COMPLETE AUTHOR LIST HYPERLINKED TO PAPERS



Abashev, V.M.MODERN RESEARCH AREAS OF SOLID HYPERSONIC RAMJET ENGINES2014_0904
Abbasi, H.NON-INTRUSIVE FLIGHT TEST INSTRUMENTATION TECHNOLOGIES2014_0256
Abdalla, A.KNOWLEDGE-BASED DESIGN FOR FUTURE COMBAT AIRCRAFT CONCEPTS2014_0600
Abdalla, A.CONCEPTUAL AIRCRAFT DESIGN MODEL MANAGEMENT DEMONSTRATED ON A 4TH GENERATION FIGHTER2014_0621
Abdalla, A.M.SELECTION OF AGRICULTURAL AIRCRAFT USING AHP AND TOPSIS METHODS IN FUZZY ENVIRONMENT2014_0875
Abedian, A.AN ANALYTICAL SOLUTION TO THE ELASTIC-PLASTIC BEHAVIOR OF METAL MATRIX COMPOSITES UNDER TENSILE LOADING2014_0678
Abedian, A.FATIGUE DAMAGE DETECTION IN LARGE THIN WALL PLATE BASED ON ULTRASONIC GUIDED WAVE BY USING A PIEZOELECTRIC SENSOR NETWORK2014_0692
Abedian, A.AGING AIRCRAFT COST ANALYSIS USING SYSTEM DYNAMICS MODELING2014_0736
Abramov, N.FLIGHT ENVELOPE EXPANSION VIA ACTIVE CONTROL SOLUTIONS FOR A GENERIC TAILLESS AIRCRAFT2014_0591
Abramovich, H.THE DIRECT PREDICTION OF BUCKLING LOADS OF SHELLS UNDER AXIAL COMPRESSION USING VCT - TOWARDS AN UPGRADED APPROACH2014_0681
Adhy Sasongko, R.A STUDY ON THE EFFECT OF WEAPON INSTALLATION TO AEROELASTIC CHARACTERISTIC OF FIGHTER AIRCRAFT WING2014_0623
Afonin, A.A.ABOUT THE CONCEPT OF STRAPDOWN VECTOR AEROGRAVIMETRIC MEASUREMENTS2014_0995
Aggromito, D.A.USING A BIODYNAMIC MODEL TO INVESTIGATE THE EFFECTS OF BODY-BORNE EQUIPMENT ON FORCES EXPERIENCED IN A SIMULATED HELICOPTER CRASH2014_0318
AHMADI, I.ANALYSIS OF INTER-LAMINAR STRESSES IN COMPOSITE THIN SHELL2014_0579
Ai, J.L.ATTITUDE PROTECTION FOR SIDE STICK-OPERATED AIRCRAFT - THE CLASSIC APPROACH2014_0526
AI, J.L.RESEARCH ON ENEMY AIRCRAFT BANK ANGLE ESTIMATION FOR AUTONOMOUS AIR COMBAT2014_0527
Akhmedzyanov, D.A.NUMERICAL INVESTIGATION OF CHARACTIRISTICS OF DUAL-CIRCUIT NOZZLES WITH CONSIDERING THE EXTERNAL FLOW2014_0548
Aksenov, A.A.NUMERICAL SOLVING PROBLEMS OF SPACECRAFT DESIGN2014_0642
Alderliesten, R.C.APPROXIMATE FUNCTION FOR FATIGUE CRACK PROPAGATION IN A DESIGN OPTIMISATION PROCEDURE FOR FIBRE METAL LAMINATES2014_0635
Aleina, S.C.AUTONOMOUS TAKE-OFF AND LANDING FOR UNMANNED AIRCRAFT SYSTEM: RISK AND SAFETY ANALYSIS2014_0587
Aleksandrovskaya, L.N.METHOD OF REQUIREMENTS CONFIRMATION TO AIRCRAFT AUTOMATIC LANDING SAFETY AT MATHEMATICS SIMULATION STAGE2014_0999
Alekseenkov, A.NEW DEVELOPMENTS OF ELECTRICALLY POWERED ELECTROHYDRAULIC AND ELECTROMECHANICAL ACTUATORS FOR THE MORE ELECTRIC AIRCRAFT2014_0747
Alem, B.FATIGUE DAMAGE DETECTION IN LARGE THIN WALL PLATE BASED ON ULTRASONIC GUIDED WAVE BY USING A PIEZOELECTRIC SENSOR NETWORK2014_0692
Alexandrov, S.VISCOUS HYPERSONIC GAS FLOW CHARACTERISTICS OVER THE DELTA WING WITH BLUNT LEADING EDGES2014_0894
Alexeev, E.B.LOW-COST TITANIUM ALLOYS FOR TITANIUM-POLYMER LAYERED COMPOSITES2014_1044
Alishahi, M.M.NUMERICAL SIMULATION AND PARAMETRIC STUDY OF SUPERSONIC WING FLUTTER2014_0947
Allegri, G.PROGRESS TOWARDS ADAPTIVE AIRCRAFT ENGINE NACELLES2014_0770
Ameduri, S.EXPERIMENTAL VALIDATION OF A SENSORIZED RING BASED ON OPTICAL FIBER FOR STRAIN MONITORING OF MORPHING STRUCTURE2014_0641
Ameduri, S.AN UAV LANDING GEAR SYSTEM ACTUATED THROUGH SMA ACTIVE ELEMENTS2014_0699
Amiryants, G.A.AEROELASTIC ANALYSIS OF THE ADAPTIVE WING WIND TUNNEL DEMONSTRATOR OF THE SADE PROJECT2014_0151
Ananenkov, A.E.MULTI-FUNCTIONAL AERODROME CONTROL RADAR BY USPR TECHNOLOGY2014_0146
Anas Bin Abd Bari, M.KINEMATIC AND UNSTEADY AERODYNAMIC MODELLING OF FLAPPING BI- AND QUAD-WING ORNITHOPTER2014_0433
Anas Bin Abd Bari, M.CONCEPTUAL DESIGN STUDY OF QUAD-BUBBLE-BUSINESS JET2014_0719
Anastasijevic , Z.MEASUREMENT OF THE CROSS-COUPLING DERIVATIVES DUE TO PITCHING IN THE HIGH REYNOLDS NUMBER BLOWDOWN WIND TUNNEL2014_0113
Andreev, G.T.INVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI2014_0107
Andreev, S.THE NUMERICAL ANALYSIS OF IMPACT OF CHANGES IN FLIGHT CONDITIONS AND IN ENGINE'S REGIME AT CRUISE ON AIRPLANE'S AERODYNAMIC CHARACTERISTICS2014_1003
Andreeva-Mori, A.EVALUATION OF SATELLITE IMAGERY INTEGRATION IN OPTIMAL AIRCRAFT OPERATION PLANNING FOR DISASTER RELIEF2014_0438
Andreychenko, I.L.LIFE VALIDATION STRATEGY2014_0974
Anghileri, M.FE-TO-SPH APPROACH APPLIED TO THE ANALYSIS OF SOFT BODY IMPACT: BIRD STRIKE AND HAIL IMPACT2014_0241
Anisimov, K.COMPUTATIONAL METHOD FOR STEADY FLOW (RANS) USING ZONAL APPROACH AND ITS IMPLEMENTATION EXPERIENCE FOR SOLUTION OF TASK OF INTERFERENCE ENGINE AND AIRFRAME2014_0499
Antunes, A.P.CFD BASED OPTIMIZATION OF HIGH-LIFT DEVICES USING A MESH MORPHING TECHNIQUE2014_0085
Anyoji, M.DBD PLASMA ACTUATOR MULTI-OBJECTIVE DESIGN OPTIMIZATION AT REYNOLDS NUMBER 63,000 : STROUHAL NUMBER EFFECT2014_0918
Aoyama, S.DEVELOPMENT OF PASSIVE SURVEILLANCE RADAR2014_0709
Arai, N.CONCEPTUAL DESIGN OF SOLAR UAV FOR LONG ENDURANCE2014_0887
Arbelo, M.A.BUCKLING OF IMPERFECTION SENSITIVE SHELL STRUCTURES: NUMERICAL MODELS TO PREDICT LESS CONSERVATIVE KNOCK-DOWN FACTORS2014_0861
Aribowo, A.CFD-BASED COLLABORATIVE DESIGN OPTIMIZATION USING ECFD2014_0739
Ariola, M.HW VS SW SENSOR REDUNDANCY: FAULT DETECTION AND ISOLATION OBSERVER BASED APPROACHES FOR INERTIAL MEASUREMENT UNITS2014_0455
Arisman, C.J.NUMERICAL INVESTIGATION OF LAMINAR NEAR WAKE SEPARATION ON CIRCULAR CYLINDERS AT SUPERSONIC VELOCITIES2014_0597
Arnaldo, R.OPTIMISED ALGORITHMS FOR EXTENDED ARRIVAL MANAGERS2014_0229
Arnaldo, R.M.A COMPARISON OF THE TWO ARRIVAL TRAFFIC SYNCHRONIZATION CONCEPTS ENVISIONED FOR NEXTGEN AND SESAR.2014_0556
Arnaldo Valdés, R.M.EUROPEAN AIR NAVIGATION SERVICE PROVIDERS’ EFFICIENCY EVALUATION THROUGH DATA ENVELOPMENT ANALYSIS (DEA)2014_0154
Artemiev, A.X-RAY COMPUTER TOMOGRAPHY INVESTIGATION FOR POLYMER COMPOSITE MATERIAL UNDER THE STATIC LOAD2014_0174
Asai, K.NUMERICAL STUDY OF WIND-TUNNEL ACOUSTIC RESONANCE INDUCED BY TWO-DIMENSIONAL AIRFOIL FLOW AT LOW REYNOLDS NUMBER2014_0195
Asai, M.RANS MODELING FOR FLOWS ON RIBLETS BASED ON EXPERIMENTAL DATA2014_0440
Ashcroft, G.GEOMETRIC VARIABILITY AND ITS INFLUENCE ON STEADY AND UNSTEADY FAN AERODYNAMIC PERFORMANCE2014_0105
Aso, S.REDUCTION OF AERODYNAMIC HEATING AND DRAG WITH OPPOSING JET THROUGH EXTENDED NOZZLE IN HIGH ENTHALPY FLOW2014_0479
Aso, S.AERODYNAMIC NOISE REDUCTION FOR HIGH LIFT DEVICES USING MORPHING FLAP CONCEPT2014_0732
Atinault, O.QUASI-ANALYTICAL AERODYNAMIC METHODS FOR PROPULSIVE FUSELAGE CONCEPTS2014_0518
Atkin, C.J. INCOMPRESSIBLE TURBULENT FLOW AT THE LEADING EDGE OF SWEPT WINGS2014_0872
Atkin, C.J.CONVERGENCE OF CALCULATED TRANSITION LOCI DURING COMPUTATIONAL ANALYSIS OF TRANSONIC AEROFOILS AND INFINITE SWEPT WINGS2014_0970
Atobe, T.OBLIQUE MODE ENHANCEMENT BY LONGITUDINAL WALL OSCILLATION IN 2D CHANNEL FLOW2014_0184
Atobe, T.NUMERICAL STUDY OF WIND-TUNNEL ACOUSTIC RESONANCE INDUCED BY TWO-DIMENSIONAL AIRFOIL FLOW AT LOW REYNOLDS NUMBER2014_0195
Aubry, S.EVALUATION OF OPERATIONS ON AN AIRPORT WITH A CIRCULAR RUNWAY2014_0450
Avelar, A.C.INVESTIGATION OF THE FLOW PATTERNS ON A SOUNDING ROCKET FORE-BODY SECTION2014_0727
Averkov, I.S.TRANSPORT AIRCRAFT WITH HIGH FUEL EFFICIENCY WITH \"ELECTROCHEMICAL\" GAS TURBINE ENGINE BASED ON SOFC2014_0217
Averkov, I.S.FUNDAMENTALS OF THE THEORY OF AVIATION \\\"ELECTROCHEMICAL\\\" GAS TURBINE ENGINES WITH SOLID OXIDE FUEL CELLS2014_0219
Avrashkov, V.DESIGN OF SUPERSONIC EJECTION SYSTEM FOR HIGH SPEED COMBUSTION INVESTIGATION AND RESULTS OF WIDE RANGE COMBUSTION CHAMBER TESTS2014_0160
Azarov, Y.A.FLUTTER CALCULATIONS AND TRANSONIC WIND TUNNEL TESTING OF DYNAMICALLY SCALED MODEL OF THE HIGH-ASPECT-RATIO WING2014_0325
Azevedo, J.L.F.CFD BASED OPTIMIZATION OF HIGH-LIFT DEVICES USING A MESH MORPHING TECHNIQUE2014_0085
Azevedo, J.L.F.LARGE EDDY SIMULATIONS OF TURBULENT FLOWS WITH ADVERSE PRESSURE GRADIENTS2014_0108
Azevedo, J.H.A.CFD – BASED STUDY ON GOLDSCHMIED PROPULSION CONCEPT APPLICATION FOR DRAG REDUCTION2014_0964
Azmetov, K.PROBLEM OF LOW CYCLE FATIGUE OF TURBOMACHINES2014_0782
Ba, Y.-L.SEPARATED LAMINAR SHEAR LAYER TRANSITION OVER A TWO-DIMENSIONAL BUMP2014_0610
Baalbergen, E.H.CFD-BASED COLLABORATIVE DESIGN OPTIMIZATION USING ECFD2014_0739
Bach, T.STEPS TO FEASIBILITY FOR LAMINAR WING DESIGN IN A MULTIDISCIPLINARY ENVIRONMENT2014_0955
Bagassi, S.AIRCRAFT PRELIMINARY DESIGN: GENETIC ALGORITHM BASED OPTIMIZATION METHOD2014_1009
Bagerman, A.Z.PLANNING OF AN EXPENDITURE OF THE RESOURSE OF GAS TURBINE ENGINE IN OPERATION2014_0179
Baier, H.POSTBUCKLING ANALYSIS AND OPTIMIZATION OF STIFFENED FUSELAGE PANELS UTILIZING VARIABLE-STIFFNESS LAMINATES2014_0435
Baier, H.PROGRESS TOWARDS ADAPTIVE AIRCRAFT ENGINE NACELLES2014_0770
Bakar, A.MULTIDISCIPLINARY OPTIMIZATION OF TRUSS-BRACED WING LAYOUT2014_0879
Bakulin, V.N.PROTECTION PROBLEM FOR THIN-WALLED COMPOSITE CONSTRUCTIONS OF AIRCRAFT FROM ACTION OF RADIATIONS AND PARTICLES FLUXES2014_1034
Balakirev, A.EXPERIMENTAL EVALUATION OF THE EFFICIENCY OF GAS TURBINE ENGINE PARTS DAMPING WITH DRY FRICTION DAMPERS USING LASER VIBROMETER2014_0866
Balland, S.DESIGN OF SUPERSONIC EJECTION SYSTEM FOR HIGH SPEED COMBUSTION INVESTIGATION AND RESULTS OF WIDE RANGE COMBUSTION CHAMBER TESTS2014_0160
Bancalero Santolaya, R.LOADS MODEL FLIGHT TEST VALIDATION BY MEANS OF INNOVATIVE, PHOTOGRAMMETRY BASED, DEFORMATION MEASUREMENT TECHNIQUE.2014_0102
