMPS | 2016_0163 |
| Gusev, S.V. | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE | 2016_0380 |
| Gusev, D.Y. | BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE | 2016_0383 |
| Gustafsson, P. | A STUDY OF THE ACCURACY OF GROUND VIBRATION TEST DATA USING A REPLICA OF THE GARTEUR SM-AG19 TESTBED STRUCTURE | 2016_0095 |
| Gårdhagen, R. | KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD OPTIMIZATION | 2016_0375 |
| Görtz, S. | COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT | 2016_0345 |
| Göttlicher, C. | FLIGHT PATH RECONSTRUCTION FOR AN UNMANNED AERIAL VEHICLE USING LOW-COST SENSORS | 2016_0414 |
| Ha, O.-K. | GENERAL MESSAGE RACES IN DATA DISTRIBUTION SERVICE PROGRAMS FOR AIRBORNE SOFTWARE | 2016_0535 |
| Hagström, P. | DETECT AND AVOID FOR REMOTELY PILOTED AIRCRAFT IN AIR TRAFFIC CONTROL SIMULATIONS | 2016_0176 |
| Hajduk, J. | OVERVIEW OF THE INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME | 2016_0313 |
| Hakkaart, J.F. | QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH | 2016_0555 |
| Halila, G.L.O. | EFFECTS OF THE BOUNDARY LAYER TRANSITION ON THE GLOBAL AERODYNAMIC COEFFICIENTS | 2016_0330 |
| Han, Z.-H. | STRUCTURAL CONSTRAINTS INVESTIGATION IN WING AERODYNAMIC/STRUCTURAL OPTIMIZATION | 2016_0086 |
| Han, S. | ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME | 2016_0096 |
| Han, J.-H. | THE EFFECTS OF BODY AERODYNAMICS ON THE DYNAMIC STABILITY OF INSECT FLIGHT | 2016_0121 |
| Han, Z.-H. | SURROOPT: A GENERIC SURROGATE-BASED OPTIMIZATION CODE FOR AERODYNAMIC AND MULTIDISCIPLINARY DESIGN | 2016_0281 |
| Han, S.Y. | PERCH LANDING ASSISTED BY THRUSTER (PLAT): SIX D.O.F. TRAJECTORY OPTIMIZATION | 2016_0334 |
| Han, D. | A DEVELOPMENT OF MESHLESS POINT GENERATION TECHNIQUE FOR ANALYSIS OF THE UNSTEADY FLOW AROUND THE MULTI-BODY | 2016_0502 |
| Han, J.-H. | SELECTION OF PARAMETERS IN SPR CAMERA SYSTEM FOR STRUCTURAL HEALTH MONITORING OF UAV MAIN WING | 2016_0505 |
| Handroos, H. | HIL TEST BENCH FOR ENGINE'S FUEL CONTROL SYSTEMS INVESTIGATION | 2016_0215 |
| Hanjie, J. | CONCEPTUAL STUDY OF AN INNOVATIVE HIGH ALTITUDE SOLAR POWERED FLIGHT VEHICLE | 2016_0015 |
| Hanlon, G. | INFLUENCE OF ETHNICITY ON PASSENGER STANDARD WEIGHT | 2016_0466 |
| Hanses, C. | AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS | 2016_0202 |
| Harada, A. | AIR TRAFFIC EFFICIENCY EVALUATION BY TRAJECTORY OPTIMIZATION AND ADS-B DATA | 2016_0621 |
| Harasani, W. | EVALUATION OF CONCEPTUAL DESIGN BASED ON MANUFACTURED ACTUAL UNMANNED SOLAR PLANE | 2016_0685 |
| Hargreaves, B.O. | STUDY OF THE COMPROMISE OF AERODYNAMIC AND STRUCTURE STANDPOINTS IN A HIGH-ASPECT RATIO WING DESIGN | 2016_0615 |
| Haselbach, F. | KEY TECHNOLOGIES FOR THE NEXT GENERATION OF CIVIL AIRCRAFT ENGINES | 2016_0366 |
| Hashim, F. | ROTORCRAFT SYSTEMS MODELLING FOR TWIN-ENGINE HEAVY HELICOPTER | 2016_0610 |
| Hasseeb, H. | APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS | 2016_0185 |
| Haug, J.P. | DESIGN AND DEVELOPMENT OF A MILITARY ENGINE INLET RESEARCH DUCT | 2016_0623 |
| He, Y. | LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER CORROSION ENVIRONMENT | 2016_0308 |
| Hecker, P. | SENSOR CONCEPT OF HIGHLY-AUTOMATED AIRPORT TUGS FOR REDUCED EMISSION TAXI OPERATIONS | 2016_0530 |
| Hein, K. | ACOUSTICAL COMPARISON OF CONVENTIONAL TAXIING AND DISPATCH TOWING - TAXIBOT´S CONTRIBUTION TO GROUND NOISE ABATEMENT | 2016_0454 |
| Herbst, S. | USING OPENVSP IN A CONCEPTUAL AIRCRAFT DESIGN ENVIRONMENT IN MATLAB | 2016_0174 |
| Hermetz, J. | DISTRIBUTED ELECTRIC PROPULSION FOR SMALL BUSINESS AIRCRAFT A CONCEPT-PLANE FOR KEY-TECHNOLOGIES INVESTIGATIONS | 2016_0461 |
| Herr, M. | BROADBAND TRAILING-EDGE NOISE: A STATUS REPORT ON CURRENT PREDICTION CAPABILITIES | 2016_0730 |
| Higuchi, Y. | EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA | 2016_0682 |
| Hirabayashi, H. | VISUALIZATION OF AIRSPACE COMPLEXITY BASED ON AIR TRAFFIC CONTROL DIFFICULTY | 2016_0160 |
| Hirabayashi, H. | BENEFITS ASSESSMENT ON TIME-BASED OCEANIC ARRIVALS TO THE TOKYO METROPOLITAN AREA | 2016_0475 |
| Hiraoka, K. | EVALUATION OF CONCEPTUAL DESIGN BASED ON MANUFACTURED ACTUAL UNMANNED SOLAR PLANE | 2016_0685 |
| Hoeijmakers, H.W.M. | EULERIAN METHOD FOR IN-ENGINE ICING: WITH APPLICATION TO ICE CRYSTAL TRAJECTORIES AND IMPACT IN A GENERIC TURBOFAN COMPRESSOR | 2016_0322 |
| Hoeijmakers, H.W.M. | EXPERIMENTAL STUDY ON AERODYNAMIC LOAD CONTROL USING SYNTHETIC JET ACTUATORS | 2016_0389 |
| Hollingsworth, P. | IDENTIFYING THE BEST DESIGN FOR UNCERTAIN MARKETS | 2016_0626 |
| Holmes, D. | TRANSFORMING MILITARY AEROSPACE SUSTAINMENT | 2016_0734 |
| Holt, J. | AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS AN OSCILLATORY PITCHING NACA0012 AEROFOIL | 2016_0249 |
| Holt, J. | GEOMETRIC ROUGHNESS EFFECTS ON THE AERODYNAMIC CHARACTERISTICS OF A SPINNING CYLINDER IN CROSSFLOW | 2016_0250 |
| Holt, J.C. | THE INFLUENCE OF A LOCAL CHANGE IN WING DIHEDRAL ON THE LOW SPEED FLOW CHARACTERISTICS OF RECTANGULAR PLANFORM WINGS | 2016_0459 |
| Holzapfel, F. | OPTIMAL APPROACH TRAJECTORIES FOR MULTIPLE AIRCRAFT CONSIDERING DISTURBANCES AND CONFIGURATION CHANGES | 2016_0051 |
| Holzapfel, F. | FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS | 2016_0073 |
| Holzapfel, F. | OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH | 2016_0287 |
| Holzapfel, F. | FLIGHT PATH RECONSTRUCTION FOR AN UNMANNED AERIAL VEHICLE USING LOW-COST SENSORS | 2016_0414 |
| Holzapfel, F. | STRATEGIES FOR MANUAL LANDING OF REMOTELY PILOTED AIRPLANES WITH LARGE TIME DELAY | 2016_0444 |
| Holzapfel, F. | FUEL STARVATION CAUSED BY HUB CLOSURE | 2016_0513 |
| Hong, Y.K. | NONLINEAR OPTIMAL CONFLICT RESOLUTION SOLVED WITH PARTICLE SWARM OPTIMIZATION | 2016_0033 |
| Hong, S.-M. | TERMINAL IMPACT ANGLE AND ANGLE-OF-ATTACK CONTROL GUIDANCE FOR SURFACE-TO-AIR MISSILE USING TVC | 2016_0568 |
| Hongbin, P. | CONCEPTUAL STUDY OF AN INNOVATIVE HIGH ALTITUDE SOLAR POWERED FLIGHT VEHICLE | 2016_0015 |
| Hornung, M. | BOARDING PROCESS ASSESSMENT OF NOVEL AIRCRAFT CABIN CONCEPTS | 2016_0218 |
| Hornung, M. | FLEET DEVELOPMENT PLANNING OF AIRLINES: INCORPORATING THE AIRCRAFT OPERATING ECONOMICS FACTOR | 2016_0357 |
| Hornung, M. | A REVIEW OF RECENT AIRCRAFT CONCEPTS EMPLOYING SYNERGISTIC PROPULSION-AIRFRAME INTEGRATION | 2016_0727 |
| Horton, B. | ADVANCED PROPULSION COLLISION DAMAGE DUE TO UNMANNED AERIAL SYSTEM INGESTION | 2016_0629 |
| Horton, B. | NUMERICAL INVESTIGATION OF FAN-BLADE OUT USING MESO-SCALE COMPOSITE MODELING | 2016_0670 |
| Hosomi, R. | THE DRONE AVIATION NAVIGATION SYSTEMS | 2016_0010 |
| Hou, Z. | THE INVESTIGATION OF TIP CLEARANCE EFFECTS IN DUCTED ROTOR AERODYNAMIC CHARACTERISTICS USED IN UNMANNED AERIAL VEHICLES | 2016_0234 |
| Hou, Y.-Y. | SOLAR UAV GUST LOAD AMENDMENT | 2016_0266 |
| Hu, G. | HANDLING QUALITIES PREDICTION BASED ON ADAPTIVE OPTIMAL CONTROL PILOT MODEL | 2016_0143 |
| Hu, W. | THE INFLUENCE OF MORPHING PROCESS ON THE AEROELASTIC CHARACTERISTICS OF A FOLDING WING | 2016_0198 |
| Hu, T. | RESEARCH ON AIRWORTHINESS REQUIREMENTS OF SUPERCOOLED LARGE DROP ICING PROTECTION FOR AIRCRAFT (§25.1420) | 2016_0205 |
| Hu, Q. | SECURE ESTIMATION FOR UNMANNED AERIAL VEHICLES AGAINST ADVERSARIAL ATTACKS | 2016_0221 |
| Hua , R.H. | EFFECT OF ELASTIC DEFORMATION ON FLIGHT DYNAMICS OF PROJECTILES WITH LARGE SLENDERNESS RATIO | 2016_0119 |
| Hua, J. | STUDY OF MODEL DEFORMATION AND STING INTERFERENCE TO THE AERODYNAMIC ESTIMATIONS OF THE CAE-AVM MODEL | 2016_0405 |
| Huang, H. | MODELING AND ANALYSIS METHOD ON CRASHWORTHINESS OF CIVILIAN AIRCRAFT FUSELAGE STRUCTURES | 2016_0178 |
| Huang, H. | LABYRINTH SEALS DYNAMIC COEFFICIENTS AND CRITICAL SPEED RESEARCH BASE OF CHILDS´ MODEL | 2016_0212 |
| Huang, W. | SEMI-A VIBRATION SUPPRESSION OF AIRCRAFT PANEL USING PIEZOELECTRIC ACTUATOR WITH SYNCHRONIZED SWITCH DAMPING TECHNIQUE | 2016_0248 |
| Huang, Z. | THE RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION FIELDMEASUREMENT BASED ON FLUORESCENT OIL FILM | 2016_0710 |
| Hufty, D. | ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS | 2016_0413 |
| Huh, J. | COMPUTATIONS OF SUPERSONIC LATERAL JET | 2016_0484 |
| Huh, J.Y. | A MESHLESS METHOD FOR SIMULATION OF HYPERSONIC VISCOUS FLOWS | 2016_0499 |
| Huh, J.Y. | A DEVELOPMENT OF MESHLESS POINT GENERATION TECHNIQUE FOR ANALYSIS OF THE UNSTEADY FLOW AROUND THE MULTI-BODY | 2016_0502 |
| Hun, R. | DYNAMIC MODELING AND STABILITY ANALYSIS OF A HIGH ALTITUDE AIRSHIP | 2016_0700 |
| Huxdorf, O. | DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM | 2016_0166 |
| Hwang, I. | FORMAL VERIFICATION OF AUTOPILOTS IN UMANNED AIRCRAFT SYSTEMS | 2016_0190 |
| Hwang, I.H. | DETERMINATION OF DESIGN ALLOWABLES FOR AIRCRAFT COMPOSITE STRUCTURES | 2016_0522 |
| Hyeon, E. | VERTICAL POSITION ERROR BOUNDING FOR INTEGRATED GPS/BAROMETER SENSORS TO SUPPORT UNMANNED AERIAL VEHICLE (UAV) | 2016_0295 |
| Hühne, C. | WEIGHT REDUCTION OF CYLINDRICAL GRID STRUCTURES USING AXIAL-HELICAL-DESIGN | 2016_0708 |
| Hållbro, A. | PLASTIC DEFORMATION OF POWDER METALLURGY TUNGSTEN ALLOY FOILS FOR SATELLITE ENCLOSURES | 2016_0274 |
| Hällqvist, R. | METHODS FOR AUTOMATING MODEL VALIDATION: STEADY-STATE IDENTIFICATION APPLIED ON GRIPEN FIGHTER ENVIRONMENTAL CONTROL SYSTEM MEASUREMENTS | 2016_0188 |
| Idei, G. | THE DRONE AVIATION NAVIGATION SYSTEMS | 2016_0010 |
| Ignatyev , D.I. | WIND TUNNEL THREE-DEGREE-OF-FREEDOM DYNAMIC RIG FOR CONTROL VALIDATION | 2016_0325 |
| Iijima, T. | OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS | 2016_0338 |
| Ilic, C. | COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT | 2016_0345 |
| Isakovic, J. | A STUDY OF WALL-INTERFERENCE EFECTS IN WIND-TUNNEL TESTING OF A STANDARD MODEL AT TRANSONIC SPEEDS | 2016_0216 |
| Ishak, I.S. | EFFECTS OF PROPELLER LOCATIONS ON THE VORTEX SYSTEM ABOVE DELTA-SHAPED UAV MODEL | 2016_0162 |
| Ishihara, A.K. | APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS | 2016_0185 |
| Ishii, H. | IMPACT OF WEATHER UNCERTAINTIES ON NOISE CONTOURS AND NOISE ABATEMENT DESCENT TRAJECTORIES | 2016_0331 |
| Isikveren, A.T. | HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS | 2016_0438 |
| Isikveren, A.T. | COMPARATIVE EFFICIENCY ANALYSIS OF DISTRIBUTED PROPULSION SYSTEMS FOR PROPULSIVE FUSELAGE AND HYBRID WING BODY CONCEPTS IN FP7 PROJECT "DISPURSAL" | 2016_0602 |
| Isikveren, A.T. | HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES | 2016_0744 |
| Isyanov, A. | COMPARATIVE EFFICIENCY ANALYSIS OF DISTRIBUTED PROPULSION SYSTEMS FOR PROPULSIVE FUSELAGE AND HYBRID WING BODY CONCEPTS IN FP7 PROJECT "DISPURSAL" | 2016_0602 |
| Ivankin, M.A. | BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE | 2016_0383 |
| Ivankin, M.A. | INVESTIGATION OF THE HYDROGEN COMBUSTION CHAMBER PERFORMANCE WITHIN THE HEXAFLY-INT PROJECT | 2016_0458 |
| Ivanyushkin, D.S. | BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE | 2016_0383 |
| Jahangirian, A. | NUMERICAL STUDY OF ACTIVE SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTION CONTROL FOR TRANSONIC AERODYNAMICS | 2016_0714 |
| Jahangirian, A. | A MESH-LESS METHOD FOR COMPRESSIBLE FLOW CALCULATIONS AT ALL SPEED CONDITIONS | 2016_0715 |
| Jahangirian, A. | AERODYNAMIC SHAPE OPTIMIZATION WITH A NEW PARALLEL EVOLUTIONARY ALGORITHM AND NUMERICAL FLOW MODELLING | 2016_0717 |
| Jahangirian, A. | NUMERICAL SIMULATION OF FLOW SEPARATION CONTROL OVER A HUMP USING DBD PLASMA ACTUATOR | 2016_0718 |
| Jang, E.-Y. | LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV | 2016_0062 |
| Jang, J.E. | MODEL FOLLOWING CONTROL FOR MD500 HELICOPTER | 2016_0498 |
| Jankovics, I. | DEVELOPMENT OF AN ADVANCED ATCO WORKSTATION | 2016_0662 |
| Jankowski, A. | RESTARTING OF A JET ENGINE DURING FLYING AND FLIGHT SAFETY | 2016_0655 |
| Jankowski, A. | RESEARCH OF ALTERNATIVE FUEL WATER-FUEL MICRO EMULSION FROM POINT OF VIEW REDUCTION OF EMISSIONS | 2016_0667 |
| Janser, F. | IN-FLIGHT VIBRATION-BASED STRUCTURAL HEALTH MONITORING OF AIRCRAFT WINGS | 2016_0404 |
| Jeong, J. | ADAPTIVE SLIDING MODE CONTROLLER DESIGN FOR RECONFIGURATION OF ORGANIC FLIGHT ARRAY | 2016_0401 |
| Jeong, S.K. | APPLICATION OF PROPER ORTHOGONAL DECOMPOSITION FOR AVIATION SAFETY | 2016_0576 |
| Jepsen, J. | COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT | 2016_0345 |
| Ji, C. | SOLAR UAV GUST LOAD AMENDMENT | 2016_0266 |
| Jiao, J. | MULTI-OBJECTIVE OPTIMAL DESIGN OF THE PROPELLER FOR HIGH ALTITUDE AIRSHIPS BASED ON HIGH EFFICIENCY AND LIGHT WEIGHT | 2016_0100 |
| Jin, L. | RESEARCH ON AIRWORTHINESS REQUIREMENTS OF SUPERCOOLED LARGE DROP ICING PROTECTION FOR AIRCRAFT (§25.1420) | 2016_0205 |
| Jin, H. | HYPERPARAMETERS OPTIMIZATION FOR ADAPTIVE DESIGN OF EXPERIMENTS APPLIED TO WIND TUNNEL TESTING | 2016_0319 |
| Jo , Y.M. | DEVELOPMENT OF A THREE-DIMENSIONAL TIGHTLY COUPLED EULER/POTENTIAL FLOW SOLVER FOR TRANSONIC FLOW | 2016_0712 |
