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10:50 | 11:20 | 1.1.1 |
INDUSTRIAL ASSESSMENT OF OVERALL AIRCRAFT DRIVEN LOCAL ACTIVE FLOW CONTROL M. Lengers, Airbus Operations GmbH, Germany | ||||
11:20 | 11:50 | 1.1.2 |
IMPACT OF INSECT CONTAMINATION ON OPERATIONAL AND ECONOMIC EFFECTIVENESS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY K. Wicke¹, M. Kruse¹, F. Linke¹, V. Gollnick¹; ¹German Aerospace Center (DLR), Germany | ||||
11:50 | 12:20 | 1.1.3 |
NATURAL LAMINAR FLOW WING DESIGN OF SUPERSONIC TRANSPORT AT HIGH REYNOLDS NUMBER CONDITION H. Ishikawa, TOUA Co. Ltd., Japan; N. Tokugawa¹, Y. Ueda, Tokyo Business Service Co. Ltd., Japan; K. Yoshida¹; ¹JAXA, Japan |
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10:50 | 11:20 | 2.1.1 |
ON THE OPTIMIZATION OF BLENDED WING BODY AIRCRAFT CONFIGURATION VIA THE SURROGATE MODELING METHOD T. Wan¹, Y.S. Chen¹; ¹Tamkang University, Taiwan | ||||
11:20 | 11:50 | 2.1.2 |
CFD BASED OPTIMIZATION OF HIGH-LIFT DEVICES USING A MESH MORPHING TECHNIQUE R.G. Silva, Universidade de São Paulo, Brazil; A.P. Antunes¹, R.B. Flatschart¹, J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil; ¹Embraer, Brazil | ||||
11:50 | 12:20 | 2.1.3 |
AERODYNAMIC OPTIMIZATION OF A GREEN ATF REGIONAL AIRCRAFT IN CRUISE CONDITION D.G. Romano¹, M. Mancini¹; ¹Piaggio Aero Industries S.p.A., Italy |
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10:50 | 11:20 | 3.1.1 |
DESIGN AND VALIDATION OF A FORCED MOTION VARIABLE STIFFNESS AEROELASTIC WIND TUNNEL APPARATUS (AATB) J. Ertveldt¹, J. Schoukens¹, R. Pintelon¹, S. Vanlanduit¹; ¹Vrije Universiteit Brussel, Belgium | ||||
11:20 | 11:50 | 3.1.2 |
COMPRESSIBLE BOUNDARY LAYER HEAT FLUX MEASUREMENT USING EMBEDDED THERMOCOUPLES X.J. Zhao¹, Y.H. Ma¹, W.Z. Xiao¹; ¹China Academy of Aerospace Aerodynamics, China | ||||
11:50 | 12:20 | 3.1.3 |
CONTROLLED BOUNDARY LAYER ON THE SOLID WALLS OF WIND TUNNELS: NEW APPROACH TO THE BOUNDARY INTERFERENCE PROBLEM A.I. Ivanov¹, E.V. Streltsov¹; ¹TsAGI, Russia |
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10:50 | 11:20 | 4.1.1 |
EXPERIMENTAL INVESTIGATIONS ON VORTEX FLOW PHENOMENA OF A DIAMOND WING CONFIGURATION A. Hövelmann¹, C. Breitsamter¹; ¹Technische Universität München, Germany | ||||
11:20 | 11:50 | 4.1.2 |
MODEL OF THE UNSTEADY AERODYNAMIC CHARACTERISTICS AT HIGH AOA WITH NONLINEAR DEPENDENCY IN ANGULAR RATE D.I. Ignatyev¹, A.N. Khrabrov¹; ¹TsAGI, Russia | ||||
11:50 | 12:20 | 4.1.3 |
SUBSONIC AND TRANSONIC FLOW SIMULATION FOR A WING OSCILLATING IN YAW AND SIDESLIP K. Isogai, Japan Aerospace Exploration Agency, Japan |
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10:50 | 11:20 | 5.1.1 |
NOVEL METAL MATRIX/CARBON COMPOSITES FOR AIRSPACE APPLICATIONS A.I. Rudskoy¹, A.G. Nasibulin, Skolkovo Institute of Science and Technology, Russia; T.S. Koltsova¹, O.V. Tolochko¹; ¹Saint Petersburg State Polytechnical University, Russia | ||||
11:20 | 11:50 | 5.1.2 |
APPROXIMATE FUNCTION FOR FATIGUE CRACK PROPAGATION IN A DESIGN OPTIMISATION PROCEDURE FOR FIBRE METAL LAMINATES I. Sen¹, R.C. Alderliesten¹, R. Bendictus¹; ¹Delft University of Technology, Netherlands | ||||
11:50 | 12:20 | 5.1.3 |
AN ANALYTICAL SOLUTION TO THE ELASTIC-PLASTIC BEHAVIOR OF METAL MATRIX COMPOSITES UNDER TENSILE LOADING S. Khosoussi¹, M. Mondali, , Islamic Azad University, Science and Research Branch, Iran; A. Abedian¹; ¹Sharif University of Technology, Iran |
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10:50 | 11:20 | 6.1.1 |
LOADS MODEL FLIGHT TEST VALIDATION BY MEANS OF INNOVATIVE, PHOTOGRAMMETRY BASED, DEFORMATION MEASUREMENT TECHNIQUE. I. Ruiz Juretschke¹, B. Villalta Oliveira¹, R. Bancalero Santolaya¹; ¹Airbus Defense and Space, Spain | ||||
11:20 | 11:50 | 6.1.2 |
UPDATING OF AIRCRAFT STRUCTURE DYNAMIC MODEL TO GROUND VIBRATION TEST RESULTS J. Cecrdle, Aeronautical Research and Test Institute (VZLU), Czech Republic | ||||
11:50 | 12:20 | 6.1.3 |
NUMERICAL SIMULATION AND WIND TUNNEL TESTING OF FLUTTER ABOUT AN ALL- MOVABLE HORIZONTAL TAIL AT TRANSONIC SPEEDS W. Qian¹, G. Yang², G. Zheng², G. Zhang¹; ¹Shenyang Aircraft Design & Research Institute, China ;²Institute of Mechanics, Chinese Academy of Science, China |
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10:50 | 11:20 | 7.1.1 |
CFD DESIGN AND ANALYSIS OF A COMPACT SINGLE-SPOOL COMPRESSOR FOR A HEAVY TRANSPORT HELICOPTER'S POWERPLANT A. Startsev¹, Y. Fokin¹, E. Steshakov¹; ¹Central Inst of Aviation Motors, Russia | ||||
11:20 | 11:50 | 7.1.2 |
VARIATION OF UNSTEADY FLOW PATTERN IN COMPRESSORS PRECEDING THE LOSS OF GASDYNAMIC STABILITY. EXPERIMENT. N.N. Ledovskaya, Central Institute of Aviation Motors, Russia | ||||
11:50 | 12:20 | 7.1.3 |
AERODYNAMIC DESIGN AND OPTIMIZATION OF BLADE CONFIGURATION IN AN INLET STAGE OF AN AIRCRAFT ENGINE COMPRESSOR O. Marakueva, Baltic State Technical University, Russia |
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10:50 | 11:20 | 8.1.1 |
THE WAYS FOR IMPROVEMENT OF AGREEMENT BETWEEN IN-FLIGHT AND GROUND-BASED SIMULATION FOR EVALUATION OF HANDLING QUALITIES AND PILOT TRAINING A.V. Efremov¹, A.V. Koshelenko¹, M.S. Tjaglik¹, A.S. Tjaglik¹; ¹Moscow aviation institute, Russia | ||||
11:20 | 11:50 | 8.1.2 |
REFINEMENT OF THE MODEL OF PILOT PERCEPTION OF AIRCRAFT MOTION IN UPSET CONDITIONS UTILIZING FLIGHT TESTS RESULTS V.V. Rogozin¹, S.A. Zuev¹, M.A. Grigoryev¹, L.E. Zaichik², Y.P. Yashin²; ¹GFRI, Russia ;²TsAGI, Russia | ||||
11:50 | 12:20 | 8.1.3 |
EVALUATIONS OF FLYING QUALITIES FOR A NEW AND AN AGING TRANSPORT AIRCRAFT IN SEVERE ATMOSPHERIC TURBULENCE R.C. Chang, China University of Science and Technology, Taiwan; C.E. Lan, University of Kansas, United States; W.-L. Guan, Aviation Safety Council, Taiwan |
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10:50 | 11:20 | 9.1.1 |
DESIGN AND FLIGHT TEST OF A SOLAR-POWERED UNMANNED AIR VEHICLE FOR LONG ENDURANCE Z. Lei¹, H. Kawamura¹; ¹Tokyo University of Science, Suwa, Japan | ||||
11:20 | 11:50 | 9.1.2 |
OPTIMAL CONTROL SURFACE MIXING OF A RHOMBOID WING UAV E. Miles, University of Pretoria, South Africa; B.A. Broughton, Incomar Aeronautic, South Africa | ||||
11:50 | 12:20 | 9.1.3 |
PREDICTED FLIGHT CHARACTERISTICS OF THE INVERTED JOINED WING SCALED DEMONSTRATOR M. Lis¹, A. Dziubinski¹, C. Galinski¹, G. Krysztofiak¹, P. Ruchala¹, K. Surmacz¹; ¹Instytut Lotnictwa, Poland |
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10:50 | 11:20 | 10.1.1 |
POLARIMETRIC AVIONIC WEATHER RADAR FOR INCREASING FLIGHT SAFETY AND EFFICIENCY A. Lupidi¹, S. Lischi¹, F. Berizzi¹, M. Martorella¹, F. Cuccoli¹; ¹CNIT - RaSS, Italy | ||||
11:20 | 11:50 | 10.1.2 |
AN INTELLIGENT ICE PROTECTION SYSTEM FOR NEXT GENERATION AIRCRAFT TRAJECTORY OPTIMISATION A. Shinkafi¹, C. Lawson¹, R. Seresinhe¹, D. Quaglia¹, I. Madani¹; ¹Cranfield University, United Kingdom | ||||
11:50 | 12:20 | 10.1.3 |
AIRFRAME SYSTEMS POWER OFF-TAKE MODELLING IN MORE-ELECTRIC LARGE AIRCRAFT FOR USE IN TRAJECTORY OPTIMISATION R. Seresinhe¹, C. Lawson¹, A. Shinkafi¹, D. Quaglia¹, I. Madani¹; ¹Cranfield University, United Kingdom |
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10:50 | 11:20 | 11.1.1 |
A SELF-SEPARATION ALGORITHM USING SPEED CONTROL FOR WIDTH-LIMITED HIGH DENSITY AIR CORRIDOR Y. Nakamura, Electronic Navigation Research Institute, Japan; N. Takeichi¹, K. Fukuoka¹; ¹Nagoya University, Japan | ||||
11:20 | 11:50 | 11.1.2 |
EVALUATING TEMPORAL INTEGRATION OF EUROPEAN AIR TRANSPORT S. Lehner¹, K. Kölker¹, K. Lütjens¹; ¹German Aerospace Center (DLR), Germany | ||||
11:50 | 12:20 | 11.1.3 |
COLLISION RISK STUDIES WITH 6DOF FLIGHT SIMULATIONS WHEN AERODROME OBSTACLE STANDARDS CANNOT BE MET A. De Marco¹, J. D\'Auria¹; ¹University of Naples Federico II, Italy |
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10:50 | 11:20 | 12.1.1 |
IMPROVING CONTROL RELIABILITY AND QUALITY OF AIRCRAFT ENGINES BY MEANS THE SOFTWARE «VIRTUAL ENGINE» F.D. Golberg¹, O.S. Gurevich¹, A.A. Petukhov¹; ¹CIAM, Russia | ||||
11:20 | 11:50 | 12.1.2 |
CONCEPTS AND TECHNOLOGIES FOR THE NEXT GENERATION OF LARGE CIVIL AIRCRAFT ENGINES F. Haselbach¹, A. Newby¹, R. Parker¹; ¹Rolls-Royce, United Kingdom |
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13:10 | 13:40 | 1.2.1 |
BLACK-BOX MODEL EPISTEMIC UNCERTAINTY AT EARLY DESIGN STAGE. AN AIRCRAFT POWER-PLANT INTEGRATION CASE STUDY A. Molina-Cristobal¹, M. Nunez¹, M.D. Guenov¹, T. Laudan², T. Druot²; ¹Cranfield University, United Kingdom ;²Airbus Operations S.A.S, France | ||||
13:40 | 14:10 | 1.2.2 |
AIRCRAFT CONFIGURATION ANALYSIS USING A LOW-FIDELITY, PHYSICS BASED AEROSPACE FRAMEWORK UNDER UNCERTAINTY CONSIDERATIONS T. Pfeiffer¹, E. Moerland¹, D. Böhnke¹, B. Nagel¹, V. Gollnick¹; ¹German Aerospace Center, Germany | ||||
14:10 | 14:40 | 1.2.3 |
FORMULATION OF AN EXPERIMENT SELECTION METHODOLOGY FOR UNCERTAINTY REDUCTION AND APPLICATION TO ACTIVE FLOW CONTROL R.B. Jacobs¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States |
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13:10 | 13:40 | 2.2.1 |
ON THE USE OF THE ADJOINT METHOD TO COMPUTE NON--GEOMETRIC SENSITIVITIES M. Hayashi, University of São Paulo, Brazil | ||||
13:40 | 14:10 | 2.2.2 |
CFD-BASED COLLABORATIVE DESIGN OPTIMIZATION USING ECFD B.I. Soemarwoto¹, A. Nugroho, Regio Aviasi Industri, Indonesia; E.H. Baalbergen¹, A. Aribowo, National Institute of Aeronautics and Space LAPAN, Indonesia; ¹National Aerospace Laboratory NLR, Netherlands | ||||
14:10 | 14:40 | 2.2.3 |
AERODYNAMIC DESIGN METHOD FOR SUPERSONIC SLENDER BODY USING AN INVERSE PROBLEM K. Matsushima¹, I. Yamamichi¹, N. Tokugawa, JAXA, Japan; ¹University of Toyama, Japan |
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13:10 | 13:40 | 3.2.1 |
AERODYNAMICS VIA AEROACOUSTICS – THE CASE FOR CIRCULATION CAPTURE M.P. Brandão, ITA, Brazil | ||||
13:40 | 14:10 | 3.2.2 |
ON THE INTERAL STRUCTURAL OF SHOCK WAVE IN RELAXING GAS L.M.B.C Campos¹, F.S. Cunha¹; ¹Instituto Superior Técnico, Universidade de Lisboa, Portugal | ||||
14:10 | 14:40 | 3.2.3 |
RANS MODELING FOR FLOWS ON RIBLETS BASED ON EXPERIMENTAL DATA K. Okabayashi¹, T. Matsue², M. Asai², H. Naito¹; ¹Japan aerospace exploration agency, Japan ;²Tokyo metropolitan university, Japan |
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13:10 | 13:40 | 4.2.1 |
STUDY ON PERFORMANCE AND FLOW CHARACTERISTICS FOR EMBEDDED DISTRIBUTED PROPULSION SYSTEM S. Lee, Hanyang University, South Korea | ||||
13:40 | 14:10 | 4.2.2 |
THE EFFECT OF PYLON TRAILING EDGE BLOWING ON THE PERFORMANCE AND NOISE PRODUCTION OF A PROPELLER L.L.M. Veldhuis¹, T. Sinnige¹; ¹Delft University of Technology, Netherlands | ||||
14:10 | 14:40 | 4.2.3 |
QUASI-ANALYTICAL AERODYNAMIC METHODS FOR PROPULSIVE FUSELAGE CONCEPTS S. Kaiser¹, R. Grenon², J. Bijewitz¹, A. Prendinger¹, O. Atinault², A.T. Isikveren¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany ;²ONERA, The French Aerospace Lab, France |
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13:10 | 13:40 | 5.2.1 |
INVESTIGATION OF MULTI-MATERIAL LAMINATES FOR SMART DROOP NOSE DEVICES M. Kintscher¹, S. Geier¹, H.P. Monner¹, M. Wiedemann¹; ¹DLR, Germany | ||||
13:40 | 14:10 | 5.2.2 |
DEFINITION OF THE BOLT SHEARING LOAD IN MULTIPLE-ROWMETAL COMPOSITE JOINTS Y.S. Borovskaya¹, M.A. Glebova¹, V.I. Grishin¹; ¹TsAGI, Russia | ||||
14:10 | 14:40 | 5.2.3 |
LOW-COST TITANIUM ALLOYS FOR TITANIUM-POLYMER LAYERED COMPOSITES P. Panin¹, N. Nochovnaya¹, D. Kablov¹, E. Alexeev¹; ¹FSUE VIAM, Russia |