Banerji, N.CHARACTERISING INTERNAL HEAT TRANSFER IN THERMAL PROTECTION SYSTEMS2014_0794
Barakos, G.SIMULATION OF FLOW AROUND FUSELAGE OF HELICOPTER USING ACTUATOR DISC THEORY2014_0622
Barakos, G.N.CFD MODELING OF 2D AEROFOIL DYNAMIC STALL2014_0774
Barakos, G.N.CFD FOR ROTORCRAFT – RECENT PROGRESS AND NEW CHALLENGES WITH THE GOAHEAD CASE2014_1031
Barbieri, B.EXPERIMENTAL INVESTIGATION OF ENDWALL FLOW FIELD, HEAT TRANSFER IN A LINEAR TURBINE BLADE CASCADE WITH CONTOURED ENDWALL2014_0756
Barbosa, I.C.J.DESIGN OF A LAMINATED COMPOSITE MULTI-CELL STRUCTURE SUBJECTED TO TORSION2014_0905
Barragán, R.EUROPEAN AIR NAVIGATION SERVICE PROVIDERS’ EFFICIENCY EVALUATION THROUGH DATA ENVELOPMENT ANALYSIS (DEA)2014_0154
Barragan, R.OPTIMISED ALGORITHMS FOR EXTENDED ARRIVAL MANAGERS2014_0229
Barragan, R.A COMPARISON OF THE TWO ARRIVAL TRAFFIC SYNCHRONIZATION CONCEPTS ENVISIONED FOR NEXTGEN AND SESAR.2014_0556
Basso, E.INVESTIGATION OF THE FLOW PATTERNS ON A SOUNDING ROCKET FORE-BODY SECTION2014_0727
Bassolillo, S.A MULTI-OBJECTIVE GENETIC ALGORITHM FOR A MAXIMUM COVERAGE FLIGHT TRAJECTORY OPTIMIZATION IN A CONSTRAINED ENVIRONMENT2014_0574
Batrakov, A.S.SIMULATION OF FLOW AROUND FUSELAGE OF HELICOPTER USING ACTUATOR DISC THEORY2014_0622
Battley, M.MULTI-TERRAIN IMPACT SIMULATIONS OF A CRASHWORTHY COMPOSITE HELICOPTER SUBFLOOR2014_0492
Batura, S.ANALYSIS OF THE PREDICTION ABILITY OF REACTION MECHANISMS FOR CFD MODELING OF THE COMBUSTION IN HIGH VELOCITY ENGINES2014_0209
Bayandor, J.A RAPID ANALYSIS METHODOLOGY FOR EARTH ENTRY VEHICLE DEVELOPMENT2014_0976
Baykov, A.V.TRANSPORT AIRCRAFT WITH HIGH FUEL EFFICIENCY WITH \"ELECTROCHEMICAL\" GAS TURBINE ENGINE BASED ON SOFC2014_0217
Baykov, A.V.FUNDAMENTALS OF THE THEORY OF AVIATION \\\"ELECTROCHEMICAL\\\" GAS TURBINE ENGINES WITH SOLID OXIDE FUEL CELLS2014_0219
Bazhenov, S.G.SIMULATION OF ON-BOARD MODEL OF AIRLINER TO EVALUATE CAPABILITY OF TRAJECTORIES AND FLIGHT SAFETY2014_0815
Bazhenov, S.G.ABOUT AIRCRAFT STABILITY DURING WING-IN-GROUND EFFECT FLIGHT2014_0959
Beaumier, P.A LOW ORDER METHOD FOR CO-AXIAL PROPELLER AND ROTOR PERFORMANCE PREDICTION2014_0448
Begnini, G.R.COMPARATIVE STUDY OF SYSTEM IDENTIFICATION METHODS APPLIED TO AEROELASTIC MODELS TESTED IN WIND TUNNEL2014_0711
Behroozifar, S.DADF ( DIGITAL AUTOMATIC DIRECTION FINDER )2014_0100
Belo, E.M.AN APPLICATION OF DIGITAL IMAGE PROCESSING FOR UAV’S AUTOMATIC LANDING SYSTEM AID2014_0915
Ben, C.NAVIGATION FOR VERTICAL PRECISION LANDING BASED ON OPTICAL TRACKING OF A SPATIAL RETROREFLECTIVE MARKER ARRAY2014_0850
Ben-Asher, J. Z.CRUISE FLIGHT THROTTLE OPTIMIZATION BY APPROXIMATE DYNAMIC PROGRAMMING2014_0134
Benderskiy, L.A.INVESTIGATION OF FLOW PARAMETERS AND NOISE OF SUBSONIC AND SUPERSONIC JETS USING RANS/ILES HIGH RESOLUTION METHOD2014_0373
Benderskiy, L.A.EFFECT OF TEMPERATURE ON FLOW CHARACTERISTICS IN SUPERSONIC IMPINGING JET USING RANS/ILES HIGH RESOLUTION METHOD2014_0375
Bendictus, R.APPROXIMATE FUNCTION FOR FATIGUE CRACK PROPAGATION IN A DESIGN OPTIMISATION PROCEDURE FOR FIBRE METAL LAMINATES2014_0635
Benitez-Montañes, L.SPINNER SHED ICE ENGINE INGESTION ASSESSMENT METHODOLOGY2014_0066
Berendorf, Y.A.EXPERIMENTAL INVESTIGATION OF ROTOR DYNAMICS IN AIRCRAFT ENGINE WITH TWO-AXIS STIFFNESS ANISOTROPY OF SUPPORTS2014_0676
Berizzi, F.POLARIMETRIC AVIONIC WEATHER RADAR FOR INCREASING FLIGHT SAFETY AND EFFICIENCY2014_0343
Berling, J.THE NETWORK FLOW ENVIRONMENT: SLOT ALLOCATION MODEL EVALUATION WITH CONVECTIVE NOWCASTING2014_0761
Berlowitz, I.PASSENGER AIRPLANE CONVERSION TO FREIGHTER2014_0001
Berseneva, N.V.THE NUMERICAL ANALYSIS OF IMPACT OF CHANGES IN FLIGHT CONDITIONS AND IN ENGINE'S REGIME AT CRUISE ON AIRPLANE'S AERODYNAMIC CHARACTERISTICS2014_1003
Bettini, P.EXPERIMENTAL VALIDATION OF A SENSORIZED RING BASED ON OPTICAL FIBER FOR STRAIN MONITORING OF MORPHING STRUCTURE2014_0641
Bezgin, L.ANALYSIS OF THE PREDICTION ABILITY OF REACTION MECHANISMS FOR CFD MODELING OF THE COMBUSTION IN HIGH VELOCITY ENGINES2014_0209
Bezgin, L.MECHANISMS OF POLLUTANT FORMATION IN THE H2 - FUELLED COMBUSTOR OF HIGH VELOCITY AIR-BREATHING ENGINE: MODELING STUDY2014_0236
Bhaskar, R.USING WAVES TO SIMULATE DISTORTION IN INTERNAL FLOWS IN AN AXIAL FLOW FAN2014_0609
Bifeng, S.AN EXPERIMENTAL STUDY ON THE INFLUENCE OF PASSIVE DEFORMATION TO LIFT AND THRUST GENERATION IN FLEXIBLE FLAPPING WING2014_0618
Bijewitz, J.QUASI-ANALYTICAL AERODYNAMIC METHODS FOR PROPULSIVE FUSELAGE CONCEPTS2014_0518
Bijewitz, J.PROGRESS TOWARDS ADAPTIVE AIRCRAFT ENGINE NACELLES2014_0770
Bijewitz, J.RECENT ADVANCES IN AIRFRAME-PROPULSION CONCEPTS WITH DISTRIBUTED PROPULSION2014_0853
Bil, C.AEROSPACE ENGINEERING: INVESTIGATING STUDENT PERCEPTIONS AND INDUSTRY REALITIES2014_0071
Bil, C.FLUID DYNAMICS ANALYSIS OF A COUNTER ROTATING DUCTED PROPELLER2014_0072
Bil, C.THE INFLUENCE OF SHM TECHNIQUES ON SCHEDULED MAINTENANCE OF AIRCRAFT COMPOSITE STRUCTURES2014_0550
Billac, T.MULTI-TERRAIN IMPACT SIMULATIONS OF A CRASHWORTHY COMPOSITE HELICOPTER SUBFLOOR2014_0492
Birukov, V.I.INVESTIGATION OF UNSTEADY FLOW ON A HIGH ASPECT RATIO WING2014_0124
Biryukov, V.V.UPSET RECOVERING SIMULATION TO ENHANCE FLIGHT SAFETY BY ON-GROUND PILOT TRAINING2014_0745
Bittner, M.A NON-COOPERATIVE BI-LEVEL OPTIMAL CONTROL PROBLEM FORMULATION FOR NOISE MINIMAL DEPARTURE TRAJECTORIES2014_0356
Bittner, M.GENERATION OF INITIAL GUESSES FOR OPTIMAL CONTROL PROBLEMS WITH MIXED INTEGER DEPENDENT CONSTRAINTS2014_0495
Blanvillain, E.A HOLISTIC APPROACH TO HYPERSONIC AIRCRAFT DESIGN: ZEHST (ZERO EMISSION HIGH SPEED TECHNOLOGIES)2014_0203
Blasi, L.A MULTI-OBJECTIVE GENETIC ALGORITHM FOR A MAXIMUM COVERAGE FLIGHT TRAJECTORY OPTIMIZATION IN A CONSTRAINED ENVIRONMENT2014_0574
Blinnik, B.S.DYNAMIC LOADS ACTING ON ENGINE FRAME ELEMENTS AFTER FAN BLADE OUT EVENT STUDY2014_0255
Bobarykina, T.INVESTIGATION OF THE OPTICAL PULSING DISCHARGE IN THE SUPERSONIC AIR FLOW2014_1012
Bogatyrev, V.V.INVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI2014_0107
Bogatyrev, M.STRUCTURAL NONLINEARITIES SIMULATION ON THE FLUTTER ELECTROMECHANICAL MODELING TEST BENCH2014_0324
Bogdanski, K.DESIGN AND OPTIMIZATION OF LOW SPEED DUCTED FAN FOR A NEW GENERATION OF JOINED WING AIRCRAFT2014_0663
Bolotov, B.EXPERIMENTAL EVALUATION OF THE EFFICIENCY OF GAS TURBINE ENGINE PARTS DAMPING WITH DRY FRICTION DAMPERS USING LASER VIBROMETER2014_0866
Bolsunovsky, A.L.NOVEL CONFIGURATION OF A BUSINESS JET WITH A DROP-SHAPED FUSELAGE2014_0387
Bolsunovsky, A.L.ARRANGEMENT AND AERODYNAMIC STUDIES FOR LONG-RANGE AIRCRAFT IN “FLYING WING” LAYOUT2014_0388
Bolsunovsky, A.L.AERODYNAMIC STUDIES ON LOW-NOISE AIRCRAFT WITH UPPER ENGINE INSTALLATION2014_0389
Bolsunovsky, A.L.INVESTIGATION OF ADAPTIVE WING BENEFITS FOR TRANSPORT AIRCRAFT2014_0390
Bommanahal, M.FLIGHT ENVELOPE EXPANSION VIA ACTIVE CONTROL SOLUTIONS FOR A GENERIC TAILLESS AIRCRAFT2014_0591
Bondarenko, A.A.TRAINING TECHNIQUE TO EXERCISE AT SIMULATOR THE DIFFICULT FLIGHT STAGES2014_0122
Bondarenko, D.A.AIR EVOLUTION IN FUEL FLOW UNDER DECREASED PRESSURE CONDITIONS: EXPERIMENTAL STUDIES AND ENGINEERING CODE DEVELOPMENT2014_0254
Borisov, I.V.COMPUTING SIMULATION FOR FIRE-FIGHTING HELICOPTER OPERATION ANALYSIS2014_0841
Borovskaya, Y.S.DEFINITION OF THE BOLT SHEARING LOAD IN MULTIPLE-ROWMETAL COMPOSITE JOINTS2014_0225
Bosnyakov, S.NUMERICAL SIMULATION OF UNSTEADY FLOWS AROUND HIGH-LIFT CONFIGURATIONS2014_0321
Botha,, J.D.M.OPTIMISATION OF A NOVEL TRAILING EDGE CONCEPT FOR A HIGH LIFT DEVICE2014_0420
Boucheze, M.DESIGN OF SUPERSONIC EJECTION SYSTEM FOR HIGH SPEED COMBUSTION INVESTIGATION AND RESULTS OF WIDE RANGE COMBUSTION CHAMBER TESTS2014_0160
Bountin, D.LAMINAR FLOW CONTROL OF A HIGH-SPEED BOUNDARY LAYER BY LOCALIZED WALL HEATING OR COOLING2014_0289
Bragin, N.N.HIGH-LIFT SYSTEM DESIGN BY NUMERICAL METHODS AND WIND TUNNEL VERIFICATION2014_0094
Bragin, N.N.INVESTIGATION OF UNSTEADY FLOW ON A HIGH ASPECT RATIO WING2014_0124
Bragin, N.N.AERODYNAMIC STUDIES ON LOW-NOISE AIRCRAFT WITH UPPER ENGINE INSTALLATION2014_0389
Brailko, I.ASSESSMENT OF AERODYNAMIC AND ACOUSTIC CHARACTERISTICS OF COUNTER-ROTATING OPEN ROTORS2014_0825
Brandão, M.P.DEVELOPMENT OF A MULTI-PURPOSE UAV WITH BIO-INSPIRED FEATURES2014_0586
Brandão, M.P.AERODYNAMICS VIA AEROACOUSTICS – THE CASE FOR CIRCULATION CAPTURE2014_0689
Brazhko, V.N.HYPERSONIC FLOWFIELD AND HEAT FLUX PECULIARITIES ON THE NEW SPACE LAUNCHER WITH WINGED REUSABLE FIRST STAGE.2014_0898
Breitsamter, C.EXPERIMENTAL INVESTIGATIONS ON VORTEX FLOW PHENOMENA OF A DIAMOND WING CONFIGURATION2014_0024
Breitsamter, C.AERODYNAMIC DESIGN OPTIMISATION FOR A HELICOPTER CONFIGURATION INCLUDING A ROTATING ROTOR HEAD2014_0686
Bridel, G.FROM ST. PETERSBURG TO ZURICH: AERONAUTICAL AND SCIENTIFIC MILESTONES FROM SWISS PERSPECTIVES AROUND THE NAMES BERNOULLI2014_1042
Brion, V.AN OVERVIEW OF RECENT EXPERIMENTAL STUDIES CONDUCTED IN ONERA S3CH TRANSONIC WIND TUNNEL2014_0519
Bronsvoort, J.TRAJECTORY PREDICTION PERFORMANCE COMPARISON TOWARDS EFFICIENT TIME-BASED METERING OPERATIONS2014_0876
Broughton, B.A.OPTIMAL CONTROL SURFACE MIXING OF A RHOMBOID WING UAV2014_0840
Brown, M.ANALYSIS OF AIR TRAFFIC EFFICIENCY USING DYNAMIC PROGRAMMING TRAJECTORY OPTIMIZATION2014_0743