| Johnson, M.A. | APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS | 2016_0185 |
| Jokinen, J. | PLASTIC DEFORMATION OF POWDER METALLURGY TUNGSTEN ALLOY FOILS FOR SATELLITE ENCLOSURES | 2016_0274 |
| Joo, S. | COMBUSTION INSTABILITY FREQUENCY MODE SHIFT OF H2/CH4 RATIO AND COMBUSTOR LENGTH IN A MODEL GAS TURBINE | 2016_0406 |
| Jouannet, C. | SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT | 2016_0390 |
| Joubert, E. | THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION | 2016_0731 |
| Joulia, A. | TOWARDS A 4D TRAFFIC MANAGEMENT OF SMALL UAS OPERATING AT VERY LOW LEVEL | 2016_0064 |
| Judt, D.M. | ROTORCRAFT SYSTEMS MODELLING FOR TWIN-ENGINE HEAVY HELICOPTER | 2016_0610 |
| Jun, S. | AIRFRAME STRUCTURAL SURVIVABILITY STUDY THROUGH HYDRODYNAMIC RAM OF WELDED METALLIC WATER TANKS | 2016_0232 |
| Jun, Y.-K. | GENERAL MESSAGE RACES IN DATA DISTRIBUTION SERVICE PROGRAMS FOR AIRBORNE SOFTWARE | 2016_0535 |
| Jung, J. | APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS | 2016_0185 |
| Jung, Y. | FLIGHT TESTS OF THE VISION-BASED TARGET SENSING AND APPROACHING | 2016_0373 |
| Jung, S.Y. | A MESHLESS METHOD FOR SIMULATION OF HYPERSONIC VISCOUS FLOWS | 2016_0499 |
| Jung, S.Y. | A DEVELOPMENT OF MESHLESS POINT GENERATION TECHNIQUE FOR ANALYSIS OF THE UNSTEADY FLOW AROUND THE MULTI-BODY | 2016_0502 |
| Kacharava, I.N. | DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS | 2016_0620 |
| Kaleta, R. | DEVELOPMENT OF THE SMALL-SCALE MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT SAFETY TAKE-OFF AND LANDING | 2016_0359 |
| Kaleta, R. | EVALUATION METHODS OF AIRCRAFT FLIGHT SAFETY | 2016_0661 |
| Kalow, S. | MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES | 2016_0596 |
| Kan, A. | INTEGRATED RESEARCH SIMULATION STAND ADVANCED AIR TRAFFIC CONTROL SYSTEMS | 2016_0490 |
| Kanadin, V. | INTEGRATED RESEARCH SIMULATION STAND ADVANCED AIR TRAFFIC CONTROL SYSTEMS | 2016_0490 |
| Kanazaki, M. | DESIGN OPTIMIZATION OF HELICOPTER BLADE USING CLASS SHAPE FUNCTION BASED GEOMETRY REPRESENTATION | 2016_0479 |
| Kanerva, M. | PLASTIC DEFORMATION OF POWDER METALLURGY TUNGSTEN ALLOY FOILS FOR SATELLITE ENCLOSURES | 2016_0274 |
| Kang, W.-H. | HISTORY OF RAPID GROWTH IN KOREAN AERONAUTICAL INDUSTRY | 2016_0035 |
| Kang, Y.-S. | LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV | 2016_0062 |
| Kang, Y.J. | A NEW SOLUTION METHOD FOR SIX DEGREE OF FREEDOM FLIGHT DYNAMICS SIMULATION OF A HIGH ASPECT RATIO WING VEHICLE | 2016_0158 |
| Kang, H. | EFFICIENT MULTI-RESOLUTION ANALYSIS FOR IMPLICIT TEMPORAL INTEGRATION | 2016_0427 |
| Kang, W.G. | DEVELOPMENT OF SMART TILT-ROTOR UAS AND THE BEGINNINGS OF KOREAN CIVILIAN DRONES | 2016_0526 |
| Kang, W.R. | PERIODICALLY OSCILLATING TWO TRAILING EDGE FLAPS ACTUATED BY SMA WIRES | 2016_0706 |
| Karkle, P.G. | ON APPLYING PISTON THEORY IN INTERFERENCE FLOWS | 2016_0225 |
| Karkle, P.G. | EXPERIMENTAL COMPARISON OF LIMIT CYCLE METHOD WITH PHASE RESONANCE AND PHASE SEPARATION METHODS FOR DETERMINING MODAL CHARACTERISTICS OF AIRCRAFT STRUCTURES | 2016_0507 |
| Kasim, K.A. | EFFECTS OF PROPELLER LOCATIONS ON THE VORTEX SYSTEM ABOVE DELTA-SHAPED UAV MODEL | 2016_0162 |
| Kato, H. | PRESSURE ANALYSIS BASED ON PIV MEASUREMENT IN AIRPLANE WAKES | 2016_0594 |
| Kawalec, M. | QUANTITATIVE EMISSIONS OF NOX, CO AND CO2 DURING AIRCRAFT OPERATIONS | 2016_0097 |
| Kazarin, P. | ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS | 2016_0413 |
| Kennell, C. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Khalili, N. | AIRLINES MAINTENANCE COST ANALYSIS USING SYSTEM DYNAMICS MODELING | 2016_0452 |
| Khatibi, A.A. | IN-FLIGHT VIBRATION-BASED STRUCTURAL HEALTH MONITORING OF AIRCRAFT WINGS | 2016_0404 |
| Khatri, A.K. | BIFURCATION ANALYSIS OF A GENERIC PUSHER TYPE TRANSPORT AIRCRAFT CONFIGURATION IN NEAR-STALL FLIGHT | 2016_0197 |
| Khlebnikova, I.G. | PREDICTION OF WFD OCCURRENCE IN LONGITUDINAL JOINTS OF A FUSELAGE FOR COMMERCIAL AIRPLANE | 2016_0639 |
| Khoshkhoo, R. | NUMERICAL SIMULATION OF FLOW SEPARATION CONTROL OVER A HUMP USING DBD PLASMA ACTUATOR | 2016_0718 |
| Khrabrov, A.N. | WIND TUNNEL THREE-DEGREE-OF-FREEDOM DYNAMIC RIG FOR CONTROL VALIDATION | 2016_0325 |
| Khromov, V. | EXTRACTION OF LINEAR INFLOW MODEL FOR MANEUVERING HELICOPTER FROM FREE-WAKE ANALYSIS | 2016_0384 |
| Kier, T. | COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT | 2016_0345 |
| KIim, B. | STUDY ON THE SYSTEM INTEGRATION FOR MULTI-ELEMENT AIRFOIL AERODYNAMIC ANALYSIS | 2016_0598 |
| Kim, Y.D. | NONLINEAR OPTIMAL CONFLICT RESOLUTION SOLVED WITH PARTICLE SWARM OPTIMIZATION | 2016_0033 |
| Kim, Y.-S. | LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV | 2016_0062 |
| Kim, J.-K. | THE EFFECTS OF BODY AERODYNAMICS ON THE DYNAMIC STABILITY OF INSECT FLIGHT | 2016_0121 |
| Kim, S.Y. | FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING | 2016_0123 |
| Kim, Y. | APPROXIMATE THREE-DIMENSIONAL PATH GENERATION FOR UAV PATH-FOLLOWING | 2016_0128 |
| Kim, Y. | CAPTURE REGION ANALYSIS FOR MISSILE GUIDANCE WITH FIELD-OF-VIEW CONSTRAINT AGAINST MOVING TARGET | 2016_0129 |
| Kim, J. | PREDICTION OF FRACTURE STRENGTH FOR NOTCHED LAMINATE SUBJECTED TO COMPRESSION LOADING | 2016_0146 |
| Kim, J. | AIRFRAME STRUCTURAL SURVIVABILITY STUDY THROUGH HYDRODYNAMIC RAM OF WELDED METALLIC WATER TANKS | 2016_0232 |
| Kim, C. | AIRFRAME STRUCTURAL SURVIVABILITY STUDY THROUGH HYDRODYNAMIC RAM OF WELDED METALLIC WATER TANKS | 2016_0232 |
| Kim, H.I. | SAMPLING-BASED MOTION PLANNING FOR COOPERATIVE AERIAL MANIPULATION | 2016_0237 |
| Kim, H.J. | SAMPLING-BASED MOTION PLANNING FOR COOPERATIVE AERIAL MANIPULATION | 2016_0237 |
| Kim, H.J. | OPTICAL FLOW ON A FLAPPING WING-MICRO AIR VEHICLE TO AVOID COLLISIONS AND STEER | 2016_0256 |
| Kim, H.-G. | IMPACT ANGLE CONTROL GUIDANCE CONSIDERING GRAVITY EFFECT | 2016_0269 |
| Kim, H.-J. | IMPACT ANGLE CONTROL GUIDANCE CONSIDERING GRAVITY EFFECT | 2016_0269 |
| Kim, C.-J. | FLIGHT TEST FOR TYPE CERTIFICATION ACQUISITION OF SMALL CIVIL AIRPLANE KC-100 | 2016_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 FOLLOWING | 2016_0379 |
| Kim, J.-H. | CLOSED-FORM COOPERATIVE GUIDANCE LAW FOR TWO MISSILES WITH COUPLED TERMINAL VELOCITY CONSTRAINTS | 2016_0387 |
| Kim, H. | GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV | 2016_0399 |
| Kim, S. | ADAPTIVE SLIDING MODE CONTROLLER DESIGN FOR RECONFIGURATION OF ORGANIC FLIGHT ARRAY | 2016_0401 |
| Kim, J. | COMBUSTION INSTABILITY FREQUENCY MODE SHIFT OF H2/CH4 RATIO AND COMBUSTOR LENGTH IN A MODEL GAS TURBINE | 2016_0406 |
| Kim, S. | COMBUSTION INSTABILITY FREQUENCY MODE SHIFT OF H2/CH4 RATIO AND COMBUSTOR LENGTH IN A MODEL GAS TURBINE | 2016_0406 |
| Kim, Y. | ON STABILITY MARGIN OF A LQR-BASED VEHICLE NETWORK | 2016_0412 |
| Kim, H. | DESIGN THE GUIDANCE LAW FOR FORMATION FLIGHT OF MULTIPLE UAVS | 2016_0415 |
| Kim, Y.J. | OPERATION SCENARIOS OF UNMANNED AIRCRAFT SYSTEMS INTEGRATED INTO THE KOREAN NATIONAL AIRSPACE SYSTEM | 2016_0445 |
| Kim, S. | REDUCED ORDER MODELING OF AVIATION ENVIRONMENTAL DESIGN TOOL WITH PROPER ORTHOGONAL DECOMPOSITION AND KRIGING | 2016_0483 |
| Kim, K.H. | A MESHLESS METHOD FOR SIMULATION OF HYPERSONIC VISCOUS FLOWS | 2016_0499 |
| Kim, K.H. | A DEVELOPMENT OF MESHLESS POINT GENERATION TECHNIQUE FOR ANALYSIS OF THE UNSTEADY FLOW AROUND THE MULTI-BODY | 2016_0502 |
| Kim, K.J. | ADAPTIVE NEURAL NETWORK CONTROLLER DESIGN FOR BLENDED-WING UAV WITH COMPLEX DAMAGE | 2016_0516 |
| Kim, S.K. | ADAPTIVE NEURAL NETWORK CONTROLLER DESIGN FOR BLENDED-WING UAV WITH COMPLEX DAMAGE | 2016_0516 |
| Kim, J.W. | DETERMINATION OF DESIGN ALLOWABLES FOR AIRCRAFT COMPOSITE STRUCTURES | 2016_0522 |
| Kim, J.W. | DEVELOPMENT OF SMART TILT-ROTOR UAS AND THE BEGINNINGS OF KOREAN CIVILIAN DRONES | 2016_0526 |
| Kim, H.-J. | GENERAL MESSAGE RACES IN DATA DISTRIBUTION SERVICE PROGRAMS FOR AIRBORNE SOFTWARE | 2016_0535 |
| Kim, J.W. | NUMERICAL SIMULATION OF MIXING IN AN INLET-FUELED HYPERSONIC AIR-BREATHING PROPULSION | 2016_0549 |
| Kim, T.-U. | NONLINEAR DAMAGE MODELING AND ANALYSIS OF VISCOPLASTIC COMPOSITE MATERIALS | 2016_0746 |
| Kim, S.-H. | NONLINEAR DAMAGE MODELING AND ANALYSIS OF VISCOPLASTIC COMPOSITE MATERIALS | 2016_0746 |
| Kimura, J. | STUDENT DESIGN PROCESSES IN INTERDISCIPLINARY COLLABORATION ACTIVITIES IN AERONAUTICS ENGINEERING EDUCATION | 2016_0252 |
| Kiselev, D.Y. | CONTROL OF CONDITION OF GAS TURBINE ENGINE ROTOR BEARINGS IN DIAGNOSTIC PARAMETERS IN A DIFFERENT PHYSICAL NATURE | 2016_0273 |
| Kiselev, Y.V. | CONTROL OF CONDITION OF GAS TURBINE ENGINE ROTOR BEARINGS IN DIAGNOSTIC PARAMETERS IN A DIFFERENT PHYSICAL NATURE | 2016_0273 |
| Kishalov, A.E. | KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES | 2016_0008 |
| Kishalov, A.E. | AUTOMATED SELECTION OF THE MATERIAL A FAN BLADE PS-90A | 2016_0068 |
| Kistan, T. | PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORIES IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS | 2016_0691 |
| Kitazume, N. | EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA | 2016_0682 |
| Klingauf, U. | AN INTERFACE CONCEPT TO SUPPORT THE COCKPIT CREW DURING TRAJECTORY-BASED DISPATCH TOWING | 2016_0080 |
| Knoth, F. | AERODYNAMIC TESTING OF HELICOPTER NOVEL AIR INTAKES | 2016_0508 |
| Ko, W.L. | APPLICATIONS OF DISPLACEMENT TRANSFER FUNCTIONS TO DEFORMED SHAPE PREDICTIONS OF THE G-III SWEPT-WING STRUCTURE | 2016_0209 |
| Kobayashi, K. | DESIGN AND PRELIMINARY EVALUATION OF AN INTEGRATED AIRCRAFT OPERATION SYSTEM FOR DISASTER RELIEF | 2016_0088 |
| Koenig, B. | EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL | 2016_0260 |
| Kolinko, K.A. | WIND TUNNEL THREE-DEGREE-OF-FREEDOM DYNAMIC RIG FOR CONTROL VALIDATION | 2016_0325 |
| Kondakov, I. | NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES | 2016_0551 |
| Konovalov, V.V. | VERIFICATION OF CFRP COMPONENTS FATIGUE EVALUATION PROCEDURE UNDER IRREGULAR CYCLING LOADING | 2016_0303 |
| Kontis, K. | CHARACTERISATION OF NS-DBD PLASMA ACTUATORS FOR SUPERSONIC FLOW CONTROL | 2016_0170 |
| Koo, S.-O. | LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV | 2016_0062 |
| Kovacic, I. | IN-FLIGHT PROVISIONING AND DISTRIBUTION OF ATM INFORMATION | 2016_0385 |
| Kowaleczko, G. | THE SUPPORT PROCESS, SIMULATION RESEARCH DESIGN AND STRUCTURE OF THE NEW HELICOPTER'S CONSTRUCTION SCHEMATICS WITH SPECIAL EMPHASIS ON GROUND RESONANCE PHENOMENON | 2016_0354 |
| Kowalski, M. | RESTARTING OF A JET ENGINE DURING FLYING AND FLIGHT SAFETY | 2016_0655 |
| Kowalski, M. | RESEARCH OF ALTERNATIVE FUEL WATER-FUEL MICRO EMULSION FROM POINT OF VIEW REDUCTION OF EMISSIONS | 2016_0667 |
| Kozuka, T. | EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA | 2016_0682 |
| Kraiko, A.N. | AERODYNAMIC SHAPES DESIGN ON THE BASE OF DIRECT NEWTON TYPE OPTIMIZATION METHOD | 2016_0220 |
| Kreerenko, O.D. | SYNTHESIS OF CONTROL LAWS OF AEROSPACE SYSTEM BASED ON A SYNERGISTIC APPROACH | 2016_0183 |
| Kreerenko, E.S. | SYNTHESIS OF CONTROL LAWS OF AEROSPACE SYSTEM BASED ON A SYNERGISTIC APPROACH | 2016_0183 |
| Krstic, B. | THE ANALYSIS OF LAMINATE LAY-UP EFFECT ON THE FLUTTER SPEED OF COMPOSITE STABILIZERS | 2016_0271 |
| Krus, P. | METHODS FOR AUTOMATING MODEL VALIDATION: STEADY-STATE IDENTIFICATION APPLIED ON GRIPEN FIGHTER ENVIRONMENTAL CONTROL SYSTEM MEASUREMENTS | 2016_0188 |
| Krus, P. | KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD OPTIMIZATION | 2016_0375 |
| Krus, P. | SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT | 2016_0390 |
| Krus, P. | DESIGN AND TESTING OF A LOW-COST FLIGHT CONTROL AND DATA ACQUISITION SYSTEM FOR UNSTABLE SUBSCALE AIRCRAFT | 2016_0449 |
| Krus, P. | KNOWLEDGE-BASED FUTURE COMBAT AIRCRAFT OPTIMIZATION | 2016_0538 |
| Krus, P. | SYSTEMS ENGINEERING: AN INTERDISCIPLINARY CHALLENGE | 2016_0752 |
| Kryuchkov, A. | HIL TEST BENCH FOR ENGINE'S FUEL CONTROL SYSTEMS INVESTIGATION | 2016_0215 |
| Kshitij, A. | THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW | 2016_0244 |
| Kukshinov, N.V. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Kukshinov, N.V. | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE | 2016_0380 |
| Kulhánek, R. | SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL | 2016_0593 |
| Kumar, V. | BIFURCATION ANALYSIS OF A GENERIC PUSHER TYPE TRANSPORT AIRCRAFT CONFIGURATION IN NEAR-STALL FLIGHT | 2016_0197 |
| Kumar, V. | SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL | 2016_0593 |
| Kumbasar, S. | A NOVEL FLIGHT CONTORL ALGORITHM FOR MULTICOPTERS | 2016_0231 |
| Kursakov, I. | EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL | 2016_0572 |
| Kuruliuk, K. | INVESTIGATION OF DEFORMATION FIELDS IN AIRCRAFT PANELS BY NON-CONTACT OPTICAL VIDEOGRAMMETRY METHOD | 2016_0368 |
| Kuzmin, P.V. | HEURISTIC MODEL OF NON-STEADY LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK | 2016_0019 |