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13:10 | 13:40 | 6.2.1 |
MULTI-TERRAIN IMPACT SIMULATIONS OF A CRASHWORTHY COMPOSITE HELICOPTER SUBFLOOR T. Billac¹, M. David², M. Battley, Center for Advanced Composite Materials, New Zealand; R. Thomson, Advanced Composite Structures Australia, CRC-ACS, Australia; C. Kindervater², R. Das¹; ¹The University of Auckland, New Zealand ;²German Aerospace Center, Germany | ||||
13:40 | 14:10 | 6.2.2 |
FOD CHARACTERISTICS OF TITANIUM METAL MATRIX COMPOSITE (TMC) TO APPLY AIRCRAFT LANDING GEAR STRUCTURE N. Takahashi¹, T. Sato¹, K. Fujiwara¹, T. Yokozeki, The University of Tokyo, Japan; A. Yoshimura², H. Shouji²; ¹Sumitomo Precision Products Co., Ltd., Japan ;²Japan Aerospace Exploration Agency, Japan | ||||
14:10 | 14:40 | 6.2.3 |
NUMERICAL SIMULATION OF BIRD STRIKE IN AIRCRAFT LEADING EDGE STRUCTURE USING A NEW DYNAMIC FAILURE MODEL Q. Sun¹, Y.J. Liu¹, R.H. Jin¹; ¹School of Aeronautics, Northwestern Polytechnical University, China |
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13:10 | 13:40 | 7.2.1 |
ANALYSIS OF THE PREDICTION ABILITY OF REACTION MECHANISMS FOR CFD MODELING OF THE COMBUSTION IN HIGH VELOCITY ENGINES V. Kopchenov¹, S. Batura¹, L. Bezgin¹, N. Titova¹, A. Starik¹; ¹CIAM, Russia | ||||
13:40 | 14:10 | 7.2.2 |
PHYSICAL INSIGHT INTO FUEL MIXING ENHANCEMENT WITH BACKWARD-FACING STEP FOR SCRAMJET ENGINES VIA MULTI-OBJECTIVE DESIGN OPTIMIZATION H. Ogawa, RMIT University, Australia; C.Y. Wen, The Hong Kong Polytechnic University, Hong Kong SAR of China; Y.C. Chang, National Cheng Kung University, Taiwan | ||||
14:10 | 14:40 | 7.2.3 |
STUDIES ON POSSIBLE UNIFICATION OF ENGINES FOR ADVANCED SMALL AND MEDIUM SUPERSONIC CIVIL AEROPLANES A. Mirzoyan¹, A. Evstigneev¹; ¹Central Institute of Aviation Motors (CIAM), Russia |
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13:10 | 13:40 | 8.2.1 |
DEVELOPMENT OF LOW-LEVEL TURBULENCE ADVISORY SYSTEM FOR AIRCRAFT OPERATION N. Matayoshi¹, T. Iijima¹, E. Yoshikawa¹, T. Ushio, Osaka University, Japan; ¹JAXA, Japan | ||||
13:40 | 14:10 | 8.2.2 |
DYNAMIC WAKE VORTEX SEPARATION COMBINING WITH TRAFFIC OPTIMIZATION N. Matayoshi, JAXA, Japan | ||||
14:10 | 14:40 | 8.2.3 |
WAKE VORTEX OBSERVATION CAMPAIGN BY ULTRA FAST-SCANNING LIDAR IN NARITA AIRPORT, JAPAN E. Yoshikawa¹, N. Matayoshi¹; ¹JAXA, Japan |
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13:10 | 13:40 | 9.2.1 |
AERODYNAMIC MODEL IDENTIFICATION FROM FLIGHT DATA FOR A NOVEL CONCEPT SCALED UAV Z.-X. Yao, SADRI, China | ||||
13:40 | 14:10 | 9.2.2 |
CONCEPTUAL DESIGN OF AIRCRAFT FOR OPTIMAL MANEUVERS N. K. SINHA, IIT-Madras, India | ||||
14:10 | 14:40 | 9.2.3 |
FLIGHT DYNAMICS OF HIGHLY FLEXIBLE SOLAR-POWERED UAV BASED ON GEOMETRICALLY NONLINEAR INTRINSIC BEAM R. Wang¹, Z. Zhou¹, X. Zhu, Institute of UAV, Northwestern Polytechnical University, China; X. Xu¹; ¹Science and Technology on UAV Laboratory, Northwestern Polytechn, China |
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13:10 | 13:40 | 10.2.1 |
UAV REMOTE POWER SUPPLY SYSTEM BY LASER RADIATION O.V. Zayats¹, V.Y. Tugaenko¹, V.P. Khvostikov, Ioffe Physico-Technical Institute, Russia; ¹S.P. Korolev Rocket And Space Corporation \\\\\\\\, Russia | ||||
13:40 | 14:10 | 10.2.2 |
EXPERIMENTAL VALIDATION OF A SENSORIZED RING BASED ON OPTICAL FIBER FOR STRAIN MONITORING OF MORPHING STRUCTURE M. Ciminello¹, P. Bettini², S. Ameduri¹, E. Guerreschi², G. Cuneo²; ¹CIRA, Italy ;²Politecnico di Milano, Italy | ||||
14:10 | 14:40 | 10.2.3 |
DEVELOPMENT OF A HYBRID ICE PROTECTION SYSTEM BASED ON NANOSTRUCTURED HYDROPHOBIC SURFACES T. Strobl¹, S. Storm¹, M. Kolb¹, J. Haag¹, M. Hornung, Technical University of Munich, Germany; ¹Airbus Group Innovations, Germany |
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13:10 | 13:40 | 11.2.1 |
OPTIMAL PUSHBACK TIME WITH EXISTING UNCERTAINTIES AT BUSY AIRPORT R. Mori, Electronic Navigation Research Institute, Japan | ||||
13:40 | 14:10 | 11.2.2 |
TERMINAL HOLDING TIME OPTIMIZATION BY DYNAMIC CDA ROUTING ALGORITHM S.M. Malaek¹, F. Enayatollahi¹, J. Parastari, Civil Aviation Technology College, Iran; ¹Sharif University of Technology, Iran |
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13:10 | 13:40 | 12.2.1 |
NUMERICAL MODELING OF FLOW IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS F.A. Slobodkina¹, V.V. Malinin¹, A.I. Tarasov, Lulka RDC, Russia; ¹Gubkin Russian State University of Oil and Gas, Russia | ||||
13:40 | 14:10 | 12.2.2 |
SENSITIVITY ANALYSIS OF TURBINE ENGINE SUSTAINMENT E.E. Iglesias¹, H. Millwater¹; ¹University of Texas at San Antonio, United States |
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15:00 | 15:30 | 1.3.1 |
THEORETICAL FRAMEWORK OF SYSTEMS DESIGN FOR THE AIR TRANSPORTATION SYSTEM INCLUDING AN INHERENTLY QUANTITATIVE PHILOSOPHY OF SCENARIO DEVELOPMENT R. Ghosh¹, T. Schilling¹, K. Wicke¹; ¹German Aerospace Center, Germany | ||||
15:30 | 16:00 | 1.3.2 |
EXPLICIT MODELING OF TECHNOLOGY IMPROVEMENT OVER TIME IN CONCEPTUAL AIRCRAFT DESIGN D. Böhnke¹, B. Nagel¹, V. Gollnick¹; ¹DLR e.V., Germany | ||||
16:00 | 16:30 | 1.3.3 |
KNOWLEDGE DISCOVERY IN CONCEPTUAL DESIGN OF SPACE PLANES USING MULTI-OBJECTIVE OPTIMIZATION AND DATA MINING T. Fujikawa, The University of Tokyo, Japan | ||||
16:30 | 17:00 | 1.3.4 |
MULTIDISCIPLINARY OPTIMIZATION OF TRUSS-BRACED WING LAYOUT K.-S. Zhang¹, A. Bakar¹, P.-B. Ji¹, Z.-H. Han¹, X.-P. Li¹; ¹Northwestern Polytechnical University, China |
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15:00 | 15:30 | 2.3.1 |
EFFICIENT STATIONARY AND NONSTATIONARY AERODYNAMIC CALCULATION ALGORITHMS FOR THE APPLIED AERODYNAMICS PROBLEMS O.V. Karas, TsAGI, Russia | ||||
15:30 | 16:00 | 2.3.2 |
COMMUTER AIRCRAFT AERODYNAMIC DESIGN: WIND-TUNNEL TESTS AND CFD ANALYSIS F. Nicolosi¹, S. Corcione¹, P. Della Vecchia¹; ¹UNIVERSITY OF NAPLES FEDERICO II, Italy | ||||
16:00 | 16:30 | 2.3.3 |
AERODYNAMIC INTERFERENCE OF WINGTIP AND WING DEVICES ON BWB MODEL H.D. Ceron-Munoz¹, D.O. Diaz-Izquierdo, São Carlos Engineering School-University of São Paulo-Brazil, Brazil; J. Solarte-Pineda¹, F.M. Catalano¹; ¹São Carlos Engineering School-University of São Paulo, Brazil | ||||
16:30 | 17:00 | 2.3.4 |
COMPUTATIONAL INVESTIGATION OF SIMULATION ON THE DYNAMIC DERIVATIVES OF FLIGHT VEHICLE B.-G. Mi¹, H. Zhan¹, B. Wang¹; ¹Northwestern Polytechnical University, China |
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15:00 | 15:30 | 3.3.1 |
PIV INTRODUCED EXPERIMENTAL INVESTIGATION OF COUNTERFLOW EJECTION ON BLUNT BODY MOVING WITH SUPERSONIC SPEED Y.Y. Zheng, University of New South Wales, Australia | ||||
15:30 | 16:00 | 3.3.2 |
HYPERSONIC FLOWFIELD AND HEAT FLUX PECULIARITIES ON THE NEW SPACE LAUNCHER WITH WINGED REUSABLE FIRST STAGE. S.M. Drozdov¹, V.N. Brazhko¹, V.E. Mosharov¹, A.S. Skuratov¹, D.S. Fedorov², V.V. Gorbatenko², P.A. Lehov², J.N. Chibisov²; ¹TsAGI, Russia ;²KSRPSC, Russia | ||||
16:00 | 16:30 | 3.3.3 |
THE FLOW IN THE PLANE OF SYMMETRY OF THE DELTA WING IN THE REGIME OF STRONG VISCOUS-INVISCID INTERACTION. G.N. Dudin, Central Aerohydrodynamic Institute (TsAGI), Russia |
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15:00 | 15:30 | 4.3.1 |
EFFECT OF ANGLE OF ATTACK KINEMATICS ON PASSIVE FLAPPING FOIL POWER GENERATION J. Young¹, J.C.S. Lai¹; ¹University of New South Wales, Australia | ||||
15:30 | 16:00 | 4.3.2 |
COMPUTATIONAL ANALYSIS FOR FLAPPING WING BY COUPLED CFD AND CSD SOLUTIONS N. Lee¹, S. Lee¹, H. Cho², J.-Y. Kwak, Korea Aerospace Research Institute, South Korea; S.J. Shin²; ¹Inha University, South Korea ;²Seoul National University, South Korea | ||||
16:00 | 16:30 | 4.3.3 |
INVESTIGATION OF AIRFOIL FOR AN INSECT-SIZED FLAPPING WING H. Nagai¹, K. Isogai¹, N. Uda¹, K. Ono¹; ¹Kyushu University, Japan | ||||
16:30 | 17:00 | 4.3.4 |
AERODYNAMIC RESEARCH OF FLEXIBLE FLAPPING WING BY COMBINING DIC AND CFD APPROACHES W. Yang¹, B. Song¹, W. Song¹, L. Wang¹, P. Fu¹, J. Xu¹; ¹Northwestern Polytechnical University, China |
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15:00 | 15:30 | 5.3.1 |
INFLUENCE OF WING ASPECT RATIO ON PASSIVE STALL CONTROL AT LOW REYNOLDS NUMBER USING SINUSOIDAL LEADING EDGES A. Esmaeili¹, J.M.M. Sousa¹; ¹IDMEC - Instituto Superior Tecnico, Portugal | ||||
15:30 | 16:00 | 5.3.2 |
A NOVEL CONCEPTIONS OF PLASMA GURNEY FLAP L.-H. Feng¹, J.-J. Wang¹, K.-S. Choi, University of Nottingham, United Kingdom; ¹Beijing University of Aeronautics and Astronautics, China | ||||
16:00 | 16:30 | 5.3.3 |
THE EFFICIENCY ANALYSIS OF GUST ALLEVIATION BASED ON ACTIVE FLOW CONTROL X. XU¹, Z. ZHOU¹, R. WANG¹; ¹Northwestern Polytechnical University, China | ||||
16:30 | 17:00 | 5.3.4 |
COMPUTATIONAL EVALUATION OF FLOW CONTROL FOR ENHANCED CONTROL AUTHORITY OF A VERTICAL TAIL A. Shmilovich¹, Y. Yadlin¹, E. Whalen¹; ¹The Boeing Company, United States |
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15:00 | 15:30 | 6.3.1 |
DYNAMIC RESPONSE OF AN AIRPLANE ELASTIC STRUCTURE IN TRANSONIC FLOW S. Kuzmina¹, F. Ishmuratov¹, O. Karas¹, A. Chizhov¹; ¹TsAGI, Russia | ||||
15:30 | 16:00 | 6.3.2 |
FE-MODELLING GUIDELINES FOR THE DIMENSIONING OF AIRCRAFT CABIN INTERIOR UNDER STATIONARY DYNAMIC LOADS R. Seemann¹, B. Plaumann¹, J. Oltmann¹, D. Krause¹; ¹TUHH, Institute PKT, Germany | ||||
16:00 | 16:30 | 6.3.3 |
FLIGHT LOADS ESTIMATION USING LOCAL MODEL NETWORKS M. Halle¹, F. Thielecke¹; ¹TUHH/FST, Germany | ||||
16:30 | 17:00 | 6.3.4 |
THE DIRECT PREDICTION OF BUCKLING LOADS OF SHELLS UNDER AXIAL COMPRESSION USING VCT - TOWARDS AN UPGRADED APPROACH E.L. Jansen¹, H. Abramovich, Technion, I.I.T., Israel; R. Rolfes¹; ¹Leibniz Universitaet Hannover, Germany |
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15:00 | 15:30 | 7.3.1 |
MECHANISMS OF POLLUTANT FORMATION IN THE H2 - FUELLED COMBUSTOR OF HIGH VELOCITY AIR-BREATHING ENGINE: MODELING STUDY L. Bezgin¹, V. Kopchenov¹, N. Titova¹, A. Starik¹; ¹CIAM, Russia | ||||
15:30 | 16:00 | 7.3.2 |
DESIGN OF SUPERSONIC EJECTION SYSTEM FOR HIGH SPEED COMBUSTION INVESTIGATION AND RESULTS OF WIDE RANGE COMBUSTION CHAMBER TESTS V. Avrashkov, MAI, Russia; M. Boucheze¹, S. Balland¹; ¹MBDA-France, France | ||||
16:00 | 16:30 | 7.3.3 |
MODERN RESEARCH AREAS OF SOLID HYPERSONIC RAMJET ENGINES V.M. Abashev¹, A.G. Prudnikov¹, E.E. Son¹; ¹Moscow Aviation Institute, Russia | ||||
16:30 | 17:00 | 7.3.4 |
HEAT FLUX LEVEL DETERMINATION IN MODEL COMBUSTION CHAMBER OF HIGH-SPEED RAMJET ENGINE M. Danilov¹, M. Frantsuzov¹, N. Kukshinov¹; ¹Central Institute of Aviation Motors, Russia |
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15:00 | 15:30 | 8.3.1 |
NEURAL NETWORK ADAPTIVE SEMI-EMPIRICAL MODELS FOR AIRCRAFT CONTROLLED MOTION M.V. Egorchev¹, D.S. Kozlov¹, Y.V. Tiumentsev¹; ¹Moscow Aviation Institute (MAI), Russia | ||||
15:30 | 16:00 | 8.3.2 |
A COMPARISON OF TECHNIQUES TO GET SPARSE RATIONAL APPROXIMATIONS FOR LINEAR FRACTIONAL REPRESENTATIONS C. Roos¹, G. Hardier¹, C. Döll¹; ¹ONERA/DCSD, France | ||||
16:00 | 16:30 | 8.3.3 |
AIRCRAFT PARAMETER IDENTIFICATION USING GENTIC ALGORITHMS M. Ulinowicz¹, J. Narkiewicz¹; ¹Warsaw University of Tchnology, Poland | ||||
16:30 | 17:00 | 8.3.4 |
APPROACHES FOR FLIGHT TESTS AIRCRAFT PARAMETER IDENTIFICATION O.N. Korsun, State Institute of Aviation Systems, Russia; B.K. Poplavsky, Gromov Flight Research Institute, Russia |
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15:00 | 15:30 | 9.3.1 |
KINEMATIC AND UNSTEADY AERODYNAMIC MODELLING OF FLAPPING BI- AND QUAD-WING ORNITHOPTER H. Djojodihardjo¹, M. Anas Bin Abd Bari¹; ¹Universiti Putra Malaysia, Malaysia | ||||