Bruna, O.PATH PLANNING FOR ULTRALIGHTS UNDER EMERGENCY CONDITIONS2014_0882
Bruna, O.EMERGENCY LANDING SITE LOCATION USING AERIAL IMAGE SEGMENTATION2014_0885
Brutyan, M.A.APPLICATION OF LIGHT SCATTERING EFFECT IN AERODYNAMIC EXPERIMENT2014_0399
Budde, R.THE NETWORK FLOW ENVIRONMENT: SLOT ALLOCATION MODEL EVALUATION WITH CONVECTIVE NOWCASTING2014_0761
Budinger, M.MISSION PROFILES ANALYSIS: GUIDELINES TO AIRCRAFT ACTUATORS NEW TECHNOLOGY SPECIFICATION2014_0194
Bukharov, K.D.REALIZATION OF A CONTINUOUS BALANCE TESTING PROCEDURE IN A COMPRESSOR-DRIVEN TRANSONIC WIND TUNNEL2014_0354
Bukharov, S.THERMOPLASTIC COMPOSITE AIRCRAFT STRUCTURE REPAIR METHODOLOGY2014_0631
Bukov, V.A DEMONSTRATOR FOR AVIONICS OF ZERO MAITENANCE EQUIPMENT2014_0557
Bukov, V.INTEGRATED ONBOARD NETWORKING FOR IMA2G2014_0899
Bulbovich, R.V.THE PROCEDURE OF LINER IMPEDANCE EDUCTION BY FINITE ELEMENT METHOD2014_0402
Bur, R.AN OVERVIEW OF RECENT EXPERIMENTAL STUDIES CONDUCTED IN ONERA S3CH TRANSONIC WIND TUNNEL2014_0519
Burger, R.PRESENTATION OF HORIZON 2020 PROGRAMME2014_1038
Buryak, Y.SECURING THE SUPPLY CHAIN OF INDUSTRIAL PRODUCTS ON THE BASIS OF THE USE OF MODERN INFORMATION TECHNOLOGIES2014_0411
Bushgens, A.G.UPSET RECOVERING SIMULATION TO ENHANCE FLIGHT SAFETY BY ON-GROUND PILOT TRAINING2014_0745
Buzoverya, N.P.NOVEL CONFIGURATION OF A BUSINESS JET WITH A DROP-SHAPED FUSELAGE2014_0387
Buzoverya, N.P.ARRANGEMENT AND AERODYNAMIC STUDIES FOR LONG-RANGE AIRCRAFT IN “FLYING WING” LAYOUT2014_0388
Buzoverya, N.P.AERODYNAMIC STUDIES ON LOW-NOISE AIRCRAFT WITH UPPER ENGINE INSTALLATION2014_0389
Buzoverya, N.P.INVESTIGATION OF ADAPTIVE WING BENEFITS FOR TRANSPORT AIRCRAFT2014_0390
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Chernyshev, S.L.THEORETICAL MODELING OF THE ELECTROGASDYNAMIC METHOD OF LAMINAR FLOW CONTROL ON A SWEPT WING2014_0303
Chernyshev, I.L.NOVEL CONFIGURATION OF A BUSINESS JET WITH A DROP-SHAPED FUSELAGE2014_0387
Chernyshev, I.L.ARRANGEMENT AND AERODYNAMIC STUDIES FOR LONG-RANGE AIRCRAFT IN “FLYING WING” LAYOUT2014_0388
Chernyshev, I.L.AERODYNAMIC STUDIES ON LOW-NOISE AIRCRAFT WITH UPPER ENGINE INSTALLATION2014_0389
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Cho, H.COMPUTATIONAL ANALYSIS FOR FLAPPING WING BY COUPLED CFD AND CSD SOLUTIONS2014_0260
Cho, H.HUMAN FACTORS STUDIES OF AN ADS-B BASED TRAFFIC ALERTING SYSTEM FOR GENERAL AVIATION2014_0419
Cho, L.S.INVESTIGATION OF THE TIP CLEARANCE EFFECT IN A COUNTER-ROTATING DUCTED FAN FOR VTOL UAV2014_0483
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Cho, Y.H.DYNAMIC CHARACTERISTICS OF THE THRUST VECTORING CONTROL BY HIGHLY COMPRESSIBLE COANDA EFFECTS2014_0857
Choi, K.-S.A NOVEL CONCEPTIONS OF PLASMA GURNEY FLAP2014_0341
Choi, H.-L.SUM-OF-SQUARES BASED STABILITY ANALYSIS FOR SKID-TO-TURN MISSILES WITH THREE-LOOP AUTOPILOT2014_0787
Choi, H.AERODYNAMIC ANALYSIS OF THE BWB BUSINESS JET USING DSTRIDUTED PROPULSION SYSTEM2014_0823
Choi, H.A.NUMERICAL INVESTIGATION ON THE CORRELATION BETWEEN SHOCK STRUCTURE AND THRUST PERFORMANCE IN AN OVEREXPANDED NOZZLE2014_0948
Chuvakhov, P.V.INVESTIGATION OF HEAT FLUX AND EFFUSION/FILM COOLING EFFICIENCY OVER A SHARP CONE SURFACE AT HIGH SUPERSONIC SPEEDS2014_0355
Chuyanov, G.A.ADVANCED AVIONICS EQUIPMENT ON THE BASIS OF SECOND GENERATION INTEGRATED MODULAR AVIONICS2014_0148
Ciampa, P.D.OPTIMIZATION OF REVENUE SPACE OF A BLENDED WING BODY2014_0740
Cid-Arroyo, S.SPINNER SHED ICE ENGINE INGESTION ASSESSMENT METHODOLOGY2014_0066
Ciliberti , D.DEVELOPMENT OF NEW PRELIMINARY DESIGN METHODOLOGIES FOR REGIONAL TURBOPROP AIRCRAFT BY CFD ANALYSES2014_0407
Ciminello, M.EXPERIMENTAL VALIDATION OF A SENSORIZED RING BASED ON OPTICAL FIBER FOR STRAIN MONITORING OF MORPHING STRUCTURE2014_0641
Ciminello, M.AN UAV LANDING GEAR SYSTEM ACTUATED THROUGH SMA ACTIVE ELEMENTS2014_0699
Claverías, S.WAKE VORTEX ENCOUNTER LOADS. FLIGHT TESTS AND NUMERICAL SIMULATIONS2014_0881
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Combrinck, M.L.EULERIAN DERIVATIONS OF NON-INERTIAL NAVIER-STOKES EQUATIONS2014_0577
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Corcione, S.COMMUTER AIRCRAFT AERODYNAMIC DESIGN: WIND-TUNNEL TESTS AND CFD ANALYSIS2014_0176
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Crespo, J.OPTIMISED ALGORITHMS FOR EXTENDED ARRIVAL MANAGERS2014_0229
Crespo, J.A COMPARISON OF THE TWO ARRIVAL TRAFFIC SYNCHRONIZATION CONCEPTS ENVISIONED FOR NEXTGEN AND SESAR.2014_0556
Cristofaro, M.TOWARDS COMPUTATIONAL FLIGHT DYNAMICS OF A PASSENGER JET AIRCRAFT2014_0462
Cristofaro, M.INVESTIGATING THE PIAGGIO AVANTI DESIGN USING CEASIOM2014_0464
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Cuerno, C.A COMPARISON OF THE TWO ARRIVAL TRAFFIC SYNCHRONIZATION CONCEPTS ENVISIONED FOR NEXTGEN AND SESAR.2014_0556
Cui, D.-G.AEROELASTIC OPTIMIZATION OF COMPOSITE WING BASED ON IMPROVED ADAPTIVE GENETIC ALGORITHM2014_0141
Cui, D.-G.AN ENGINEERING ANALYSIS METHOD OF POST-BUCKLING FOR COMPOSITE STIFFENED PANELS2014_0142
Cui, D.-G.OPTIMIZATION DESIGN OF COMPOSITE WING WITH MULTIPLE LOAD CASES AND LARGE SCALE DESIGN VARIABLES2014_0484
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Cuneo, G.EXPERIMENTAL VALIDATION OF A SENSORIZED RING BASED ON OPTICAL FIBER FOR STRAIN MONITORING OF MORPHING STRUCTURE2014_0641
Cunha, F.S.ON THE INTERAL STRUCTURAL OF SHOCK WAVE IN RELAXING GAS2014_0987
Curcic, D.LIVING WITH SUPERSONIC STARTING LOADS IN THE T-38 TRISONIC WIND TUNNEL OF VTI2014_0138
Cusati, V.DEVELOPMENT OF NEW PRELIMINARY DESIGN METHODOLOGIES FOR REGIONAL TURBOPROP AIRCRAFT BY CFD ANALYSES2014_0407
Czekalowski, P.APPLICATION OF ARTIFICIAL NEURAL NETWORK IN MODELING OF ENTOMOPTER DYNAMICS2014_0659
D'Amato, E.HW VS SW SENSOR REDUNDANCY: FAULT DETECTION AND ISOLATION OBSERVER BASED APPROACHES FOR INERTIAL MEASUREMENT UNITS2014_0455
D'Amato, E.A MULTI-OBJECTIVE GENETIC ALGORITHM FOR A MAXIMUM COVERAGE FLIGHT TRAJECTORY OPTIMIZATION IN A CONSTRAINED ENVIRONMENT2014_0574
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Da Ronch, A.TOWARDS COMPUTATIONAL FLIGHT DYNAMICS OF A PASSENGER JET AIRCRAFT2014_0462
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da Silva, R.G.A.COMPARATIVE STUDY OF SYSTEM IDENTIFICATION METHODS APPLIED TO AEROELASTIC MODELS TESTED IN WIND TUNNEL2014_0711
Dadashi, J.IDENTIFICATION AND TRACKING CONTROL OF FLAPPING MOTIONS IN ROBOTIC BATS2014_1011
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Dala, L.N.EULERIAN DERIVATIONS OF NON-INERTIAL NAVIER-STOKES EQUATIONS2014_0577
Dalmau, R.REAL-TIME AIRCRAFT CONTINUOUS DESCENT TRAJECTORY OPTIMIZATION WITH ATC TIME CONSTRAINTS USING DIRECT COLLOCATION METHODS2014_0306
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Danilin, A.I.OPTIMALITY CRITERIA FOR STRUCTURAL DESIGN OF AIRFRAMES WITH DYNAMIC REQUIREMENTS2014_0053
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Dastoom Laatleyli, H.NONLINEAR STABILITY ANALYSIS OF CARBON NANOTUBES BASED ON TIMOSHENKO BEAM THEORY AND MODIFIED COUPLE STRESS THEORY2014_0655
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de Gelder, N.REAL-TIME AIRCRAFT CONTINUOUS DESCENT TRAJECTORY OPTIMIZATION WITH ATC TIME CONSTRAINTS USING DIRECT COLLOCATION METHODS2014_0306
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de Oliveira, L.C.AEROELASTIC BEHAVIOR OF COMPOSITE WINGS IN POSTBUCKLING REGIME2014_0789
Dedesh, V.T.ECOLOGICAL OPTIMIZATION OF JET AIRCRAFT FLIGHTS IN VIEW OF CONTRAILS AND CONTRAIL CIRRUS FORMATION2014_0400
Defoort, S.LAPCAT-II: DESIGN OF A COMBINED PROPULSION SYSTEM FOR A HYPERSONIC CRUISER2014_0886
Degenhardt, R.AEROELASTIC BEHAVIOR OF COMPOSITE WINGS IN POSTBUCKLING REGIME2014_0789
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Deivasigamani, APROXIMITY EFFECTS OF PIEZOELECTRIC ENERGY HARVESTERS IN FLUID FLOW2014_0992
Della Vecchia, P.COMMUTER AIRCRAFT AERODYNAMIC DESIGN: WIND-TUNNEL TESTS AND CFD ANALYSIS2014_0176
Della Vecchia, P.DEVELOPMENT OF NEW PRELIMINARY DESIGN METHODOLOGIES FOR REGIONAL TURBOPROP AIRCRAFT BY CFD ANALYSES2014_0407
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Denti, E.DYNAMIC NOTCH FILTERING CONTROL FOR FAULT-TOLERANT ACTUATORS OF FLY-BY-WIRE HELICOPTERS2014_0669
Denti, E.SIMULATION OF AN ALL-ELECTRIC FLIGHT CONTROL SYSTEM FOR THE EVALUATION OF POWER CONSUMPTION2014_0897
Desyatnik, P.A.UPSET RECOVERING SIMULATION TO ENHANCE FLIGHT SAFETY BY ON-GROUND PILOT TRAINING2014_0745
Di Francesco, G.TRANSITION CONTROL AND REDUNDANCY MANAGEMENT FOR A TILT ROTOR UAV USING GENETIC ALGORITHMS2014_0285
Di Meo, G.A.AUTONOMOUS TAKE-OFF AND LANDING FOR UNMANNED AIRCRAFT SYSTEM: RISK AND SAFETY ANALYSIS2014_0587
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Didenko, Y.I.PRINCIPLES OF THE AUTOMATED CONTROL FOR THE CIVIL AIRCRAFT, WHICH PROVIDE FLIGHT SAFETY2014_0121
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Djojodihardjo, H.CONCEPTUAL DESIGN STUDY OF QUAD-BUBBLE-BUSINESS JET2014_0719
Djuknic, G.IMPROVEMENT OF THE AIRCRAFT GENERAL OVERHAUL PROCEDURE2014_0543
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Dong, W.NUMERICAL STUDY OF ICE ACCRETION ON ROTATING AERO-ENGINE CONE2014_0035
Dong, Y.Q.ATTITUDE PROTECTION FOR SIDE STICK-OPERATED AIRCRAFT - THE CLASSIC APPROACH2014_0526