| Kweon, J.H. | A STUDY ON FAILURE BEHAVIORS OF REPAIRED COMPOSITE STRUCTURES WITH SCARF BONDED PATCH | 2016_0335 |
| Kwiatkowski, T. | SOURCE TERM MODEL FOR STREAMWISE JET VORTEX GENERATOR MODELLING | 2016_0521 |
| Kwon, H.-H. | MISSILE AUTOPILOT DESIGN USING CONTRACTION THEORY-BASED OUTPUT FEEDBACK CONTROL | 2016_0474 |
| Kwon, O.J. | NUMERICAL SIMULATION OF MIXING IN AN INLET-FUELED HYPERSONIC AIR-BREATHING PROPULSION | 2016_0549 |
| Kwon, O.-J. | NUMERICAL INVESTIGATION OF SUBSONIC RAREFIED FLOWS USING DSMC-IP METHODS | 2016_0556 |
| Kächele, T. | STUDY ON EFFICIENT FULL ANNULUS URANS COMPUTATIONS OF AN INTAKE COMPRESSOR CONFIGURATION | 2016_0548 |
| Ladyzynska-Kozdras, E. | DEVELOPMENT OF THE SMALL-SCALE MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT SAFETY TAKE-OFF AND LANDING | 2016_0359 |
| Lambert, J.-C. | THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION | 2016_0731 |
| Lambert, P.-A. | HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES | 2016_0744 |
| Lanshin, A. | DEVELOPMENT OF TECHNOLOGY ADVANCE FOR FUTURE PROPULSION SYSTEMS OF HAUL AIRCRAFT | 2016_0542 |
| Lapis, M.B. | AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS | 2016_0202 |
| Laskaridis, P. | HYBRID TURBO-ELECTRIC DISTRIBUTED PROPULSION APPLIED TO SHORT RANGE AIRCRAFT | 2016_0748 |
| Lauderdale, T.A. | A STUDY ON SAFETY ASSURANCE FOR INCREASINGLY AUTONOMOUS TRAFFIC FLOW MANAGEMENT SYSTEM | 2016_0672 |
| Lawson, C.P. | ROTORCRAFT SYSTEMS MODELLING FOR TWIN-ENGINE HEAVY HELICOPTER | 2016_0610 |
| Lee, S.-Y. | LCC ESTIMATION AND CASE STUDY USING RELIABILITY AND MAINTAINABILITY ANALYSIS | 2016_0031 |
| Lee, K.J. | NONLINEAR OPTIMAL CONFLICT RESOLUTION SOLVED WITH PARTICLE SWARM OPTIMIZATION | 2016_0033 |
| Lee, S.-Y. | HISTORY OF RAPID GROWTH IN KOREAN AERONAUTICAL INDUSTRY | 2016_0035 |
| Lee, R. | SIMULATION OF UNSTEADY SHIP AIRWAKES USING OPENFOAM | 2016_0094 |
| Lee, B.-Y. | ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME | 2016_0096 |
| Lee, N. | FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING | 2016_0123 |
| Lee, S. | FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING | 2016_0123 |
| Lee, S. | CAPTURE REGION ANALYSIS FOR MISSILE GUIDANCE WITH FIELD-OF-VIEW CONSTRAINT AGAINST MOVING TARGET | 2016_0129 |
| Lee, M. | PREDICTION OF FRACTURE STRENGTH FOR NOTCHED LAMINATE SUBJECTED TO COMPRESSION LOADING | 2016_0146 |
| Lee, H.B. | SAMPLING-BASED MOTION PLANNING FOR COOPERATIVE AERIAL MANIPULATION | 2016_0237 |
| Lee, J.G. | OPTICAL FLOW ON A FLAPPING WING-MICRO AIR VEHICLE TO AVOID COLLISIONS AND STEER | 2016_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 TESTING | 2016_0319 |
| Lee, J. | HYPERPARAMETERS OPTIMIZATION FOR ADAPTIVE DESIGN OF EXPERIMENTS APPLIED TO WIND TUNNEL TESTING | 2016_0319 |
| Lee, B.Y. | PERCH LANDING ASSISTED BY THRUSTER (PLAT): SIX D.O.F. TRAJECTORY OPTIMIZATION | 2016_0334 |
| Lee, D. | CLOSED-FORM COOPERATIVE GUIDANCE LAW FOR TWO MISSILES WITH COUPLED TERMINAL VELOCITY CONSTRAINTS | 2016_0387 |
| Lee, J. | DESIGN THE GUIDANCE LAW FOR FORMATION FLIGHT OF MULTIPLE UAVS | 2016_0415 |
| Lee, K. | REDUCED ORDER MODELING OF AVIATION ENVIRONMENTAL DESIGN TOOL WITH PROPER ORTHOGONAL DECOMPOSITION AND KRIGING | 2016_0483 |
| Lee, S. | COMPUTATIONS OF SUPERSONIC LATERAL JET | 2016_0484 |
| Lee, T.I. | QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH | 2016_0555 |
| Lee, J. | STUDY ON THE SYSTEM INTEGRATION FOR MULTI-ELEMENT AIRFOIL AERODYNAMIC ANALYSIS | 2016_0598 |
| Lee, K.-J. | FIGHTER AIRCRAFT HIGH AOA DIRECTIONAL STABILITY IMPROVEMENT DESIGN | 2016_0600 |
| Lee, C. | MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR FIGHTER AIRCRAFT CONFIGURATION | 2016_0607 |
| Lee, D.J. | DEVELOPMENT OF HIGH-ORDER AND HIGH-RESOLUTION SCHEMES FOR EFFICIENT SHOCK CAPTURING IN HIGH-SPEED FLOWS | 2016_0705 |
| Lee, D.J. | PERIODICALLY OSCILLATING TWO TRAILING EDGE FLAPS ACTUATED BY SMA WIRES | 2016_0706 |
| Lee, D.J. | DEVELOPMENT OF A THREE-DIMENSIONAL TIGHTLY COUPLED EULER/POTENTIAL FLOW SOLVER FOR TRANSONIC FLOW | 2016_0712 |
| Lee, H.-I. | EVOLUTIONARY GAME BASED MULTI-OBJECTIVE OPTIMIZATION FOR MULTI-AGENT NETWORK RESILIENCE | 2016_0722 |
| Lei, D. | DEVELOPMENT OF HALF-MODEL TEST CAPABILITY AT THE NF-3 WIND TUNNEL | 2016_0034 |
| Lengyel-Kampmann, T. | MISSION BASED COMPARISON OF SINGLE- AND COUNTER-ROTATING FAN DESIGNS | 2016_0259 |
| Lesire, C. | NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION | 2016_0370 |
| Levchenko, E.A. | EXPERIENCE OF USING NONLINEAR NUMERICAL ANALYSIS TO ESTIMATE AIRCRAFT PRIMARY STRUCTURE STRENGTH | 2016_0201 |
| Level, C. | HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS | 2016_0438 |
| Lewe, J.-H. | AN EXPLORATION OF EVOLUTION PATHS FOR AIR TRANSPORTATION NETWORKS | 2016_0674 |
| Lewe, J.-H. | A REVIEW AND A CLASSIFICATION SCHEME FOR AIR TRANSPORTATION NETWORK RESEARCH | 2016_0688 |
| Li, M. | 3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION | 2016_0039 |
| Li, X. | ENGINEERING APPLICATION OF GAO-YONG RATIONAL TURBULENCE MODEL TO AN INTER-COOLED DUCT | 2016_0065 |
| Li, Q. | WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS | 2016_0091 |
| Li, Y. | STUDY ON THE SAFETY RISK AND CAPACITY OF THE ONE-WAY CIRCULATION AIR ROUTE IN CHINA | 2016_0115 |
| Li, J. | RESEARCH ON LOAD SPECTRUM OF AERO HYDRAULIC PUMP BASED ON ACCELERATED DEGRADATION TESTING | 2016_0181 |
| Li, X. | THE INVESTIGATION OF TIP CLEARANCE EFFECTS IN DUCTED ROTOR AERODYNAMIC CHARACTERISTICS USED IN UNMANNED AERIAL VEHICLES | 2016_0234 |
| Li, K. | SEMI-A VIBRATION SUPPRESSION OF AIRCRAFT PANEL USING PIEZOELECTRIC ACTUATOR WITH SYNCHRONIZED SWITCH DAMPING TECHNIQUE | 2016_0248 |
| Li, Y. | EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL | 2016_0260 |
| Li, C. | LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER CORROSION ENVIRONMENT | 2016_0308 |
| Li, X. | LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER CORROSION ENVIRONMENT | 2016_0308 |
| Li, F.-M. | MAKING HEALTH MANAGEMENT MORE CONCISE AND EFFICIENT: AIRCRAFT CONDITION MONITORING BASED ON COMPRESSED SENSING | 2016_0400 |
| Li, X. | UNSTEADY AERODYNAMICS MODELLING AND ITS APPLICATION IN AEROELASTIC STABILITY ANALYSIS | 2016_0407 |
| Li, J. | RESEARCH ON THE IMPACT OF SHOCK WAVE TO EXTENSIONALITY OF POD METHOD | 2016_0409 |
| Li, X.-T. | RESEARCH ON THE IMPACT OF SHOCK WAVE TO EXTENSIONALITY OF POD METHOD | 2016_0409 |
| Li, L. | THE RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION FIELDMEASUREMENT BASED ON FLUORESCENT OIL FILM | 2016_0710 |
| Liao, D. | DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL | 2016_0403 |
| Liao, M. | RESEARCH ADVANCES ON AIRCRAFT STRUCTURAL INTEGRITY AND SUSTAINMENT AT NRC | 2016_0726 |
| Liepelt, R. | COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT | 2016_0345 |
| Lim, Y. | AUTOMATED SEPARATION ASSURANCE AND COLLISION AVOIDANCE FUNCTIONS IN THE CNS+A CONTEXT | 2016_0027 |
| Lim, C.H. | DEVELOPMENT OF SMART TILT-ROTOR UAS AND THE BEGINNINGS OF KOREAN CIVILIAN DRONES | 2016_0526 |
| Lim, Y. | PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORIES IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS | 2016_0691 |
| Limonin, M.V. | EXPERIENCE OF USING NONLINEAR NUMERICAL ANALYSIS TO ESTIMATE AIRCRAFT PRIMARY STRUCTURE STRENGTH | 2016_0201 |
| Linderholt, A. | A STUDY OF THE ACCURACY OF GROUND VIBRATION TEST DATA USING A REPLICA OF THE GARTEUR SM-AG19 TESTBED STRUCTURE | 2016_0095 |
| Lipatov, V.D. | KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES | 2016_0008 |
| Lis, M. | OVERVIEW OF THE INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME | 2016_0313 |
| Liseykin, G.V. | EXPERIMENTAL COMPARISON OF LIMIT CYCLE METHOD WITH PHASE RESONANCE AND PHASE SEPARATION METHODS FOR DETERMINING MODAL CHARACTERISTICS OF AIRCRAFT STRUCTURES | 2016_0507 |
| Liu, J. | 3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION | 2016_0039 |
| Liu, Z.-T. | WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS | 2016_0091 |
| Liu, G. | TOTAL TEMPERATURE RECOVERY CHARACTERISTICS TEST TECHNIQUE BASED ON TOTAL PRESSURE CALIBRATION WIND TUNNEL | 2016_0112 |
| Liu, F. | INVESTIGATION ON OBLIQUE SHOCK WAVE CONTROL BY SURFACE ARC DISCHARGE PLASMA | 2016_0124 |
| Liu, J. | HANDLING QUALITIES PREDICTION BASED ON ADAPTIVE OPTIMAL CONTROL PILOT MODEL | 2016_0143 |
| Liu, Z.-Q. | SOLAR UAV GUST LOAD AMENDMENT | 2016_0266 |
| Liu, X.-W. | NUMERICAL INVESTIGATION OF INLET STARTING CHARACTERISTICS | 2016_0296 |
| Liu, Y.-F. | NUMERICAL INVESTIGATION OF UNSTEADY INTERACTION CHARACTERISTIC INDUCED BY IMPULSIVE JET | 2016_0362 |
| Liu, Y.-W. | NUMERICAL INVESTIGATION OF UNSTEADY INTERACTION CHARACTERISTIC INDUCED BY IMPULSIVE JET | 2016_0362 |
| Liu, N. | LINEAR MODELING BASED ON INSTRUMENTAL MODEL ESTIMATION AND PID PARAMETERS TUNING IN FREQUENCY-DOMAIN OF AIRCRAFT ENGINE | 2016_0702 |
| Liu, H. | STRATEGIES TO ENHANCE A CONFIGURATION FOR HIGH-PRECISION MULTI DISCIPLINARY OPTIMIZATION | 2016_0707 |
| Liying, S. | CONCEPTUAL STUDY OF AN INNOVATIVE HIGH ALTITUDE SOLAR POWERED FLIGHT VEHICLE | 2016_0015 |
| Lobanova, M.A. | LARGE-SCALE VORTEX STRUCTURE OF FLOW IN THE NEAR WAKE BEHIND AN AIRLINER DURING TAKEOFF AND LANDING | 2016_0666 |
| Lu, C. | MAKING HEALTH MANAGEMENT MORE CONCISE AND EFFICIENT: AIRCRAFT CONDITION MONITORING BASED ON COMPRESSED SENSING | 2016_0400 |
| Lu, C. | AIRCRAFT SECURITY ENHANCEMENT: ROTATING MACHINERY FAULT DIAGNOSIS AND HEALTH ASSESSMENT USING MANIFOLD LEARNING AND DYNAMIC TIME WARPING | 2016_0435 |
| Lucchi, F. | AUGMENTED AND VIRTUAL REALITY IN THE AIRPORT CONTROL TOWER | 2016_0719 |
| Lucchi, F. | GENERATIVE DESIGN: ADVANCED DESIGN OPTIMIZATION PROCESSES FOR AERONAUTICAL APPLICATIONS | 2016_0720 |
| Ludwig, T. | ADVANCED RNP TO ILS AUTOLAND APPROACHES FOR OPTIMAL BENEFITS FROM PBN: FLIGHT TESTING PROCEDURES WITH AN A320 | 2016_0147 |
| Lundström, D. | SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT | 2016_0390 |
| Lundström, D. | DESIGN AND TESTING OF A LOW-COST FLIGHT CONTROL AND DATA ACQUISITION SYSTEM FOR UNSTABLE SUBSCALE AIRCRAFT | 2016_0449 |
| Lung, S.-F. | APPLICATIONS OF DISPLACEMENT TRANSFER FUNCTIONS TO DEFORMED SHAPE PREDICTIONS OF THE G-III SWEPT-WING STRUCTURE | 2016_0209 |
| Lunin, V.Y. | BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE | 2016_0383 |
| Luo, X.L. | TAXIING ROUTE PLANNING BASED ON AIRPORT HOTSPOTS | 2016_0402 |
| Lysenkov, A. | EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL | 2016_0572 |
| Ma, C. | SYNTHESIZED ANALYSIS FROM DESIGN RANGE TO THE CONCETUAL DESIGN OF WIDEBODY AIRLINER | 2016_0058 |
| Ma, W. | LABYRINTH SEALS DYNAMIC COEFFICIENTS AND CRITICAL SPEED RESEARCH BASE OF CHILDS´ MODEL | 2016_0212 |
| Ma, C. | A CONCEPTUAL ANALYSIS OF AN AIRCRAFT WITH REAR-MOUNTED OPEN ROTOR ENGINES | 2016_0253 |
| MacKunis, W. | ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS | 2016_0413 |
| Mahiddini, F. | COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN "MORE ELECTRICAL AIRCRAFT" | 2016_0105 |
| Mainz, H. | MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES | 2016_0596 |
| Malenko, V. | EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL | 2016_0572 |
| Manecy, A. | NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION | 2016_0370 |
| Mansor, S. | IMPORTANCE OF TRANSIENT AERODYNAMIC DERIVATIVES FOR V-TAIL AIRCRAFT FLIGHT DYNAMIC DESIGN | 2016_0515 |
| Mare, J.-C. | SPECIAL CONSIDERATIONS TO THERMAL BEHAVIOR MODELING AND SIMULATION OF AN AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEM | 2016_0554 |
| Mareskin, I. | MULTIDISCIPLINARY OPTIMIZATION OF PRO-COMPOSITE STRUCTURAL LAYOUTS OF HIGH LOADED AIRCRAFT CONSTRUCTIONS | 2016_0622 |
| Marini, M. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Markina, K.V. | KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES | 2016_0008 |
| Markina, K.V. | AUTOMATED SELECTION OF THE MATERIAL A FAN BLADE PS-90A | 2016_0068 |
| Marks, T. | INFLUENCE OF AIRCRAFT TYPE AND ORDER ON FUEL SAVINGS GAINED BY TWO-AIRCRAFT FORMATIONS | 2016_0592 |
| Martegani, M. | DESIGN, MANUFACTURING AND VALIDATION OF A GUST GENERATOR FOR WIND TUNNEL TEST OF A LARGE SCALE AEROELASTIC MODEL | 2016_0676 |
| Martins-Abdalla, A. | CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING | 2016_0397 |
| Marzocca, P. | ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES | 2016_0467 |
| Marzocca, P. | CHARACTERIZATION OF THE NONLINEAR AEROELASTIC BEHAVIOR OF AN AIRFOIL WITH FREEPLAY AND AERODYNAMIC NONLINEARITY | 2016_0716 |
| Maslov, V.P. | EFFECT OF REYNOLDS NUMBER, OPERATING MODE, TURBULENCE PARAMETERS ON PROFILE AND SECONDARY LOSSES OF LPT | 2016_0276 |
| Maslov, A.A. | STUDY OF THE UNSTEADY STRUCTURES EVOLUTION IN SHOCK WAVE / BOUNDARY LAYER INTERACTION FOR VARIOUS UPSTREAM CONDITIONS | 2016_0560 |
| Masotti, N. | AUGMENTED AND VIRTUAL REALITY IN THE AIRPORT CONTROL TOWER | 2016_0719 |