15:30 | 16:00 | 9.3.2 |
APPLICATION OF ARTIFICIAL NEURAL NETWORK IN MODELING OF ENTOMOPTER DYNAMICS P. Czekalowski, Institute of Aviation, Poland; K.-S. Sibilski¹, A. Zyluk¹; ¹Air Force Institute of Technology, Poland | ||||
16:00 | 16:30 | 9.3.3 |
IDENTIFICATION AND TRACKING CONTROL OF FLAPPING MOTIONS IN ROBOTIC BATS J. Dadashi, Virginia Polytechnic Institute and State University, United States | ||||
16:30 | 17:00 | 9.3.4 |
DEVELOPMENT OF A MULTI-PURPOSE UAV WITH BIO-INSPIRED FEATURES R.K. Rangel, BRVANT / BRV UAV& Flight Systems , Brazil; K.H. Kienitz¹, M.P. Brandão¹; ¹Technological Institute of Aeronautics - ITA, Brazil |
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15:00 | 15:30 | 10.3.1 |
ADVANCED AVIONICS EQUIPMENT ON THE BASIS OF SECOND GENERATION INTEGRATED MODULAR AVIONICS G.A. Chuyanov¹, V.V. Kosyanchuk¹, N.I. Selvesyuk¹, E.Y. Zybin¹; ¹State Research Institute of Aviation Systems, Russia | ||||
15:30 | 16:00 | 10.3.2 |
INTEGRATED ONBOARD NETWORKING FOR IMA2G Y. Sheynin¹, E. Suvorova¹, V. Bukov², V. Shurman²; ¹Saint-Petersburg State University of Aerospace Instrumentation, Russia ;²PLC Scientific and Research Institute of Avionic Equipment, Russia | ||||
16:00 | 16:30 | 10.3.3 |
METHOD OF SEARCHING FOR ROUTES WITH DELAY AND JITTER LIMITATION N. Matveeva, Saint-Petersburg State University of Aerospace Instrumentation, Russia | ||||
16:30 | 17:00 | 10.3.4 |
TOOLSET FOR ONBOARD NETWORKS DESIGN AND CONFIGURATION Y. Sheynin¹, E. Suvorova¹, A. Syschikov¹, B. Sedov¹, N. Matveeva¹, D. Raszhivin¹; ¹SUAI, Russia |
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15:00 | 15:30 | 11.3.1 |
A COMPARISON OF THE TWO ARRIVAL TRAFFIC SYNCHRONIZATION CONCEPTS ENVISIONED FOR NEXTGEN AND SESAR. J. Crespo¹, C. Cuerno¹, R.M. Arnaldo¹, J. Saez Nieto¹, M. Sadornil¹, J. Pérez¹, R. Barragan, CRIDA, Spain; ¹Technical University of Madrid (UPM), Spain | ||||
15:30 | 16:00 | 11.3.2 |
VALIDATION AND SIMULATION STUDY OF THE ARRIVAL MERGING PROCEDURE MODEL K. Kageyama, ENRI, Japan; B. Park, KOTI, South Korea | ||||
16:00 | 16:30 | 11.3.3 |
OPTIMISED ALGORITHMS FOR EXTENDED ARRIVAL MANAGERS R. Barragan, CRIDA, Spain; J.A. Perez Castan¹, M. Sadornil¹, F. Saez Nieto¹, J. Crespo¹, R. Arnaldo¹, C. Cuerno¹; ¹UPM, Spain | ||||
16:30 | 17:00 | 11.3.4 |
TRAJECTORY PREDICTION PERFORMANCE COMPARISON TOWARDS EFFICIENT TIME-BASED METERING OPERATIONS G. Enea, Engility Corporation, United States; G. McDonald¹, J. Bronsvoort¹; ¹AirServices Australia, Australia |
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15:00 | 15:30 | 12.3.1 |
RESEARCH OF EFFICIENCY OF THE MID-FLIGHT POWER PLANT BASED ON THE HYBRID ENGINES FOR ADVANCED AIRLINERS P. Ryabov, CIAM, Russia | ||||
15:30 | 16:00 | 12.3.2 |
THE HYBRID PROPULSION SYSTEMS FOR THE ADVANCED AIRCRAFT A.V. Lukovnikov¹, O.D. Selivanov¹, P.A. Ryabov¹, Y.A. Ezrokhi¹, S.M. Kalensky¹; ¹CIAM, Russia | ||||
16:00 | 16:30 | 12.3.3 |
INVESTIGATION OF UNIVERSALLY ELECTRIC PROPULSION SYSTEMS FOR TRANSPORT AIRCRAFT P.C. Vratny¹, P. Forsbach¹, A. Seitz¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany | ||||
16:30 | 17:00 | 12.3.4 |
ANALYSIS OF POSSIBILITIES TO APPLY ELECTRIC TECHNOLOGIES FOR HELICOPTER PROPULSION SYSTEM O. Gurevich¹, A. Lukovnikov¹, A. Gulienko¹, V. Zakharchenko¹, I. Kovalenko¹, P. Suntsov¹; ¹CIAM, Russia |
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10:00 | 10:30 | 1.4.1 |
A CONCEPTUAL DESIGN AND ANALYSIS METHOD FOR CONVENTIONAL AND UNCONVENTIONAL AIRPLANES R. Elmendorp¹, R. Vos¹, G. La Rocca¹; ¹TU Delft, Netherlands | ||||
10:30 | 11:00 | 1.4.2 |
SET-BASED DESIGN SPACE EXPLORATION ENABLED BY DYNAMIC CONSTRAINT ANALYSIS J.R. Kizer¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
11:00 | 11:30 | 1.4.3 |
DESIGN AND OPTIMIZATION OF AIRCRAFT ASSEMBLING BASED ON COMPREHENSIVE SIMULATION OF MANUFACTURING PROCESSES A.V. Rozhdestvensky¹, O.S. Samsonov¹; ¹“MATI” – Russian State University of Aviation Technology, Russia | ||||
11:30 | 12:00 | 1.4.4 |
MULTI-CRITERIAL AERODYNAMIC SYNTHESIS METHOD OF MISSION-ORIENTED AIRCRAFT DESIGN S. Kachel, Faculty of Mechatronics and Av/Military University of Technology, Poland |
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10:00 | 10:30 | 2.4.1 |
URBAN WIND FIELD GENERATION USING LES FOR APPLICATION TO QUADROTOR FLIGHT M. Sutherland¹, J. Etele¹; ¹Carleton University, Canada | ||||
10:30 | 11:00 | 2.4.2 |
NUMERICAL SIMULATION OF SELF-PROPELLED FLYING OF A THREE-DIMENSIONAL BIRD WITH FLAPPING WINGS C.-J. WU¹, L.-L. ZHU¹; ¹School of Aeronautics and Astronautics, DUT, China | ||||
11:00 | 11:30 | 2.4.3 |
FLUID DYNAMICS ANALYSIS OF A COUNTER ROTATING DUCTED PROPELLER C. Xu¹, C. Bil¹, C.P. Cheung¹; ¹RMIT University, Australia | ||||
11:30 | 12:00 | 2.4.4 |
COMPUTATIONAL COMPARATIVE STUDY FOR DESIGN OF LOW REYNOLDS NUMBER AIRFOIL K. Kondo, Tokyo University of Science, Japan |
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10:00 | 10:30 | 3.4.1 |
FLOW FIELD AROUND DIMPLED SHORT PIN-FINS IN A STAGGERED ARRAY S.M. Roux¹, G.I. Mahmood¹, J.P. Meyer¹; ¹University of Pretoria, South Africa | ||||
10:30 | 11:00 | 3.4.2 |
AN OVERVIEW OF RECENT EXPERIMENTAL STUDIES CONDUCTED IN ONERA S3CH TRANSONIC WIND TUNNEL R. Bur¹, V. Brion¹, P. Molton¹; ¹ONERA, France | ||||
11:00 | 11:30 | 3.4.3 |
THE EFFECT OF A SYNTHETIC JET ON THE PRESSURE DISTRIBUTION OF A FLAT PLATE Y.-H. Kim, Emirates Aviation University, United Arab Emirates; K.P. Garry, Cranfield University, Germany | ||||
11:30 | 12:00 | 3.4.4 |
EXPERIMENTAL RESEARCH ON FLOW SEPARATION CONTROL USING SYNTHETIC JET ACTUATORS E. Koopmans¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands |
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10:00 | 10:30 | 4.4.1 |
AERODYNAMIC MODELLING OF A REFUELLING BOOM L. Manfriani¹, M. Righi¹; ¹ZHAW, Switzerland | ||||
10:30 | 11:00 | 4.4.2 |
TRANSONIC AIRFOILS, WINGS, AND PROJECTILES ADMITTING ANOMALOUS BEHAVIOR OF AERODYNAMIC COEFFICIENTS A. Kuzmin¹, A. Ryabinin¹; ¹St. Petersburg State University, Russia | ||||
11:00 | 11:30 | 4.4.3 |
TRANSONIC STORE SEPARATION ANALYSES USING MODERN DESIGN OF EXPERIMENTS AND QUANTITATIVE GRADING OF RESULTS K.A. Jamison, Council of Scientific and Industrial Research, South Africa |
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10:00 | 10:30 | 5.4.1 |
EXPERIMENTAL EVALUATION OF THE EFFICIENCY OF GAS TURBINE ENGINE PARTS DAMPING WITH DRY FRICTION DAMPERS USING LASER VIBROMETER A. Balakirev¹, B. Bolotov¹, A. Golovkin¹, M. Nikhamkin¹, N. Sazhenkov¹, L. Voronov¹, I. Konev¹; ¹Perm National Research Polytechnic University, Russia | ||||
10:30 | 11:00 | 5.4.2 |
PROBLEM OF LOW CYCLE FATIGUE OF TURBOMACHINES J. Temis¹, K. Azmetov¹, A. Fakeev¹; ¹Central Institute of Aviation Motors, Russia | ||||
11:00 | 11:30 | 5.4.3 |
ANALYSIS AND COUNTERMEASURE ON AERO-ENGINE BLADE DEFECT Z. Sun¹, Z. Guo¹, G. Liu¹; ¹AVIC Xi’an Aero-engine (Group) LTD., China | ||||
11:30 | 12:00 | 5.4.4 |
HIGH TEMPERATURES TURBINE BLADES DAMAGE PREDICTION TAKING INTO ACCOUNT LOADING HISTORY DURING A FLIGHT CYCLE B.E. Vasilyev¹, L.A. Magerramova¹; ¹CIAM, Russia |
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10:00 | 10:30 | 6.4.1 |
STRUCTURE DESIGN AND MECHANICAL SIMULATION ON THE SC-MR SUPPORT FOR ROTOR SYSTEM Y.H. Ma¹, H.X. Zhu¹, J. Hong¹; ¹Beihang University, China | ||||
10:30 | 11:00 | 6.4.2 |
A RAPID ANALYSIS METHODOLOGY FOR EARTH ENTRY VEHICLE DEVELOPMENT S. Perino¹, J. Bayandor¹; ¹Virginia Tech, United States | ||||
11:00 | 11:30 | 6.4.3 |
DESIGN AND PERFORMANCE TEST OF A TWIN-FUSELAGE CONFIGURATION SOLAR-POWERED UAV X.-Z. Gao¹, Z.-X. Hou¹, Z. Guo¹, X.-Q. Chen¹; ¹National University of Defense Technology, China | ||||
11:30 | 12:00 | 6.4.4 |
AN ENGINEERING ANALYSIS METHOD OF POST-BUCKLING FOR COMPOSITE STIFFENED PANELS F.-F. Wang, AMECO, China; D.-G. Cui, AVIC, China |
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10:00 | 10:30 | 7.4.1 |
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF LOADING LEVELS AND DISTRIBUTIONS ON LOW PRESSURE TURBINE PERFORMANCE A.R. Wadia, GE Aviation, United States | ||||
10:30 | 11:00 | 7.4.2 |
ABOUT APPROACHES TO RESEARCH OF FLAT LPT CASCADES AT LOW RE NUMBERS V.D. Venediktov, Central Institute of Aviation Motors, Russia | ||||
11:00 | 11:30 | 7.4.3 |
TURBULENCE MEASUREMENTS IN A FLOW PART OF TURBOMACHINES USING A HIGH-FREQUENCY PRESSURE PROBE A.D. Nepomnyashchiy, Central Institute of Aviation Motors, Russia | ||||
11:30 | 12:00 | 7.4.4 |
MULTIDISCIPLINARY ANALYSIS OF HIGH AND LOW PRESSURE TURBINES ON TRANSITIVE MODES IN THE FLIGHT CYCLE S.V. Kharkovskiy ¹, R.Z. Nigmatullin¹, V.S. Kinzburskiy¹, V.V. Starodubtsev¹; ¹CIAM, Russia |
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10:00 | 10:30 | 8.4.1 |
UPSET RECOVERING SIMULATION TO ENHANCE FLIGHT SAFETY BY ON-GROUND PILOT TRAINING A.G. Bushgens¹, L.E. Zaychik¹, A.N. Khrabrov¹, I.I. Grishin¹, P.A. Desyatnik¹, V.V. Biryukov, FRI, Russia; ¹TsAGI, Russia | ||||
10:30 | 11:00 | 8.4.2 |
EVALUATION OF LANDING CHARACTERISTICS ACHIEVED BY SIMULATIONS AND FLIGHT TESTS ON A SMALL-SCALED MODEL RELATED TO MAGNETICALLY LEVITATED ADVANCED TAKE-OFF AND LANDING OPERATIONS. D. Rohacs, REA-TECH, Hungary; M. Voskuijl, Delft University of Technology, Netherlands; N. Siepenkötter, RWTH Aachen, Germany | ||||
11:00 | 11:30 | 8.4.3 |
NEW FEATURES OF UNGUIDED BODY REENTRY WITH SUBCIRCULAR VELOCITY AND PECULIARITIES OF ITS SIMULATION A.S. Filatyev¹, A.A. Golikov¹; ¹Central Aerohydrodynamic Institute, Russia | ||||
11:30 | 12:00 | 8.4.4 |
COMPUTATIONAL INVESTIGATION OF UNSTEADY AERODYNAMIC CHARACTERISTICS OF A MODERN AIRLINER A.N. Khrabrov¹, D.A. Kravchenko¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia |
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10:00 | 10:30 | 9.4.1 |
COMPARATIVE ANALYSIS OF RUSSIAN AND WESTERN APPROACHES TO THE PROBLEM OF ALTERNATIVE FUEL USAGE IN AVIATION V.N. Zhuravlev, Moscow Aviation Institute, Russia | ||||
10:30 | 11:00 | 9.4.2 |
CONTROLLED HYDROGEN GENERATOR AND ADDITIONAL SOURCE OF ELECTRICAL CURRENT FOR INDEPENDENT OXYGEN-HYDROGEN POWER PLANTS K.V. Pushkin, Moscow Aviation Institute (National Research University), MAI, Russia | ||||
11:00 | 11:30 | 9.4.3 |
EVALUATION OF EMISSION CHARACTERISTICS OF GAS TURBINE ENGINES USING ALTERNATIVE FUELS A.M. Savel’ev¹, V.A. Skibin¹, A.M. Starik¹; ¹Central Institute of Aviation Motors, Russia |
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10:00 | 10:30 | 10.4.1 |
DADF ( DIGITAL AUTOMATIC DIRECTION FINDER ) M. Mirzaee¹, M. Sam kan, Sattari University, Iran; S. Behroozifar¹; ¹University of Science and Applied of SAMAPARAN, Iran | ||||
10:30 | 11:00 | 10.4.2 |
HIGH ALTITUDE TURBULENCE DETECTION USING AN AIRBORNE DOPPLER LIDAR H. Inokuchi¹, M. Furuta¹, T. Inagaki¹; ¹JAXA, Japan | ||||
11:00 | 11:30 | 10.4.3 |
ABOUT THE CONCEPT OF STRAPDOWN VECTOR AEROGRAVIMETRIC MEASUREMENTS A.A. Afonin¹, A.S. Sulakov¹, G.G. Yamashev¹; ¹MAI, Russia | ||||
11:30 | 12:00 | 10.4.4 |
ON A CONCEPT OF CREATION OF AN AIRPORT ADVANCED SURFACE MOVEMENT AND GROUND CONTROL SYSTEM Konstantin K. Veremeenko, Moscow Aviation Institute (National Research University), Russia |
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10:00 | 10:30 | 11.4.1 |
4D TRAJECTORY BASED OPERATION IN HIGH DENSITY TERMINAL CONTROL AREA CONSIDERING THE UNCERTAINTY OF WEATHER FORECAST DATA A. Tezuka, Waseda University, Japan | ||||
10:30 | 11:00 | 11.4.2 |