Dong, Y.Q.RESEARCH ON ENEMY AIRCRAFT BANK ANGLE ESTIMATION FOR AUTONOMOUS AIR COMBAT2014_0527
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Drobysh, M.DEVELOPMENT OF KEY TECHNOLOGIES FOR MICRO REGENERATIVE GAS TURBINES2014_1007
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Dubinina, M.M.INFLUENCE NUMERICAL SCHEMES TO ESTIMATE ERROR OF AIR PRESSURE PROBE2014_0687
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Dudarkov, Y.I.SOME LAMINATE DEFORMATIONS FEATURES2014_0226
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Galinski, C.PREDICTED FLIGHT CHARACTERISTICS OF THE INVERTED JOINED WING SCALED DEMONSTRATOR2014_0552
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Gao, Z.AN EVALUATING MODEL FOR CONTROL EFFECTOR SUPERIORITY BASED ON PERFORMANCE REQUIREMENTS2014_0421
Gao, X.Z.THE VERY FLEXIBLE AIRCRAFTS AND ALBATROSS FLIGHT2014_0755
Gao, Z.H.EFFICIENT AERO-STRUCTURAL DESIGN OPTIMIZATION BASED ON HIGH-FIDELITY METHODS2014_0771
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Goman, M.FLIGHT ENVELOPE EXPANSION VIA ACTIVE CONTROL SOLUTIONS FOR A GENERIC TAILLESS AIRCRAFT2014_0591
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Goraj, Z.-J.A SPECIALIZED UAV FOR SURVEILLANCE IN WINDY, TURBULENT ENVIRONMENT OF THE ANTARCTIC COAST2014_0693
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Gorbushin, A.R.REALIZATION OF A CONTINUOUS BALANCE TESTING PROCEDURE IN A COMPRESSOR-DRIVEN TRANSONIC WIND TUNNEL2014_0354
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Gowree, E.R. INCOMPRESSIBLE TURBULENT FLOW AT THE LEADING EDGE OF SWEPT WINGS2014_0872
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Grigoryev, M.A.MATHEMATICAL MODEL OF AIRCRAFT WAKE VORTICES DEVELOPMENT FOR TAKE-OFF/LANDING PHASES FOR WAKE VORTEX SAFETY SYSTEMS2014_0417
Grigoryev, M.A.REFINEMENT OF THE MODEL OF PILOT PERCEPTION OF AIRCRAFT MOTION IN UPSET CONDITIONS UTILIZING FLIGHT TESTS RESULTS2014_0588
Grishin, V.I.DEFINITION OF THE BOLT SHEARING LOAD IN MULTIPLE-ROWMETAL COMPOSITE JOINTS2014_0225
Grishin, I.WIND TUNNEL INVESTIGATION OF CRITICAL FLIGHT REGIMES USING DYNAMICALLY SCALED ACTIVELY CONTROLLED MODEL IN 3 DOF GIMBAL2014_0415
Grishin, I.I.UPSET RECOVERING SIMULATION TO ENHANCE FLIGHT SAFETY BY ON-GROUND PILOT TRAINING2014_0745
Gromyko, Y.LAMINAR FLOW CONTROL OF A HIGH-SPEED BOUNDARY LAYER BY LOCALIZED WALL HEATING OR COOLING2014_0289
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Guan, W.-L.EVALUATIONS OF FLYING QUALITIES FOR A NEW AND AN AGING TRANSPORT AIRCRAFT IN SEVERE ATMOSPHERIC TURBULENCE2014_0319
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Gubanova, I.A.INVERSE METHODS FOR AERODYNAMIC DESIGN USING THE NAVIER-STOKES EQUATIONS2014_0062
Gubanova, M.A.INVERSE METHODS FOR AERODYNAMIC DESIGN USING THE NAVIER-STOKES EQUATIONS2014_0062
Gubanova, M.A.HIGH-LIFT SYSTEM DESIGN BY NUMERICAL METHODS AND WIND TUNNEL VERIFICATION2014_0094
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Guglieri, G.L1 ADAPTIVE CONTROLLER DESIGN FOR GUST LOAD ALLEVIATION2014_0237
Guigon, A.CONCEPTUAL FEASIBILITY STUDY FOR A FULLY ELECTRICALLY POWERED REGIONAL TRANSPORT AIRCRAFT2014_1021
Guillaume, M.STRUCTURAL INTEGRITY FOR AGING AIRPLANES2014_0414
Gulienko, A.DEMONSTRATION SYSTEMS OF THE “ELECTRIC” GAS TURBINE ENGINE2014_0218
Gulienko, A.ANALYSIS OF POSSIBILITIES TO APPLY ELECTRIC TECHNOLOGIES FOR HELICOPTER PROPULSION SYSTEM2014_0404
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Guo, Z.DESIGN AND PERFORMANCE TEST OF A TWIN-FUSELAGE CONFIGURATION SOLAR-POWERED UAV2014_0408
Gurevich, O.S.IMPROVING CONTROL RELIABILITY AND QUALITY OF AIRCRAFT ENGINES BY MEANS THE SOFTWARE «VIRTUAL ENGINE»2014_0198
Gurevich, O.DEMONSTRATION SYSTEMS OF THE “ELECTRIC” GAS TURBINE ENGINE2014_0218
Gurevich, B.I.ARRANGEMENT AND AERODYNAMIC STUDIES FOR LONG-RANGE AIRCRAFT IN “FLYING WING” LAYOUT2014_0388
Gurevich, O.ANALYSIS OF POSSIBILITIES TO APPLY ELECTRIC TECHNOLOGIES FOR HELICOPTER PROPULSION SYSTEM2014_0404
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Guzairov, M.B.NUMERICAL INVESTIGATION OF CHARACTIRISTICS OF DUAL-CIRCUIT NOZZLES WITH CONSIDERING THE EXTERNAL FLOW2014_0548
Haag, J.DEVELOPMENT OF A HYBRID ICE PROTECTION SYSTEM BASED ON NANOSTRUCTURED HYDROPHOBIC SURFACES2014_0891
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Hajduk, J.INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME2014_0551
Hall, P.TRANSMISSION COEFFICIENT OF TOLLMIEN-SCHLICHTING WAVES UNDERGOING SMALL INDENTATION/HUMP DISTORTION2014_1001
Hall, P.THE EFFECTS OF NONLINEARITY ON CROSSFLOW RECEPTIVITY2014_1002
Halle, M.FLIGHT LOADS ESTIMATION USING LOCAL MODEL NETWORKS2014_0555
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Han, Z.-H.MULTIDISCIPLINARY OPTIMIZATION OF TRUSS-BRACED WING LAYOUT2014_0879
Hanjie, J.RESEARCH ON FLYING-PYLON TECHNOLOGY2014_0301
Hansman, R.J. HUMAN FACTORS STUDIES OF AN ADS-B BASED TRAFFIC ALERTING SYSTEM FOR GENERAL AVIATION2014_0419
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Harasani, W.CONCEPTUAL DESIGN OF SOLAR UAV FOR LONG ENDURANCE2014_0887
Hardier, G.A COMPARISON OF TECHNIQUES TO GET SPARSE RATIONAL APPROXIMATIONS FOR LINEAR FRACTIONAL REPRESENTATIONS2014_0664
Harkov, V.P.ENERGY APPROACH FOR AIRCRAFT VELOCITY OPTIMAL CONTROL DESIGN2014_0561
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Haselbach, F.CONCEPTS AND TECHNOLOGIES FOR THE NEXT GENERATION OF LARGE CIVIL AIRCRAFT ENGINES2014_0078
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Haussener, S.CHARACTERISING INTERNAL HEAT TRANSFER IN THERMAL PROTECTION SYSTEMS2014_0794
Hayashi, M.ON THE USE OF THE ADJOINT METHOD TO COMPUTE NON--GEOMETRIC SENSITIVITIES2014_0929
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Hellstein, P.IMAGE-BASED STRUCTURAL HEALTH MONITORING OF COMPOSITE STRUCTURES2014_0416
Henne, J.GEARING UP FOR HIGH VOLUME GTFTM PRODUCTION2014_1025
Hermanutz, A.PROGRESS TOWARDS ADAPTIVE AIRCRAFT ENGINE NACELLES2014_0770
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Hiraguri, H.MODELING OF DUST DEVIL ON MARS AND FLIGHT SIMULATION OF MARS AIRPLANE2014_0099
Hiraoka, K.CONCEPTUAL DESIGN OF SOLAR UAV FOR LONG ENDURANCE2014_0887
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Hoeijmakers, H.W.M.AIRCRAFT ICING IN FLIGHT: EFFECTS OF IMPACT OF SUPERCOOLED LARGE DROPLETS2014_0925
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Holzapfel, F.A NON-COOPERATIVE BI-LEVEL OPTIMAL CONTROL PROBLEM FORMULATION FOR NOISE MINIMAL DEPARTURE TRAJECTORIES2014_0356
Holzapfel, F.GENERATION OF INITIAL GUESSES FOR OPTIMAL CONTROL PROBLEMS WITH MIXED INTEGER DEPENDENT CONSTRAINTS2014_0495
Holzapfel, F.INCIDENT PREDICTION USING SUBSET SIMULATION2014_0758
Holzäpfel, F.SIMULATION OF AIRCRAFT WAKE VORTICES DURING LANDING WITH DECAY ENHANCING OBSTACLES2014_0796
Honda, M.D-SEND#2 FLIGHT DEMONSTRATION FOR LOW SONIC BOOM DESIGN TECHNOLOGY2014_0505
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Hornung, M.PROFIT-BASED NETWORK LEVEL EVALUATION OF AIRCRAFT BLOCK TIMES2014_0593
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Hou, Z.-X.DESIGN AND PERFORMANCE TEST OF A TWIN-FUSELAGE CONFIGURATION SOLAR-POWERED UAV2014_0408
Hou, Z.X.THE VERY FLEXIBLE AIRCRAFTS AND ALBATROSS FLIGHT2014_0755
Howarth, D.K.AIMING AND MISSING IN MULTIPLE DIMENSIONS2014_0097
Hsu, J.J.L.INVESTIGATION OF THE FLOW PATTERNS ON A SOUNDING ROCKET FORE-BODY SECTION2014_0727
Hu, L.RESEARCH ON INTEGRATION OF VAPOR CYCLE/LIQUID-COOLED REFRIGERATION SYSTEM FOR HELICOPTERS2014_0080
Hu, R.DETACHED-EDDY SIMULATION OF FLOW PAST A BACKWARD-FACING STEP WITH A HARMONIC ACTUATION2014_0877
Huang Hu, H.H.RESEARCH ON CORRECTIONS OF CFD SIMULATION TECHNIQUE FOR COMPLEX SHAPED CAVITY FLOW BASED ON THE WIND TUNNEL TEST DATA2014_0268
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Huber, N.DAMAGE TOLERANCE IMPROVEMENT OF LASER BEAM WELDED FUSELAGE STRUCTURES VIA CRENELLATIONS2014_0386
Huber, N.THE COOLING GRADIENT AND MICROSTRUCTURE CONTROL IN LASER BEAM WELDED TIAL ALLOY ASSISTED BY TEMPERATURE FIELD SIMULATION2014_0638
Huh, J.Y.MESHLESS METHOD FOR SIMULATION OF COMPRESSIBLE REACTING FLOW2014_0851
Hühne, C.STEPS TO FEASIBILITY FOR LAMINAR WING DESIGN IN A MULTIDISCIPLINARY ENVIRONMENT2014_0955
Hövelmann, A.EXPERIMENTAL INVESTIGATIONS ON VORTEX FLOW PHENOMENA OF A DIAMOND WING CONFIGURATION2014_0024
Iakobovski, M.V.VIRTUAL PROTOTYPING MODELING IN THE CAVE 3D ENVIRONMENT2014_0309
Iglesias, E.E.SENSITIVITY ANALYSIS OF TURBINE ENGINE SUSTAINMENT2014_1023
Ignatkin, Y.M.COMPUTATIONAL MODELING OF HELICOPTER'S MAIN AND TAIL ROTOR INTERFERENCE ON THE BASE OF NON-LINEAR BLADE VORTICAL MODEL2014_0101
Ignatyev, D.I.MODEL OF THE UNSTEADY AERODYNAMIC CHARACTERISTICS AT HIGH AOA WITH NONLINEAR DEPENDENCY IN ANGULAR RATE2014_0449
Iijima, T.DEVELOPMENT OF LOW-LEVEL TURBULENCE ADVISORY SYSTEM FOR AIRCRAFT OPERATION2014_0710
Iijima, T.DEVELOPMENT AND EVALUATION OF LOW-LEVEL TURBULENCE ADVISORY DISPLAY FOR AIRCRAFT OPERATION2014_0714
Ikeda, T.NUMERICAL STUDY OF WIND-TUNNEL ACOUSTIC RESONANCE INDUCED BY TWO-DIMENSIONAL AIRFOIL FLOW AT LOW REYNOLDS NUMBER2014_0195