| Mat, S. | EFFECTS OF PROPELLER LOCATIONS ON THE VORTEX SYSTEM ABOVE DELTA-SHAPED UAV MODEL | 2016_0162 |
| Mat, S. | EFFECTS OF REYNOLDS NUMBER ON THE ONSET OF LEADING EDGE VORTEX SEPARATION ABOVE BLUNT-EDGE DELTA WING VFE-2 CONFIGURATIONS | 2016_0608 |
| Matayoshi, N. | OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS | 2016_0338 |
| Matsuda, T. | FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS | 2016_0393 |
| Matsushima, K. | PRESSURE ANALYSIS BASED ON PIV MEASUREMENT IN AIRPLANE WAKES | 2016_0594 |
| Matta, A. | LOW ORDER MODELING OF THE UNSTEADY AND 3D EFFECTS OF CONTINUOUS WAKE FLAPPING FLIGHT | 2016_0651 |
| Mattei, M. | MODEL PREDICTIVE CONTROL FOR A SWARM OF FIXED WING UAVS | 2016_0326 |
| Mattei, M. | NONLINEAR DYNAMIC INVERSION WITH NEURAL NETWORKS FOR THE FLIGHT CONTROL OF A LOW COST TILT ROTOR UAV | 2016_0637 |
| Maury, C. | HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS | 2016_0438 |
| Mavris, D. | LINKING TECHNOLOGY READINESS TO UNCERTAINTY REDUCTION | 2016_0632 |
| Mavris, D.N. | UNCERTAINTY QUANTIFICATION OF AIRFOIL DESIGN FOR ADVANCED PROPELLER MODELS | 2016_0665 |
| Mavris, D.N. | AN EXPLORATION OF EVOLUTION PATHS FOR AIR TRANSPORTATION NETWORKS | 2016_0674 |
| Mavris, D.N. | A REVIEW AND A CLASSIFICATION SCHEME FOR AIR TRANSPORTATION NETWORK RESEARCH | 2016_0688 |
| Mavris, D.N. | UNMANNED VEHICLE COLLABORATION RESEARCH ENVIRONMENT FOR MARITIME SEARCH AND RESCUE | 2016_0728 |
| Mavris, D.N. | VIRTUAL EXPERIMENTATION AND VISUAL ANALYTICS IN SUPPORT OF SYSTEMS ENGINEERING AND SYSTEMS OF SYSTEMS ENGINEERING EFFORTS | 2016_0729 |
| Mavris, D.N. | TECHNOLOGY INTEGRATION AND SYSTEM ASSESSMENTS WITH UNCERTAINTY MODELLING | 2016_0742 |
| Mazur, M. | IS TO BE THE MICRODRONE | 2016_0646 |
| McCartney, B. | THE EFFECT OF LEADING EDGE ROUNDING ON A CARET WAVERIDER CONFIGURATION AT MACH 8.2 | 2016_0242 |
| McLaughlin, C. | AN INVESTIGATION OF EFFECTS OF FLIGHT MANEUVERS ON A SUPERSONIC AIRCRAFT WITH HORIZONTAL TAIL ACTUATOR FAILURE | 2016_0251 |
| Medeiros, J.G. | EXPERIMENTAL STUDY OF GEOMETRIC VARIATIONS EFFECT ON THE FLOW PATTERNS ON A HAMMERHEAD SATELLITE LAUNCH VEHICLE | 2016_0683 |
| Meijer, M.-C. | ON APPLYING PISTON THEORY IN INTERFERENCE FLOWS | 2016_0225 |
| Meleshin, B.A. | HEURISTIC MODEL OF NON-STEADY LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK | 2016_0019 |
| Meshennikov, P.A. | BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE | 2016_0383 |
| Meyer, J.P. | OPTIMISATION OF A WING-BODY-TAIL CONFIGURATION WITH AN ALTERNATIVE LOW DRAG FUSELAGE AND BODY TRAILING EDGE | 2016_0223 |
| Mi, B.-G. | MODELLING NONLINEAR HIGH-PRECISION UNSTEADY AERODYNAMICS FOR ADVANCED AIRCRAFT AT HIGH ANGLE OF ATTACK | 2016_0152 |
| Mieloszyk, J. | UNCONVENTIONAL CONFIGURATIONS - DESIGN AND OPTIMIZATION | 2016_0067 |
| Mikhailova , M.K. | NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN | 2016_0550 |
| Mileshin, V.I. | DEVELOPMENT OF THE FAN STAGE WITH ULTRA-LOW ROTATIONAL SPEED | 2016_0261 |
| Millan, P. | COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN "MORE ELECTRICAL AIRCRAFT" | 2016_0105 |
| Miller, M. | THE ROUGHNESS POSITION INFLUENCE ON LAMINAR AEROFOIL AERODYNAMIC CHARACTERISTIC IN TRANSONIC FLOW REGIME | 2016_0561 |
| Min, J.K. | THE ROLLS-ROYCE PLC ULTRAFAN HEAT MANAGEMENT CHALLENGE | 2016_0344 |
| Mirzoyan, A. | DEVELOPMENT OF TECHNOLOGY ADVANCE FOR FUTURE PROPULSION SYSTEMS OF HAUL AIRCRAFT | 2016_0542 |
| Mirzoyan, A. | COMPARATIVE EFFICIENCY ANALYSIS OF DISTRIBUTED PROPULSION SYSTEMS FOR PROPULSIVE FUSELAGE AND HYBRID WING BODY CONCEPTS IN FP7 PROJECT "DISPURSAL" | 2016_0602 |
| Miyata, S. | APPLICATION OF FLAME MEASUREMENT TECHNIC BY DENSELY INSTALLED ION-PROBES ON 2-STROKE GASOLINE ENGINE | 2016_0418 |
| Miyazawa, Y. | EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA | 2016_0682 |
| Mizutani, K. | FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS | 2016_0393 |
| Modi, H.C. | APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS | 2016_0185 |
| Moerland, E. | EXPLORING PROPAGATED UNCERTAINTIES IN A MULTI-DISCIPLINARY AIRCRAFT DESIGN FRAMEWORK | 2016_0145 |
| Moerland, E. | COLLABORATIVE AIRCRAFT DESIGN USING AN INTEGRATED AND DISTRIBUTED MULTIDISCIPLINARY PRODUCT DEVELOPMENT PROCESS | 2016_0328 |
| Moerland, E. | THE COLLABORATIVE ENGINEER: HOW EDUCATION SHOULD BRING FORTH THE NEW GENERATION OF ENGINEERS | 2016_0750 |
| Mohammadi-Amin, M. | CFD-BASED AERODYNAMIC SHAPE OPTIMIZATION OF A MANNED RE-ENTRY VEHICLE | 2016_0627 |
| Molina-Cristobal, A. | ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN | 2016_0525 |
| Molokanov, A. | THE FOAMING PROPERTIES OF LUBRICATING OILS FOR AIRCRAFT GAS TURBINE ENGINES | 2016_0270 |
| Monner, H.P. | DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM | 2016_0166 |
| Moon, G.-H. | AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY CONSTRAINTS | 2016_0355 |
| Moon, J. | GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV | 2016_0399 |
| Moon, J.H. | MODEL FOLLOWING CONTROL FOR MD500 HELICOPTER | 2016_0498 |
| Moormann, D. | PRECISION LANDING BASED ON ATMOSPHERIC DISTURBANCE MONITORING AND MODEL PREDICTIVE CONTROL | 2016_0290 |
| Mori, R. | NOVEL PILOT CONTROL MODEL WITH STOCHASTIC AND PERIODICAL MOVEMENT | 2016_0026 |
| Mori, R. | IMPROVEMENT OF PUSHBACK TIME ASSIGNMENT UNDER UNCERTAINTIES | 2016_0048 |
| Moroe, T. | FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS | 2016_0393 |
| Mudhar, H.S. | EFFECTIVENESS OF VORTEX GENERATORS IN HIGHLY 3D FLOWS | 2016_0577 |
| Mughal, S. | EFFECT OF A 3D INDENTATION ON BOUNDARY LAYER INSTABILITY | 2016_0578 |
| Munjulury, R.C. | KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD OPTIMIZATION | 2016_0375 |
| Munjulury, R.C. | KNOWLEDGE-BASED FUTURE COMBAT AIRCRAFT OPTIMIZATION | 2016_0538 |
| Musa, N.A. | IMPORTANCE OF TRANSIENT AERODYNAMIC DERIVATIVES FOR V-TAIL AIRCRAFT FLIGHT DYNAMIC DESIGN | 2016_0515 |
| Muscat, A. | CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION | 2016_0211 |
| Musiak, J.D. | AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS | 2016_0202 |
| Müller, R. | A FOLDABLE FLAPPING WING DESIGN INSPIRED BY THE ELBOW-WRIST ANATOMY OF BATS | 2016_0609 |
| Müller-Wiesner, D. | THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION | 2016_0731 |
| Myong, R.S. | NUMERICAL SIMULATION OF DROPLET IMPINGEMENT ON A MULTI-ELEMENT HIGH-LIFT AIRFOIL | 2016_0267 |
| Nagai, H. | EFFECT OF YAW-TILTED HINGE AXIS ON DEPLOYMENT ROBUSTNESS OF MARS AIRPLANE | 2016_0477 |
| Nagaoka, S. | VISUALIZATION OF AIRSPACE COMPLEXITY BASED ON AIR TRAFFIC CONTROL DIFFICULTY | 2016_0160 |
| Nagel, B. | EXPLORING PROPAGATED UNCERTAINTIES IN A MULTI-DISCIPLINARY AIRCRAFT DESIGN FRAMEWORK | 2016_0145 |
| Nagel, B. | COLLABORATIVE AIRCRAFT DESIGN USING AN INTEGRATED AND DISTRIBUTED MULTIDISCIPLINARY PRODUCT DEVELOPMENT PROCESS | 2016_0328 |
| Nagel, B. | TOWARDS THE 3RD GENERATION MDO COLLABORATIVE ENVIRONMENT | 2016_0563 |
| Nagel, B. | COLLABORATIVE SYSTEMS DRIVEN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION | 2016_0585 |
| Nagel, B. | INTEGRATION OF HYBRID PROPULSION SYSTEM IN A CS23 COMMUTER DESIGN | 2016_0595 |
| Nagel, B. | THE COLLABORATIVE ENGINEER: HOW EDUCATION SHOULD BRING FORTH THE NEW GENERATION OF ENGINEERS | 2016_0750 |
| Nakakita, K. | NON-INTRUSIVE UNSTEADY PSP TECHNIQUE FOR INVESTIGATION OF TRANSONIC BUFFETING | 2016_0553 |
| Nakakita, K. | UNSTEADY AERODYNAMIC INFORMATION EXTRACTION USING FFT-BASED UNSTEADY PRESSURE-SENSITIVE PAINT MEASUREMENT | 2016_0681 |
| Nam, D. | STUDY ON THE SYSTEM INTEGRATION FOR MULTI-ELEMENT AIRFOIL AERODYNAMIC ANALYSIS | 2016_0598 |
| Namba, R. | PRESSURE ANALYSIS BASED ON PIV MEASUREMENT IN AIRPLANE WAKES | 2016_0594 |
| Naruoka, M. | A WAVELET BASED FLIGHT DATA PREPROCESSING METHOD FOR FLIGHT CHARACTERISTICS ESTIMATION AND FAULT DETECTION | 2016_0437 |
| Nasiri, M. | INSTANTANEOUS BASELINE MULTIPLE DAMAGE DETECTION AND LOCALIZATION IN AN ALUMINIUM PLATE USING LAMB WAVES | 2016_0640 |
| Nayko, Y.A. | THE ACTIVE AEROELASTICITY CONCEPT - THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT | 2016_0436 |
| Neely, A.J. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Nepomnyashchiy, A.D. | EFFECT OF REYNOLDS NUMBER, OPERATING MODE, TURBULENCE PARAMETERS ON PROFILE AND SECONDARY LOSSES OF LPT | 2016_0276 |
| Nesterenko, V.G. | IMPROVEMENT OF THE DESIGN AND METHODS OF DESIGNING TUBULER AIR-TO-AIR HEAT EXHANGERS COOLING SYSTEMS OF GAS TURBINES | 2016_0433 |
| Neu, E. | IN-FLIGHT VIBRATION-BASED STRUCTURAL HEALTH MONITORING OF AIRCRAFT WINGS | 2016_0404 |
| Nguyen, A.-T. | THE EFFECTS OF BODY AERODYNAMICS ON THE DYNAMIC STABILITY OF INSECT FLIGHT | 2016_0121 |
| Nguyen, K.H. | A STUDY ON FAILURE BEHAVIORS OF REPAIRED COMPOSITE STRUCTURES WITH SCARF BONDED PATCH | 2016_0335 |
| Ni, Z.-Y. | EXPERIMENTAL INVESTIGATION OF LATERAL PULSE JET INTERACTION FLOWFIELD IN HYPERSONIC FLOW | 2016_0391 |
| Nie, B.-W. | WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS | 2016_0091 |
| Niehuis, R. | STUDY ON EFFICIENT FULL ANNULUS URANS COMPUTATIONS OF AN INTAKE COMPRESSOR CONFIGURATION | 2016_0548 |
| Niehuis, R. | DESIGN AND DEVELOPMENT OF A MILITARY ENGINE INLET RESEARCH DUCT | 2016_0623 |
| Niermann, C.A. | CAN 3D-AUDIO IMPROVE STATE-OF-THE-ART PILOT-ASSISTANCE SYSTEMS? | 2016_0082 |
| Nikaido, B. | APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS | 2016_0185 |
| Nikolaev, A.A. | INVESTIGATION OF THE HYDROGEN COMBUSTION CHAMBER PERFORMANCE WITHIN THE HEXAFLY-INT PROJECT | 2016_0458 |
| Nishida, M. | FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS | 2016_0393 |
| Norde, E. | EULERIAN METHOD FOR IN-ENGINE ICING: WITH APPLICATION TO ICE CRYSTAL TRAJECTORIES AND IMPACT IN A GENERIC TURBOFAN COMPRESSOR | 2016_0322 |
| Notaro, I. | MODEL PREDICTIVE CONTROL FOR A SWARM OF FIXED WING UAVS | 2016_0326 |
| Novikov, A.V. | DIRECT NUMERICAL SIMULATION OF DISTURBANCES IN A THREE-DIMENSIONAL HYPERSONIC NEAR-WALL FLOW OVER FLAT PLATE AND COMPRESSION CORNER | 2016_0536 |
| Ochi, Y. | PILOT'S CG LOCATION AND ATTITUDE CONTROL FOR LATERAL MANEUVER OF A HANG GLIDER | 2016_0087 |
| Ocokoljic, G. | A STUDY OF WALL-INTERFERENCE EFECTS IN WIND-TUNNEL TESTING OF A STANDARD MODEL AT TRANSONIC SPEEDS | 2016_0216 |
| Ogawa, H. | CHARACTERIZATION OF THE NONLINEAR AEROELASTIC BEHAVIOR OF AN AIRFOIL WITH FREEPLAY AND AERODYNAMIC NONLINEARITY | 2016_0716 |
| Oguntona, O. | FLEET DEVELOPMENT PLANNING OF AIRLINES: INCORPORATING THE AIRCRAFT OPERATING ECONOMICS FACTOR | 2016_0357 |
| Oh, S. | AN INVESTIGATION OF EFFECTS OF FLIGHT MANEUVERS ON A SUPERSONIC AIRCRAFT WITH HORIZONTAL TAIL ACTUATOR FAILURE | 2016_0251 |
| Oh, S. | EFFICIENT MULTI-RESOLUTION ANALYSIS FOR IMPLICIT TEMPORAL INTEGRATION | 2016_0427 |
| Okubo, T. | THE DRONE AVIATION NAVIGATION SYSTEMS | 2016_0010 |
| Okuno, Y. | DESIGN AND PRELIMINARY EVALUATION OF AN INTEGRATED AIRCRAFT OPERATION SYSTEM FOR DISASTER RELIEF | 2016_0088 |
| Orekhov, I.K. | DEVELOPMENT OF THE FAN STAGE WITH ULTRA-LOW ROTATIONAL SPEED | 2016_0261 |
| Orifici, A.C. | IN-FLIGHT VIBRATION-BASED STRUCTURAL HEALTH MONITORING OF AIRCRAFT WINGS | 2016_0404 |
| Otten, T. | MISSION BASED COMPARISON OF SINGLE- AND COUNTER-ROTATING FAN DESIGNS | 2016_0259 |
| Otto, O. | ELECTRIC PROPULSION FOR AIRCRAFT | 2016_0737 |
| Oyama, A. | EFFECT OF YAW-TILTED HINGE AXIS ON DEPLOYMENT ROBUSTNESS OF MARS AIRPLANE | 2016_0477 |
| Pak, C.-G. | UNSTEADY AERODYNAMIC FORCE SENSING FROM MEASURED STRAIN | 2016_0021 |
| Palchekovskaya, N. | NUMERICAL SIMULATION OF AEROTHERMODYNAMIC CHARACTERISTICS OF FLOW OVER SPACE VEHICLE MODEL | 2016_0381 |
| Palchekovskaya, N.V. | AEROTHERMODYNAMICS CHARACTERISTICS OF A SPACE PROBE IN THE MARTIAN ATMOSPHERE | 2016_0386 |
| Pan, K. | SEMI-A VIBRATION SUPPRESSION OF AIRCRAFT PANEL USING PIEZOELECTRIC ACTUATOR WITH SYNCHRONIZED SWITCH DAMPING TECHNIQUE | 2016_0248 |
| Pan, W.J. | TAXIING ROUTE PLANNING BASED ON AIRPORT HOTSPOTS | 2016_0402 |
| Pankov, S.V. | DEVELOPMENT OF THE FAN STAGE WITH ULTRA-LOW ROTATIONAL SPEED | 2016_0261 |
| Pankov, A.V. | VERIFICATION OF CFRP COMPONENTS FATIGUE EVALUATION PROCEDURE UNDER IRREGULAR CYCLING LOADING | 2016_0303 |
| Park, B.-J. | LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV | 2016_0062 |
| Park, H.-J. | ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME | 2016_0096 |
| Park, J. | ON MORE EFFECTIVE AERODYNAMIC DATA GENERATION FOR SIMULATION BASED AIRCRAFT CONCEPTUAL DESIGN | 2016_0151 |
| Park, S. | CFD OF BLENDED WING BODY UCAV WITH VORTEX GENERATOR | 2016_0246 |
| Park, S.-H. | REAL-TIME GENERATION OF WAYPOINTS ENHANCING UAV SURVIVABILITY | 2016_0485 |
| Park, K.-K. | REAL-TIME GENERATION OF WAYPOINTS ENHANCING UAV SURVIVABILITY | 2016_0485 |
| Park, S.-S. | REAL-TIME GENERATION OF WAYPOINTS ENHANCING UAV SURVIVABILITY | 2016_0485 |