THE NETWORK FLOW ENVIRONMENT: SLOT ALLOCATION MODEL EVALUATION WITH CONVECTIVE NOWCASTING A. Lau¹, R. Budde, Advanced Traffic Solutions (ATRiCS), Germany; J. Berling, Technical University of Hamburg (TUHH), Germany; V. Gollnick¹; ¹German Aerospace Center (Air Transportation Systems) , Germany | ||||
11:00 | 11:30 | 11.4.3 |
DEVELOPMENT AND EVALUATION OF LOW-LEVEL TURBULENCE ADVISORY DISPLAY FOR AIRCRAFT OPERATION T. Iijima¹, N. Matayoshi¹, E. Yoshikawa¹; ¹JAXA, Japan | ||||
11:30 | 12:00 | 11.4.4 |
APPLICATION OF SUBOPTIMAL 4-D NAVIGATION ALGORITHMS FOR FLIGHT PLANNING AND CONTROL CONSIDERING WEATHER CONDITIONS N. Grevtsov¹, A. Dymchenko¹; ¹TsAGI, Russia |
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10:00 | 10:30 | 12.4.1 |
AEROELASTIC DAMPING PREDICTIONS FOR MULTISTAGE TURBOMACHINERY APPLICATIONS A. Placzek, Onera, France | ||||
10:30 | 11:00 | 12.4.2 |
STRENGTH RELIABILITY OF TURBINE ROTOR ENSURING BASED ON MULTIDISCIPLINARY OPTIMIZATION A. Salnikov, CIAM, Russia | ||||
11:00 | 11:30 | 12.4.3 |
BIMETALLIC BLISK DESIGN FOR HIGH TEMPERATURE TURBINES OF GAS TURBINE ENGINE OF DIFFERENT APPLICATION L. Magerramova, Central Institute of Aviation Motors, Russia | ||||
11:30 | 12:00 | 12.4.4 |
LIFE VALIDATION STRATEGY A.A. Inozemtsev¹, L.B. Polatidi¹, I.L. Andreychenko¹; ¹Aviadvigatel OJSC, Russia |
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14:00 | 14:30 | 1.5.1 |
A HOLISTIC APPROACH TO HYPERSONIC AIRCRAFT DESIGN: ZEHST (ZERO EMISSION HIGH SPEED TECHNOLOGIES) E. Blanvillain, Airbus Group Innovations, France | ||||
14:30 | 15:00 | 1.5.2 |
THE LAPCAT-MR2 HYPERSONIC CRUISER CONCEPT J. Steelant¹, T. Langener¹; ¹ESA-ESTEC, Netherlands | ||||
15:00 | 15:30 | 1.5.3 |
LAPCAT-II: DESIGN OF A COMBINED PROPULSION SYSTEM FOR A HYPERSONIC CRUISER S. Defoort, Onera, France |
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14:00 | 14:30 | 2.5.1 |
SIMULATION OF AIRCRAFT WAKE VORTICES DURING LANDING WITH DECAY ENHANCING OBSTACLES A. Stephan¹, F. Holzäpfel¹, T. Misaka, Tohoku University, Institute of Fluid Science, Japan; ¹Deutsches Zentrum für Luft- und Raumfahrt (DLR), Germany | ||||
14:30 | 15:00 | 2.5.2 |
DYNAMICS OF A VORTEX RING AROUND A MAIN ROTOR HELICOPTER K. Surmacz, Institute of Aviation, Poland | ||||
15:00 | 15:30 | 2.5.3 |
NUMERICAL INVESTIGATION ON ENGINE INLET DISTORTION UNDER CROSSWIND FOR A COMMERCIAL TRANSPORT AIRCRAFT K. Liu¹, Y. Sun¹, Y. Zhong¹, H. Zhang¹, K. Zhang, Nanjing University of Aeronautics and Astronautics, China; H. Yang¹; ¹Shanghai Aircraft Design and Research Institute, China |
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14:00 | 14:30 | 3.5.1 |
EFFECT OF ELASTICITY IN THE BIRD-LIKE PRIMARY FEATHER WING ON THE FLIGHT STABILITY M. Motomatsu, Graduate school of Tokai University, Japan; Y. Inada, Tokai University, Japan | ||||
14:30 | 15:00 | 3.5.2 |
EXPERIMENTAL CHARACTERIZATION OF A FLEXIBLE MEMBRANE FLAPPING-WING IN FORWARD FLIGHT L.G. Wang¹, B.F. Song¹, W.Q. Yang¹, P. Fu¹; ¹Northwestern Polytechnical University, China | ||||
15:00 | 15:30 | 3.5.3 |
AN EXPERIMENTAL STUDY ON THE INFLUENCE OF PASSIVE DEFORMATION TO LIFT AND THRUST GENERATION IN FLEXIBLE FLAPPING WING F. Peng¹, S. Bifeng¹, W. Liguang¹; ¹Northwestern Polytechnical University, China |
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14:00 | 14:30 | 4.5.1 |
THREE-DIMENSIONAL NUMERICAL SIMULATION OF ICE ACCRETION USING A MORPHOGENETIC APPROACH K. Szilder, Aerospace, National Research Council, Canada | ||||
14:30 | 15:00 | 4.5.2 |
THE INFLUENCE OF ICE ACCRETION ON THE AERODYNAMIC PERFORMENCE OF A UAS AIRFOIL K. Szilder, National Research Council, Canada | ||||
15:00 | 15:30 | 4.5.3 |
EXPERIMENTAL AND THEORETICAL INVESTIGATIONS OF AIRCRAFT ICING IN THE CASE OF CRYSTAL AND MIXED-PHASE FLOWS A.B. Miller¹, Y.F. Potapov¹, A.L. Stasenko¹; ¹TsAGI, Russia |
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14:00 | 14:30 | 5.5.1 |
SOME LAMINATE DEFORMATIONS FEATURES Y.I. Dudarkov¹, E.A. Levchenko¹, M.V. Limonin¹; ¹TsAGI, Russia | ||||
14:30 | 15:00 | 5.5.2 |
DESIGN OF A LAMINATED COMPOSITE MULTI-CELL STRUCTURE SUBJECTED TO TORSION I.C.J. Barbosa¹, M.A.R. Loja¹; ¹GI-MOSM/ISEL, IDMEC/LAETA , Portugal | ||||
15:00 | 15:30 | 5.5.3 |
IMPROVED METHODS FOR MODELLING IMPERFECTIONS FOR BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELLS J. Kepple¹, G. Prusty¹, G. Pearce¹, D. Kelly¹, R. Thomson, Cooperative Research Centre for Advanced Composite Structures, Australia; ¹The University of New South Wales, Australia |
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14:00 | 14:30 | 6.5.1 |
EFFICIENT AERO-STRUCTURAL DESIGN OPTIMIZATION BASED ON HIGH-FIDELITY METHODS Y.T. Zuo¹, Z.H. Gao¹, G. Chen, Xi’ an Jiaotong University, China; ¹Northwestern Polytechnical University, China | ||||
14:30 | 15:00 | 6.5.2 |
STEPS TO FEASIBILITY FOR LAMINAR WING DESIGN IN A MULTIDISCIPLINARY ENVIRONMENT S. Dähne¹, T. Bach¹, C. Hühne¹; ¹Germen Aerospace Center (DLR), Germany | ||||
15:00 | 15:30 | 6.5.3 |
MAIN BENEFITS OF PRO-COMPOSITE LAYOUTS FOR WING AND FUSELAGE PRIMARY STRUCTURE UNITS A. Shanygin¹, M. Zichenkov¹, I. Kondakov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia |
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14:00 | 14:30 | 7.5.1 |
AERODYNAMIC INLET DESIGN FOR CIVIL AIRCRAFT NACELLE A.A. Savelyev¹, S.V. Mikhaylov¹, N.A. Zlenko¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
14:30 | 15:00 | 7.5.2 |
PROGRESS TOWARDS ADAPTIVE AIRCRAFT ENGINE NACELLES L. da Rocha-Schmidt¹, A. Hermanutz¹, H. Baier¹, A. Seitz², J. Bijewitz², A.T. Isikveren², F. Scarpa³, G. Allegri³, C. Remillat³, E. Feuilloley³, F. Majic*, C. O\'Reilly*, G. Efraimsson*; ¹Technische Universität München, Germany ;²Bauhaus Luftfahrt e.V., Germany ;³University of Bristol, United Kingdom ;*Kungliga Tekniska Högskolan, Sweden | ||||
15:00 | 15:30 | 7.5.3 |
NEW CHALLENGES FOR ENGINE NACELLE COMPARTMENTS PRESSURE AND THERMAL LOADS MANAGEMENT WITH AIRCRAFT ENGINE EVOLUTION O. Verseux¹, Y. Sommerer¹; ¹Airbus Operation SAS, France |
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14:00 | 14:30 | 8.5.1 |
SLOSHING MECHANICAL MODEL FOR STABILITY AND HANDLING QUALITIES EVALUATION OF THE C295 AIRCRAFT WITH THE OSD SYSTEM R. Rodríguez Robles¹, J. Pérez Serrano¹; ¹Airbus Military, Spain | ||||
14:30 | 15:00 | 8.5.2 |
NON-INTRUSIVE FLIGHT TEST INSTRUMENTATION TECHNOLOGIES H. Abbasi, National Research Council Canada, Canada | ||||
15:00 | 15:30 | 8.5.3 |
WIND TUNNEL INVESTIGATION OF CRITICAL FLIGHT REGIMES USING DYNAMICALLY SCALED ACTIVELY CONTROLLED MODEL IN 3 DOF GIMBAL I. Grishin¹, A. Khrabrov¹, A. Kolinko¹, M. Sidoryuk¹, A. Vyalkov¹; ¹TsAGI, Russia |
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14:00 | 14:30 | 9.5.1 |
ECOLOGICAL OPTIMIZATION OF JET AIRCRAFT FLIGHTS IN VIEW OF CONTRAILS AND CONTRAIL CIRRUS FORMATION V.I. Vid¹, V.T. Dedesh¹, S.N. Kiose¹, R.H. Tenishev¹, E.G. Pavlova¹, R.L. Kagarmanov¹, V.V. Popov¹, G.P. Rumyantseva¹, M.A. Lavrov¹, R.V. Enchilik¹, M.A. Grigoryev¹, A.N. Zamyatin¹, I.V. Voronich, Moscow Institute of Physics and Technology, Russia; A.I. Lanshin², A.A. Evstigneev²; ¹GFRI, Russia ;²Central Institute of Aviation, Russia | ||||
14:30 | 15:00 | 9.5.2 |
A STUDY OF FLOW AND INITIAL STAGE OF WATER CONDENSATION IN THE TWO-PHASE JET-VORTEX WAKE BEHIND A CRUISE AIRCRAFT M.A. Lobanova, Baltic State Technical University, Russia |
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14:00 | 14:30 | 10.5.1 |
MULTI-FUNCTIONAL AERODROME CONTROL RADAR BY USPR TECHNOLOGY A.E. Ananenkov¹, A.V. Konovaltsev¹, V.M. Nuzhdin¹, V.V. Rastorguev¹, V.N. Skosyrev, Moscow State Technical University, Russia; ¹Moscow Aviation Institute, Russia | ||||
14:30 | 15:00 | 10.5.2 |
ARTIFICIAL NEURAL NETWORK BASED SIGNAL PROCESSING FOR PERSPECTIVE ONBOARD SYSTEMS E. Efimov¹, T. Shevgunov¹, A. Valaytite¹, E. Sadovskaya¹; ¹Moscow Aviation Institute (National Research University), Russia | ||||
15:00 | 15:30 | 10.5.3 |
GAN POWER AMPLIFIER FOR ON-BOARD DIGITAL ANTENNA ARRAY R. Malakhov, The Moscow Aviation Institute (National Research University), Russia |
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14:00 | 14:30 | 11.5.1 |
NUMERICAL INVESTIGATION OF FUSELAGE-STABILIZER-CONTROL SURFACE INTERFERENCE FOR A HYPERSONIC WAVERIDER VEHICLE X.-P. Li¹, W.-P. Song¹, Z.-H. Han¹; ¹Northwestern Polytechnical Universtity, China | ||||
14:30 | 15:00 | 11.5.2 |
MACH NUMBER EFFECT ON THE FLOWFIELD STRUCTURE OF HYPERSONIC GAP FLOWS L.T.L.C. Paolicchi¹, W.F.N. Santos¹; ¹National Institute for Space Research (INPE), Brazil | ||||
15:00 | 15:30 | 11.5.3 |
THE STUDY OF NONQUILIBRIUM GAS-DYNAMIC PROCESSES IN THE FLOW AROUND BODIES IN THE WIND TUNNEL IT-2M TSAGI V.A. Levin, Institute of mechanics MSU, Russia |
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14:00 | 14:30 | 12.5.1 |
RECOVERY OF HIGH-SPEED AND THROTTLE CHARACTERISTICS TURBOJET ENGINE BASED ON THE EMPIRICAL DATA G. Veresnikov, IPU, Russia | ||||
14:30 | 15:00 | 12.5.2 |
EVALUATIONS OF PROBLEM AREAS ON CAUSES OF EXCESSIVE FUEL CONSUMPTION FOR TURBOFAN ENGINES R.C. Chang¹, S. Tan¹; ¹China University of Science and Technology, Taiwan | ||||
15:00 | 15:30 | 12.5.3 |
ANALYSIS OF PROPULSION AND ENERGY SYSTEM’S INFLUENCE ON THE PERFORMANCE OF HIGH ALTITUDE AIRSHIP S. ChenB. SongH. Wa |
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16:00 | 16:30 | 1.6.1 |
PROPULSION/AIRFRAME INTEGRATION CONSIDERING LOW DRAG AND LOW SONIC BOOM A. Ueno¹, Y. Watanabe¹; ¹JAXA, Japan | ||||
16:30 | 17:00 | 1.6.2 |
CONCEPTUAL DESIGN STUDY ON LH2 FUELED SST - ENVIRONMENTAL IMPACTS REDUCED BY AIRFRAME/PROPULSION SYSTEM INTEGRATION - T. Yuhara¹, K. Rinoie, University of Tokyo, Japan; Y. Makino¹; ¹JAXA, Japan | ||||
17:00 | 17:30 | 1.6.3 |
D-SEND#2 FLIGHT DEMONSTRATION FOR LOW SONIC BOOM DESIGN TECHNOLOGY M. Honda¹, K. Yoshida¹; ¹JAXA, Japan | ||||
17:30 | 18:00 | 1.6.4 |
DEVELOPMENT OF A SMALL-SCALE SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED K. Mizobata¹, R. Minato¹, K. Higuchi¹, M. Ueba¹, S. Takagi¹, D. Nakata¹, N. Katsumata¹, K. Higashino¹, N. Tanatsugu¹; ¹Muroran Institute of Technology, Japan |
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16:00 | 16:30 | 2.6.1 |
COMPUTER MODELLING TECHNIQUE AERODYNAMIC CHARACTERISTICS MODELLING OF THE STAND WITH LONG-RANGE LARGE DIAMETER AIR JET N.-A Sidenko, Research-and-development center “CENTRE COMPOSITE” Joint Venture, Latvia | ||||
16:30 | 17:00 | 2.6.2 |
DAHWIN - DIGITAL/ANALOG-HYBRID WIND TUNNEL - FOR INNOVATIVE EFD/CFD INTEGRATION S. Watanabe¹, S. Kuchi-ishi¹, K. Murakami¹, A. Hashimoto¹, H. Kato¹, K. Yasue¹, H. Saiki², J. Ogino²; ¹JAXA, Japan ;²Ryoyu Systems Co., Ltd., Japan | ||||
17:00 | 17:30 | 2.6.3 |
VERIFICATION OF MODELLING OF FLUID-STRUCTURE INTERACTION (FSI) PROBLEMS BASED ON EXPERIMENTAL RESEARCH OF BLUFF BODY OSCILLATIONS IN FLUIDS O. Kotsur¹, G. Scheglov, BMSTU, Russia; P. Leyland¹; ¹EPFL, Switzerland |
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16:00 | 16:30 | 3.6.1 |
DYNAMIC CHARACTERISTICS OF THE THRUST VECTORING CONTROL BY HIGHLY COMPRESSIBLE COANDA EFFECTS Y. Lee¹, S.H. Park¹, H.B. Chang¹, Y.H. Cho, Seyon Engineering & System Co., South Korea; ¹Korea Aerospace University, South Korea | ||||
16:30 | 17:00 | 3.6.2 |
ARTIFICIAL TURBULIZATION OF THE SUPERSONIC BOUNDARY LAYER BY DIELECTRIC BARRIER DISCHARGE P.A. Polivanov¹, A.A. Sidorenko¹, A.A. Maslov¹; ¹ITAM SB RAS, Russia | ||||
17:00 | 17:30 | 3.6.3 |
CONTROL OF SONIC BOOM LEVEL BY CRYOGENIC ACTION ON THE PROCESS OF FLOW AROUND THE AIRCRAFT V.F. Chirkashenko¹, V.M. Fomin¹, A.M. Kharitonov ¹, V.F. Volkov¹; ¹ITAM SB RAS, Russia | ||||