Ilic, Z.IMPACT OF IRREGULARITIES IN THE PISTON ENGINE OPERATION ON THE INFLIGHT VIBRATION LEVEL2014_0581
Inada, Y.FLEXIBLE FORMATION SHAPE CONTROL BASED ON THE LOCAL INTERACTION AMONG AIR VEHICLES2014_0441
Inada, Y.EFFECT OF ELASTICITY IN THE BIRD-LIKE PRIMARY FEATHER WING ON THE FLIGHT STABILITY2014_0528
Inagaki, T.HIGH ALTITUDE TURBULENCE DETECTION USING AN AIRBORNE DOPPLER LIDAR2014_0208
Inokuchi, H.HIGH ALTITUDE TURBULENCE DETECTION USING AN AIRBORNE DOPPLER LIDAR2014_0208
Inozemtsev, A.A.LIFE VALIDATION STRATEGY2014_0974
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Isakovic, J.USABILITY OF COMPARATIVE EXPERIMENTAL - NUMERICAL SUPERSONIC TEST CASES WITH THE HB REFERENCE MODEL2014_0162
Iscold, P.H.CFD – BASED STUDY ON GOLDSCHMIED PROPULSION CONCEPT APPLICATION FOR DRAG REDUCTION2014_0964
Ishikawa, H.NATURAL LAMINAR FLOW DESIGN OF FUSELAGE NOSE FOR SMALL SUPERSONIC CIVIL TRANSPORT2014_0228
Ishikawa, H.NATURAL LAMINAR FLOW WING DESIGN OF SUPERSONIC TRANSPORT AT HIGH REYNOLDS NUMBER CONDITION2014_0752
Ishmuratov, F.NONLINEARITIES AND UNCERTAINTIES OF AEROELASTICITY CHARACTERISTICS IN AIRCRAFT DESIGN AND CERTIFICATION2014_0139
Ishmuratov, F.DYNAMIC RESPONSE OF AN AIRPLANE ELASTIC STRUCTURE IN TRANSONIC FLOW2014_0140
Isikveren, A.T.QUASI-ANALYTICAL AERODYNAMIC METHODS FOR PROPULSIVE FUSELAGE CONCEPTS2014_0518
Isikveren, A.T.PROFIT-BASED NETWORK LEVEL EVALUATION OF AIRCRAFT BLOCK TIMES2014_0593
Isikveren, A.T.PROGRESS TOWARDS ADAPTIVE AIRCRAFT ENGINE NACELLES2014_0770
Isikveren, A.T.RECENT ADVANCES IN AIRFRAME-PROPULSION CONCEPTS WITH DISTRIBUTED PROPULSION2014_0853
Isogai, K.SUBSONIC AND TRANSONIC FLOW SIMULATION FOR A WING OSCILLATING IN YAW AND SIDESLIP2014_0048
Isogai, K.INVESTIGATION OF AIRFOIL FOR AN INSECT-SIZED FLAPPING WING2014_0456
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Ito, T.AERODYNAMIC NOISE REDUCTION FOR HIGH LIFT DEVICES USING MORPHING FLAP CONCEPT2014_0732
Ivanov, I.I.DYNAMIC LOADS ACTING ON ENGINE FRAME ELEMENTS AFTER FAN BLADE OUT EVENT STUDY2014_0255
Ivanov, M.J.THERMODYNAMICALLY COMPATIBLE THEORY OF HIGH TEMPERATURE TURBOJET ENGINES2014_0461
Ivanov, I.E.NUMERICAL SIMULATION OF HIGH-SPEED SEPARATION FLOW IN THE AEROSPACE PROPULSION SYSTEMS2014_0634
Ivanov, A.I.CONTROLLED BOUNDARY LAYER ON THE SOLID WALLS OF WIND TUNNELS: NEW APPROACH TO THE BOUNDARY INTERFERENCE PROBLEM2014_0914
Ivanteeva, L.G.NUMERICAL INVESTIGATIONS ON THE SLENDER AXISYMMETRIC BODIES AERODYNAMICS IN WIDE RANGE OF MACH NUMBERS AND ANGLES OF ATTACK FROM 0° TO 180°2014_0084
Ivanyushkin, D.S.NOSES OF MINIMAL WAVE DRAG IN SUPERSONIC FLOW2014_0181
Ivanyushkin, A.K.AERODYNAMIC STUDIES ON LOW-NOISE AIRCRAFT WITH UPPER ENGINE INSTALLATION2014_0389
Jacobs, R.B.FORMULATION OF AN EXPERIMENT SELECTION METHODOLOGY FOR UNCERTAINTY REDUCTION AND APPLICATION TO ACTIVE FLOW CONTROL2014_0697
Jamison, K.A.TRANSONIC STORE SEPARATION ANALYSES USING MODERN DESIGN OF EXPERIMENTS AND QUANTITATIVE GRADING OF RESULTS2014_0691
Jang, D.-S.SUM-OF-SQUARES BASED STABILITY ANALYSIS FOR SKID-TO-TURN MISSILES WITH THREE-LOOP AUTOPILOT2014_0787
Jankovics, I.SUBJECTIVE FACTORS IN CONTROLLERS' DECISIONS2014_0973
Jansen, E.L.THE DIRECT PREDICTION OF BUCKLING LOADS OF SHELLS UNDER AXIAL COMPRESSION USING VCT - TOWARDS AN UPGRADED APPROACH2014_0681
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Jeon, B.-J.EXTENDED KALMAN FILTER DESIGN USING BEARING AND TIME-TO-GO MEASUREMENT FOR A HOMING MISSILE GUIDANCE2014_0742
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Ji, G.S.CONCEPTUAL DESIGN OF THREE ALTERNATIVE CONFIGURATIONS OF NEW-GENERATION 19-SEAT BUSH AIRCRAFT2014_0394
Ji, P.-B.MULTIDISCIPLINARY OPTIMIZATION OF TRUSS-BRACED WING LAYOUT2014_0879
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Jin Wei, J.W. RESEARCH ON CORRECTIONS OF CFD SIMULATION TECHNIQUE FOR COMPLEX SHAPED CAVITY FLOW BASED ON THE WIND TUNNEL TEST DATA2014_0268
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Kachalin, A.M.TRAINING OF THE FLIGHT STAFF ON FLIGHT SIMULATORS USING VIDEO CONFERENCE SYSTEMS2014_0381
Kachalin, A.M.INNOVATIVE TECHNOLOGIES AND VIDEO CONFERENCE SYSTEMS IN TECHNOLOGICAL PROCESS OF AIRCRAFT ENGINE PRODUCTION2014_0382
Kachel, S.MULTI-CRITERIAL AERODYNAMIC SYNTHESIS METHOD OF MISSION-ORIENTED AIRCRAFT DESIGN2014_0180
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Kageyama, K.VALIDATION AND SIMULATION STUDY OF THE ARRIVAL MERGING PROCEDURE MODEL2014_0159
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Kajikawa, Y.A BIBLIOMETRICS APPLICATION FOR EVALUATING CONTRIBUTION OF A RESEARCH INSTITUTE TO SCIENCE2014_0515
Kalensky, S.M.THE HYBRID PROPULSION SYSTEMS FOR THE ADVANCED AIRCRAFT2014_0820
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Kalinowski, M.INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME2014_0551
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Karas, O.DYNAMIC RESPONSE OF AN AIRPLANE ELASTIC STRUCTURE IN TRANSONIC FLOW2014_0140
Karas, O.V.EFFICIENT STATIONARY AND NONSTATIONARY AERODYNAMIC CALCULATION ALGORITHMS FOR THE APPLIED AERODYNAMICS PROBLEMS2014_0173
Karpel, M.WAKE VORTEX ENCOUNTER LOADS. FLIGHT TESTS AND NUMERICAL SIMULATIONS2014_0881
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Kartashev, Y.V.REALIZATION OF A CONTINUOUS BALANCE TESTING PROCEDURE IN A COMPRESSOR-DRIVEN TRANSONIC WIND TUNNEL2014_0354
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Kartovitskiy, L.NUMERICAL AND EXPERIMENTAL INVESTIGATION OF NON-STATIONARY PROCESSES IN SUPERSONIC GAS EJECTOR2014_0839
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Kashaev, N.THE COOLING GRADIENT AND MICROSTRUCTURE CONTROL IN LASER BEAM WELDED TIAL ALLOY ASSISTED BY TEMPERATURE FIELD SIMULATION2014_0638
Kaspar, J.EREA AND FUTURE SKY2014_1039
Kato, H.DAHWIN - DIGITAL/ANALOG-HYBRID WIND TUNNEL - FOR INNOVATIVE EFD/CFD INTEGRATION2014_0908
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Kawamura, H.DESIGN AND FLIGHT TEST OF A SOLAR-POWERED UNMANNED AIR VEHICLE FOR LONG ENDURANCE2014_0838
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Khaletskiy, Y.COMPARISON OF DUCTED AND UNDUCTED COUNTER ROTATING FAN MODEL NOISE2014_0485
Khaletskiy, Y.D.FAR-FIELD FAN NOISE ESTIMATION WITH THE APPLICATION OF 3D AEROACOUSTIC CALCULATION2014_0632
Kharitonov , A.M.CONTROL OF SONIC BOOM LEVEL BY CRYOGENIC ACTION ON THE PROCESS OF FLOW AROUND THE AIRCRAFT2014_1013
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Khlebnikova, I.G.CONSIDERATION OF THE SERVICE LIFE TAKING INTO ACCOUNT A LOT OF ONE-TYPE STRESSED UNIT ELEMENTS2014_0611
Khlopkov, Y.I.HYPERSONIC AEROTHERMODYNAMICS INVESTIGATION FOR AEROSPACE SYSTEM2014_0275
Khlopkov, A.Y.HYPERSONIC AEROTHERMODYNAMICS INVESTIGATION FOR AEROSPACE SYSTEM2014_0275
Khlopkov, Y.I.MONTE CARLO METHODS IN APPLIED MATHEMATICS AND COMPUTATIONAL AERODYNAMICS2014_0472
Khlopkov, A.Y.MONTE CARLO METHODS IN APPLIED MATHEMATICS AND COMPUTATIONAL AERODYNAMICS2014_0472
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Khrabrov, A.WIND TUNNEL INVESTIGATION OF CRITICAL FLIGHT REGIMES USING DYNAMICALLY SCALED ACTIVELY CONTROLLED MODEL IN 3 DOF GIMBAL2014_0415
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Khrabrov, A.N.MODEL OF THE UNSTEADY AERODYNAMIC CHARACTERISTICS AT HIGH AOA WITH NONLINEAR DEPENDENCY IN ANGULAR RATE2014_0449
Khrabrov, A.N.UPSET RECOVERING SIMULATION TO ENHANCE FLIGHT SAFETY BY ON-GROUND PILOT TRAINING2014_0745
Khromov, V.OPTIMUM AND DESIGN TRENDS OF COMPOUND HELICOPTERS2014_0089
Khvostikov, V.P.UAV REMOTE POWER SUPPLY SYSTEM BY LASER RADIATION2014_0274
Kienitz, K.H.DEVELOPMENT OF A MULTI-PURPOSE UAV WITH BIO-INSPIRED FEATURES2014_0586
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Kim, J.A DEVELOPMENT AND VERIFICATION OF DENSITY BASED SOLVER USING LU-SGS ALGORITHM IN OPENFOAM2014_0128
Kim, K.A DEVELOPMENT AND VERIFICATION OF DENSITY BASED SOLVER USING LU-SGS ALGORITHM IN OPENFOAM2014_0128
Kim, H.J.REAL-TIME LEADER-FOLLOWER UAV FORMATION FLIGHT BASED ON MODIFIED NONLINEAR GUIDANCE2014_0189
Kim, Y.REAL-TIME LEADER-FOLLOWER UAV FORMATION FLIGHT BASED ON MODIFIED NONLINEAR GUIDANCE2014_0189
Kim, Y.-H.THE EFFECT OF A SYNTHETIC JET ON THE PRESSURE DISTRIBUTION OF A FLAT PLATE2014_0536
Kim, S.J.DESIGN AND EXPERIMENT OF TWO-ROTORED UAV CYCLOCOPTER2014_0725
Kim, K.H.MESHLESS METHOD FOR SIMULATION OF COMPRESSIBLE REACTING FLOW2014_0851
Kim, J.S.NUMERICAL INVESTIGATION ON THE CORRELATION BETWEEN SHOCK STRUCTURE AND THRUST PERFORMANCE IN AN OVEREXPANDED NOZZLE2014_0948
Kindervater, C.MULTI-TERRAIN IMPACT SIMULATIONS OF A CRASHWORTHY COMPOSITE HELICOPTER SUBFLOOR2014_0492
Kintscher, M.INVESTIGATION OF MULTI-MATERIAL LAMINATES FOR SMART DROOP NOSE DEVICES2014_0489
Kinzburskiy, V.S.MULTIDISCIPLINARY ANALYSIS OF HIGH AND LOW PRESSURE TURBINES ON TRANSITIVE MODES IN THE FLIGHT CYCLE2014_0871
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Kiselev, A.P.THE LAMINAR-TURBULENT TRANSITION ZONE IN 2D AND 3D BOUNDARY LAYERS WITH EMPHASIS ON EFFECT OF FREE STREAM TURBULENCE2014_0374
Kiselev, N.P.FLOW STRUCTURE IN THE BASE REGION OF RE-ENTRY VEHICLE WITH SUPERSONIC BRAKING PLUMES IMPINGING WITH LANDING SURFACE2014_0640
Kishalov, A.E.NUMERICAL INVESTIGATION OF CHARACTIRISTICS OF DUAL-CIRCUIT NOZZLES WITH CONSIDERING THE EXTERNAL FLOW2014_0548