| Park, J.G. | MODEL FOLLOWING CONTROL FOR MD500 HELICOPTER | 2016_0498 |
| Park, M.S. | MODEL FOLLOWING CONTROL FOR MD500 HELICOPTER | 2016_0498 |
| Park, S.Y. | DEPTH IMAGE BASED DIRECT SLAM FOR SMALL UAVS | 2016_0503 |
| Park, Y.G.J. | WIND VELOCITY ESTIMATION WITHOUT AN AIR SPEED SENSOR USING KALMAN FILTER UNDER THE COLORED MEASUREMENT NOISE | 2016_0545 |
| Park, C.G. | WIND VELOCITY ESTIMATION WITHOUT AN AIR SPEED SENSOR USING KALMAN FILTER UNDER THE COLORED MEASUREMENT NOISE | 2016_0545 |
| Park, S.H. | DEVELOPMENT OF A THREE-DIMENSIONAL TIGHTLY COUPLED EULER/POTENTIAL FLOW SOLVER FOR TRANSONIC FLOW | 2016_0712 |
| Park, I.K. | NONLINEAR DAMAGE MODELING AND ANALYSIS OF VISCOPLASTIC COMPOSITE MATERIALS | 2016_0746 |
| Paryshev, S.E. | THE ACTIVE AEROELASTICITY CONCEPT - THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT | 2016_0436 |
| Pátek, Z. | EXPERIMENATAL AND COMPUTATIONAL STUDY OF GROUND EFFECT ON AIRFOIL SECTION | 2016_0122 |
| Pátek, Z. | SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL | 2016_0593 |
| Patnaik, P. | RESEARCH ADVANCES ON AIRCRAFT STRUCTURAL INTEGRITY AND SUSTAINMENT AT NRC | 2016_0726 |
| Pellicer, J. | EXPERIMENTAL INVESTIGATION OF FLOW AROUND AIRFOILS WITH UNDULATING LEADING EDGES | 2016_0724 |
| Pereira, L. | SYSTEMS ENGINEERING: AN INTERDISCIPLINARY CHALLENGE | 2016_0752 |
| Persiani, F. | GENERATIVE DESIGN: ADVANCED DESIGN OPTIMIZATION PROCESSES FOR AERONAUTICAL APPLICATIONS | 2016_0720 |
| Peters, L. | THE DESIGN OF AN AUTOMATIC BEACON EJECTING SYSTEM FOR AIRCRAFT | 2016_0465 |
| Petrov, A.V. | NEW METHOD OF TRANSONIC BUFFET DECREASING ON SUPERCRITICAL AIRFOIL | 2016_0127 |
| Petrov, A.V. | INVESTIGATION OF FLOW CONTROL OVER THE SUPERCRITICAL AIRFOIL BY TANGENTIAL JET BLOWING AT TRANSONIC SPEEDS | 2016_0173 |
| Pezzella, G. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Pezzella, G. | AERODYNAMIC ANALYSIS WITH SEPARATION DYNAMICS OF A LAUNCHER AT STAGING CONDITIONS | 2016_0570 |
| Pfeiffer, T. | EXPLORING PROPAGATED UNCERTAINTIES IN A MULTI-DISCIPLINARY AIRCRAFT DESIGN FRAMEWORK | 2016_0145 |
| Pinon, O.J. | VIRTUAL EXPERIMENTATION AND VISUAL ANALYTICS IN SUPPORT OF SYSTEMS ENGINEERING AND SYSTEMS OF SYSTEMS ENGINEERING EFFORTS | 2016_0729 |
| Piranian, A. | STORE SEPARATION FROM WEAPON BAYS | 2016_0156 |
| Placek, R. | INVESTIGATION OF UNSTEADY TRANSONIC FLOW FIELD ABOVE LAMINAR AIRFOIL BY PIV METHOD | 2016_0300 |
| Placek, R. | THE ROUGHNESS POSITION INFLUENCE ON LAMINAR AEROFOIL AERODYNAMIC CHARACTERISTIC IN TRANSONIC FLOW REGIME | 2016_0561 |
| Ploetner, K. | FLEET DEVELOPMENT PLANNING OF AIRLINES: INCORPORATING THE AIRCRAFT OPERATING ECONOMICS FACTOR | 2016_0357 |
| Polev, A. | DEVELOPMENT OF TECHNOLOGY ADVANCE FOR FUTURE PROPULSION SYSTEMS OF HAUL AIRCRAFT | 2016_0542 |
| Polivanov, P.A. | STUDY OF THE UNSTEADY STRUCTURES EVOLUTION IN SHOCK WAVE / BOUNDARY LAYER INTERACTION FOR VARIOUS UPSTREAM CONDITIONS | 2016_0560 |
| Polsinelli, C. | ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES | 2016_0467 |
| Popelniuk, I.A. | IMPROVING THE EFFICIENCY AND RELIABILITY ASSESSMENT TECHNICAL STATE LIQUID SYSTEMS AIRCRAFT DURING ACCEPTANCE TESTS | 2016_0192 |
| Pornet, C. | HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS | 2016_0438 |
| Posse, C. | AN IN-FLIGHT AID TO NEGOTIATE A MORE EFFICIENT FLIGHT PATH | 2016_0463 |
| Potapchik, A.V. | NEW METHOD OF TRANSONIC BUFFET DECREASING ON SUPERCRITICAL AIRFOIL | 2016_0127 |
| Potapchik, A.V. | INVESTIGATION OF FLOW CONTROL OVER THE SUPERCRITICAL AIRFOIL BY TANGENTIAL JET BLOWING AT TRANSONIC SPEEDS | 2016_0173 |
| Potter, I. | RTO\'S AND TECHNOLOGY DE-RISKING | 2016_0735 |
| Prakash, T. | FEASIBILITY ANALYSIS OF SPAN EXTENSION OF MORPHING HALE UAV WING | 2016_0701 |
| Prince, S. | THE EFFECT OF LEADING EDGE ROUNDING ON A CARET WAVERIDER CONFIGURATION AT MACH 8.2 | 2016_0242 |
| Prince, S. | THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW | 2016_0244 |
| Prince, S. | AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS AN OSCILLATORY PITCHING NACA0012 AEROFOIL | 2016_0249 |
| Prince, S. | GEOMETRIC ROUGHNESS EFFECTS ON THE AERODYNAMIC CHARACTERISTICS OF A SPINNING CYLINDER IN CROSSFLOW | 2016_0250 |
| Prince, S.A. | THE INFLUENCE OF A LOCAL CHANGE IN WING DIHEDRAL ON THE LOW SPEED FLOW CHARACTERISTICS OF RECTANGULAR PLANFORM WINGS | 2016_0459 |
| Prince Raj, L. | NUMERICAL SIMULATION OF DROPLET IMPINGEMENT ON A MULTI-ELEMENT HIGH-LIFT AIRFOIL | 2016_0267 |
| Prokhorov, A.N. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Prokhorov, A.N. | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE | 2016_0380 |
| Pronin, M.A. | EXPERIMENTAL COMPARISON OF LIMIT CYCLE METHOD WITH PHASE RESONANCE AND PHASE SEPARATION METHODS FOR DETERMINING MODAL CHARACTERISTICS OF AIRCRAFT STRUCTURES | 2016_0507 |
| Pugach, M.A. | AEROTHERMODYNAMICS CHARACTERISTICS OF A SPACE PROBE IN THE MARTIAN ATMOSPHERE | 2016_0386 |
| Qian, G.P. | NUMERICAL STUDY OF FIXED TRANSITION LOCATION EFFECT ON SUPERCRITICAL WING AERODYNAMIC CHARACTERISTICS | 2016_0154 |
| Qian, W.Q. | ANALYSIS ON OFFLINE AND ONLINE IDENTIFICATION METHODS FOR AIRCRAFT STABILITY AND CONTROL DERIVATIVES | 2016_0203 |
| Qian, W. | DESIGN, MANUFACTURE AND FREQUENCY EXPERIMENT OF A NOVEL FLUTTER MODEL FOR AGARD WING 445.6 WITH STRUCTURE-SIMILARITY | 2016_0519 |
| Qian, W. | INFLUENCE OF THE RHOMBOID ZONE ON AEROELASTIC EXPERIMENTS OF SUPERSONIC AIRCRAFT | 2016_0564 |
| Qian, W. | THE MANUFACTURE AND APPLICATION FOR COMPOSITES AEROELASTIC MODEL OF CIVIL AIRLINER WING IN FL-26 TRANSONIC WIND-TUNNEL | 2016_0587 |
| Qian, J.P. | A FOLDABLE FLAPPING WING DESIGN INSPIRED BY THE ELBOW-WRIST ANATOMY OF BATS | 2016_0609 |
| Qin, H. | DETACHED EDDY SIMULATION OF AIRCRAFT MASSIVELY SEPARATED FLOWS | 2016_0140 |
| Qin, X.H. | NUMERICAL STUDY OF FIXED TRANSITION LOCATION EFFECT ON SUPERCRITICAL WING AERODYNAMIC CHARACTERISTICS | 2016_0154 |
| Qin, J. | RESEARCH ON VIBRATION CHARACTERISTIC FOR VARIABLE ROTATING VELOCITY BLADES | 2016_0189 |
| Qin, N. | THE EFFECT OF LEADING EDGE ROUNDING ON A CARET WAVERIDER CONFIGURATION AT MACH 8.2 | 2016_0242 |
| Qiu, S. | MULTI-POINT DESIGN OPTIMIZATION OF A HIGH BYPASS RATIO FAN BLADE | 2016_0172 |
| Qu, Z. | UNCERTAINTY QUANTIFICATION AND GLOBAL SENSITIVITY ANALYSIS FOR HYPERSONIC AEROTHERMOELASTIC ANALYSIS | 2016_0135 |
| Qu, X. | DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL | 2016_0403 |
| Rademakers, R.P.M. | DESIGN AND DEVELOPMENT OF A MILITARY ENGINE INLET RESEARCH DUCT | 2016_0623 |
| Radestock, M. | DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM | 2016_0166 |
| Raj, P. | ON MORE EFFECTIVE AERODYNAMIC DATA GENERATION FOR SIMULATION BASED AIRCRAFT CONCEPTUAL DESIGN | 2016_0151 |
| Raj, P. | USING INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN PROJECTS TO ENHANCE UNDERGRADUATE DESIGN EDUCATION: LESSONS LEARNED | 2016_0650 |
| Rajchel, J. | RESTARTING OF A JET ENGINE DURING FLYING AND FLIGHT SAFETY | 2016_0655 |
| Rajchel, J. | EVALUATION METHODS OF AIRCRAFT FLIGHT SAFETY | 2016_0661 |
| Ramasamy, S. | AUTOMATED SEPARATION ASSURANCE AND COLLISION AVOIDANCE FUNCTIONS IN THE CNS+A CONTEXT | 2016_0027 |
| Ramirez Gonzalez, V. | XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES | 2016_0193 |
| Rand, O. | EXTRACTION OF LINEAR INFLOW MODEL FOR MANEUVERING HELICOPTER FROM FREE-WAKE ANALYSIS | 2016_0384 |
| Rangel, R.K. | DEVELOPMENT OF PEST\'S BIOLOGICAL CONTROL TOOL USING VTOL UAV SYSTEMS | 2016_0207 |
| Rasuo, B. | A STUDY OF WALL-INTERFERENCE EFECTS IN WIND-TUNNEL TESTING OF A STANDARD MODEL AT TRANSONIC SPEEDS | 2016_0216 |
| Rasuo, B. | GENERAL APPROACH TO THE ANALYSIS OF THE ASYMMETRICALLY LOADED AIRPLANE FLIGHT LIMITATIONS | 2016_0227 |
| Rasuo, B. | THE ANALYSIS OF LAMINATE LAY-UP EFFECT ON THE FLUTTER SPEED OF COMPOSITE STABILIZERS | 2016_0271 |
| Razin, A. | NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES | 2016_0551 |
| Reimann, B. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Rein-Weston, K. | AN IN-FLIGHT AID TO NEGOTIATE A MORE EFFICIENT FLIGHT PATH | 2016_0463 |
| Reis, F.C. | SYSTEM IDENTIFICATION OF A SCALE HELICOPTER IN HOVERING FLIGHT | 2016_0686 |
| Ren, H. | A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM | 2016_0321 |
| Reulet, P. | COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN "MORE ELECTRICAL AIRCRAFT" | 2016_0105 |
| Revanth Reddy, A. | IMPROVEMENT OF THE DESIGN AND METHODS OF DESIGNING TUBULER AIR-TO-AIR HEAT EXHANGERS COOLING SYSTEMS OF GAS TURBINES | 2016_0433 |
| Rhee, J.S. | A MESHLESS METHOD FOR SIMULATION OF HYPERSONIC VISCOUS FLOWS | 2016_0499 |
| Rhee, J.S. | A DEVELOPMENT OF MESHLESS POINT GENERATION TECHNIQUE FOR ANALYSIS OF THE UNSTEADY FLOW AROUND THE MULTI-BODY | 2016_0502 |
| Riaz, A. | ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN | 2016_0525 |
| Ribeiro, A.F.P. | EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL | 2016_0260 |
| Ricci, S. | DESIGN, MANUFACTURING AND VALIDATION OF A GUST GENERATOR FOR WIND TUNNEL TEST OF A LARGE SCALE AEROELASTIC MODEL | 2016_0676 |
| Riccobene, L. | DESIGN, MANUFACTURING AND VALIDATION OF A GUST GENERATOR FOR WIND TUNNEL TEST OF A LARGE SCALE AEROELASTIC MODEL | 2016_0676 |
| Ridel, M. | COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN "MORE ELECTRICAL AIRCRAFT" | 2016_0105 |
| Ridel, M. | DISTRIBUTED ELECTRIC PROPULSION FOR SMALL BUSINESS AIRCRAFT A CONCEPT-PLANE FOR KEY-TECHNOLOGIES INVESTIGATIONS | 2016_0461 |
| Rieck, M. | OPTIMAL APPROACH TRAJECTORIES FOR MULTIPLE AIRCRAFT CONSIDERING DISTURBANCES AND CONFIGURATION CHANGES | 2016_0051 |
| Rieck, M. | FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS | 2016_0073 |
| Rieck, M. | OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH | 2016_0287 |
| Riemenschneider, J. | DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM | 2016_0166 |
| Riemenschneider, J. | MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES | 2016_0596 |
| Rinoie, K. | INTEGRATED CONCEPTUAL DESIGN METHOD CONSIDERING ADVANCED AIRCRAFT SYSTEMS AND AIRCRAFT TRAJECTORY | 2016_0317 |
| Rinoie, K. | AIRCRAFT DESIGN EDUCATION FOR UNDERGRADUATE AND GRADUATE STUDENTS AT THE UNIVERSITY OF TOKYO | 2016_0749 |
| Rivero Arevalo, I. | XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES | 2016_0193 |
| Roberts, W. | UNMANNED VEHICLE COLLABORATION RESEARCH ENVIRONMENT FOR MARITIME SEARCH AND RESCUE | 2016_0728 |
| Rodionov, L. | HIL TEST BENCH FOR ENGINE'S FUEL CONTROL SYSTEMS INVESTIGATION | 2016_0215 |
| Rodríguez Robles, R. | ELASTIC MODES ADAPTIVE CANCELLATION ALGORITHM FOR THE A330 MRTT FLYING BOOM CONTROL LAWS | 2016_0528 |
| Rohacs, D. | DEVELOPMENT OF AN ADVANCED ATCO WORKSTATION | 2016_0662 |
| Rohacs, J. | DEVELOPMENT OF AN ADVANCED ATCO WORKSTATION | 2016_0662 |
| Rooseleer, F. | WAKE TURBULENCE RE-CATEGORISATION ON APPROACH AND DEPARTURE FOR SAFE AND MORE EFFICIENT AIR TRAFFIC MANAGEMENT | 2016_0230 |
| Rothfeld, R. | BOARDING PROCESS ASSESSMENT OF NOVEL AIRCRAFT CABIN CONCEPTS | 2016_0218 |
| Roussel, A. | THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW | 2016_0244 |
| Ruchala, P. | INVESTIGATION OF UNSTEADY TRANSONIC FLOW FIELD ABOVE LAMINAR AIRFOIL BY PIV METHOD | 2016_0300 |
| Ruchala, P. | THE ROUGHNESS POSITION INFLUENCE ON LAMINAR AEROFOIL AERODYNAMIC CHARACTERISTIC IN TRANSONIC FLOW REGIME | 2016_0561 |
| Ruchala, P. | ANALYSES OF AIRFLOW AROUND DUCTED FAN PROPULSION SYSTEM IN PUSHER CONFIGURATION USING PIV METHOD | 2016_0659 |
| Russell, A. | CHARACTERISATION OF NS-DBD PLASMA ACTUATORS FOR SUPERSONIC FLOW CONTROL | 2016_0170 |
| Ryemill, M. | THE ROLLS-ROYCE PLC ULTRAFAN HEAT MANAGEMENT CHALLENGE | 2016_0344 |
| Ryoo, C.-K. | REAL-TIME GENERATION OF WAYPOINTS ENHANCING UAV SURVIVABILITY | 2016_0485 |
| Ryu, S.W. | OPTICAL FLOW ON A FLAPPING WING-MICRO AIR VEHICLE TO AVOID COLLISIONS AND STEER | 2016_0256 |
| Sabatini, R. | AUTOMATED SEPARATION ASSURANCE AND COLLISION AVOIDANCE FUNCTIONS IN THE CNS+A CONTEXT | 2016_0027 |
| Sabatini, R. | PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORIES IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS | 2016_0691 |
| Said, M. | EFFECTS OF PROPELLER LOCATIONS ON THE VORTEX SYSTEM ABOVE DELTA-SHAPED UAV MODEL | 2016_0162 |
| Said, M. | EFFECTS OF REYNOLDS NUMBER ON THE ONSET OF LEADING EDGE VORTEX SEPARATION ABOVE BLUNT-EDGE DELTA WING VFE-2 CONFIGURATIONS | 2016_0608 |
| Salanne, J.-P. | HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS | 2016_0438 |
| Sanchez, F. | SURROGATE MODELING TECHNIQUE FOR THE CONCEPTUAL AND PRELIMINARY DESIGN OF EMBEDDED ACTUATION SYSTEMS AND COMPONENTS | 2016_0184 |
| Santana, L.D. | EXPERIMENTAL ANALYSES OF DROOP, WINGTIPS AND FENCES ON A BWB MODEL | 2016_0262 |
| Santoro, F. | CABIN ESCAPE SYSTEM: A WAY TO ENSURE CREW SAFETY DURING SUBORBITAL FLIGHTS | 2016_0506 |
| Sanz de Blas, A. | ELASTIC MODES ADAPTIVE CANCELLATION ALGORITHM FOR THE A330 MRTT FLYING BOOM CONTROL LAWS | 2016_0528 |