17:30 | 18:00 | 3.6.4 |
INVESTIGATION OF THE OPTICAL PULSING DISCHARGE IN THE SUPERSONIC AIR FLOW T. Bobarykina, ITAM SB RAS, Russia |
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16:00 | 16:30 | 4.6.1 |
INNOVATIVE SUPERSONIC TRANSPORT CONFIGURATION BY BIPLANE WING / TWIN-BODY FUSELAGE W. Yamazaki, Nagaoka University of Technology, Japan; K. Kusunose, Japan Aerospace Exploration Agency, Japan | ||||
16:30 | 17:00 | 4.6.2 |
LEE-SIDE FLOW SIMULATIONS OF CRUCIFORM WING-BODY CONFIGURATIONS AT INCOMPRESSIBLE MACH NUMBERS J. Versteegh, University of the Witwatersrand, South Africa | ||||
17:00 | 17:30 | 4.6.3 |
THE AERODYNAMIC DESIGN OF THE A350 XWB-900 HIGH LIFT SYSTEM H. Strüber, Airbus Operations GmbH, Germany | ||||
17:30 | 18:00 | 4.6.4 |
OPTIMISATION OF A NOVEL TRAILING EDGE CONCEPT FOR A HIGH LIFT DEVICE J.D.M. Botha,, University of the Witwatersrand, South Africa; L. Dala, CSIR, South Africa; S. Schaber, Airbus, Germany |
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16:00 | 16:30 | 5.6.1 |
SMALL CRACKS IN ALUMINUM STRUCTURES UNDER STATIC AND CYCLIC LOADING V.V. Konovalov¹, A.A. Sviridov¹; ¹TsAGI, Russia | ||||
16:30 | 17:00 | 5.6.2 |
CONSIDERATION OF THE SERVICE LIFE TAKING INTO ACCOUNT A LOT OF ONE-TYPE STRESSED UNIT ELEMENTS A.V. Pankov¹, I.G. Khlebnikova¹; ¹TsAGI, Russia | ||||
17:00 | 17:30 | 5.6.3 |
THE PRINCIPLES OF FATIGUE APPROVAL FOR TRANSPORT AIRCRAFT AFTER ITS PRINCIPAL STRUCTURE ELEMENTS MODIFICATION V.I. Kleptsov, Beriev Aircraft Company, Russia | ||||
17:30 | 18:00 | 5.6.4 |
CONTROL OF COMPOSITE MATERIAL CRACK BRANCHING FOR IMPROVED FRACTURE TOUGHNESS A.C. Orifici, RMIT University, Australia |
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16:00 | 16:30 | 6.6.1 |
A METHODICAL APPROACH FOR DYNAMIC SYSTEM ANALYSIS & SYNTHESIS IN THE DIMENSIONING OF VARIANT LIGHTWEIGHT CABIN INTERIOR B. Plaumann¹, D. Krause¹; ¹TUHH, Institute PKT, Germany | ||||
16:30 | 17:00 | 6.6.2 |
AEROELASTIC OPTIMIZATION OF COMPOSITE WING BASED ON IMPROVED ADAPTIVE GENETIC ALGORITHM Q. Xiong, CASIC, China; D.-G. Cui, AVIC, China | ||||
17:00 | 17:30 | 6.6.3 |
ASSESSING STRUCTURAL TECHNOLOGY PERFORMANCE FOR THE HYBRID WING BODY THROUGH PROBABILISTIC WEIGHT ESTIMATION J.A. Corman¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
17:30 | 18:00 | 6.6.4 |
ANALYTICAL METHOD FOR LIMIT LOAD CAPACITY CALCULATION OF THIN WALLED AIRCRAFT STRUCTURES A. Pistek, Brno Univerzity of Technology, Czech Republic |
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16:00 | 16:30 | 7.6.1 |
ON THE OPTIMAL LOCATION OF BLEED PORTS FOR GAS TURBINE COOLING A.C. Marta, LAETA, CCTAE, Instituto Superior Técnico, Universidade de Lisboa, Portugal; S. Shankaran, Fluid Mechanics Lab, Global Research Center, General Electric, United States | ||||
16:30 | 17:00 | 7.6.2 |
IMPROVEMENT OF THE DESIGN AND METHODS OF DESIGNING CRITICAL COMPONENTS OF GAS FLOW PATH OF MODULAR AIRCRAFT GAS TURBINE V.G. Nesterenko¹, A.A. Matushkin¹, V.V. Nesterenko¹; ¹MAI, Russia | ||||
17:00 | 17:30 | 7.6.3 |
AERODYNAMIC DESIGN OF HIGH PERFORMANCES INTER-TURBINE TRANSITION DUCTS A. Mahallati, National Research Council of Canada, Canada |
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16:00 | 16:30 | 8.6.1 |
BOOST-PHASE MISSILE ATTITUDE CONTROLLER DESIGN USING HIGHER-ORDER SLIDING MODES Y. Lee¹, Y. Kim¹, G. Moon², B.-E. Jun²; ¹Seoul National University, South Korea ;²Agency for Defense Development, South Korea | ||||
16:30 | 17:00 | 8.6.2 |
CONTROL INPUT BLENDING LOGIC WITH AERODYNAMIC CONTROL AND REACTION JET CONTROL M.-G. Seo¹, C.-H. Lee², M.-J. Tahk¹, J.-I. Lee², B.-E. Jun²; ¹KAIST, South Korea ;²Agency for Defense Development, South Korea | ||||
17:00 | 17:30 | 8.6.3 |
EXTENDED KALMAN FILTER DESIGN USING BEARING AND TIME-TO-GO MEASUREMENT FOR A HOMING MISSILE GUIDANCE S.W. Shim¹, B.-G. Park², B.-J. Jeon¹, M.-J. Tahk¹, H.H. Kwon²; ¹KAIST, South Korea ;²LIG Nex1, South Korea | ||||
17:30 | 18:00 | 8.6.4 |
SUM-OF-SQUARES BASED STABILITY ANALYSIS FOR SKID-TO-TURN MISSILES WITH THREE-LOOP AUTOPILOT H.-H. Kwon¹, M.-W. Seo¹, D.-S. Jang¹, H.-L. Choi¹; ¹KAIST, South Korea |
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16:00 | 16:30 | 9.6.1 |
PERFORMANCE ASSESSMENT OF ALTERNATIVE FUELS AT THE AIR TRANSPORTATION SYSTEM LEVEL A.A. Okhapkin, Central Aerohydrodynamic Institute, Russia | ||||
16:30 | 17:00 | 9.6.2 |
MODELING STUDY OF POLLUTANT FORMATION IN HOMOGENEOUS METHANE AND SYNGAS FUELED COMBUSTOR V.E. Kozlov¹, A.M. Starik¹, N.S. Titova¹; ¹Central Institute of Aviation Motors, Russia | ||||
17:00 | 17:30 | 9.6.3 |
PERFORMANCE AND EMISSIONS CHARACTERISTICS OF ALTERNATIVE AVIATION FUELS W.A. Chishty, National Research Council Canada, Canada |
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16:00 | 16:30 | 10.6.1 |
MISSION PROFILES ANALYSIS: GUIDELINES TO AIRCRAFT ACTUATORS NEW TECHNOLOGY SPECIFICATION A. Reysset¹, M. Budinger¹, J.-C. Maré¹; ¹Institut Clément Ader, France | ||||
16:30 | 17:00 | 10.6.2 |
QUANTITATIVE FIDELITY MANAGEMENT AND SELECTION OF PHYSICS-BASED MULTIDISCIPLINARY DESIGN ENVIRONMENTS K.N. Gatian¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
17:00 | 17:30 | 10.6.3 |
SELECTION OF AGRICULTURAL AIRCRAFT USING AHP AND TOPSIS METHODS IN FUZZY ENVIRONMENT G.S. Schwening¹, A.M. Abdalla¹; ¹Escola de Engenharia de São Carlos - Universidade de São Paulo, Brazil | ||||
17:30 | 18:00 | 10.6.4 |
RESEARCH ON TECHNOLOGY READINESS ASSESSMENT MODEL FOR SYSTEM OF SYSTEMS W. CHENG¹, C. XING¹, H. ZHANG¹, Y. WU¹; ¹Aviation Industry Development Research Center of China (ADR), China |
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16:00 | 16:30 | 11.6.1 |
HUMAN FACTORS STUDIES OF AN ADS-B BASED TRAFFIC ALERTING SYSTEM FOR GENERAL AVIATION S.S. Silva¹, H. Cho¹, R.J. Hansman¹; ¹MIT, United States | ||||
16:30 | 17:00 | 11.6.2 |
MENTAL EFFORT AND SAFETY IN CURVED APPROACHES J.O. Entzinger¹, T. Uemura¹, S. Suzuki¹; ¹The University of Tokyo, Japan | ||||
17:00 | 17:30 | 11.6.3 |
DEVELOPMENT AND FLIGHT RESEARCH OF NON-INTRUSIVE AIRBORNE SYSTEM OF PILOT PSYCHOPHYSIOLOGICAL STATUS MONITORING A.D. Mironov¹, A.Y. Nakvasin¹; ¹GROMOV FLIGHT RESEARCH INSTITUTE (LII GROMOV), Russia | ||||
17:30 | 18:00 | 11.6.4 |
SUBJECTIVE FACTORS IN CONTROLLERS' DECISIONS I. Jankovics, Budapest University of Technology and Economics, Hungary |
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16:00 | 16:30 | 12.6.1 |
DETAILED RESEARCH ON RICH-LEAN TYPE SINGLE SECTOR AND FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT ENGINE M. MAKIDA¹, H. YAMADA¹, K. SHIMODAIRA¹; ¹Japan Aerospace Exploration Agency, Japan | ||||
16:30 | 17:00 | 12.6.2 |
NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF LASER IGNITION IN COMBUSTION CHAMBERS S.G. Rebrov, FSUE Keldysh Research Centre, France; P.V. Kholodov, Moscow Aviation Institute, Russia; G.R. Yakhina, Ecole Centrale de Lyon, France | ||||
17:00 | 17:30 | 12.6.3 |
MECHANISM OF FLAMEHOLDING IN PLASMA-ASSISTED SUPERSONIC COMBUSTOR S. Leonov, Ohio State University, MAE, Columbus, United States; V. Sabelnikov¹, A. Vincent-Randonnier¹, A. Firsov², D. Yarantsev²; ¹ONERA, the French Aerospace Lab, France ;²Joint Institute for High Temperature RAS, Russia | ||||
17:30 | 18:00 | 12.6.4 |
TECHNOLOGY AND CODE FOR NUMERICAL SIMULATION OF DIFFERENT COMBUSTION TYPES IN HIGH-SPEED VISCOUS GAS TURBULENT FLOWS A. Shiryaeva, TsAGI, Russia |
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09:30 | 10:00 | 1.7.1 |
MULTIFUNCTIONAL WING MOVEABLES: DESIGN OF THE A350XWB AND THE WAY TO FUTURE CONCEPTS D. Reckzeh, Airbus, Germany | ||||
10:00 | 10:30 | 1.7.2 |
OPTIMIZATION OF REVENUE SPACE OF A BLENDED WING BODY J. Fuchte¹, T. Pfeiffer¹, P.D. Ciampa¹, B. Nagel¹, V. Gollnick¹; ¹German Aerospace Center, Germany | ||||
10:30 | 11:00 | 1.7.3 |
RECENT ADVANCES IN AIRFRAME-PROPULSION CONCEPTS WITH DISTRIBUTED PROPULSION A.T. Isikveren¹, A. Seitz¹, J. Bijewitz¹, M. Hornung¹, A. Mirzoyan², A. Isyanov², J.-L. Godard, ONERA, France; S. Stueckl³, J. van Toor³; ¹Bauhaus Luftfahrt e.V., Germany ;²Central Institute of Aviation Motors, Russia ;³Airbus Group, Germany | ||||
11:00 | 11:30 | 1.7.4 |
AERODYNAMIC ANALYSIS OF THE BWB BUSINESS JET USING DSTRIDUTED PROPULSION SYSTEM H. Choi, Hanyang Univetsity, South Korea | ||||
11:30 | 12:00 | 1.7.5 |
CONCEPTUAL DESIGN STUDY OF QUAD-BUBBLE-BUSINESS JET H. Djojodihardjo, Universiti Putra Malysia, Malaysia; M. Anas Bin Abd Bari, Universiti Putra Malaysia, Malaysia |
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09:30 | 10:00 | 2.7.1 |
RAPID LARGE-SCALE CARTESIAN MESHING FOR AERODYNAMIC COMPUTATIONS D. Sasaki, Kanazawa Institute of Technology, Japan; K. Nakahashi, JAXA, Japan | ||||
10:00 | 10:30 | 2.7.2 |
A DEVELOPMENT AND VERIFICATION OF DENSITY BASED SOLVER USING LU-SGS ALGORITHM IN OPENFOAM J. Kim, Korea Aerospace Research Institute(KARI), South Korea; K. Kim, Seoul National University, South Korea | ||||
10:30 | 11:00 | 2.7.3 |
A MESH ADAPTATION METHOD FOR SIMULATION OF UNSTEADY FLOWS C.H. Zhou, Nanjing University of Aeronautics and Astronautics, China | ||||
11:00 | 11:30 | 2.7.4 |
MESHLESS METHOD FOR SIMULATION OF COMPRESSIBLE REACTING FLOW J.Y. Huh¹, K.H. Kim¹, S.Y. Jung, Agency for Defense Development, South Korea; ¹Seoul National University, South Korea | ||||
11:30 | 12:00 | 2.7.5 |
COMPUTATIONAL METHOD FOR STEADY FLOW (RANS) USING ZONAL APPROACH AND ITS IMPLEMENTATION EXPERIENCE FOR SOLUTION OF TASK OF INTERFERENCE ENGINE AND AIRFRAME K. Anisimov¹, E. Kazhan¹, A. Lysenkov¹; ¹TsAGI, Russia |
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09:30 | 10:00 | 3.7.1 |
THE LAMINAR-TURBULENT TRANSITION ZONE IN 2D AND 3D BOUNDARY LAYERS WITH EMPHASIS ON EFFECT OF FREE STREAM TURBULENCE A.P. Kiselev¹, V.A. Kuzminsky¹, D.S. Sboev¹; ¹TsAGI, Russia | ||||
10:00 | 10:30 | 3.7.2 |
ROUGHNESS EFFECTS ON SWEPT-WING CROSSFLOW TRANSITION IN MODERATE FREE-STREAM TURBULENCE T.I. Saeed¹, J.F. Morrison¹, M.S. Mughal¹; ¹Imperial College London, United Kingdom | ||||
10:30 | 11:00 | 3.7.3 |
THE ROLE OF LOCALIZED ROUGHNESS ON THE LAMINAR-TURBULENT TRANSITION ON THE OBLIQUE WING S.N. Tolkachev¹, V.N. Gorev¹, V.V. Kozlov¹; ¹ITAM SB RAS, Russia | ||||
11:00 | 11:30 | 3.7.4 |
LAMINAR-TURBULENT TRANSITION CONTROL BY DIELECTRIC BARRIER DISCHARGE. THEORY AND EXPERIMENT M.V. Ustinov¹, A.A. Uspensky¹, A.Y. Urusov¹, D.A. Rusianov¹; ¹TsAGI, Russia | ||||
11:30 | 12:00 | 3.7.5 |
APPLICATION OF LIGHT SCATTERING EFFECT IN AERODYNAMIC EXPERIMENT M.A. Brutyan¹, A.V. Petrov¹, A.V. Potapchik¹; ¹TsAGI, Russia |
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09:30 | 10:00 | 4.7.1 |
NUMERICAL INVESTIGATIONS ON THE SLENDER AXISYMMETRIC BODIES AERODYNAMICS IN WIDE RANGE OF MACH NUMBERS AND ANGLES OF ATTACK FROM 0° TO 180° N.V. Voevodenko¹, L.G. Ivanteeva¹, V.J. Lunin¹; ¹TsAGI, Russia | ||||
10:00 | 10:30 | 4.7.2 |
HYPERSONIC AEROTHERMODYNAMICS INVESTIGATION FOR AEROSPACE SYSTEM Y.I. Khlopkov¹, S.L. Chernyshev¹, Z.Y. Myo Myint², A.Y. Khlopkov²; ¹Central Aerohydrodynamic Institute, Russia ;²Moscow Institute of Physics and Technology, Russia | ||||
10:30 | 11:00 | 4.7.3 |
POTENTIAL USE OF WAVERIDER AND BUSEMANN BIPLANE IN AERODYNAMIC DESIGN OF HIGH-SPEED VEHICLES WITH AIR-BREATHING ENGINES A.A. Gubanov¹, D.Y. Gusev¹; ¹Central Aerohydrodynamic Institute n.a. Prof. N.E. Zhukovsky, Russia | ||||
11:00 | 11:30 | 4.7.4 |
NUMERICAL INVESTIGATION OF LAMINAR NEAR WAKE SEPARATION ON CIRCULAR CYLINDERS AT SUPERSONIC VELOCITIES W.S. Hinman¹, C.T. Johansen¹, C.J. Arisman¹, W.C. Galuppo¹; ¹University of Calgary, Canada | ||||