Kishimoto, N.RELATIONSHIP BETWEEN POROSITY INSIDE CFRP SPECIMEN AND RESOLUTION OF MICRO X-RAY CT2014_0187
Kitanina, E.E.AIR EVOLUTION IN FUEL FLOW UNDER DECREASED PRESSURE CONDITIONS: EXPERIMENTAL STUDIES AND ENGINEERING CODE DEVELOPMENT2014_0254
Kizer, J.R.SET-BASED DESIGN SPACE EXPLORATION ENABLED BY DYNAMIC CONSTRAINT ANALYSIS2014_0934
Klepka, A.NONLINEAR ACOUSTICS FOR HEALTH MONITORING OF COMPOSITE SCARF REPAIRS2014_0413
Kleptsov, V.I.THE PRINCIPLES OF FATIGUE APPROVAL FOR TRANSPORT AIRCRAFT AFTER ITS PRINCIPAL STRUCTURE ELEMENTS MODIFICATION2014_0919
Klimmek, T.AEROELASTIC BEHAVIOR OF COMPOSITE WINGS IN POSTBUCKLING REGIME2014_0789
Knecht, C.P.NOTES TRAINING IN ATM – A NEW APPROACH USING COMPUTER-BASED SIMULATION METHODS: RESEARCH METHODS2014_0833
Kobayashi, K.EVALUATION OF SATELLITE IMAGERY INTEGRATION IN OPTIMAL AIRCRAFT OPERATION PLANNING FOR DISASTER RELIEF2014_0438
Kolb, M.DEVELOPMENT OF A HYBRID ICE PROTECTION SYSTEM BASED ON NANOSTRUCTURED HYDROPHOBIC SURFACES2014_0891
Kolesnikov, E.FLIGHT ENVELOPE EXPANSION VIA ACTIVE CONTROL SOLUTIONS FOR A GENERIC TAILLESS AIRCRAFT2014_0591
Kolinko, A.WIND TUNNEL INVESTIGATION OF CRITICAL FLIGHT REGIMES USING DYNAMICALLY SCALED ACTIVELY CONTROLLED MODEL IN 3 DOF GIMBAL2014_0415
Koltsova, T.S.NOVEL METAL MATRIX/CARBON COMPOSITES FOR AIRSPACE APPLICATIONS2014_0906
Komarov, G.THERMOPLASTIC COMPOSITE AIRCRAFT STRUCTURE REPAIR METHODOLOGY2014_0631
Kondakov, I.MAIN BENEFITS OF PRO-COMPOSITE LAYOUTS FOR WING AND FUSELAGE PRIMARY STRUCTURE UNITS2014_0651
Kondo, K. COMPUTATIONAL COMPARATIVE STUDY FOR DESIGN OF LOW REYNOLDS NUMBER AIRFOIL2014_0818
Konev, I.EXPERIMENTAL EVALUATION OF THE EFFICIENCY OF GAS TURBINE ENGINE PARTS DAMPING WITH DRY FRICTION DAMPERS USING LASER VIBROMETER2014_0866
Konishi, Y.NUMERICAL STUDY OF WIND-TUNNEL ACOUSTIC RESONANCE INDUCED BY TWO-DIMENSIONAL AIRFOIL FLOW AT LOW REYNOLDS NUMBER2014_0195
Konopatova, A.V.PLANNING OF AN EXPENDITURE OF THE RESOURSE OF GAS TURBINE ENGINE IN OPERATION2014_0179
Konovalov, V.V.SMALL CRACKS IN ALUMINUM STRUCTURES UNDER STATIC AND CYCLIC LOADING2014_0216
Konovaltsev, A.V.MULTI-FUNCTIONAL AERODROME CONTROL RADAR BY USPR TECHNOLOGY2014_0146
Koopmans, E.EXPERIMENTAL RESEARCH ON FLOW SEPARATION CONTROL USING SYNTHETIC JET ACTUATORS2014_0694
Kopchenov, V.ANALYSIS OF THE PREDICTION ABILITY OF REACTION MECHANISMS FOR CFD MODELING OF THE COMBUSTION IN HIGH VELOCITY ENGINES2014_0209
Kopchenov, V.MECHANISMS OF POLLUTANT FORMATION IN THE H2 - FUELLED COMBUSTOR OF HIGH VELOCITY AIR-BREATHING ENGINE: MODELING STUDY2014_0236
Korepanova, O.V.EXPERIMENTAL INVESTIGATION OF ROTOR DYNAMICS IN AIRCRAFT ENGINE WITH TWO-AXIS STIFFNESS ANISOTROPY OF SUPPORTS2014_0676
Korolkov, V.I.METHOD DISTURBANCES IN THE LIMIT DEFORMATIONS IN THE CROSS-SECTION WING IS2014_0931
Korolyov, V.S.ABOUT AIRCRAFT STABILITY DURING WING-IN-GROUND EFFECT FLIGHT2014_0959
Korsun, O.N.APPROACHES FOR FLIGHT TESTS AIRCRAFT PARAMETER IDENTIFICATION2014_0210
Korsun, O.N.ENERGY APPROACH FOR AIRCRAFT VELOCITY OPTIMAL CONTROL DESIGN2014_0561
Korzhnev, V.N.NUMERICAL AND EXPERIMENTAL INVESTIGATIONS BYPASS-FLOW FANS FOR AN ADVANCED CIVIL AIRCRAFT ENGINE2014_0104
Koshelenko, A.V.THE WAYS FOR IMPROVEMENT OF AGREEMENT BETWEEN IN-FLIGHT AND GROUND-BASED SIMULATION FOR EVALUATION OF HANDLING QUALITIES AND PILOT TRAINING2014_0165
Koshelenko, A.V.AERODYNAMICS AND FLIGHT DYNAMICS PROBLEMS OF HIGH SPEED VEHICLES AND WAYS FOR THEIR SOLUTION2014_0487
Kostukov, S.P.SYNTHESIS OF AIRCRAFT MOTION CONTROL LAWS USING AGGREGATIVE CONTROLLER ANALYTICAL DESIGN PROCEDURE DURING AUTOMATIC IN-FLIGHT REFUELING2014_1005
Kosyanchuk, V.V.ADVANCED AVIONICS EQUIPMENT ON THE BASIS OF SECOND GENERATION INTEGRATED MODULAR AVIONICS2014_0148
Kotsur, O.VERIFICATION OF MODELLING OF FLUID-STRUCTURE INTERACTION (FSI) PROBLEMS BASED ON EXPERIMENTAL RESEARCH OF BLUFF BODY OSCILLATIONS IN FLUIDS2014_0953
Kovalenko, I.ANALYSIS OF POSSIBILITIES TO APPLY ELECTRIC TECHNOLOGIES FOR HELICOPTER PROPULSION SYSTEM2014_0404
Koverninskiy, I.V.UNIFIED TOOLS OF DEVELOPMENT OF THE ONBOARD EQUIPMENT BASED ON THE INTEGRATED MODULAR AVIONICS2014_0358
Kovrizhina, V.N.PROBLEMS AND ACHIEVEMENTS IN PANORAMIC SHEAR STRESS DIAGNOSTICS BY LIQUID CRYSTALS2014_0098
Kozharinov, E.RELIABILITY IMPROVEMENT OF ACCESSORY GEARBOX BEVEL DRIVES2014_0345
Kozlov, V.E.MODELING STUDY OF POLLUTANT FORMATION IN HOMOGENEOUS METHANE AND SYNGAS FUELED COMBUSTOR2014_0150
Kozlov, D.S.NEURAL NETWORK ADAPTIVE SEMI-EMPIRICAL MODELS FOR AIRCRAFT CONTROLLED MOTION2014_0530
Kozlov, V.V.THE ROLE OF LOCALIZED ROUGHNESS ON THE LAMINAR-TURBULENT TRANSITION ON THE OBLIQUE WING2014_0993
Kozorez, D.A.DEVELOPMENT OF HIGH SPEED FLYING VEHICLE ON-BOARD INTEGRATED NAVIGATION, CONTROL AND GUIDANCE SYSTEM2014_0329
Kozuka, T.ANALYSIS OF AIR TRAFFIC EFFICIENCY USING DYNAMIC PROGRAMMING TRAJECTORY OPTIMIZATION2014_0743
Krasilshchikov, M.N.DEVELOPMENT OF HIGH SPEED FLYING VEHICLE ON-BOARD INTEGRATED NAVIGATION, CONTROL AND GUIDANCE SYSTEM2014_0329
Krause, D.A METHODICAL APPROACH FOR DYNAMIC SYSTEM ANALYSIS & SYNTHESIS IN THE DIMENSIONING OF VARIANT LIGHTWEIGHT CABIN INTERIOR2014_0333
Krause, D.FE-MODELLING GUIDELINES FOR THE DIMENSIONING OF AIRCRAFT CABIN INTERIOR UNDER STATIONARY DYNAMIC LOADS2014_0460
Krause, D.DEVELOPMENT OF A SOLID PROPELLANT GAS GENERATOR (SPGG) SYSTEM FOR FIRE SUPPRESSION IN AVIATION - DESIGN OF AN INJECTOR2014_0672
Kravchenko, D.A.COMPUTATIONAL INVESTIGATION OF UNSTEADY AERODYNAMIC CHARACTERISTICS OF A MODERN AIRLINER2014_0442
Kreerenko, O.COMBINED SYNTHESIS OF CONTROL LAWS OF THE AIRCRAFT BRAKING ON THE RUNWAY DURING LANDING2014_1000
Kreerenko, E.COMBINED SYNTHESIS OF CONTROL LAWS OF THE AIRCRAFT BRAKING ON THE RUNWAY DURING LANDING2014_1000
Kritsky, V.IMPLEMENTATION OF HIGH STRENGTH COMPOSITE CERAMIC MATERIALS FOR PRODUCING TRIBOTECHNICAL PARTS OF GAS TURBINE ENGINES AS CONSTRUCTIONAL NANO-STRUCTURED MATERIALS2014_0746
Krivonosova, D.THE BE-200ES FIREFIGHTING AMPHIBIOUS AIRCRAFT EFFECTIVENESS DURING THE FIRE SEASONS 2004÷2011 YEARS IN THE EUROPEAN UNION COUNTRIES2014_0930
Krivosheev, I.A.NUMERICAL INVESTIGATION OF CHARACTIRISTICS OF DUAL-CIRCUIT NOZZLES WITH CONSIDERING THE EXTERNAL FLOW2014_0548
Kroll, E.LEARNING FROM THE DESIGN METHODOLOGY OF FAMOUS AEROSPACE INNOVATORS2014_0299
Krus, P.KNOWLEDGE-BASED DESIGN FOR FUTURE COMBAT AIRCRAFT CONCEPTS2014_0600
Krus, P.CONCEPTUAL AIRCRAFT DESIGN MODEL MANAGEMENT DEMONSTRATED ON A 4TH GENERATION FIGHTER2014_0621
Kruse, M.IMPACT OF INSECT CONTAMINATION ON OPERATIONAL AND ECONOMIC EFFECTIVENESS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY2014_0068
Krusz, W.DESIGN AND OPTIMIZATION OF LOW SPEED DUCTED FAN FOR A NEW GENERATION OF JOINED WING AIRCRAFT2014_0663
Krysztofiak, G.PREDICTED FLIGHT CHARACTERISTICS OF THE INVERTED JOINED WING SCALED DEMONSTRATOR2014_0552
Kryukov, I.A.NUMERICAL SIMULATION OF HIGH-SPEED SEPARATION FLOW IN THE AEROSPACE PROPULSION SYSTEMS2014_0634
Kuchi-ishi, S.DAHWIN - DIGITAL/ANALOG-HYBRID WIND TUNNEL - FOR INNOVATIVE EFD/CFD INTEGRATION2014_0908
Kudrov, M.ON THE FLIGHT OPERATING SAFETY IN THE MOUNTAINOUS ZONE AIRPORT2014_0351
Kuijpers, H.M.JNOISE ABATEMENT PATH PLANNING USING VIRTUAL FORCES2014_0031
Kukshinov, N.HEAT FLUX LEVEL DETERMINATION IN MODEL COMBUSTION CHAMBER OF HIGH-SPEED RAMJET ENGINE2014_0847
Kulesh, V.P.AEROELASTIC ANALYSIS OF THE ADAPTIVE WING WIND TUNNEL DEMONSTRATOR OF THE SADE PROJECT2014_0151
Kulida, E.L.ABOUT AIRCRAFT STABILITY DURING WING-IN-GROUND EFFECT FLIGHT2014_0959
Kulkov, V.M.ANALYSIS FOR POSSIBILITY TO USE SPACE PLATFORM WITH ELECTRIC PROPULSION SYSTEM IN COMBINATION WITH THE LAUNCH VEHICLE FOR AIR LAUNCH2014_0451
Kuprianowicz, S.THE JOINED WING SCALED DEMONSTRATOR RESULTS OF CFD2014_0514
Kursakov, I.A.FIN AND REAR STINGS SUPPORT EFFECTS ON THE FLOW AROUND THE AIRCRAFT MODEL2014_0190
Kursakov, I.NUMERICAL SIMULATION OF UNSTEADY FLOWS AROUND HIGH-LIFT CONFIGURATIONS2014_0321
Kuryachii, A.P.THEORETICAL MODELING OF THE ELECTROGASDYNAMIC METHOD OF LAMINAR FLOW CONTROL ON A SWEPT WING2014_0303
Kusunose, K.INNOVATIVE SUPERSONIC TRANSPORT CONFIGURATION BY BIPLANE WING / TWIN-BODY FUSELAGE2014_0735
Kusyumov, A.N. SIMULATION OF FLOW AROUND FUSELAGE OF HELICOPTER USING ACTUATOR DISC THEORY2014_0622
Kusyumov, A.N. CFD MODELING OF 2D AEROFOIL DYNAMIC STALL2014_0774
Kuzin, A.K.VIRTUAL PROTOTYPING MODELING IN THE CAVE 3D ENVIRONMENT2014_0309
Kuzmin, A.TRANSONIC AIRFOILS, WINGS, AND PROJECTILES ADMITTING ANOMALOUS BEHAVIOR OF AERODYNAMIC COEFFICIENTS2014_0087
Kuzmin, Y.V.THE CONTRIBUTION OF DIFFERENT COUNTRIES TO AIRPLANE DEVELOPMENT AND MANUFACTURE - PART II. HOW MANY AIRPLANES WERE THERE?2014_1036
Kuzmina, S.DYNAMIC RESPONSE OF AN AIRPLANE ELASTIC STRUCTURE IN TRANSONIC FLOW2014_0140
Kuzminsky, V.A.THE LAMINAR-TURBULENT TRANSITION ZONE IN 2D AND 3D BOUNDARY LAYERS WITH EMPHASIS ON EFFECT OF FREE STREAM TURBULENCE2014_0374
Kuznetsov, A.G.METHOD OF REQUIREMENTS CONFIRMATION TO AIRCRAFT AUTOMATIC LANDING SAFETY AT MATHEMATICS SIMULATION STAGE2014_0999
Kwak, J.-Y.COMPUTATIONAL ANALYSIS FOR FLAPPING WING BY COUPLED CFD AND CSD SOLUTIONS2014_0260