| Saprykin, A. | EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL | 2016_0572 |
| Sarlin, E. | PLASTIC DEFORMATION OF POWDER METALLURGY TUNGSTEN ALLOY FOILS FOR SATELLITE ENCLOSURES | 2016_0274 |
| Sattarzadeh, S. | A MESH-LESS METHOD FOR COMPRESSIBLE FLOW CALCULATIONS AT ALL SPEED CONDITIONS | 2016_0715 |
| Savelyev, A.A. | AERODYNAMIC OPTIMIZATION OF AIRPLANE PROPULSION SYSTEM WITHIN THE FRAMEWORK OF AGILE PROJECT | 2016_0583 |
| Sboev, D.S. | DISTURBANCES IN AN ACCELERATED BOUNDARY LAYER UNDER INFLUENCE OF MODERATE FREE-STREAM TURBULENCE | 2016_0358 |
| Scalabrin, L.C. | EFFECTS OF SOME NUMERICAL FORMULATION ASPECTS IN HIGH-LIFT CONFIGURATION SIMULATIONS | 2016_0713 |
| Schachtebeck, P.M. | SENSOR CONCEPT OF HIGHLY-AUTOMATED AIRPORT TUGS FOR REDUCED EMISSION TAXI OPERATIONS | 2016_0530 |
| Schatz, S. | FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS | 2016_0073 |
| Schelyaev , A.E. | NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN | 2016_0550 |
| Schepanyuk, B.A. | LARGE-SCALE VORTEX STRUCTURE OF FLOW IN THE NEAR WAKE BEHIND AN AIRLINER DURING TAKEOFF AND LANDING | 2016_0666 |
| Scherer, J. | COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT | 2016_0345 |
| Schettini, F. | EXPERIMENTAL AND SIMULATION STUDY OF THE DYNAMICS OF AN ELECTRO-MECHANICAL LANDING GEAR ACTUATOR | 2016_0049 |
| Schettini, F. | NONLINEAR MODEL IDENTIFICATION OF A SMALL-SCALE UNMANNED ROTORCRAFT | 2016_0076 |
| Schmidt, M. | BOARDING PROCESS ASSESSMENT OF NOVEL AIRCRAFT CABIN CONCEPTS | 2016_0218 |
| Schneider, T. | STUDY ON EFFICIENT FULL ANNULUS URANS COMPUTATIONS OF AN INTAKE COMPRESSOR CONFIGURATION | 2016_0548 |
| Schrefl, M. | IN-FLIGHT PROVISIONING AND DISTRIBUTION OF ATM INFORMATION | 2016_0385 |
| Schroeder, K. | ADVANCED PROPULSION COLLISION DAMAGE DUE TO UNMANNED AERIAL SYSTEM INGESTION | 2016_0629 |
| Schwartz, K.G. | LINKING TECHNOLOGY READINESS TO UNCERTAINTY REDUCTION | 2016_0632 |
| Schwartz, H.D. | UNCERTAINTY QUANTIFICATION OF AIRFOIL DESIGN FOR ADVANCED PROPELLER MODELS | 2016_0665 |
| Schwartz, K.G. | TECHNOLOGY INTEGRATION AND SYSTEM ASSESSMENTS WITH UNCERTAINTY MODELLING | 2016_0742 |
| Seifollahi Moghadam , Z. | NUMERICAL STUDY OF ACTIVE SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTION CONTROL FOR TRANSONIC AERODYNAMICS | 2016_0714 |
| Seitz, A. | A REVIEW OF RECENT AIRCRAFT CONCEPTS EMPLOYING SYNERGISTIC PROPULSION-AIRFRAME INTEGRATION | 2016_0727 |
| Seo, G. | ON STABILITY MARGIN OF A LQR-BASED VEHICLE NETWORK | 2016_0412 |
| Seo, M.-G. | TERMINAL IMPACT ANGLE AND ANGLE-OF-ATTACK CONTROL GUIDANCE FOR SURFACE-TO-AIR MISSILE USING TVC | 2016_0568 |
| Serokhvostov, S.V. | OPTIMIZATION OF THE TRAJECTORY AND ACCUMULATOR MASS FOR THE SOLAR-POWERED AIRPLANE | 2016_0388 |
| Serokhvostov, S. | SMALL HEIGHT DUCT DESIGN FOR MULTICOPTER FAN | 2016_0611 |
| Shang, S. | NUMERICAL SIMULATION OF RCS FOR A SPHERICAL CONVERGENT FLAP NOZZLE WITH A NON-RECTANGULAR DIVERGENT DUCT | 2016_0077 |
| Shanygin, A. | NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES | 2016_0551 |
| Shanygin, A.N. | DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS | 2016_0620 |
| Shchurovskiy, Y.M. | INVESTIGATION OF CHARACTERISTICS OF THE OIL SYSTEM WITH ELECTRICALLY DRIVEN PUMPS FOR GAS TURBINE ENGINE | 2016_0165 |
| Sheen, d.-J. | CFD OF BLENDED WING BODY UCAV WITH VORTEX GENERATOR | 2016_0246 |
| Shelyukhin, Y.F. | HEURISTIC MODEL OF NON-STEADY LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK | 2016_0019 |
| Shen, Q. | AN EXPERIMENT INVESTIGATION ON SHOCKINDUCED TURBULENT BOUNDARY LAYER SEPARATION FLOW-FIELD | 2016_0339 |
| Sheng, X.J. | THE MANUFACTURE AND APPLICATION FOR COMPOSITES AEROELASTIC MODEL OF CIVIL AIRLINER WING IN FL-26 TRANSONIC WIND-TUNNEL | 2016_0587 |
| Sherwin, S.-J. | EFFECT OF A 3D INDENTATION ON BOUNDARY LAYER INSTABILITY | 2016_0578 |
| Shi-Pu, Y. | AERODYNAMIC ANALYSIS OF FLUSH-MOUNTED STATIC PORTS PLACEMENT ON THE COMMERCIAL TRANSPORT AIRCRAFT | 2016_0589 |
| Shim, S.-W. | AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY CONSTRAINTS | 2016_0355 |
| Shim, D.H. | FLIGHT TESTS OF THE VISION-BASED TARGET SENSING AND APPROACHING | 2016_0373 |
| Shim, D.H. | DESIGN THE GUIDANCE LAW FOR FORMATION FLIGHT OF MULTIPLE UAVS | 2016_0415 |
| Shim, T.M. | OPERATION SCENARIOS OF UNMANNED AIRCRAFT SYSTEMS INTEGRATED INTO THE KOREAN NATIONAL AIRSPACE SYSTEM | 2016_0445 |
| Shim, D.H. | DEPTH IMAGE BASED DIRECT SLAM FOR SMALL UAVS | 2016_0503 |
| Shin, S.J. | FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING | 2016_0123 |
| Shin, S.J. | A NEW SOLUTION METHOD FOR SIX DEGREE OF FREEDOM FLIGHT DYNAMICS SIMULATION OF A HIGH ASPECT RATIO WING VEHICLE | 2016_0158 |
| Shin, H. | DESIGN THE GUIDANCE LAW FOR FORMATION FLIGHT OF MULTIPLE UAVS | 2016_0415 |
| Shin, H.B. | KAI SURION HELICOPTER FULL-SCALE AIR INTAKE TESTING AT CIRA ICING WIND TUNNEL | 2016_0496 |
| Shin, H.-S. | EVOLUTIONARY GAME BASED MULTI-OBJECTIVE OPTIMIZATION FOR MULTI-AGENT NETWORK RESILIENCE | 2016_0722 |
| Shin, H.-S. | MULTI-STEP TRAJECTORY OPTIMIZATION FOR ATM BASED ON APPROXIMATED OPTIMAL PATH | 2016_0723 |
| Shindo, M. | DESIGN AND PRELIMINARY EVALUATION OF AN INTEGRATED AIRCRAFT OPERATION SYSTEM FOR DISASTER RELIEF | 2016_0088 |
| Shiva Prakasha, P. | COLLABORATIVE SYSTEMS DRIVEN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION | 2016_0585 |
| Shukhovtsov, D.V. | HEURISTIC MODEL OF NON-STEADY LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK | 2016_0019 |
| Shvalev, Y.G. | BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE | 2016_0383 |
| Si, J.T. | NUMERICAL STUDY OF FIXED TRANSITION LOCATION EFFECT ON SUPERCRITICAL WING AERODYNAMIC CHARACTERISTICS | 2016_0154 |
| Sibilska-Mroziewicz, A.-M. | DEVELOPMENT OF THE SMALL-SCALE MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT SAFETY TAKE-OFF AND LANDING | 2016_0359 |
| Sibilski, K.-S. | AN EXPERIMENTAL STUDY OF MICRO-ELECTROMECHANICAL FLYING INSECT FLAPPING WINGS AERODYNAMIC PERFORMANCE | 2016_0025 |
| Sibilski, K. | DEVELOPMENT OF THE SMALL-SCALE MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT SAFETY TAKE-OFF AND LANDING | 2016_0359 |
| Sidorenko, A.A. | STUDY OF THE UNSTEADY STRUCTURES EVOLUTION IN SHOCK WAVE / BOUNDARY LAYER INTERACTION FOR VARIOUS UPSTREAM CONDITIONS | 2016_0560 |
| Sidoryuk, M.E. | WIND TUNNEL THREE-DEGREE-OF-FREEDOM DYNAMIC RIG FOR CONTROL VALIDATION | 2016_0325 |
| Siepenkötter, N. | PRECISION LANDING BASED ON ATMOSPHERIC DISTURBANCE MONITORING AND MODEL PREDICTIVE CONTROL | 2016_0290 |
| Sieradzki, A. | INFLUENCE OF POWER UNIT CONFIGURATION LAYOUT OF A REGIONAL JET ON PERFORMANCE AND DIRECT OPERATING COST | 2016_0150 |
| Siggel, M. | COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT | 2016_0345 |
| Simakova , T.V. | NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN | 2016_0550 |
| Singh, R. | THE FUTURE JOURNEY OF CIVIL AEROSPACE: WEATHER, ENVIRONMENT AND CLIMATE | 2016_0736 |
| Sinha, N.K. | DYNAMIC MODELING AND STABILITY ANALYSIS OF A HIGH ALTITUDE AIRSHIP | 2016_0700 |
| Sinnige, T. | ANALYSIS OF SWIRL RECOVERY VANES FOR INCREASED PROPULSIVE EFFICIENCY IN TRACTOR PROPELLER AIRCRAFT | 2016_0060 |
| Siri, O. | THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION | 2016_0731 |
| Skawinski, I. | IS TO BE THE MICRODRONE | 2016_0646 |
| Slawinski, Z. | RESEARCH OF ALTERNATIVE FUEL WATER-FUEL MICRO EMULSION FROM POINT OF VIEW REDUCTION OF EMISSIONS | 2016_0667 |
| Smith, L. | OPTIMISATION OF A WING-BODY-TAIL CONFIGURATION WITH AN ALTERNATIVE LOW DRAG FUSELAGE AND BODY TRAILING EDGE | 2016_0223 |
| Sobieszek, A. | MODERN MATERIALS IN AEROSPACE INDUSTRY - MAGNESIUM ALLOY CONTROL SYSTEM LEVER OF THE UNMANNED ILX - 27 HELICOPTER | 2016_0457 |
| Sobron, A. | SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT | 2016_0390 |
| Sobron, A. | DESIGN AND TESTING OF A LOW-COST FLIGHT CONTROL AND DATA ACQUISITION SYSTEM FOR UNSTABLE SUBSCALE AIRCRAFT | 2016_0449 |
| Song, C. | EFFICIENT AERODYNAMIC OPTIMIZATION USING HIERARCHICAL KRIGING COMBINED WITH GRADIENT | 2016_0020 |
| Song, W.-P. | EFFICIENT AERODYNAMIC OPTIMIZATION USING HIERARCHICAL KRIGING COMBINED WITH GRADIENT | 2016_0020 |
| Song, B.-S. | LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV | 2016_0062 |
| Song, B.-F. | MULTI-OBJECTIVE OPTIMAL DESIGN OF THE PROPELLER FOR HIGH ALTITUDE AIRSHIPS BASED ON HIGH EFFICIENCY AND LIGHT WEIGHT | 2016_0100 |
| Song, G. | FAIRING OPTIMIZATION DESIGN OF WING STRUCTURE | 2016_0282 |
| Song, B. | THE PROPULSIVE EFFICIENCY OF FLEXIBLE FLAPPING-WING | 2016_0299 |
| Song, G. | APPLICATION OF BUCKLING/POST-BUCKLING ANALYSIS FOR COMPOSITE STIFFENED PANELS | 2016_0337 |
| Song, Y.K. | CHARACTERIZATION OF DISTORTED FLUID FLOW ALONG ADVANCED HIGH-BYPASS PROPULSION SYSTEM | 2016_0628 |
| Song, Y.K. | ADVANCED PROPULSION COLLISION DAMAGE DUE TO UNMANNED AERIAL SYSTEM INGESTION | 2016_0629 |
| Song, K. | AN EXPLORATION OF EVOLUTION PATHS FOR AIR TRANSPORTATION NETWORKS | 2016_0674 |
| Song, K. | A REVIEW AND A CLASSIFICATION SCHEME FOR AIR TRANSPORTATION NETWORK RESEARCH | 2016_0688 |
| Soria, D. | A STRESS INTENSITY FACTOR SOLUTION INSPIRED BY SOAP BUBBLES FRAMEWORK | 2016_0288 |
| Sorokin, S. | EFFECT OF FEEL SYSTEM CHARACTERISTICS ON PILOT MODEL PARAMETERS | 2016_0258 |
| Soudakov, V.G. | INVESTIGATION OF FLOW CONTROL OVER THE SUPERCRITICAL AIRFOIL BY TANGENTIAL JET BLOWING AT TRANSONIC SPEEDS | 2016_0173 |
| Spedding, G.R. | OPTIMISATION OF A WING-BODY-TAIL CONFIGURATION WITH AN ALTERNATIVE LOW DRAG FUSELAGE AND BODY TRAILING EDGE | 2016_0223 |
| Spiteri, A. | CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION | 2016_0211 |
| Staack, I. | DESIGN AND TESTING OF A LOW-COST FLIGHT CONTROL AND DATA ACQUISITION SYSTEM FOR UNSTABLE SUBSCALE AIRCRAFT | 2016_0449 |
| Staack, I. | KNOWLEDGE-BASED FUTURE COMBAT AIRCRAFT OPTIMIZATION | 2016_0538 |
| Stalewski, W. | OVERVIEW OF THE INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME | 2016_0313 |
| Stalewski, W. | EFFECTS OF LAMINAR-TURBULENT TRANSITION ON BUFFET ONSET AND TRANSONIC CHARACTERISTICS OF LAMINAR AIRFOIL | 2016_0455 |
| Stalewski, W. | FLOW CONTROL ON HELICOPTER-ROTOR BLADES VIA ACTIVE GURNEY FLAP | 2016_0527 |
| Startsev, A.N. | MULTI-DISCIPLINARY DESIGN OF HIGH-SPEED COMPRESSORS FOR PROSPECTIVE TURBO-SHAFT ENGINE | 2016_0481 |
| Staudenmaier, A. | USING OPENVSP IN A CONCEPTUAL AIRCRAFT DESIGN ENVIRONMENT IN MATLAB | 2016_0174 |
| Steelant, J. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Steenhuizen, D. | IMPROVED DESIGN OF A HIGH LIFT SYSTEM FOR GENERAL AVIATION AIRCRAFT | 2016_0347 |
| Steiner, D. | IN-FLIGHT PROVISIONING AND DISTRIBUTION OF ATM INFORMATION | 2016_0385 |
| Steshakov, E.G. | MULTI-DISCIPLINARY DESIGN OF HIGH-SPEED COMPRESSORS FOR PROSPECTIVE TURBO-SHAFT ENGINE | 2016_0481 |
| Stoeßel, M. | DESIGN AND DEVELOPMENT OF A MILITARY ENGINE INLET RESEARCH DUCT | 2016_0623 |
| Stojakovic, P. | GENERAL APPROACH TO THE ANALYSIS OF THE ASYMMETRICALLY LOADED AIRPLANE FLIGHT LIMITATIONS | 2016_0227 |
| Stokkermans, T. | ANALYSIS OF SWIRL RECOVERY VANES FOR INCREASED PROPULSIVE EFFICIENCY IN TRACTOR PROPELLER AIRCRAFT | 2016_0060 |
| Stollery, J. | THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW | 2016_0244 |
| Strack, M. | INTEGRATION OF HYBRID PROPULSION SYSTEM IN A CS23 COMMUTER DESIGN | 2016_0595 |
| Stremousov, K. | SMALL HEIGHT DUCT DESIGN FOR MULTICOPTER FAN | 2016_0611 |
| Stromberger, J.H. | HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES | 2016_0744 |
| Stryczniewicz, W. | INVESTIGATION OF UNSTEADY TRANSONIC FLOW FIELD ABOVE LAMINAR AIRFOIL BY PIV METHOD | 2016_0300 |
| Stryczniewicz, W. | COMPARATIVE ANALYSIS OF AIR FLOW IN THE COMPRESSOR OF THE GTD-350 ENGINE | 2016_0417 |
| Stryczniewicz, W. | ANALYSES OF AIRFLOW AROUND DUCTED FAN PROPULSION SYSTEM IN PUSHER CONFIGURATION USING PIV METHOD | 2016_0659 |
| Stuhlberger, J. | HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES | 2016_0744 |
| Subagyo, S. | INLET DUCT ENGINE TEST FACILITIES IN INDONESIA LOW SPEED TUNNEL (ILST) | 2016_0196 |
| Sugioka, Y. | NON-INTRUSIVE UNSTEADY PSP TECHNIQUE FOR INVESTIGATION OF TRANSONIC BUFFETING | 2016_0553 |
| Sugiura, M. | DESIGN OPTIMIZATION OF HELICOPTER BLADE USING CLASS SHAPE FUNCTION BASED GEOMETRY REPRESENTATION | 2016_0479 |
| Suk, J. | ADAPTIVE SLIDING MODE CONTROLLER DESIGN FOR RECONFIGURATION OF ORGANIC FLIGHT ARRAY | 2016_0401 |
| Suk, J.Y. | ADAPTIVE NEURAL NETWORK CONTROLLER DESIGN FOR BLENDED-WING UAV WITH COMPLEX DAMAGE | 2016_0516 |
| Sun, H.-S. | WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS | 2016_0091 |
| Sun, Q. | TOTAL TEMPERATURE RECOVERY CHARACTERISTICS TEST TECHNIQUE BASED ON TOTAL PRESSURE CALIBRATION WIND TUNNEL | 2016_0112 |
| Suntsov , S.V. | EFFECT OF REYNOLDS NUMBER, OPERATING MODE, TURBULENCE PARAMETERS ON PROFILE AND SECONDARY LOSSES OF LPT | 2016_0276 |