11:30 | 12:00 | 4.7.5 |
HYPERSONIC AERODYNAMIC APPRAISAL OF WINGED BLUNT, RATHER SHARP AND SPATULED BODY RE-ENTRY VEHICLES A. Viviani, Second University of Naples, Italy; G. Pezzella, Italian Aerospace Research Center, Italy |
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09:30 | 10:00 | 5.7.1 |
SYNTHESYS OF RADAR ABSORBING MATERIALS FOR STEALTH AIRCRAFT BY USING NANOMATERIALS AND EVOLUTIONARY COMPUTATION D. Micheli¹, R. Pastore¹, A. Vricella¹, R.-B. Morles¹, M. Marchetti¹; ¹Sapienza University, Italy | ||||
10:00 | 10:30 | 5.7.2 |
CHARACTERISING INTERNAL HEAT TRANSFER IN THERMAL PROTECTION SYSTEMS N. Banerji¹, P. Leyland¹, S. Haussener¹; ¹Ecole Polytechnique Fédérale de Lausanne, Switzerland | ||||
10:30 | 11:00 | 5.7.3 |
PREPARATION, CHARACTERIZATION AND APPLICATION OF ABRASION-RESISTANT HYBRID COATINGS ON POLYCARBONATE TRANSPARENCIES Y.-H. CHEN¹, Y. YUAN¹; ¹Beijing Institute of Aeronautical Materials, China | ||||
11:00 | 11:30 | 5.7.4 |
MICROSTRUCTURE AND EVOLUTION OF PORES DURING THE DENSIFICATION CYCLES OF ZRC DOPED CARBON/CARNON COMPOSITES Z. Chen, Nanjing University of Aeronautics and Astronautics, China | ||||
11:30 | 12:00 | 5.7.5 |
A NEW 3D PROGRESSIVE DAMAGE MODEL FOR COMPOSITE LAMINATES Z. Ni, Shanghai Aircraft Design and Research Institute, China |
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09:30 | 10:00 | 6.7.1 |
ON-LINE MONITORING AND FLUTTER SPEED PREDICTION BASED ON IDENTIFICATION OF A TIME-VARYING SYSTEM J. Ertveldt, Vrije Universiteit Brussel - Dept. MECH, Belgium | ||||
10:00 | 10:30 | 6.7.2 |
AEROELASTIC PREDICTION FOR MISSILE FINS IN SUPERSONIC FLOWS M.-C. Meijer, University of the Witwatersrand, South Africa | ||||
10:30 | 11:00 | 6.7.3 |
PROXIMITY EFFECTS OF PIEZOELECTRIC ENERGY HARVESTERS IN FLUID FLOW A Deivasigamani¹, J.M. McCarthy¹, S.J. John¹, S. Watkins¹, F. Coman, FCST Pty. Ltd., Australia; ¹RMIT University, Australia | ||||
11:00 | 11:30 | 6.7.4 |
A SIMPLE APPROACH TO COMPUTATIONAL AEROELASTICITY OF NASA ROTOR 67 R. Wiranegara¹, A. Turan¹; ¹University of Manchester, United Kingdom | ||||
11:30 | 12:00 | 6.7.5 |
NUMERICAL ANALYSIS OF TRANSONIC FLUTTER OF SUPERCRITICAL AIRFOIL OF A BUSINESS JET Q.Y. Chen, COMAC, China |
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09:30 | 10:00 | 7.7.1 |
GEOMETRIC VARIABILITY AND ITS INFLUENCE ON STEADY AND UNSTEADY FAN AERODYNAMIC PERFORMANCE R. Schnell¹, G. Ashcroft¹; ¹DLR, Germany | ||||
10:00 | 10:30 | 7.7.2 |
A STUDY ON AERODYNAMIC DESIGN OF HIGH-EFFICIENCY PROPELLERS AT HIGH-ALTITUDE J.-H. Xu¹, W.-P. Song¹, W.-Q. Yang¹; ¹Northwestern Polytechnical University, China | ||||
10:30 | 11:00 | 7.7.3 |
RELIABILITY IMPROVEMENT OF ACCESSORY GEARBOX BEVEL DRIVES E. Kozharinov, Central Institute of Aviation Motors, Russia | ||||
11:00 | 11:30 | 7.7.4 |
MODEL FORM UNCERTAINTY REPRESENTATION TO ENABLE MULTIFIDELITY DESIGN OF ADVANCED CONCEPTS H.D. Schwartz¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States | ||||
11:30 | 12:00 | 7.7.5 |
A LOW ORDER METHOD FOR CO-AXIAL PROPELLER AND ROTOR PERFORMANCE PREDICTION P. Beaumier, Onera, France |
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09:30 | 10:00 | 8.7.1 |
FLIGHT CONTROL SYSTEMS FOR WIG-CRAFT A.V. Nebylov, State University of Aerospace Instrumentation, Russia | ||||
10:00 | 10:30 | 8.7.2 |
AERODYNAMICS AND FLIGHT DYNAMICS PROBLEMS OF HIGH SPEED VEHICLES AND WAYS FOR THEIR SOLUTION A.V. Efremov¹, S.A. Popov¹, I.A. Nikitchenko¹, A.V. Koshelenko¹, Y.V. Tiumentzev¹; ¹Moscow aviation institute, Russia | ||||
10:30 | 11:00 | 8.7.3 |
ENERGY APPROACH FOR AIRCRAFT VELOCITY OPTIMAL CONTROL DESIGN O.N. Korsun, State Institute of Aviation Systems, Russia; V.P. Harkov, Experimental Enterprise Nauka-Soft, Russia | ||||
11:00 | 11:30 | 8.7.4 |
FLIGHT ENVELOPE EXPANSION VIA ACTIVE CONTROL SOLUTIONS FOR A GENERIC TAILLESS AIRCRAFT N. Abramov¹, M. Bommanahal², S. Chetty², M. Goman¹, E. Kolesnikov¹, P.V.S. Murthy²; ¹De Montfort University, United Kingdom ;²CSIR-National Aerospace Laboratories, India | ||||
11:30 | 12:00 | 8.7.5 |
PERFORMANCE OF SWITCHING TYPE DATABASE REFERENCED NAVIGATION ALGORITHM USING TERRAIN HEIGHT AND GRAVITY ANOMALY W. Lee, Seoul Nat'l Univ., South Korea |
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09:30 | 10:00 | 9.7.1 |
REAL-TIME LEADER-FOLLOWER UAV FORMATION FLIGHT BASED ON MODIFIED NONLINEAR GUIDANCE C. Park¹, H.J. Kim¹, Y. Kim¹; ¹Seoul National University, South Korea | ||||
10:00 | 10:30 | 9.7.2 |
FLEXIBLE FORMATION SHAPE CONTROL BASED ON THE LOCAL INTERACTION AMONG AIR VEHICLES Y. Inada, Tokai University, Japan | ||||
10:30 | 11:00 | 9.7.3 |
DYNAMICS MODELING AND ROBUST CONTROLLER DESIGN OF THE MULTI-UAV TRANSPORTATION SYSTEM H.-I. Lee¹, B.-Y. Lee¹, D.-W. Yoo¹, G.-H. Moon¹, M.-J. Tahk¹; ¹KAIST, South Korea | ||||
11:00 | 11:30 | 9.7.4 |
FORMATION FLIGHT OF FIXED-WING UAVS USING ARTIFICIAL POTENTIAL FIELD Y. Nagao¹, K. Uchiyama¹; ¹Nihon University, Japan | ||||
11:30 | 12:00 | 9.7.5 |
HARDWARE IMPLEMENTATION OF COOPERATIVE AUTONOMOUS COLLISION AVOIDANCE STRATEGY FOR UNMANNED AERIAL VEHICLES Y.I. Jenie, Delft University of Technology, Faculty of Aerospace Engineering, Netherlands |
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09:30 | 10:00 | 10.7.1 |
DYNAMIC NOTCH FILTERING CONTROL FOR FAULT-TOLERANT ACTUATORS OF FLY-BY-WIRE HELICOPTERS G. Di Rito¹, R. Galatolo¹, E. Denti¹, F. Schettini¹; ¹Università di Pisa - Dip. di Ingegneria Civile ed Industriale, Italy | ||||
10:00 | 10:30 | 10.7.2 |
AN UAV LANDING GEAR SYSTEM ACTUATED THROUGH SMA ACTIVE ELEMENTS S. Ameduri¹, L. Pellone¹, N. Favaloro¹, M. Ciminello¹; ¹Centro Italiano Ricerche Aerospaziali, Italy | ||||
10:30 | 11:00 | 10.7.3 |
NEW DEVELOPMENTS OF ELECTRICALLY POWERED ELECTROHYDRAULIC AND ELECTROMECHANICAL ACTUATORS FOR THE MORE ELECTRIC AIRCRAFT I. Ogoltsov¹, S. Samsonovich¹, A. Selivanov¹, A. Alekseenkov¹; ¹Moscow Aviation Institute (National Research University), Russia | ||||
11:00 | 11:30 | 10.7.4 |
RECENT ADVANCES IN ELECTRICAL LANDING GEAR SYSTEMS P Nevoret, Safran / Messier-Bugatti-Dowty, France | ||||
11:30 | 12:00 | 10.7.5 |
COMBINED SYNTHESIS OF CONTROL LAWS OF THE AIRCRAFT BRAKING ON THE RUNWAY DURING LANDING O. Kreerenko, Beriev Aircraft Company, Russia; E. Kreerenko, Southern Federal University , Russia |
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09:30 | 10:00 | 11.7.1 |
4D TRAJECTORY MANAGEMENT SUPPORT IN THE C-SHARE PROJECT D. Nieuwenhuisen, National Aerospace Laboratory, Netherlands | ||||
10:00 | 10:30 | 11.7.2 |
STOCHASTIC CONFLICT-FREE 4D TRAJECTORY OPTIMIZATION IN THE PRESENCE OF UNCERTAINTY Y. Matsuno, The University of Tokyo, Japan | ||||
10:30 | 11:00 | 11.7.3 |
ANALYSIS OF AIR TRAFFIC EFFICIENCY USING DYNAMIC PROGRAMMING TRAJECTORY OPTIMIZATION A. Harada¹, T. Kozuka¹, Y. Miyazawa¹, N.K. Wickramasinghe², M. Brown², Y. Fukuda²; ¹Kyushu University, Japan ;²ENRI Japan, Japan | ||||
11:00 | 11:30 | 11.7.4 |
EUROPEAN AIR NAVIGATION SERVICE PROVIDERS’ EFFICIENCY EVALUATION THROUGH DATA ENVELOPMENT ANALYSIS (DEA) R.M. Arnaldo Valdés¹, V.F. Gomez Comendador¹, R. Barragán, CRIDA, Spain; L. Perez¹; ¹UPM, Spain | ||||
11:30 | 12:00 | 11.7.5 |
DIFFEREING AIR TRAFFIC CONTROLLER RESPONSES TO SIMILAR TRAJECTORY PREDICTION ERRORS J. Mercer, San Jose State University / NASA Ames Research Center, United States |
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09:30 | 10:00 | 12.7.1 |
THE CONTRIBUTION OF DIFFERENT COUNTRIES TO AIRPLANE DEVELOPMENT AND MANUFACTURE- PART I. INVENTION OF AIRPLANE D.A. Sobolev, Institute for the History of Science and Technology, Russia | ||||
10:00 | 10:30 | 12.7.2 |
THE CONTRIBUTION OF DIFFERENT COUNTRIES TO AIRPLANE DEVELOPMENT AND MANUFACTURE - PART II. HOW MANY AIRPLANES WERE THERE? Y.V. Kuzmin, Institute for the History of Science and Technology, Russia | ||||
10:30 | 11:00 | 12.7.3 |
FROM ST. PETERSBURG TO ZURICH: AERONAUTICAL AND SCIENTIFIC MILESTONES FROM SWISS PERSPECTIVES AROUND THE NAMES BERNOULLI G. Bridel, Switzerland | ||||
11:00 | 11:30 | 12.7.4 |
CREATING THE MODERN AIRLINER: U.S. GOVERNMENT AND BUSINESS, 1918-2014 F.R. van der Linden, Smithsonian National Air and Space Museum, United States | ||||
11:30 | 12:00 | 12.7.5 |
FIRST AIRFIELDS OF SAINT PETERSBURG - FIRST AIRFIELDS OF RUSSIA V.V. Lebedev, Institute for History for Science and Technology, Russia |
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14:00 | 14:30 | 1.8.1 |
WING-LOAD CONTROL BASED ON THE \"LEAKY WING\" CONCEPT W. Stalewski, INSTITUTE of AVIATION, Poland | ||||
14:30 | 15:00 | 1.8.2 |
OPTIMUM AND DESIGN TRENDS OF COMPOUND HELICOPTERS O. Rand¹, V. Khromov¹; ¹Technion - Israel Institute of Technology, Israel | ||||
15:00 | 15:30 | 1.8.3 |
CONCEPTUAL DESIGN OF A PASSENGER AIRCRAFT FOR AERIAL REFUELING OPERATIONS G. La Rocca¹, M. Li¹, P.P.M. van der Linden¹, R.J.M. Elmendorp¹; ¹Delft University of Technology, Netherlands |
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14:00 | 14:30 | 2.8.1 |
THE ANALYSIS OF UNDEREXPANDED JET FLOWS FOR HYPERSONIC AEROTHERMODYNAMIC APPLICATIONS V.V. Riabov, Rivier University, United States | ||||
14:30 | 15:00 | 2.8.2 |
NUMERICAL INVESTIGATION OF LIQUID JET INJECTION INTO A SUPERSONIC CROSSFLOW L. Haixu¹, G. Yincheng¹, L. Wenyi¹; ¹Tsinghua University, China | ||||
15:00 | 15:30 | 2.8.3 |
NUMERICAL SIMULATIONT OF GAS AND MULTIPHASE SUPERSONIC JETS WITH NON-EQUILIBRIUM PROCESSES A.M. Molchanov, Moscow Aviation Institute, Russia |
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14:00 | 14:30 | 3.8.1 |
EXPERIMENTAL INVESTIGATION OF ENDWALL FLOW FIELD, HEAT TRANSFER IN A LINEAR TURBINE BLADE CASCADE WITH CONTOURED ENDWALL B. Barbieri, University of Pretoria, South Africa | ||||
14:30 | 15:00 | 3.8.2 |
INCOMPRESSIBLE TURBULENT FLOW AT THE LEADING EDGE OF SWEPT WINGS E.R. Gowree¹, C.J. Atkin¹; ¹City University London, United Kingdom | ||||
15:00 | 15:30 | 3.8.3 |
FLOW STRUCTURE IN THE BASE REGION OF RE-ENTRY VEHICLE WITH SUPERSONIC BRAKING PLUMES IMPINGING WITH LANDING SURFACE A.A. Dyadkin¹, V.P. Sukhorukov¹, G.A. Trashkov¹, V.F. Volkov², V.I. Zapryagaev², N.P. Kiselev²; ¹Korolev Energiya Rocket and Space Corporation, Russia ;²Khristianovich Institute of Theoretical and Applied Mechanics SB, Russia |
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14:00 | 14:30 | 4.8.1 |
NUMERICAL STUDY OF WIND-TUNNEL ACOUSTIC RESONANCE INDUCED BY TWO-DIMENSIONAL AIRFOIL FLOW AT LOW REYNOLDS NUMBER T. Ikeda¹, T. Atobe¹, Y. Konishi², H. Nagai², K. Asai²; ¹Japan Aerospace Exploration Agency, Japan ;²Tohoku University, Japan | ||||
14:30 | 15:00 | 4.8.2 |
AERODYNAMIC STUDIES ON LOW-NOISE AIRCRAFT WITH UPPER ENGINE INSTALLATION A.L. Bolsunovsky¹, N.N. Bragin¹, N.P. Buzoverya¹, I.L. Chernyshev¹, A.K. Ivanyushkin¹, S.I. Skomorohov¹; ¹TsAGI, Russia | ||||
15:00 | 15:30 | 4.8.3 |
AERODYNAMIC NOISE REDUCTION FOR HIGH LIFT DEVICES USING MORPHING FLAP CONCEPT Y. Tani¹, K. Miyazaki¹, S. Aso¹, H. Ura², T. Ito²; ¹Kyushu University, Japan ;²JAXA, Japan |
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14:00 | 14:30 | 5.8.1 |
NONLINEAR ACOUSTICS FOR HEALTH MONITORING OF COMPOSITE SCARF REPAIRS L. Pieczonka¹, A. Klepka¹, S. Pavlopoulou², W.J. Staszewski¹, C. Soutis²; ¹AGH University, Poland ;²Manchester University, United Kingdom | ||||
14:30 | 15:00 | 5.8.2 |
DAMAGE IDENTIFICATION USING FIBRE BRAGG GRATING SENSORS EMBEDDED WITHIN A COMPOSITE PLATE M.H. Safaei, Iran | ||||
15:00 | 15:30 | 5.8.3 |