Kwiek, A.AERODYNAMIC DESIGN OF THE STRAKE FOR THE ROCKET PLANE IN TAILLESS CONFIGURATION.2014_0163
Kwiek, A.STUDY ON CONTROL AND STABILITY OF THE ROCKET PLANE TO SPACE TOURISM2014_0893
Kwon, H.H.EXTENDED KALMAN FILTER DESIGN USING BEARING AND TIME-TO-GO MEASUREMENT FOR A HOMING MISSILE GUIDANCE2014_0742
Kwon, H.-H.SUM-OF-SQUARES BASED STABILITY ANALYSIS FOR SKID-TO-TURN MISSILES WITH THREE-LOOP AUTOPILOT2014_0787
Kölker, K.EVALUATING TEMPORAL INTEGRATION OF EUROPEAN AIR TRANSPORT2014_0617
La Rocca, G.CONCEPTUAL DESIGN OF A PASSENGER AIRCRAFT FOR AERIAL REFUELING OPERATIONS2014_0425
La Rocca, G.A CONCEPTUAL DESIGN AND ANALYSIS METHOD FOR CONVENTIONAL AND UNCONVENTIONAL AIRPLANES2014_0776
Lai, J.C.S.EFFECT OF ANGLE OF ATTACK KINEMATICS ON PASSIVE FLAPPING FOIL POWER GENERATION2014_0051
Lan, C.E.EVALUATIONS OF FLYING QUALITIES FOR A NEW AND AN AGING TRANSPORT AIRCRAFT IN SEVERE ATMOSPHERIC TURBULENCE2014_0319
Langener, T.TRAJECTORY SIMULATION AND OPTIMIZATION OF THE LAPCAT-MR2 HYPERSONIC CRUISER CONCEPT2014_0232
Langener, T.THE LAPCAT-MR2 HYPERSONIC CRUISER CONCEPT2014_0428
Lanshin, A.I.ANALYSIS OF TRENDS AND FORECAST OF GTE DEVELOPMENT FOR SUBSONIC CIVIL AIRCRAFT2014_0396
Lanshin, A.I.PERSPECTIVE OF SMALL GAS TURBINE ENGINES DEVELOPMENT2014_0397
Lanshin, A.I.ECOLOGICAL OPTIMIZATION OF JET AIRCRAFT FLIGHTS IN VIEW OF CONTRAILS AND CONTRAIL CIRRUS FORMATION2014_0400
Lanshin, A.DEVELOPMENT OF KEY TECHNOLOGIES FOR MICRO REGENERATIVE GAS TURBINES2014_1007
Larina, E.V.NUMERICAL SIMULATION OF HIGH-SPEED SEPARATION FLOW IN THE AEROSPACE PROPULSION SYSTEMS2014_0634
Larionova, T.V.RAPID SOLIDIFIED MG-CA-ZN ALLOYS WITH MICROALLOYING OF LA, ND, Y, ZR2014_0907
Lau, A.THE NETWORK FLOW ENVIRONMENT: SLOT ALLOCATION MODEL EVALUATION WITH CONVECTIVE NOWCASTING2014_0761
Laudan, T.BLACK-BOX MODEL EPISTEMIC UNCERTAINTY AT EARLY DESIGN STAGE. AN AIRCRAFT POWER-PLANT INTEGRATION CASE STUDY2014_0073
Lavrov, M.A.ECOLOGICAL OPTIMIZATION OF JET AIRCRAFT FLIGHTS IN VIEW OF CONTRAILS AND CONTRAIL CIRRUS FORMATION2014_0400
Lawson, C.AN INTELLIGENT ICE PROTECTION SYSTEM FOR NEXT GENERATION AIRCRAFT TRAJECTORY OPTIMISATION2014_0395
Lawson, C.AIRFRAME SYSTEMS POWER OFF-TAKE MODELLING IN MORE-ELECTRIC LARGE AIRCRAFT FOR USE IN TRAJECTORY OPTIMISATION2014_0398
Lebedev, A.THERMOPLASTIC COMPOSITE AIRCRAFT STRUCTURE REPAIR METHODOLOGY2014_0631
Lebedev, V.G.ABOUT AIRCRAFT STABILITY DURING WING-IN-GROUND EFFECT FLIGHT2014_0959
Lebedev, V.V.FIRST AIRFIELDS OF SAINT PETERSBURG - FIRST AIRFIELDS OF RUSSIA2014_1037
Ledovskaya, N.N.VARIATION OF UNSTEADY FLOW PATTERN IN COMPRESSORS PRECEDING THE LOSS OF GASDYNAMIC STABILITY. EXPERIMENT.2014_0095
Lee, Y.BOOST-PHASE MISSILE ATTITUDE CONTROLLER DESIGN USING HIGHER-ORDER SLIDING MODES2014_0114
Lee, N.COMPUTATIONAL ANALYSIS FOR FLAPPING WING BY COUPLED CFD AND CSD SOLUTIONS2014_0260
Lee, S.COMPUTATIONAL ANALYSIS FOR FLAPPING WING BY COUPLED CFD AND CSD SOLUTIONS2014_0260
Lee, H.-I.DYNAMICS MODELING AND ROBUST CONTROLLER DESIGN OF THE MULTI-UAV TRANSPORTATION SYSTEM2014_0316
Lee, B.-Y.DYNAMICS MODELING AND ROBUST CONTROLLER DESIGN OF THE MULTI-UAV TRANSPORTATION SYSTEM2014_0316
Lee, C.-H.CONTROL INPUT BLENDING LOGIC WITH AERODYNAMIC CONTROL AND REACTION JET CONTROL2014_0427
Lee, J.-I.CONTROL INPUT BLENDING LOGIC WITH AERODYNAMIC CONTROL AND REACTION JET CONTROL2014_0427
Lee, S.STUDY ON PERFORMANCE AND FLOW CHARACTERISTICS FOR EMBEDDED DISTRIBUTED PROPULSION SYSTEM2014_0482
Lee, C.H.DESIGN AND EXPERIMENT OF TWO-ROTORED UAV CYCLOCOPTER2014_0725
Lee, J.W.DESIGN AND EXPERIMENT OF TWO-ROTORED UAV CYCLOCOPTER2014_0725
Lee, W.PERFORMANCE OF SWITCHING TYPE DATABASE REFERENCED NAVIGATION ALGORITHM USING TERRAIN HEIGHT AND GRAVITY ANOMALY2014_0734
Lee, B.Y.MULITLE TASK ASSIGNMENT FOR COOPERATIVE TRANSPORT SYSTEM WITH GROUP BUYING APPROACH2014_0765
Lee, H.I.MULITLE TASK ASSIGNMENT FOR COOPERATIVE TRANSPORT SYSTEM WITH GROUP BUYING APPROACH2014_0765
Lee, J.H.NUMERICAL AND EXPERIMENTAL INVESTIGATION OF NON-STATIONARY PROCESSES IN SUPERSONIC GAS EJECTOR2014_0839
Lee, Y.DYNAMIC CHARACTERISTICS OF THE THRUST VECTORING CONTROL BY HIGHLY COMPRESSIBLE COANDA EFFECTS2014_0857
Legendre, C.ON SOUND ABSORPTION BY AN ACOUSTIC LINER WITH BIAS FLOW2014_0988
Lehner, S.EVALUATING TEMPORAL INTEGRATION OF EUROPEAN AIR TRANSPORT2014_0617
Lehov, P.A. HYPERSONIC FLOWFIELD AND HEAT FLUX PECULIARITIES ON THE NEW SPACE LAUNCHER WITH WINGED REUSABLE FIRST STAGE.2014_0898
Lei, Z.DESIGN AND FLIGHT TEST OF A SOLAR-POWERED UNMANNED AIR VEHICLE FOR LONG ENDURANCE2014_0838
Lengers, M.INDUSTRIAL ASSESSMENT OF OVERALL AIRCRAFT DRIVEN LOCAL ACTIVE FLOW CONTROL2014_0175
Leonov, S.MECHANISM OF FLAMEHOLDING IN PLASMA-ASSISTED SUPERSONIC COMBUSTOR2014_0014
Leonova, I.P.PLANNING OF AN EXPENDITURE OF THE RESOURSE OF GAS TURBINE ENGINE IN OPERATION2014_0179
Leonteva, R.V.PROCEDURE OF GROUND VIBRATION EXPERIMENTS ON AIRCRAFT WITH SIMULATING FORCES DUE TO ENGINE IMBALANCE AT BLADE LOSS2014_0859
Levchenko, E.A.SOME LAMINATE DEFORMATIONS FEATURES2014_0226
Levin, V.A.THE STUDY OF NONQUILIBRIUM GAS-DYNAMIC PROCESSES IN THE FLOW AROUND BODIES IN THE WIND TUNNEL IT-2M TSAGI2014_0573
Levora, T.PATH PLANNING FOR ULTRALIGHTS UNDER EMERGENCY CONDITIONS2014_0882
Levora, T.EMERGENCY LANDING SITE LOCATION USING AERIAL IMAGE SEGMENTATION2014_0885
Leyland, P.CHARACTERISING INTERNAL HEAT TRANSFER IN THERMAL PROTECTION SYSTEMS2014_0794
Leyland, P.VERIFICATION OF MODELLING OF FLUID-STRUCTURE INTERACTION (FSI) PROBLEMS BASED ON EXPERIMENTAL RESEARCH OF BLUFF BODY OSCILLATIONS IN FLUIDS2014_0953
Li, D.APPLICATION OF SCALE ADAPTIVE SIMULATION BASED ON K-(OMEGA) SST TURBULENCE MODEL2014_0040
Li, L.NUMERICAL SIMULATIONS AND EXPERIMENTS ON THE INJECTION MOLDING OF AIRCRAFT TRANSPARENCIES2014_0049
Li, X.-P.NUMERICAL INVESTIGATION OF FUSELAGE-STABILIZER-CONTROL SURFACE INTERFERENCE FOR A HYPERSONIC WAVERIDER VEHICLE2014_0290
Li, M.CONCEPTUAL DESIGN OF A PASSENGER AIRCRAFT FOR AERIAL REFUELING OPERATIONS2014_0425
Li, F.ADAPTIVE FEEDFORWARD CONTROL DESIGN FOR GUST LOADS ALLEVIATION AND LCO SUPPRESSION2014_0463
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Li, B.A THREE-DIMENSIONAL FLAPPING WING MECHANISM FOR WIND TUNNEL EXPERIMENTS2014_0601
Li, L.DETACHED-EDDY SIMULATION OF FLOW PAST A BACKWARD-FACING STEP WITH A HARMONIC ACTUATION2014_0877
Li, X.-P.MULTIDISCIPLINARY OPTIMIZATION OF TRUSS-BRACED WING LAYOUT2014_0879
Liguang, W.AN EXPERIMENTAL STUDY ON THE INFLUENCE OF PASSIVE DEFORMATION TO LIFT AND THRUST GENERATION IN FLEXIBLE FLAPPING WING2014_0618
Lima, L.S.M.CFD – BASED STUDY ON GOLDSCHMIED PROPULSION CONCEPT APPLICATION FOR DRAG REDUCTION2014_0964
Limonin, M.V.SOME LAMINATE DEFORMATIONS FEATURES2014_0226
Linke, F.IMPACT OF INSECT CONTAMINATION ON OPERATIONAL AND ECONOMIC EFFECTIVENESS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY2014_0068
Lipatov, I.I.NUMERICAL MODELING OF THE BUFFET ONSET IN 2-D AND 3-D FLOWS2014_0769
Lipatov, I.I.SHOCK WAVE BOUNDARY LAYER INTERACTION PROCESSES. BUFFET CONTROL METHODS2014_1033
Lis, M.PREDICTED FLIGHT CHARACTERISTICS OF THE INVERTED JOINED WING SCALED DEMONSTRATOR2014_0552
Lischi, S.POLARIMETRIC AVIONIC WEATHER RADAR FOR INCREASING FLIGHT SAFETY AND EFFICIENCY2014_0343
Liseykin, G.STRUCTURAL NONLINEARITIES SIMULATION ON THE FLUTTER ELECTROMECHANICAL MODELING TEST BENCH2014_0324
Liseykin, G.V.FLUTTER CALCULATIONS AND TRANSONIC WIND TUNNEL TESTING OF DYNAMICALLY SCALED MODEL OF THE HIGH-ASPECT-RATIO WING2014_0325
Liu, Y.J.NUMERICAL SIMULATION OF BIRD STRIKE IN AIRCRAFT LEADING EDGE STRUCTURE USING A NEW DYNAMIC FAILURE MODEL2014_0111
Liu, G.ANALYSIS AND COUNTERMEASURE ON AERO-ENGINE BLADE DEFECT2014_0143
Liu, Y.AN EVALUATING MODEL FOR CONTROL EFFECTOR SUPERIORITY BASED ON PERFORMANCE REQUIREMENTS2014_0421
Liu, C.FAILURE ANALYSIS ON REAR GEARBOX OUTPUT GEAR OF HELICOPTER2014_0512
Liu, D.FAILURE ANALYSIS ON REAR GEARBOX OUTPUT GEAR OF HELICOPTER2014_0512
Liu, K.NUMERICAL INVESTIGATION ON ENGINE INLET DISTORTION UNDER CROSSWIND FOR A COMMERCIAL TRANSPORT AIRCRAFT2014_0560
Liu, J.THE COOLING GRADIENT AND MICROSTRUCTURE CONTROL IN LASER BEAM WELDED TIAL ALLOY ASSISTED BY TEMPERATURE FIELD SIMULATION2014_0638
Liu , Z.W.THE VERY FLEXIBLE AIRCRAFTS AND ALBATROSS FLIGHT2014_0755
Lobanova, M.A.A STUDY OF FLOW AND INITIAL STAGE OF WATER CONDENSATION IN THE TWO-PHASE JET-VORTEX WAKE BEHIND A CRUISE AIRCRAFT2014_0917
Loja, M.A.R.DESIGN OF A LAMINATED COMPOSITE MULTI-CELL STRUCTURE SUBJECTED TO TORSION2014_0905
Lomazov, V.DEVELOPMENT OF KEY TECHNOLOGIES FOR MICRO REGENERATIVE GAS TURBINES2014_1007
Lopanitsyn, D.E.AIRLINERS CONTROL SYSTEMS AUTOMATION FUNCTIONS ENCHANCEMENT IN BEHALF OF AIRPLANE STRUCTURAL STRENGTH2014_0960
Loth, S.EVALUATION OF OPERATIONS ON AN AIRPORT WITH A CIRCULAR RUNWAY2014_0450
Lu, G.THE TRANSFORM PRINCIPLE AND MODEL FOR AIRCRAFT MTTR IN THREE-DIMENSIONAL DIGITAL DESIGN CONDITION2014_0235
Lu, J.DAMAGE TOLERANCE IMPROVEMENT OF LASER BEAM WELDED FUSELAGE STRUCTURES VIA CRENELLATIONS2014_0386
Lucchi, F.USING BCIS (BRAIN COMPUTER INTERFACES) TO EVALUATE EMOTIONAL PERCEPTION OF PASSENGER CABIN DESIGN IN VIRTUAL ENVIRONMENTS2014_0668
Lucchi, F.AIRCRAFT PRELIMINARY DESIGN: GENETIC ALGORITHM BASED OPTIMIZATION METHOD2014_1009