| Surmacz, K. | EFFECTS OF LAMINAR-TURBULENT TRANSITION ON BUFFET ONSET AND TRANSONIC CHARACTERISTICS OF LAMINAR AIRFOIL | 2016_0455 |
| Surmacz, K.-A. | AN AERODYNAMIC ANALYSIS OF THE 3D FLOW AROUND THE SSC-A09 AIRFOIL | 2016_0671 |
| Suzuki, S. | OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS | 2016_0338 |
| Sviridov, A.A. | PREDICTION OF WFD OCCURRENCE IN LONGITUDINAL JOINTS OF A FUSELAGE FOR COMMERCIAL AIRPLANE | 2016_0639 |
| Szczepaniak, R. | COMPARATIVE ANALYSIS OF AIR FLOW IN THE COMPRESSOR OF THE GTD-350 ENGINE | 2016_0417 |
| Sznajder, J. | EFFECTS OF LAMINAR-TURBULENT TRANSITION ON BUFFET ONSET AND TRANSONIC CHARACTERISTICS OF LAMINAR AIRFOIL | 2016_0455 |
| Tahk, M.-J. | ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME | 2016_0096 |
| Tahk, M.J. | PERCH LANDING ASSISTED BY THRUSTER (PLAT): SIX D.O.F. TRAJECTORY OPTIMIZATION | 2016_0334 |
| Tahk, M.-J. | AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY CONSTRAINTS | 2016_0355 |
| Tahk, M.-J. | TRAJECTORY DESIGN WITH PATH PREDICTION FOR TERRAIN FOLLOWING | 2016_0379 |
| Tahk, M.-J. | TERMINAL IMPACT ANGLE AND ANGLE-OF-ATTACK CONTROL GUIDANCE FOR SURFACE-TO-AIR MISSILE USING TVC | 2016_0568 |
| Tai, J. | TECHNOLOGY INTEGRATION AND SYSTEM ASSESSMENTS WITH UNCERTAINTY MODELLING | 2016_0742 |
| Takase, M. | THE DRONE AVIATION NAVIGATION SYSTEMS | 2016_0010 |
| Takatani, K. | APPLICATION OF FLAME MEASUREMENT TECHNIC BY DENSELY INSTALLED ION-PROBES ON 2-STROKE GASOLINE ENGINE | 2016_0418 |
| Takovitskii, S.A. | AERODYNAMIC SHAPES DESIGN ON THE BASE OF DIRECT NEWTON TYPE OPTIMIZATION METHOD | 2016_0220 |
| Talebi, B. | OPTIMIZATION OF COMPOSITE PATCH REPAIR FOR INCLINED CRACK ON ALUMINUM PLATE USING GENETIC ALGORITHM | 2016_0500 |
| Talyzin, V.A. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Talyzin, V.A. | BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE | 2016_0383 |
| Talyzin, V.A. | INVESTIGATION OF THE HYDROGEN COMBUSTION CHAMBER PERFORMANCE WITHIN THE HEXAFLY-INT PROJECT | 2016_0458 |
| Tamura, K. | EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA | 2016_0682 |
| Tan, Z.G. | A CONCEPTUAL ANALYSIS OF AN AIRCRAFT WITH REAR-MOUNTED OPEN ROTOR ENGINES | 2016_0253 |
| Tanabe, Y. | DESIGN OPTIMIZATION OF HELICOPTER BLADE USING CLASS SHAPE FUNCTION BASED GEOMETRY REPRESENTATION | 2016_0479 |
| Tanaka, M. | THE DRONE AVIATION NAVIGATION SYSTEMS | 2016_0010 |
| Tang, G. | DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL | 2016_0403 |
| Tang, C. | FLIGHT DYNAMIC RESPONSE ANALYSIS OF THE FLEXIBLE AIRCRAFT FLYING THROUGH THE WIND FIELD OVER COMPLEX TERRAINS | 2016_0497 |
| Tang, C. | FLIGHT DYNAMIC STABILITY ANALYSIS OF A FLEXIBLE FLYING WING | 2016_0532 |
| Tanguy, G. | THE INFLUENCE OF A LOCAL CHANGE IN WING DIHEDRAL ON THE LOW SPEED FLOW CHARACTERISTICS OF RECTANGULAR PLANFORM WINGS | 2016_0459 |
| Tartaglione, G. | MODEL PREDICTIVE CONTROL FOR A SWARM OF FIXED WING UAVS | 2016_0326 |
| Tartaglione, G. | NONLINEAR DYNAMIC INVERSION WITH NEURAL NETWORKS FOR THE FLIGHT CONTROL OF A LOW COST TILT ROTOR UAV | 2016_0637 |
| Tavernari, V.D. | LOW REYNOLDS PROPELLER META-MODEL FOR MULTIDICIPLYNARY OPTIMIZATION | 2016_0003 |
| Tekinalp, O. | A NOVEL FLIGHT CONTORL ALGORITHM FOR MULTICOPTERS | 2016_0231 |
| Temis, Y.M. | MULTI-DISCIPLINARY DESIGN OF HIGH-SPEED COMPRESSORS FOR PROSPECTIVE TURBO-SHAFT ENGINE | 2016_0481 |
| Thoraval, B. | HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS | 2016_0438 |
| Tian, Y. | AIRCRAFT SECURITY ENHANCEMENT: ROTATING MACHINERY FAULT DIAGNOSIS AND HEALTH ASSESSMENT USING MANIFOLD LEARNING AND DYNAMIC TIME WARPING | 2016_0435 |
| Tomlin, C.J. | SECURE ESTIMATION FOR UNMANNED AERIAL VEHICLES AGAINST ADVERSARIAL ATTACKS | 2016_0221 |
| Treve, V. | WAKE TURBULENCE RE-CATEGORISATION ON APPROACH AND DEPARTURE FOR SAFE AND MORE EFFICIENT AIR TRAFFIC MANAGEMENT | 2016_0230 |
| Troshin, A.I. | COMPUTATIONAL EFFICIENCY AND QUALITY OF DIFFERENT VERSIONS OF DISCONTINUOUS GALERKIN METHOD FOR LES/DES APPLICATIONS | 2016_0099 |
| Truong, V.H. | A STUDY ON FAILURE BEHAVIORS OF REPAIRED COMPOSITE STRUCTURES WITH SCARF BONDED PATCH | 2016_0335 |
| Tsirkunov, Y.M. | LARGE-SCALE VORTEX STRUCTURE OF FLOW IN THE NEAR WAKE BEHIND AN AIRLINER DURING TAKEOFF AND LANDING | 2016_0666 |
| Tsourdos, A. | EVOLUTIONARY GAME BASED MULTI-OBJECTIVE OPTIMIZATION FOR MULTI-AGENT NETWORK RESILIENCE | 2016_0722 |
| Tsourdos, A. | MULTI-STEP TRAJECTORY OPTIMIZATION FOR ATM BASED ON APPROXIMATED OPTIMAL PATH | 2016_0723 |
| Tsvetkov, A.I. | LARGE-SCALE VORTEX STRUCTURE OF FLOW IN THE NEAR WAKE BEHIND AN AIRLINER DURING TAKEOFF AND LANDING | 2016_0666 |
| Tuktarov, S.A. | MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS | 2016_0226 |
| Tutty, M. | STORE SEPARATION FROM WEAPON BAYS | 2016_0156 |
| Tyaglik, M.S. | THE FLYING QUALITIES IMPROVEMENT FOR THE VEHICLES WITH TIME DELAY IN THEIR DYNAMICS | 2016_0043 |
| Tyaglik, A.S. | THE FLYING QUALITIES IMPROVEMENT FOR THE VEHICLES WITH TIME DELAY IN THEIR DYNAMICS | 2016_0043 |
| Uemura, T. | OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS | 2016_0338 |
| Ueno, S. | MINIMUM-TIME FORMATION USING OPTIMAL SOLUTIONS OF SINGLE FIXED-WING AIRCRAFT | 2016_0195 |
| Ulrey, M.L. | AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS | 2016_0202 |
| Um, T.-Y. | CAPTURE REGION ANALYSIS FOR MISSILE GUIDANCE WITH FIELD-OF-VIEW CONSTRAINT AGAINST MOVING TARGET | 2016_0129 |
| Uranga, A. | THE D8 AIRCRAFT CONCEPT AND ITS BOUNDARY LAYER INGESTION BENEFIT | 2016_0747 |
| Uskov, V.M. | MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS | 2016_0226 |
| van de Kamp, B. | MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES | 2016_0596 |
| van der Hoorn, L. | TOWARDS A MORE HARMONISED AND WIDER USE OF SHORT-TERM ATFCM MEASURES (STAM) | 2016_0055 |
| van der Vorst, J. | QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH | 2016_0555 |
| van der Weide, E.T.A. | EULERIAN METHOD FOR IN-ENGINE ICING: WITH APPLICATION TO ICE CRYSTAL TRAJECTORIES AND IMPACT IN A GENERIC TURBOFAN COMPRESSOR | 2016_0322 |
| van Heerden, A.S.J. | ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN | 2016_0525 |
| Vassiliev, V. | NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES | 2016_0551 |
| Veerasamy, D. | EXPERIMENTAL STUDY OF AEROFOIL-WAKE INDUCED TRANSITION IN BOUNDARY LAYERS | 2016_0083 |
| Veldhuis, L. | ANALYSIS OF SWIRL RECOVERY VANES FOR INCREASED PROPULSIVE EFFICIENCY IN TRACTOR PROPELLER AIRCRAFT | 2016_0060 |
| Veldhuis, L.L.M. | IMPROVED DESIGN OF A HIGH LIFT SYSTEM FOR GENERAL AVIATION AIRCRAFT | 2016_0347 |
| Velicki, A. | STITCHED, RESIN-INFUSED, HWB AIRCRAFT STRUCTURAL DEVELOPMENTS | 2016_0739 |
| Verstraete, D. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Viguer, M. | THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW | 2016_0244 |
| Villace, V. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Viola, N. | SELECTION OF AN UAV CONFIGURATION LAYOUT FOR OPTIMISATION OF TELEDETECTION MISSION USING HYPERSPECTRAL SENSORS | 2016_0318 |
| Viola, N. | CABIN ESCAPE SYSTEM: A WAY TO ENSURE CREW SAFETY DURING SUBORBITAL FLIGHTS | 2016_0506 |
| Viola, N. | INVESTIGATIONS OF GROUND INFRASTRUCTURES FOR UAS FLIGHT MONITORING | 2016_0514 |
| Viviani, A. | AERODYNAMIC ANALYSIS WITH SEPARATION DYNAMICS OF A LAUNCHER AT STAGING CONDITIONS | 2016_0570 |
| Vlasenko, V.V. | COMPUTATIONAL EFFICIENCY AND QUALITY OF DIFFERENT VERSIONS OF DISCONTINUOUS GALERKIN METHOD FOR LES/DES APPLICATIONS | 2016_0099 |
| Vodicka, R. | TRANSFORMING MILITARY AEROSPACE SUSTAINMENT | 2016_0734 |
| Voevodenko, N.V. | NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT | 2016_0353 |
| Voevodenko, N.V. | BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE | 2016_0383 |
| Voloschenko, O.V. | INVESTIGATION OF THE HYDROGEN COMBUSTION CHAMBER PERFORMANCE WITHIN THE HEXAFLY-INT PROJECT | 2016_0458 |
| Vrchota, P. | EXPERIMENATAL AND COMPUTATIONAL STUDY OF GROUND EFFECT ON AIRFOIL SECTION | 2016_0122 |
| Vukovic, D. | A STUDY OF WALL-INTERFERENCE EFECTS IN WIND-TUNNEL TESTING OF A STANDARD MODEL AT TRANSONIC SPEEDS | 2016_0216 |
| Vukovic, D. | A GENERALISATION OF THE MATHEMATICAL MODEL OF INTERNAL WIND TUNNEL BALANCES | 2016_0329 |
| Wall, A. | SIMULATION OF UNSTEADY SHIP AIRWAKES USING OPENFOAM | 2016_0094 |
| Wan Omar, W.Z. | IMPORTANCE OF TRANSIENT AERODYNAMIC DERIVATIVES FOR V-TAIL AIRCRAFT FLIGHT DYNAMIC DESIGN | 2016_0515 |
| Wang, S. | COMPUTATIONAL INVESTIGATION FOR FREE-FLIGHT AERODYNAMICS AND FLIGHT DYNAMICS OF SUBSONIC AND SUPERSONIC PROJECTILES | 2016_0005 |
| Wang, Z. | DISPATCH RELIABILITY ORIENTED MMEL FORMULATION TECHNOLOGY RESEARCH | 2016_0030 |
| Wang, K. | DISTRIBUTED PROPELLERS SLIPSTREAM EFFECTS ON WING AT LOW REYNOLDS NUMBER | 2016_0074 |
| Wang, H.-B. | NUMERICAL SIMULATION OF THE PROPELLER/WING INTERACTIONS AT LOW REYNOLDS NUMBER | 2016_0075 |
| Wang, R. | MODELING AND CONTROL OF HIGHLY FLEXIBLE FLYING-WING UAV WITH MULTIPLE ELEVONS AND PROPELLERS | 2016_0101 |
| Wang, Z.P. | MODELING AND CONTROL OF HIGHLY FLEXIBLE FLYING-WING UAV WITH MULTIPLE ELEVONS AND PROPELLERS | 2016_0101 |
| Wang, L. | TOTAL TEMPERATURE RECOVERY CHARACTERISTICS TEST TECHNIQUE BASED ON TOTAL PRESSURE CALIBRATION WIND TUNNEL | 2016_0112 |
| Wang, L. | STUDY ON THE SAFETY RISK AND CAPACITY OF THE ONE-WAY CIRCULATION AIR ROUTE IN CHINA | 2016_0115 |
| Wang, G. | AERODYNAMIC CHARACTERISTIC COMPARISON OF THE FORWARD AND BACKWARD-SWEPT WINGS | 2016_0125 |
| Wang, X. | COMBAT EFFECTIVENESS EVALUATION-ORIENTED AVIONICS SYSTEM MODELING | 2016_0137 |
| Wang, F.-W. | DETACHED EDDY SIMULATION OF AIRCRAFT MASSIVELY SEPARATED FLOWS | 2016_0140 |
| Wang, W. | MODELING AND ANALYSIS METHOD ON CRASHWORTHINESS OF CIVILIAN AIRCRAFT FUSELAGE STRUCTURES | 2016_0178 |
| Wang, B.-W. | RESEARCH ON VIBRATION CHARACTERISTIC FOR VARIABLE ROTATING VELOCITY BLADES | 2016_0189 |
| Wang, Q. | ANALYSIS ON OFFLINE AND ONLINE IDENTIFICATION METHODS FOR AIRCRAFT STABILITY AND CONTROL DERIVATIVES | 2016_0203 |
| Wang, J. | A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM | 2016_0321 |
| Wang, Z.-Y. | MAKING HEALTH MANAGEMENT MORE CONCISE AND EFFICIENT: AIRCRAFT CONDITION MONITORING BASED ON COMPRESSED SENSING | 2016_0400 |
| Wang, X. | TAXIING ROUTE PLANNING BASED ON AIRPORT HOTSPOTS | 2016_0402 |
| Wang, G.L. | STUDY OF MODEL DEFORMATION AND STING INTERFERENCE TO THE AERODYNAMIC ESTIMATIONS OF THE CAE-AVM MODEL | 2016_0405 |
| Wang, Z.-L. | AIRCRAFT SECURITY ENHANCEMENT: ROTATING MACHINERY FAULT DIAGNOSIS AND HEALTH ASSESSMENT USING MANIFOLD LEARNING AND DYNAMIC TIME WARPING | 2016_0435 |
| Wang, L. | FLIGHT DYNAMIC RESPONSE ANALYSIS OF THE FLEXIBLE AIRCRAFT FLYING THROUGH THE WIND FIELD OVER COMPLEX TERRAINS | 2016_0497 |
| Wang, C. | FUEL STARVATION CAUSED BY HUB CLOSURE | 2016_0513 |
| Wang, D. | DESIGN, MANUFACTURE AND FREQUENCY EXPERIMENT OF A NOVEL FLUTTER MODEL FOR AGARD WING 445.6 WITH STRUCTURE-SIMILARITY | 2016_0519 |
| Wang, L. | FLIGHT DYNAMIC STABILITY ANALYSIS OF A FLEXIBLE FLYING WING | 2016_0532 |
| Wang, P. | LINEAR MODELING BASED ON INSTRUMENTAL MODEL ESTIMATION AND PID PARAMETERS TUNING IN FREQUENCY-DOMAIN OF AIRCRAFT ENGINE | 2016_0702 |
| Wang, H.W. | THE RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION FIELDMEASUREMENT BASED ON FLUORESCENT OIL FILM | 2016_0710 |
| Watanabe, Y. | NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION | 2016_0370 |
| Wei, L. | AN EXPERIMENT INVESTIGATION ON SHOCKINDUCED TURBULENT BOUNDARY LAYER SEPARATION FLOW-FIELD | 2016_0339 |
| Wei, L.F. | THE RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION FIELDMEASUREMENT BASED ON FLUORESCENT OIL FILM | 2016_0710 |
| Wei-qi, Q. | ESTIMATION OF TEMPERATURE-DEPENDANT THERMAL CONDUCTIVITY OF MATERIAL WITH GENETIC ALGORITHM | 2016_0291 |
| Werter, N.P.M. | DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM | 2016_0166 |
| Whurr, J. | HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES | 2016_0744 |
| Wiart, L. | AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS | 2016_0092 |
| Wickramasinghe, N.K. | BENEFITS ASSESSMENT ON TIME-BASED OCEANIC ARRIVALS TO THE TOKYO METROPOLITAN AREA | 2016_0475 |
| Winter, M. | SENSITIVITY ANALYSIS OF UNSTEADY AERODYNAMIC REDUCED-ORDER MODELS ROBUST TO FREESTREAM PARAMETER VARIATIONS | 2016_0206 |
| Wojtas, M. | MODERN MATERIALS IN AEROSPACE INDUSTRY - MAGNESIUM ALLOY CONTROL SYSTEM LEVER OF THE UNMANNED ILX - 27 HELICOPTER | 2016_0457 |
| Wolkov, A.V. | COMPUTATIONAL EFFICIENCY AND QUALITY OF DIFFERENT VERSIONS OF DISCONTINUOUS GALERKIN METHOD FOR LES/DES APPLICATIONS | 2016_0099 |
| Wolkov, A.V. | INFLUENCE OF SURFACE FRACTAL MICROSTRUCTURE ON THE CHARACTERISTICS OF A TURBULENT BOUNDARY LAYER | 2016_0138 |