FATIGUE DAMAGE DETECTION IN LARGE THIN WALL PLATE BASED ON ULTRASONIC GUIDED WAVE BY USING A PIEZOELECTRIC SENSOR NETWORK B. Alem¹, A. Abedian¹; ¹Sharif university of technology, Iran |
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14:00 | 14:30 | 6.8.1 |
POSTBUCKLING ANALYSIS AND OPTIMIZATION OF STIFFENED FUSELAGE PANELS UTILIZING VARIABLE-STIFFNESS LAMINATES T. Ungwattanapanit¹, H. Baier¹; ¹TU München, Germany | ||||
14:30 | 15:00 | 6.8.2 |
STRENGTH ANALYSIS TECHNIQUE FOR HIGH LOADED ELEMENTS OF COMPOSITE AIRFRAMES E. Dubovikov¹, V. Fomin¹; ¹TsAGI, Russia | ||||
15:00 | 15:30 | 6.8.3 |
MULTI-OBJECTIVE OPTIMIZATION OF THE COMPOSITE WING BOX OF SOLAR POWERED HALE UAV G. Romeo¹, F. Danzi¹, E. Cestino¹; ¹Politecnico di Torino, Italy |
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14:00 | 14:30 | 7.8.1 |
ASSESSMENT OF AERODYNAMIC AND ACOUSTIC CHARACTERISTICS OF COUNTER-ROTATING OPEN ROTORS I. Brailko¹, V. Mileshin¹, A. Rossikhin¹; ¹Central Institute of Aviation Motors, Russia | ||||
14:30 | 15:00 | 7.8.2 |
COMPARISON OF DUCTED AND UNDUCTED COUNTER ROTATING FAN MODEL NOISE Y. Khaletskiy¹, V. Mileshin¹; ¹Central Institute of Aviation Motors, Russia |
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14:00 | 14:30 | 8.8.1 |
ITERATIVE LEARNING IDENTIFICATION AGAINST NON-ZERO INITIAL STATES AND ESTIMATION OF AERODYNAMIC DERIVATIVES A. Fujimori¹, S. Oh-hara¹; ¹University of Yamanashi, Japan | ||||
14:30 | 15:00 | 8.8.2 |
A TIME SERIES MODEL OF ANGLE OF ATTACK AND PITCH RATE FOR A WIDE RANGE OF ALTITUDE AND VELOCITY N. Yoshitani, TEIKYO UNIVERSITY, Japan | ||||
15:00 | 15:30 | 8.8.3 |
FLIGHT DATA CLASSIFIER FOR EFFECTIVE AIRCRAFT PERFORMANCE ANALYSIS M. Naruoka, Japan Aerospace Exploration Agency, Japan |
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14:00 | 14:30 | 9.8.1 |
ON UAV ROBUST NONLINEAR CONTROL IN PRESENCE OF PARAMETRIC UNCERTAINTIES V.V. Golubev¹, W. MacKunis¹; ¹ERAU, United States | ||||
14:30 | 15:00 | 9.8.2 |
GENERATION OF INITIAL GUESSES FOR OPTIMAL CONTROL PROBLEMS WITH MIXED INTEGER DEPENDENT CONSTRAINTS M. Rieck¹, M. Richter¹, M. Bittner¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, Germany | ||||
15:00 | 15:30 | 9.8.3 |
L1 ADAPTIVE ATTITUDE CONTROLLER FOR A TAIL-SITTER MAV IN HOVER FLIGHT J. Wang¹, B. Song¹, L. Wang¹; ¹School of Aeronautics,Northwestern Polytechnical Unversity, China |
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14:00 | 14:30 | 10.8.1 |
REDUCTION OF VIBROACOUSTIC LOAD IN AVIATION COMBINED PUMPS S.A. Gafurov¹, A.B. Prokofiev¹, E.V. Shakhmatov ¹; ¹Samara State Aerospace University (National Research University), Russia | ||||
14:30 | 15:00 | 10.8.2 |
AIR EVOLUTION IN FUEL FLOW UNDER DECREASED PRESSURE CONDITIONS: EXPERIMENTAL STUDIES AND ENGINEERING CODE DEVELOPMENT E.E. Kitanina, Saint-Petersburg State Technical University, Russia; D.A. Bondarenko, EADS RTO SK LLC, Russia; D. Morrison, Airbus Operations Ltd, United Kingdom | ||||
15:00 | 15:30 | 10.8.3 |
DEVELOPMENT OF A SOLID PROPELLANT GAS GENERATOR (SPGG) SYSTEM FOR FIRE SUPPRESSION IN AVIATION - DESIGN OF AN INJECTOR E. Richter, EADS Deutschland GmbH, Germany; D. Krause, Otto-Von-Guericke University, Germany |
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14:00 | 14:30 | 11.8.1 |
EVALUATION OF OPERATIONS ON AN AIRPORT WITH A CIRCULAR RUNWAY M. Dupeyrat¹, S. Aubry¹, H. Hesselink², S. Loth, DLR, Germany; A. Remiro, ISDEFE, Spain; P. Schmollgruber¹, R. Verbeek², C. Welman²; ¹ONERA, France ;²NLR, Netherlands | ||||
14:30 | 15:00 | 11.8.2 |
ANALYSES ON A CIVIL AIR TO AIR REFUELING NETWORK IN A TRAFFIC SIMULATION F. Morscheck, DLR, Germany | ||||
15:00 | 15:30 | 11.8.3 |
MODELING AN OPERATIONS CONCEPT FOR COMMERCIAL AIR-TO-AIR REFUELING BASED ON A VEHICLE ROUTING PROBLEM FORMULATION M.M. van Lith , TU Delft , Netherlands; H.G. Visser¹, H.S. Hosseini¹; ¹TU Delft, Netherlands |
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14:00 | 14:30 | 12.8.1 |
TECHNOLOGIES FOR THE NEXT ENGINE GENERATION A.R. Wadia, GE Aviation, United States | ||||
14:30 | 15:00 | 12.8.2 |
GEARING UP FOR HIGH VOLUME GTFTM PRODUCTION J. Henne, MTU, Germany | ||||
15:00 | 15:30 | 12.8.3 |
CHALLENGES IN FAN AND HIGH PRESSURE COMPRESSOR DEVELOPMENT V. Mileshin, CIAM, Russia |
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16:00 | 16:30 | 1.9.1 |
KNOWLEDGE-BASED DESIGN FOR FUTURE COMBAT AIRCRAFT CONCEPTS R.C Munjulury¹, I. Staack¹, A. Abdalla, USP, Brazil; T. Melin¹, C. Jouannet¹, P. Krus¹; ¹Linköping University, Sweden | ||||
16:30 | 17:00 | 1.9.2 |
CONCEPTUAL AIRCRAFT DESIGN MODEL MANAGEMENT DEMONSTRATED ON A 4TH GENERATION FIGHTER I. Staack¹, R.C. Munjulury ¹, T. Melin¹, A. Abdalla, University of São Carlos, Brazil; P. Krus¹; ¹Linköping University, Sweden | ||||
17:00 | 17:30 | 1.9.3 |
PASSENGER AIRPLANE CONVERSION TO FREIGHTER I. Berlowitz, Israel Aerospace Industries, Israel | ||||
17:30 | 18:00 | 1.9.4 |
CONCEPTUAL DESIGN OF THREE ALTERNATIVE CONFIGURATIONS OF NEW-GENERATION 19-SEAT BUSH AIRCRAFT J.P. Fielding¹, A.J. Stewart¹, G.S. Ji¹, G. Rojas¹; ¹Cranfield University, United Kingdom |
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16:00 | 16:30 | 2.9.1 |
STUDY OF INSTALLATION EFFECTS ON A HIGH-LIFT WING SECTION IN AN OPEN WIND TUNNEL L. Tysell, FOI, Sweden | ||||
16:30 | 17:00 | 2.9.2 |
AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM COMPATIBLE WITH A NATURAL LAMINAR FLOW WING WITHIN THE DESIREH PROJECT H. Strüber, Airbus Operations GmbH, Germany; J. Wild, Deutsches Zentrum für Luft- und Raumfahrt, Germany | ||||
17:00 | 17:30 | 2.9.3 |
NUMERICAL SIMULATION OF UNSTEADY FLOWS AROUND HIGH-LIFT CONFIGURATIONS S. Bosnyakov¹, I. Kursakov¹, A. Lysenkov¹, S. Mikhaylov¹; ¹TsAGI, Russia | ||||
17:30 | 18:00 | 2.9.4 |
NUMERICAL INVESTIGATION OF AN AILERON HINGE MOMENTS AND EFFECTIVENESS ON A HIGH LIFT WING AIRFOIL K.A. Makarov¹, A.A. Pavlenko¹; ¹TsAGI, Russia |
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16:00 | 16:30 | 3.9.1 |
LAMINAR FLOW CONTROL OF A HIGH-SPEED BOUNDARY LAYER BY LOCALIZED WALL HEATING OR COOLING A.V. Fedorov¹, V.G. Soudakov¹, I.V. Egorov¹, A.A. Sidorenko², Y. Gromyko², D. Bountin²; ¹TsAGI, Russia ;²ITAM SB RAS and NSU, Russia | ||||
16:30 | 17:00 | 3.9.2 |
INVESTIGATION OF HEAT FLUX AND EFFUSION/FILM COOLING EFFICIENCY OVER A SHARP CONE SURFACE AT HIGH SUPERSONIC SPEEDS P.V. Chuvakhov, Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
17:00 | 17:30 | 3.9.3 |
A BLUNTED CONE IN A SUPERSONIC HIGH-ENTHALPY NONEQUILIBRIUM UNDEREXPANDED AIR JET V.I. Sakharov¹, V.V. Shtapov¹, E.B. Vasilevskiy¹, B.E. Zhestkov¹; ¹TsAGI, Russia | ||||
17:30 | 18:00 | 3.9.4 |
TO THE NON-UNIQUENESS PROBLEM OF HYPERSONIC STEADY-STATE FLOW ON THE BLUNTED BODIES LEADING AGE. S.M. Drozdov, TsAGI, Russia |
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16:00 | 16:30 | 4.9.1 |
ARRANGEMENT AND AERODYNAMIC STUDIES FOR LONG-RANGE AIRCRAFT IN “FLYING WING” LAYOUT A.L. Bolsunovsky¹, N.P. Buzoverya¹, I.L. Chernyshev¹, B.I. Gurevich¹, A.P. Tsyganov¹; ¹TsAGI, Russia | ||||
16:30 | 17:00 | 4.9.2 |
TOWARDS COMPUTATIONAL FLIGHT DYNAMICS OF A PASSENGER JET AIRCRAFT M. Cristofaro¹, Y. Wang, China Academy of Aerospace Aerodynamics, China; A. Da Ronch¹; ¹University of Southampton, United Kingdom | ||||
17:00 | 17:30 | 4.9.3 |
MISSION ADAPTIVE WING-LET OPTIMIZATION FOR REDUCTING VORTEX DRAG F.M. Catalano, University of Sao Paulo, Brazil | ||||
17:30 | 18:00 | 4.9.4 |
DEVELOPMENT OF AERODYNAMIC DESIGN PROCESS FOR REUSABLE WINGED SPACE VEHICLE USING OPENVSP S. Taishi, Tokyo Metropolitan University, Japan |
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16:00 | 16:30 | 5.9.1 |
PROFIT-BASED NETWORK LEVEL EVALUATION OF AIRCRAFT BLOCK TIMES M. Schmidt¹, K.O. Plötner¹, A. Seitz¹, A.T. Isikveren¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany | ||||
16:30 | 17:00 | 5.9.2 |
SECURING THE SUPPLY CHAIN OF INDUSTRIAL PRODUCTS ON THE BASIS OF THE USE OF MODERN INFORMATION TECHNOLOGIES Y. Buryak¹, S. Zheltov¹; ¹State Institute of Aviation Systems, Russia | ||||
17:00 | 17:30 | 5.9.3 |
DEVELOPMENT OF INSTRUCTIONS FOR CONTINUING AIRWORTHINESS AND AIRCRAFT LOGISTIC SUPPORT ANALYSIS A.N. Petrov, Gromov Flight Research Institute, Russia | ||||
17:30 | 18:00 | 5.9.4 |
THE INFLUENCE OF SHM TECHNIQUES ON SCHEDULED MAINTENANCE OF AIRCRAFT COMPOSITE STRUCTURES X. Chen¹, H. Ren¹, C. Bil¹; ¹RMIT, Australia |
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16:00 | 16:30 | 6.9.1 |
STRUCTURAL NONLINEARITIES SIMULATION ON THE FLUTTER ELECTROMECHANICAL MODELING TEST BENCH G. Liseykin¹, M. Bogatyrev¹, M. Pronin¹, V. Smyslov¹; ¹TsAGI, Russia | ||||
16:30 | 17:00 | 6.9.2 |
A STUDY ON THE EFFECT OF WEAPON INSTALLATION TO AEROELASTIC CHARACTERISTIC OF FIGHTER AIRCRAFT WING R. Adhy Sasongko, Institut Teknologi Bandung, Indonesia | ||||
17:00 | 17:30 | 6.9.3 |
FLUTTER CALCULATIONS AND TRANSONIC WIND TUNNEL TESTING OF DYNAMICALLY SCALED MODEL OF THE HIGH-ASPECT-RATIO WING Y.A. Azarov¹, G.V. Liseykin¹, M.A. Pronin¹, O.A. Orlova¹; ¹TsAGI, Russia | ||||
17:30 | 18:00 | 6.9.4 |
AIRLINERS CONTROL SYSTEMS AUTOMATION FUNCTIONS ENCHANCEMENT IN BEHALF OF AIRPLANE STRUCTURAL STRENGTH V.K. Svyatodukh¹, D.E. Lopanitsyn¹, A.S. Ustinov¹; ¹TsAGI, Russia |
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16:00 | 16:30 | 7.9.1 |
FAR-FIELD FAN NOISE ESTIMATION WITH THE APPLICATION OF 3D AEROACOUSTIC CALCULATION A.A. Rossikhin¹, Y.D. Khaletskiy, Central Institute of Aviation Motors , Russia; V.I. Mileshin¹; ¹Central Institute of Aviation Motors, Russia | ||||
16:30 | 17:00 | 7.9.2 |
USING WAVES TO SIMULATE DISTORTION IN INTERNAL FLOWS IN AN AXIAL FLOW FAN K. Prashant¹, R. Bhaskar¹; ¹Indian Institute of Technology Bombay, India | ||||
17:00 | 17:30 | 7.9.3 |
DYNAMIC LOADS ACTING ON ENGINE FRAME ELEMENTS AFTER FAN BLADE OUT EVENT STUDY I.I. Ivanov¹, B.S. Blinnik¹; ¹Central Institute of Aviation Motors, Russia | ||||
17:30 | 18:00 | 7.9.4 |
NUMERICAL AND EXPERIMENTAL INVESTIGATIONS BYPASS-FLOW FANS FOR AN ADVANCED CIVIL AIRCRAFT ENGINE S.V. Pankov¹, V.I. Mileshin¹, V.N. Korzhnev¹; ¹Central Institute of Aviation Motors, Russia |
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16:00 | 16:30 | 8.9.1 |
SIMULATION OF ON-BOARD MODEL OF AIRLINER TO EVALUATE CAPABILITY OF TRAJECTORIES AND FLIGHT SAFETY S.G. Bazhen | ||||
16:30 | 17:00 | 8.9.2 |
ON THE COMPENSATION AND DAMPING OF ROLL INDUCED BY WAKE VORTICES L.M.B.C. Campos, Instituto Superior Técnico, Portugal; J.M.G. Marques, Universidade Lusófona de Humanidades e Tecnologias, Portugal | ||||
17:00 | 17:30 | 8.9.3 |
ATTITUDE PROTECTION FOR SIDE STICK-OPERATED AIRCRAFT - THE CLASSIC APPROACH Y.Q. Dong¹, L.D. Zhang¹, J.L. Ai¹; ¹Fudan University, China | ||||
17:30 | 18:00 | 8.9.4 |
SYNTHESIS OF AIRCRAFT MOTION CONTROL LAWS USING AGGREGATIVE CONTROLLER ANALYTICAL DESIGN PROCEDURE DURING AUTOMATIC IN-FLIGHT REFUELING S.P. Kostukov, Beriev Aircraft Company, Russia |
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16:00 | 16:30 | 9.9.1 |
NOISE ABATEMENT PATH PLANNING USING VIRTUAL FORCES H.M.J Kuijpers, TU Delft , Netherlands; H.G. Visser, TU Delft, Netherlands | ||||
16:30 | 17:00 | 9.9.2 |
A NON-COOPERATIVE BI-LEVEL OPTIMAL CONTROL PROBLEM FORMULATION FOR NOISE MINIMAL DEPARTURE TRAJECTORIES M. Richter¹, M. Bittner¹, M. Rieck¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TUM, Germany | ||||
17:00 | 17:30 | 9.9.3 |
MULTI-OBJECTIVE TRAJECTORY OPTIMIZATION TO REDUCE AIRCRAFT EMISSIONS IN CASE OF UNFORESEEN WEATHER EVENTS G. Serafino, Università degli studi di trieste; Selex ES, Italy | ||||