Lukovnikov, A.ANALYSIS OF POSSIBILITIES TO APPLY ELECTRIC TECHNOLOGIES FOR HELICOPTER PROPULSION SYSTEM2014_0404
Lukovnikov, A.V.THE HYBRID PROPULSION SYSTEMS FOR THE ADVANCED AIRCRAFT2014_0820
Lunin, V.J.NUMERICAL INVESTIGATIONS ON THE SLENDER AXISYMMETRIC BODIES AERODYNAMICS IN WIDE RANGE OF MACH NUMBERS AND ANGLES OF ATTACK FROM 0° TO 180°2014_0084
Lupidi, A.POLARIMETRIC AVIONIC WEATHER RADAR FOR INCREASING FLIGHT SAFETY AND EFFICIENCY2014_0343
Lutovinov, V.M.EXAMPLES OF PIV APPLICATIONS TO SUBSONIC FLOWS2014_0376
Lysenkov, A.NUMERICAL SIMULATION OF UNSTEADY FLOWS AROUND HIGH-LIFT CONFIGURATIONS2014_0321
Lysenkov, A.COMPUTATIONAL METHOD FOR STEADY FLOW (RANS) USING ZONAL APPROACH AND ITS IMPLEMENTATION EXPERIENCE FOR SOLUTION OF TASK OF INTERFERENCE ENGINE AND AIRFRAME2014_0499
Lysenkova, N.B.PRINCIPLES OF THE AUTOMATED CONTROL FOR THE CIVIL AIRCRAFT, WHICH PROVIDE FLIGHT SAFETY2014_0121
Lütjens, K.EVALUATING TEMPORAL INTEGRATION OF EUROPEAN AIR TRANSPORT2014_0617
Lyubimov, D.A.INVESTIGATION OF FLOW PARAMETERS AND NOISE OF SUBSONIC AND SUPERSONIC JETS USING RANS/ILES HIGH RESOLUTION METHOD2014_0373
Lyubimov, D.A.INVESTIGATION OF SYNTHETIC JETS EFFICIENCY ON SEPARATION FLOW IN DIFFUSERS OF DIFFERENT GEOMETRY WITH RANS/ILES-METHOD2014_0546
Ma, Y.H.STRUCTURE DESIGN AND MECHANICAL SIMULATION ON THE SC-MR SUPPORT FOR ROTOR SYSTEM2014_0317
Ma, Y.H.COMPRESSIBLE BOUNDARY LAYER HEAT FLUX MEASUREMENT USING EMBEDDED THERMOCOUPLES2014_0741
MacKunis, W.ON UAV ROBUST NONLINEAR CONTROL IN PRESENCE OF PARAMETRIC UNCERTAINTIES2014_0731
Madani, I.AN INTELLIGENT ICE PROTECTION SYSTEM FOR NEXT GENERATION AIRCRAFT TRAJECTORY OPTIMISATION2014_0395
Madani, I.AIRFRAME SYSTEMS POWER OFF-TAKE MODELLING IN MORE-ELECTRIC LARGE AIRCRAFT FOR USE IN TRAJECTORY OPTIMISATION2014_0398
Magerramova, L.A.HIGH TEMPERATURES TURBINE BLADES DAMAGE PREDICTION TAKING INTO ACCOUNT LOADING HISTORY DURING A FLIGHT CYCLE2014_0120
Magerramova, L.BIMETALLIC BLISK DESIGN FOR HIGH TEMPERATURE TURBINES OF GAS TURBINE ENGINE OF DIFFERENT APPLICATION2014_0193
Mahallati, A.GEOMETRIC AND FLOW PARAMETERS EFFECTING THE AERO-THERMAL PERFORMANCE OF TURBOFAN FORCED MIXERS2014_0977
Mahallati, A.AERODYNAMIC DESIGN OF HIGH PERFORMANCES INTER-TURBINE TRANSITION DUCTS2014_0978
Mahmood, G.I.FLOW FIELD AROUND DIMPLED SHORT PIN-FINS IN A STAGGERED ARRAY2014_0302
Majic, F.PROGRESS TOWARDS ADAPTIVE AIRCRAFT ENGINE NACELLES2014_0770
Makarov, A.Y.EXPERIMENTAL STUDY OF SYNTHETIC JETS FOR THE CONTROL OF FLOWS SEPARATION IN THE ENGINE'S DUCTS2014_0280
Makarov, K.A.NUMERICAL INVESTIGATION OF AN AILERON HINGE MOMENTS AND EFFECTIVENESS ON A HIGH LIFT WING AIRFOIL2014_0599
Makarov, V.THE NUMERICAL ANALYSIS OF IMPACT OF CHANGES IN FLIGHT CONDITIONS AND IN ENGINE'S REGIME AT CRUISE ON AIRPLANE'S AERODYNAMIC CHARACTERISTICS2014_1003
Makeev, P.V.COMPUTATIONAL MODELING OF HELICOPTER'S MAIN AND TAIL ROTOR INTERFERENCE ON THE BASE OF NON-LINEAR BLADE VORTICAL MODEL2014_0101
MAKIDA, M.DETAILED RESEARCH ON RICH-LEAN TYPE SINGLE SECTOR AND FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT ENGINE2014_0628
Makino, Y.CONCEPTUAL DESIGN STUDY ON LH2 FUELED SST - ENVIRONMENTAL IMPACTS REDUCED BY AIRFRAME/PROPULSION SYSTEM INTEGRATION -2014_0475
Maksimov, F.EXISTENCE CRITERIA OF NON-VISCOUS VORTICAL STRUCTURES IN SHOCK LAYERS OF CONICAL GAS FLOWS2014_0571
Malaek, S.M.TERMINAL HOLDING TIME OPTIMIZATION BY DYNAMIC CDA ROUTING ALGORITHM2014_0250
Malakhov, R.GAN POWER AMPLIFIER FOR ON-BOARD DIGITAL ANTENNA ARRAY2014_0767
Malinin, V.V.NUMERICAL MODELING OF FLOW IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS2014_0509
Malysheva, L.EXTREME INFLUENCE OF ENVIRONMENT AND RISKS OF THE FLIGHT SAFETY DEGRADATION DUE TO THE CHANGE OF THE A/C T/O-AND-L PERF2014_0205
Malyutin, V.A.AEROELASTIC ANALYSIS OF THE ADAPTIVE WING WIND TUNNEL DEMONSTRATOR OF THE SADE PROJECT2014_0151
Mamaev, V.K.THERMODYNAMICALLY COMPATIBLE THEORY OF HIGH TEMPERATURE TURBOJET ENGINES2014_0461
Mancini, M.AERODYNAMIC OPTIMIZATION OF A GREEN ATF REGIONAL AIRCRAFT IN CRUISE CONDITION2014_0263
Mandic, S.USABILITY OF COMPARATIVE EXPERIMENTAL - NUMERICAL SUPERSONIC TEST CASES WITH THE HB REFERENCE MODEL2014_0162
Manfriani, L.AERODYNAMIC MODELLING OF A REFUELLING BOOM2014_0969
Mannarino, A.ADAPTIVE CONTROL OF AEROELASTIC SYSTEMS: AN IMMERSION AND INVARIANCE APPROACH2014_0060
Mantegazza, P.ADAPTIVE CONTROL OF AEROELASTIC SYSTEMS: AN IMMERSION AND INVARIANCE APPROACH2014_0060
Manuilovich , S.V.THEORETICAL MODELING OF THE ELECTROGASDYNAMIC METHOD OF LAMINAR FLOW CONTROL ON A SWEPT WING2014_0303
Marakueva, O.AERODYNAMIC DESIGN AND OPTIMIZATION OF BLADE CONFIGURATION IN AN INLET STAGE OF AN AIRCRAFT ENGINE COMPRESSOR2014_0590
Marchetti, M.SYNTHESYS OF RADAR ABSORBING MATERIALS FOR STEALTH AIRCRAFT BY USING NANOMATERIALS AND EVOLUTIONARY COMPUTATION2014_0534
Maré, J.-C.MISSION PROFILES ANALYSIS: GUIDELINES TO AIRCRAFT ACTUATORS NEW TECHNOLOGY SPECIFICATION2014_0194
Marinkovski , D.MEASUREMENT OF THE CROSS-COUPLING DERIVATIVES DUE TO PITCHING IN THE HIGH REYNOLDS NUMBER BLOWDOWN WIND TUNNEL2014_0113
Marinkovski, D.LIVING WITH SUPERSONIC STARTING LOADS IN THE T-38 TRISONIC WIND TUNNEL OF VTI2014_0138
Markina, K.V.NUMERICAL INVESTIGATION OF CHARACTIRISTICS OF DUAL-CIRCUIT NOZZLES WITH CONSIDERING THE EXTERNAL FLOW2014_0548
Marques, J.M.G.ON THE COMPENSATION AND DAMPING OF ROLL INDUCED BY WAKE VORTICES2014_0990
Marta, A.C.ON THE OPTIMAL LOCATION OF BLEED PORTS FOR GAS TURBINE COOLING2014_0517
Marta, A.C.LONG ENDURANCE ELECTRIC UAV FOR CIVILIAN SURVEILLANCE MISSIONS2014_0547
Marta, A.C.FRAMEWORK FOR LOW-NOISE WIND TURBINE BLADE DESIGN2014_0589
Martorella, M.POLARIMETRIC AVIONIC WEATHER RADAR FOR INCREASING FLIGHT SAFETY AND EFFICIENCY2014_0343
Maslov, V.P.EXPERIMENTAL STUDY OF SYNTHETIC JETS FOR THE CONTROL OF FLOWS SEPARATION IN THE ENGINE'S DUCTS2014_0280
Maslov, A.A.ARTIFICIAL TURBULIZATION OF THE SUPERSONIC BOUNDARY LAYER BY DIELECTRIC BARRIER DISCHARGE2014_0323
Masur, V.N.METHOD OF REQUIREMENTS CONFIRMATION TO AIRCRAFT AUTOMATIC LANDING SAFETY AT MATHEMATICS SIMULATION STAGE2014_0999
Matayoshi, N.WAKE VORTEX OBSERVATION CAMPAIGN BY ULTRA FAST-SCANNING LIDAR IN NARITA AIRPORT, JAPAN2014_0185
Matayoshi, N.DETECTION AND ESTIMATION OF WAKE VORTEX ON ULTRA FAST-SCANNING PULSED-DOPPLER LIDAR2014_0186
Matayoshi, N.DYNAMIC WAKE VORTEX SEPARATION COMBINING WITH TRAFFIC OPTIMIZATION2014_0639
Matayoshi, N.DEVELOPMENT OF LOW-LEVEL TURBULENCE ADVISORY SYSTEM FOR AIRCRAFT OPERATION2014_0710
Matayoshi, N.DEVELOPMENT AND EVALUATION OF LOW-LEVEL TURBULENCE ADVISORY DISPLAY FOR AIRCRAFT OPERATION2014_0714
Matsue, T.RANS MODELING FOR FLOWS ON RIBLETS BASED ON EXPERIMENTAL DATA2014_0440
Matsuno, Y.STOCHASTIC CONFLICT-FREE 4D TRAJECTORY OPTIMIZATION IN THE PRESENCE OF UNCERTAINTY2014_0724
Matsushima, K.AERODYNAMIC DESIGN METHOD FOR SUPERSONIC SLENDER BODY USING AN INVERSE PROBLEM2014_0874
Mattei, M.TRANSITION CONTROL AND REDUNDANCY MANAGEMENT FOR A TILT ROTOR UAV USING GENETIC ALGORITHMS2014_0285
Mattei, M.CONSTRAINED PREDICTIVE STRATEGIES FOR FLIGHT CONTROL SYSTEMS2014_0412
Mattei, M.HW VS SW SENSOR REDUNDANCY: FAULT DETECTION AND ISOLATION OBSERVER BASED APPROACHES FOR INERTIAL MEASUREMENT UNITS2014_0455
Matushkin, A.A.PREDICTION OF OPERATIONAL CHARACTERISTICS OF FLUID-FILM AND GAS BEARINGS FOR HIGH-SPEED TURBOMACHINERY USING COMPUTATIONAL FLUID DYNAMICS2014_0119
Matushkin, A.A.IMPROVEMENT OF THE DESIGN AND METHODS OF DESIGNING CRITICAL COMPONENTS OF GAS FLOW PATH OF MODULAR AIRCRAFT GAS TURBINE2014_0272
Matveenko, A.M.PROTECTION PROBLEM FOR THIN-WALLED COMPOSITE CONSTRUCTIONS OF AIRCRAFT FROM ACTION OF RADIATIONS AND PARTICLES FLUXES2014_1034
Matveeva, N.TOOLSET FOR ONBOARD NETWORKS DESIGN AND CONFIGURATION2014_0937
Matveeva, N.METHOD OF SEARCHING FOR ROUTES WITH DELAY AND JITTER LIMITATION2014_0984
Mavris, D.N.FORMULATION OF AN EXPERIMENT SELECTION METHODOLOGY FOR UNCERTAINTY REDUCTION AND APPLICATION TO ACTIVE FLOW CONTROL2014_0697
Mavris, D.N.MODEL FORM UNCERTAINTY REPRESENTATION TO ENABLE MULTIFIDELITY DESIGN OF ADVANCED CONCEPTS2014_0716
Mavris, D.N.QUANTITATIVE FIDELITY MANAGEMENT AND SELECTION OF PHYSICS-BASED MULTIDISCIPLINARY DESIGN ENVIRONMENTS2014_0717
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Panfilov, S.V.COMPUTATIONAL SIMULATION OF TWO-PHASE GAS-PARTICLE FLOW IN AN INLET “ROTOR-STATOR” STAGE OF A TURBOJET ENGINE COMPRESSOR2014_0856
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Pérez, J.A COMPARISON OF THE TWO ARRIVAL TRAFFIC SYNCHRONIZATION CONCEPTS ENVISIONED FOR NEXTGEN AND SESAR.2014_0556
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Pfeiffer, T.AIRCRAFT CONFIGURATION ANALYSIS USING A LOW-FIDELITY, PHYSICS BASED AEROSPACE FRAMEWORK UNDER UNCERTAINTY CONSIDERATIONS2014_0750
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Rohacs, J.DEVELOPING THE MAGLEV ASSISTED AIRCRAFT TAKE-OFF AND LANDING (GABRIEL CONCEPT)2014_0971
Rojas, G.CONCEPTUAL DESIGN OF THREE ALTERNATIVE CONFIGURATIONS OF NEW-GENERATION 19-SEAT BUSH AIRCRAFT2014_0394
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Rui, KangBALANCED ALLOCATION ON ARRIVAL AIR TRAFFIC FLOW2014_0952
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