| Wróblewski, W. | DEVELOPMENT OF THE SMALL-SCALE MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT SAFETY TAKE-OFF AND LANDING | 2016_0359 |
| Wu, X. | EXTENDED LOCAL SCATTERING THEORY AND THE ROLE OF A SCATTER ON BOUNDARY-LAYER INSTABILITY AND ACOUSTIC RADIATION | 2016_0333 |
| Wu, X. | STOCHASTIC TRANSONIC AERODYNAMICS ANALYSIS | 2016_0398 |
| Wu, Z.H. | A FOLDABLE FLAPPING WING DESIGN INSPIRED BY THE ELBOW-WRIST ANATOMY OF BATS | 2016_0609 |
| Wu, Y. | A STUDY ON SAFETY ASSURANCE FOR INCREASINGLY AUTONOMOUS TRAFFIC FLOW MANAGEMENT SYSTEM | 2016_0672 |
| Xiang, J. | HANDLING QUALITIES PREDICTION BASED ON ADAPTIVE OPTIMAL CONTROL PILOT MODEL | 2016_0143 |
| Xiang, X. | AN EXPERIMENT INVESTIGATION ON SHOCKINDUCED TURBULENT BOUNDARY LAYER SEPARATION FLOW-FIELD | 2016_0339 |
| Xiao, H. | 3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION | 2016_0039 |
| Xiaoqian, C. | THE EFFECT OF SATELLITE FORMATION FLYING ON AUTONOMOUS NAVOGATION | 2016_0316 |
| Xiong, H.L. | THE RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION FIELDMEASUREMENT BASED ON FLUORESCENT OIL FILM | 2016_0710 |
| Xu, J. | INVESTIGATION ON OBLIQUE SHOCK WAVE CONTROL BY SURFACE ARC DISCHARGE PLASMA | 2016_0124 |
| Xu, L. | EXPERIMENTAL INVESTIGATION OF LATERAL PULSE JET INTERACTION FLOWFIELD IN HYPERSONIC FLOW | 2016_0391 |
| Xu, H. | EFFECT OF A 3D INDENTATION ON BOUNDARY LAYER INSTABILITY | 2016_0578 |
| Xue, R.R. | AERODYNAMIC CHARACTERISTIC COMPARISON OF THE FORWARD AND BACKWARD-SWEPT WINGS | 2016_0125 |
| Xue, D. | THE PROPULSIVE EFFICIENCY OF FLEXIBLE FLAPPING-WING | 2016_0299 |
| Yadav, A. | AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS AN OSCILLATORY PITCHING NACA0012 AEROFOIL | 2016_0249 |
| Yakovleva, V.A. | BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE | 2016_0383 |
| Yakushev, D.A. | MULTI-DISCIPLINARY DESIGN OF HIGH-SPEED COMPRESSORS FOR PROSPECTIVE TURBO-SHAFT ENGINE | 2016_0481 |
| Yamada, S. | THE DRONE AVIATION NAVIGATION SYSTEMS | 2016_0010 |
| Yamada, K. | FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS | 2016_0393 |
| Yan, H. | INVESTIGATION ON OBLIQUE SHOCK WAVE CONTROL BY SURFACE ARC DISCHARGE PLASMA | 2016_0124 |
| Yan, M. | NUMERICAL INVESTIGATION OF INLET STARTING CHARACTERISTICS | 2016_0296 |
| Yan, Z.B. | THE MANUFACTURE AND APPLICATION FOR COMPOSITES AEROELASTIC MODEL OF CIVIL AIRLINER WING IN FL-26 TRANSONIC WIND-TUNNEL | 2016_0587 |
| Yang, X.-D. | EFFICIENT AERODYNAMIC OPTIMIZATION USING HIERARCHICAL KRIGING COMBINED WITH GRADIENT | 2016_0020 |
| Yang, S.P. | SYNTHESIZED ANALYSIS FROM DESIGN RANGE TO THE CONCETUAL DESIGN OF WIDEBODY AIRLINER | 2016_0058 |
| Yang, Q. | NUMERICAL SIMULATION OF RCS FOR A SPHERICAL CONVERGENT FLAP NOZZLE WITH A NON-RECTANGULAR DIVERGENT DUCT | 2016_0077 |
| Yang, L. | EFFECT OF ELASTIC DEFORMATION ON FLIGHT DYNAMICS OF PROJECTILES WITH LARGE SLENDERNESS RATIO | 2016_0119 |
| Yang, M.-H. | MODELLING NONLINEAR HIGH-PRECISION UNSTEADY AERODYNAMICS FOR ADVANCED AIRCRAFT AT HIGH ANGLE OF ATTACK | 2016_0152 |
| Yang, B.J. | FORMAL VERIFICATION OF AUTOPILOTS IN UMANNED AIRCRAFT SYSTEMS | 2016_0190 |
| Yang, Z.C. | THE INFLUENCE OF MORPHING PROCESS ON THE AEROELASTIC CHARACTERISTICS OF A FOLDING WING | 2016_0198 |
| Yang, W. | THE PROPULSIVE EFFICIENCY OF FLEXIBLE FLAPPING-WING | 2016_0299 |
| Yang, G. | DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL | 2016_0403 |
| Yang, R. | THE MANUFACTURE AND APPLICATION FOR COMPOSITES AEROELASTIC MODEL OF CIVIL AIRLINER WING IN FL-26 TRANSONIC WIND-TUNNEL | 2016_0587 |
| Yang, F. | AERODYNAMIC ANALYSIS OF FLUSH-MOUNTED STATIC PORTS PLACEMENT ON THE COMMERCIAL TRANSPORT AIRCRAFT | 2016_0589 |
| Yanishevsky, M. | RESEARCH ADVANCES ON AIRCRAFT STRUCTURAL INTEGRITY AND SUSTAINMENT AT NRC | 2016_0726 |
| Yanovskiy, L. | THE FOAMING PROPERTIES OF LUBRICATING OILS FOR AIRCRAFT GAS TURBINE ENGINES | 2016_0270 |
| Yao, M. | 3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION | 2016_0039 |
| Yatsufusa, T. | APPLICATION OF FLAME MEASUREMENT TECHNIC BY DENSELY INSTALLED ION-PROBES ON 2-STROKE GASOLINE ENGINE | 2016_0418 |
| Ye, Z. | COMPUTATIONAL INVESTIGATION FOR FREE-FLIGHT AERODYNAMICS AND FLIGHT DYNAMICS OF SUBSONIC AND SUPERSONIC PROJECTILES | 2016_0005 |
| Ye, Z.Y. | EFFECT OF ELASTIC DEFORMATION ON FLIGHT DYNAMICS OF PROJECTILES WITH LARGE SLENDERNESS RATIO | 2016_0119 |
| Ye, Z.Y. | AERODYNAMIC CHARACTERISTIC COMPARISON OF THE FORWARD AND BACKWARD-SWEPT WINGS | 2016_0125 |
| Ye, K. | UNCERTAINTY QUANTIFICATION AND GLOBAL SENSITIVITY ANALYSIS FOR HYPERSONIC AEROTHERMOELASTIC ANALYSIS | 2016_0135 |
| Ye, Z.Y. | UNCERTAINTY QUANTIFICATION AND GLOBAL SENSITIVITY ANALYSIS FOR HYPERSONIC AEROTHERMOELASTIC ANALYSIS | 2016_0135 |
| Ye, Z.Y. | NUMERICAL STUDY ON TRANSONIC BUFFET ACTIVE CONTROL BY OPEN AND CLOSED-LOOP STRATEGIES | 2016_0346 |
| Yee, K. | EFFICIENT MULTI-RESOLUTION ANALYSIS FOR IMPLICIT TEMPORAL INTEGRATION | 2016_0427 |
| Yee, K.J. | APPLICATION OF PROPER ORTHOGONAL DECOMPOSITION FOR AVIATION SAFETY | 2016_0576 |
| Yi, W. | THE EFFECT OF SATELLITE FORMATION FLYING ON AUTONOMOUS NAVOGATION | 2016_0316 |
| Yi-Feng, S. | AERODYNAMIC ANALYSIS OF FLUSH-MOUNTED STATIC PORTS PLACEMENT ON THE COMMERCIAL TRANSPORT AIRCRAFT | 2016_0589 |
| Yim, J.B. | FROM 500MD TO LAH - CHALLENGE TOWARD VERTICAL LIFT IN KOREA | 2016_0301 |
| Ying, S.X. | REPORT FROM ICAS WORKSHOP ON COMPLEX SYSTEMS INTEGRATION IN AERONAUTICS | 2016_0732 |
| Yokoyama, N. | INFERENCE OF FLIGHT INTENT BASED ON INVERSE OPTIMAL CONTROL | 2016_0501 |
| Yong, Z. | THE EFFECT OF SATELLITE FORMATION FLYING ON AUTONOMOUS NAVOGATION | 2016_0316 |
| Yongwei, G. | DEVELOPMENT OF HALF-MODEL TEST CAPABILITY AT THE NF-3 WIND TUNNEL | 2016_0034 |
| Yoo, C.-S. | LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV | 2016_0062 |
| Yoo, D.-W. | ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME | 2016_0096 |
| Yoon, J. | COMBUSTION INSTABILITY FREQUENCY MODE SHIFT OF H2/CH4 RATIO AND COMBUSTOR LENGTH IN A MODEL GAS TURBINE | 2016_0406 |
| Yoon, Y. | COMBUSTION INSTABILITY FREQUENCY MODE SHIFT OF H2/CH4 RATIO AND COMBUSTOR LENGTH IN A MODEL GAS TURBINE | 2016_0406 |
| Yu, J. | DETACHED EDDY SIMULATION OF AIRCRAFT MASSIVELY SEPARATED FLOWS | 2016_0140 |
| Yu, Z. | ESTIMATION OF TEMPERATURE-DEPENDANT THERMAL CONDUCTIVITY OF MATERIAL WITH GENETIC ALGORITHM | 2016_0291 |
| Yu, Y. | DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL | 2016_0403 |
| Yuan, W. | SIMULATION OF UNSTEADY SHIP AIRWAKES USING OPENFOAM | 2016_0094 |
| Yuan, S. | TOTAL TEMPERATURE RECOVERY CHARACTERISTICS TEST TECHNIQUE BASED ON TOTAL PRESSURE CALIBRATION WIND TUNNEL | 2016_0112 |
| Yuan, H. | MAKING HEALTH MANAGEMENT MORE CONCISE AND EFFICIENT: AIRCRAFT CONDITION MONITORING BASED ON COMPRESSED SENSING | 2016_0400 |
| Yun, J.-M. | SELECTION OF PARAMETERS IN SPR CAMERA SYSTEM FOR STRUCTURAL HEALTH MONITORING OF UAV MAIN WING | 2016_0505 |
| Yuzhu, B. | THE EFFECT OF SATELLITE FORMATION FLYING ON AUTONOMOUS NAVOGATION | 2016_0316 |
| Zakharov, V.S. | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE | 2016_0380 |
| Zammit-Mangion, D. | CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION | 2016_0211 |
| Zang , J. | COMBAT EFFECTIVENESS EVALUATION-ORIENTED AVIONICS SYSTEM MODELING | 2016_0137 |
| Zarati, K. | HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS | 2016_0438 |
| Zare-Behtash, H. | CHARACTERISATION OF NS-DBD PLASMA ACTUATORS FOR SUPERSONIC FLOW CONTROL | 2016_0170 |
| Zenghong, H. | DEVELOPMENT OF HALF-MODEL TEST CAPABILITY AT THE NF-3 WIND TUNNEL | 2016_0034 |
| Zeyghami, S. | STRATEGIES FOR ACHIEVING BACKWARD FLIGHT BY A DRAGONFLY | 2016_0754 |
| Zhan, H. | MODELLING NONLINEAR HIGH-PRECISION UNSTEADY AERODYNAMICS FOR ADVANCED AIRCRAFT AT HIGH ANGLE OF ATTACK | 2016_0152 |
| Zhang, Q. | COMPUTATIONAL INVESTIGATION FOR FREE-FLIGHT AERODYNAMICS AND FLIGHT DYNAMICS OF SUBSONIC AND SUPERSONIC PROJECTILES | 2016_0005 |
| Zhang, K.-S. | STRUCTURAL CONSTRAINTS INVESTIGATION IN WING AERODYNAMIC/STRUCTURAL OPTIMIZATION | 2016_0086 |
| Zhang, H. | STRUCTURAL CONSTRAINTS INVESTIGATION IN WING AERODYNAMIC/STRUCTURAL OPTIMIZATION | 2016_0086 |
| Zhang, Y.-G. | MULTI-OBJECTIVE OPTIMAL DESIGN OF THE PROPELLER FOR HIGH ALTITUDE AIRSHIPS BASED ON HIGH EFFICIENCY AND LIGHT WEIGHT | 2016_0100 |
| Zhang, H. | COMBAT EFFECTIVENESS EVALUATION-ORIENTED AVIONICS SYSTEM MODELING | 2016_0137 |
| Zhang, Y. | HANDLING QUALITIES PREDICTION BASED ON ADAPTIVE OPTIMAL CONTROL PILOT MODEL | 2016_0143 |
| Zhang, J. | RESEARCH ON LOAD SPECTRUM OF AERO HYDRAULIC PUMP BASED ON ACCELERATED DEGRADATION TESTING | 2016_0181 |
| Zhang, L. | SEMI-A VIBRATION SUPPRESSION OF AIRCRAFT PANEL USING PIEZOELECTRIC ACTUATOR WITH SYNCHRONIZED SWITCH DAMPING TECHNIQUE | 2016_0248 |
| Zhang, R. | EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL | 2016_0260 |
| Zhang, B. | PHYSICALLY-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION FRAMEWORK COUPLING AIRFRAME AND PROPULSION | 2016_0268 |
| Zhang, R. | FAIRING OPTIMIZATION DESIGN OF WING STRUCTURE | 2016_0282 |
| Zhang, T. | LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER CORROSION ENVIRONMENT | 2016_0308 |
| Zhang, S. | LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER CORROSION ENVIRONMENT | 2016_0308 |
| Zhang, W.W. | NUMERICAL STUDY ON TRANSONIC BUFFET ACTIVE CONTROL BY OPEN AND CLOSED-LOOP STRATEGIES | 2016_0346 |
| Zhang, W. | STOCHASTIC TRANSONIC AERODYNAMICS ANALYSIS | 2016_0398 |
| Zhang , W. | UNSTEADY AERODYNAMICS MODELLING AND ITS APPLICATION IN AEROELASTIC STABILITY ANALYSIS | 2016_0407 |
| Zhang, W.-W. | RESEARCH ON THE IMPACT OF SHOCK WAVE TO EXTENSIONALITY OF POD METHOD | 2016_0409 |
| Zhang, Z.-Y. | INVESTIGATION ON FLOW SEPARATION EFFECTS ON AIRCRAFT LONGITUDINAL MOMENT CHARACTERISTIC FOR FUSELAGE-MOUNTED AIRCRAFT | 2016_0421 |
| Zhang, M. | A CONCEPTUAL DESIGN PLATFORM FOR BLENDED-WING-BODY TRANSPORTS | 2016_0510 |
| Zhang, B. | A CONCEPTUAL DESIGN PLATFORM FOR BLENDED-WING-BODY TRANSPORTS | 2016_0510 |
| Zhang, X.G. | CO-EVOLUTION OF COMPLEX AERONAUTICAL SYSTEM & COMPLEX SYSTEM ENGINEERING | 2016_0751 |
| Zhao, M. | 3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION | 2016_0039 |
| Zhao, X.J. | PANEL VIBRO-ACOUSTIC RESPONSE PREDICTION BASED ON TURBULENT BOUNDARY LAYER MEASUREMENT | 2016_0040 |
| Zhao, H.W. | PID TUNING FOR MULTI-CHANNEL STRUCTURAL FATIGUE TESTING SYSTEM | 2016_0159 |
| Zhao, M. | MODELING AND ANALYSIS METHOD ON CRASHWORTHINESS OF CIVILIAN AIRCRAFT FUSELAGE STRUCTURES | 2016_0178 |
| Zhao, X. | AN EXPERIMENT INVESTIGATION ON SHOCKINDUCED TURBULENT BOUNDARY LAYER SEPARATION FLOW-FIELD | 2016_0339 |
| Zharckova , V.V. | NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN | 2016_0550 |
| Zheng, W. | ENGINEERING APPLICATION OF GAO-YONG RATIONAL TURBULENCE MODEL TO AN INTER-COOLED DUCT | 2016_0065 |
| Zhi, L. | A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM | 2016_0321 |
| Zhong, Y. | NUMERICAL STUDY OF FIXED TRANSITION LOCATION EFFECT ON SUPERCRITICAL WING AERODYNAMIC CHARACTERISTICS | 2016_0154 |
| Zhong, M. | STUDY OF MODEL DEFORMATION AND STING INTERFERENCE TO THE AERODYNAMIC ESTIMATIONS OF THE CAE-AVM MODEL | 2016_0405 |
| Zhong, Y. | INVESTIGATION ON FLOW SEPARATION EFFECTS ON AIRCRAFT LONGITUDINAL MOMENT CHARACTERISTIC FOR FUSELAGE-MOUNTED AIRCRAFT | 2016_0421 |
| Zhou, Z. | DISTRIBUTED PROPELLERS SLIPSTREAM EFFECTS ON WING AT LOW REYNOLDS NUMBER | 2016_0074 |
| Zhou, Z. | NUMERICAL SIMULATION OF THE PROPELLER/WING INTERACTIONS AT LOW REYNOLDS NUMBER | 2016_0075 |
| Zhou, Z. | MODELING AND CONTROL OF HIGHLY FLEXIBLE FLYING-WING UAV WITH MULTIPLE ELEVONS AND PROPELLERS | 2016_0101 |
| Zhou, W.-J. | NUMERICAL INVESTIGATION OF INLET STARTING CHARACTERISTICS | 2016_0296 |
| Zhu, X.P. | DISTRIBUTED PROPELLERS SLIPSTREAM EFFECTS ON WING AT LOW REYNOLDS NUMBER | 2016_0074 |
| Zhu, X.-P. | NUMERICAL SIMULATION OF THE PROPELLER/WING INTERACTIONS AT LOW REYNOLDS NUMBER | 2016_0075 |
| Zhu, X.P. | MODELING AND CONTROL OF HIGHLY FLEXIBLE FLYING-WING UAV WITH MULTIPLE ELEVONS AND PROPELLERS | 2016_0101 |
| Zhu, Y. | LINEAR MODELING BASED ON INSTRUMENTAL MODEL ESTIMATION AND PID PARAMETERS TUNING IN FREQUENCY-DOMAIN OF AIRCRAFT ENGINE | 2016_0702 |
| Zhuoyi, D. | CONCEPTUAL STUDY OF AN INNOVATIVE HIGH ALTITUDE SOLAR POWERED FLIGHT VEHICLE | 2016_0015 |
| Zill, T. | INTEGRATION OF HYBRID PROPULSION SYSTEM IN A CS23 COMMUTER DESIGN | 2016_0595 |
| Zlobina, Y.P. | IMPROVING THE EFFICIENCY AND RELIABILITY ASSESSMENT TECHNICAL STATE LIQUID SYSTEMS AIRCRAFT DURING ACCEPTANCE TESTS | 2016_0192 |
| Zurawski, R. | MODERN MATERIALS IN AEROSPACE INDUSTRY - MAGNESIUM ALLOY CONTROL SYSTEM LEVER OF THE UNMANNED ILX - 27 HELICOPTER | 2016_0457 |
| Zurek, J. | EVALUATION METHODS OF AIRCRAFT FLIGHT SAFETY | 2016_0661 |
| Zyluk, A. | AN EXPERIMENTAL STUDY OF MICRO-ELECTROMECHANICAL FLYING INSECT FLAPPING WINGS AERODYNAMIC PERFORMANCE | 2016_0025 |