17:30 | 18:00 | 9.9.4 |
A QUASI-REAL-TIME GROUND-BASED TRAJECTORY OPTIMIZATION TOOL FOR GREENER OPERATIONS M. Micallef¹, K. Chircop¹, D. Zammit-Mangion¹, A. Sammut¹, M. Xuereb¹, A. Muscat, Qu Aero Ltd., Malta; ¹University of Malta, Malta |
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16:00 | 16:30 | 10.9.1 |
USING BCIS (BRAIN COMPUTER INTERFACES) TO EVALUATE EMOTIONAL PERCEPTION OF PASSENGER CABIN DESIGN IN VIRTUAL ENVIRONMENTS F. De Crescenzio¹, F. Lucchi¹, N. Mezannar¹, F. Persiani¹; ¹University of Bologna, Italy | ||||
16:30 | 17:00 | 10.9.2 |
NUMERICAL SIMULATIONS AND EXPERIMENTS ON THE INJECTION MOLDING OF AIRCRAFT TRANSPARENCIES T. WangY. YanL. | ||||
17:00 | 17:30 | 10.9.3 |
UNIFIED TOOLS OF DEVELOPMENT OF THE ONBOARD EQUIPMENT BASED ON THE INTEGRATED MODULAR AVIONICS I.V. Koverninskiy¹, A.V. Kan¹; ¹FSUE GosNIIAS, Russia |
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16:00 | 16:30 | 11.9.1 |
SPINNER SHED ICE ENGINE INGESTION ASSESSMENT METHODOLOGY L.P. Ruiz-Calavera¹, S. Cid-Arroyo¹, L. Benitez-Montañes¹; ¹Airbus Defense and Space, Spain | ||||
16:30 | 17:00 | 11.9.2 |
INVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI G.T. Andreev¹, V.V. Bogatyrev¹; ¹TsAGI, Russia | ||||
17:00 | 17:30 | 11.9.3 |
AIRCRAFT ICING IN FLIGHT: EFFECTS OF IMPACT OF SUPERCOOLED LARGE DROPLETS E. Norde¹, J.M. Hospers¹, E. van der Weide¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands | ||||
17:30 | 18:00 | 11.9.4 |
EXTREME INFLUENCE OF ENVIRONMENT AND RISKS OF THE FLIGHT SAFETY DEGRADATION DUE TO THE CHANGE OF THE A/C T/O-AND-L PERF L. Malysheva, Moscow State Technical University of Civil Aviation, Russia |
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16:00 | 16:30 | 12.9.1 |
LEARNING FROM THE DESIGN METHODOLOGY OF FAMOUS AEROSPACE INNOVATORS E. Kroll¹, I. Farbman¹; ¹Technion, Israel | ||||
16:30 | 17:00 | 12.9.2 |
AIRCADIA - AN INTERACTIVE TOOL FOR THE COMPOSITION AND EXPLORATION OF AIRCRAFT COMPUTATIONAL STUDIES AT EARLY DESIGN STAGE M.D. Guenov¹, M. Nunez¹, A. Molina-Cristobal¹, V.C. Datta¹, A. Riaz¹; ¹Cranfield University, United Kingdom | ||||
17:00 | 17:30 | 12.9.3 |
DOCTORAL PROGRAMS AND TRAINING: EUROPEAN PERSPECTIVES F. Quagliotti, Politecnico di Torino, Italy |
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10:00 | 10:30 | 1.10.1 |
A PARAMETRIC STUDY OF THE DEPLOYABLE WING AIRPLANE FOR MARS EXPLORATION K. Fujita, Tohoku University, Japan | ||||
10:30 | 11:00 | 1.10.2 |
LONG ENDURANCE ELECTRIC UAV FOR CIVILIAN SURVEILLANCE MISSIONS A.C. Marta, LAETA, CCTAE, Instituto Superior Técnico, Universidade de Lisboa, Portugal; P.V. Gamboa, Aerospace Sciences Department, Universidade da Beira Interior, Portugal | ||||
11:00 | 11:30 | 1.10.3 |
A GENERAL DESIGN METHODOLOGY FOR YEAR-ROUND SOLAR-POWERED STRATOSPHERIC UAVS FROM LOW TO MIDDLE LATITUDES M. Chang¹, Z. Zhou¹, R. Wang¹, X.-P. Xu¹; ¹NWPU, China | ||||
11:30 | 12:00 | 1.10.4 |
CONCEPTUAL DESIGN OF SOLAR UAV FOR LONG ENDURANCE N. Arai¹, W. Harasani, King Abdulaziz University, Saudi Arabia; K. Hiraoka¹; ¹Tokai University, Japan | ||||
12:00 | 12:30 | 1.10.5 |
THE JOINED WING SCALED DEMONSTRATOR RESULTS OF CFD A. Dziubinski¹, S. Kuprianowicz¹, K. Surmacz¹, C. Galinski¹, J. Zóltak¹; ¹Instytut Lotnictwa, Poland |
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10:00 | 10:30 | 2.10.1 |
IMPLEMENTATION OF EARSM TURBULENCE MODEL WITHIN DISCONTINUOUS GALERKIN METHOD A.I. Troshin¹, V.V. Vlasenko¹, A.V. Wolkov¹; ¹TsAGI, Russia | ||||
10:30 | 11:00 | 2.10.2 |
CONVERGENCE OF CALCULATED TRANSITION LOCI DURING COMPUTATIONAL ANALYSIS OF TRANSONIC AEROFOILS AND INFINITE SWEPT WINGS C.J. Atkin, City University, United Kingdom | ||||
11:00 | 11:30 | 2.10.3 |
APPLICATION OF SCALE ADAPTIVE SIMULATION BASED ON K-(OMEGA) SST TURBULENCE MODEL X.Y. Wang¹, D. Li¹; ¹Northwestern Polytechnical University, China | ||||
11:30 | 12:00 | 2.10.4 |
UNSTEADY FLOW OVER A SD7003 AIRFOIL AT LOW REYNOLDS NUMBERS USING A HIGH-ORDER ACCURATE FLUX RECONSTRUCTION SCHEME V. Skarolek¹, K. Miyaji¹; ¹Yokohama National University, Japan | ||||
12:00 | 12:30 | 2.10.5 |
LARGE EDDY SIMULATIONS OF TURBULENT FLOWS WITH ADVERSE PRESSURE GRADIENTS A.B. Jesus¹, L.A.C.A. Schiavo¹, J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil; W.R. Wolf, Universidade Estadual de Campinas, Brazil; ¹Instituto Tecnológico de Aeronáutica, Brazil |
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10:00 | 10:30 | 3.10.1 |
THE EFFECTS OF NONLINEARITY ON CROSSFLOW RECEPTIVITY C. Thomas¹, P. Hall¹, C. Davies, Cardiff University, United Kingdom; ¹Imperial College, United Kingdom | ||||
10:30 | 11:00 | 3.10.2 |
TRANSMISSION COEFFICIENT OF TOLLMIEN-SCHLICHTING WAVES UNDERGOING SMALL INDENTATION/HUMP DISTORTION H. Xu¹, S. Sherwin¹, P. Hall, Department of Mathematics, Imperial College London, United Kingdom; ¹Department of Aeronautics, Imperial College London, United Kingdom | ||||
11:00 | 11:30 | 3.10.3 |
THEORETICAL MODELING OF THE ELECTROGASDYNAMIC METHOD OF LAMINAR FLOW CONTROL ON A SWEPT WING S.L. Chernyshev¹, A.P. Kuryachii¹, S.V. Manuilovich ¹, D.A. Rusyanov¹, M.D. Gamirullin¹; ¹Central Aerohydrodynamic Institute, Russia | ||||
11:30 | 12:00 | 3.10.4 |
INFLUENCE OF SMALL SPATIAL PERTURBATIONS OF SUPERSONIC FLOW VELOCITY ON THE HEAT FLUX TO THE CYLINDER SURFACE I.V. Egorov, TsAGI, Russia | ||||
12:00 | 12:30 | 3.10.5 |
SEPARATED LAMINAR SHEAR LAYER TRANSITION OVER A TWO-DIMENSIONAL BUMP Y.-L. Ba¹, C. Pan¹, J.-J. Wang¹; ¹Beijing University of Aeronautics and Astronautics, China |
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10:00 | 10:30 | 5.10.1 |
INTRODUCING RESIDUAL STRESSES IN THIN ALUMINIUM STRUCTURES BY LASER GENERATED TEMPERATURE FIELDS A. Groth¹, N. Kashaev¹, N. Huber¹; ¹Helmholtz-Zentrum Geesthacht, Germany | ||||
10:30 | 11:00 | 5.10.2 |
THE COOLING GRADIENT AND MICROSTRUCTURE CONTROL IN LASER BEAM WELDED TIAL ALLOY ASSISTED BY TEMPERATURE FIELD SIMULATION J. Liu¹, P. Staron¹, D. Schnubel¹, N. Schell¹, N. Huber¹, N. Kashaev¹; ¹Helmholtz-Zentrum Geesthacht, Germany | ||||
11:00 | 11:30 | 5.10.3 |
X-RAY COMPUTER TOMOGRAPHY INVESTIGATION FOR POLYMER COMPOSITE MATERIAL UNDER THE STATIC LOAD S. Vasiliev¹, A. Artemiev¹, S. Jurgenson¹; ¹MAI, Russia | ||||
11:30 | 12:00 | 5.10.4 |
RELATIONSHIP BETWEEN POROSITY INSIDE CFRP SPECIMEN AND RESOLUTION OF MICRO X-RAY CT Y. Morimoto¹, N. Kishimoto¹; ¹Setsunan Univ., Japan | ||||
12:00 | 12:30 | 5.10.5 |
OWN SPECTRUM BANDS OF MECHANICAL SYSTEMS I. Ovchinnikov, Bauman Moscow State Technical University, Russia |
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10:00 | 10:30 | 6.10.1 |
AIRWORTHINESS INVESTIGATION OF A HIGHLY NONPLANAR FLEXIBLE WING CONCEPT K. Seywald¹, F. Hellmundt¹, A. Wildschek¹, F. Holzapfel, TUM, Germany; ¹Airbus Group Innovations, Germany | ||||
10:30 | 11:00 | 6.10.2 |
NONLINEARITIES AND UNCERTAINTIES OF AEROELASTICITY CHARACTERISTICS IN AIRCRAFT DESIGN AND CERTIFICATION M. Zichenkov¹, F. Ishmuratov¹; ¹TsAGI, Russia | ||||
11:00 | 11:30 | 6.10.3 |
AEROELASTIC BEHAVIOR OF COMPOSITE WINGS IN POSTBUCKLING REGIME L.C. de Oliveira¹, R. Degenhardt¹, T. Klimmek¹; ¹DLR, Germany | ||||
11:30 | 12:00 | 6.10.4 |
AEROELASTIC RESPONSE SIMULATION FOR DIFFERENT EXCITATION TECHNIQUES IN FLIGHT FLUTTER TEST OF MODERN CIVIL F. Yang, Shanghai Aircraft Design and Research Institute of COMAC, China; J. Xie, Civil Aviation University of China, China | ||||
12:00 | 12:30 | 6.10.5 |
NUMERICAL SIMULATION AND PARAMETRIC STUDY OF SUPERSONIC WING FLUTTER M.M. Entezari¹, M. Mohammadi-Amin¹, M.M. Alishahi, Shiraz University, Iran; ¹Astronautics Research Institute, Iran |
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10:00 | 10:30 | 7.10.1 |
EXPERIMENTAL STUDY OF SYNTHETIC JETS FOR THE CONTROL OF FLOWS SEPARATION IN THE ENGINE'S DUCTS V.A. Stepanov¹, A.Y. Makarov¹, V.P. Maslov¹; ¹CIAM, Russia | ||||
10:30 | 11:00 | 7.10.2 |
GEOMETRIC AND FLOW PARAMETERS EFFECTING THE AERO-THERMAL PERFORMANCE OF TURBOFAN FORCED MIXERS A. Mahallati, National Research Council of Canada, Canada | ||||
11:00 | 11:30 | 7.10.3 |
AERODYNAMIC DESIGN OF SINGLE-EXPANSION-RAMP NOZZLE FOR AIRCRAFT WITH SUPERSONIC CRUISE SPEED OF FLIGHT A.V. Shenkin¹, A.P. Mazurov¹, A.P. Bykov¹; ¹TsAGI, Russia | ||||
11:30 | 12:00 | 7.10.4 |
NUMERICAL INVESTIGATION OF CHARACTIRISTICS OF DUAL-CIRCUIT NOZZLES WITH CONSIDERING THE EXTERNAL FLOW M.B. Guzairov¹, I.A. Krivosheev¹, D.A. Akhmedzyanov¹, A.E. Kishalov¹, K.V. Markina¹; ¹Ufa State Aviation Technical University, Russia | ||||
12:00 | 12:30 | 7.10.5 |
SUPERSONIC NOZZLE THRUST AUGMENTATION S.A. Takovitskii, TsAGI, Russia |
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10:00 | 10:30 | 8.10.1 |
TRAJECTORY SIMULATION AND OPTIMIZATION OF THE LAPCAT-MR2 HYPERSONIC CRUISER CONCEPT T. Langener¹, S. Erb¹, J. Steelant¹; ¹ESA, Netherlands | ||||
10:30 | 11:00 | 8.10.2 |
REAL-TIME AIRCRAFT CONTINUOUS DESCENT TRAJECTORY OPTIMIZATION WITH ATC TIME CONSTRAINTS USING DIRECT COLLOCATION METHODS R. Verhoeven¹, R. Dalmau², X. Prats², N. de Gelder¹; ¹NLR, Netherlands ;²UPC, Spain | ||||
11:00 | 11:30 | 8.10.3 |
THROUGH OPTIMIZATION OF A WINGED BOOSTER TRAJECTORY OF REUSABLE AEROSPACE SYSTEM AND PECULIARITIES OF ITS FLIGHT TRY-OUT A.S. Filatyev¹, O.V. Yanova¹, N.N. Ryabukha, Gromov Flight Research Institute (FRI), Russia; ¹Central Aerohydrodynamic Institute (TsAGI), Russia | ||||
11:30 | 12:00 | 8.10.4 |
NEW PERIODIC SOLUTIONS IN THE AIRCRAFT MAXIMUM RANGE PROBLEM A.E. Sagalakov¹, A.S. Filatyev¹; ¹Central Aerohydrodynamic institute (TsAGI), Russia | ||||
12:00 | 12:30 | 8.10.5 |
CRUISE FLIGHT THROTTLE OPTIMIZATION BY APPROXIMATE DYNAMIC PROGRAMMING M. Dobrovinsky¹, J. Z. Ben-Asher¹; ¹Technion, Israel |
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10:00 | 10:30 | 9.10.1 |
CONCEPTUAL AIRCRAFT DESIGN BASED ON LIFE CYCLE ASSESSMENT A. Johanning¹, D. Scholz¹; ¹Hamburg University of Applied Sciences, Germany | ||||
10:30 | 11:00 | 9.10.2 |
HYDRAULIC SYSTEM NOISE REDUCTION BY A COMBINED CONSIDERATION OF FLUID BORNE NOISE AND STRUCTURE BORNE NOISE A. Waitschat¹, V. Pommier-Budinger, Institut Supérieur de l\'Aéronautique et de l\'Espace , France; F. Thielecke¹; ¹Hamburg University of Technology, Germany | ||||
11:00 | 11:30 | 9.10.3 |
ON SOUND ABSORPTION BY AN ACOUSTIC LINER WITH BIAS FLOW C. Legendre, Free Field Technologies, Belgium; L.M.B.C. Campos, Instituto Superior Tecnico, Portugal |
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10:00 | 10:30 | 10.10.1 |
RESEARCH ON INTEGRATION OF VAPOR CYCLE/LIQUID-COOLED REFRIGERATION SYSTEM FOR HELICOPTERS L. Hu, Nanjing Engineering Institute of Aircraft Systems,AVIC, China | ||||
10:30 | 11:00 | 10.10.2 |
OPTIMIZATION OF ADSORPTION-BASED DEHUMIDIFICATION DEVICES FOR FUEL-TANK INERTING APPLICATIONS R. Trott, EADS Innovation Works Germany, Germany | ||||
11:00 | 11:30 | 10.10.3 |
HEAT EXCHANGER THERMAL STRATIFICATION MODEL C.Y. Nakashima¹, L. Tobaldini Neto¹; ¹Embraer, Brazil | ||||
11:30 | 12:00 | 10.10.4 |
MODELING, SIMULATION AND VALIDATION OF A BLEED SYSTEM MODEL C.Y. Nakashima, Embraer, Brazil | ||||
12:00 | 12:30 | 10.10.5 |
THE EFFECT OF THE HUMIDITY ON THE CORRECTION COEFFICIENT OF THE SONIC THERMOCOUPLE USED IN AVIATION Q. Yuwu¹, Z. Ning¹, Z. Xingmin¹; ¹Xi’an Aero-engine ( Group ) Ltd., China |
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10:00 | 10:30 | 11.10.1 |
INCIDENT PREDICTION USING SUBSET SIMULATION C. Wang¹, L. Drees¹, F. Holzapfel¹; ¹Technische Universität München - Inst. of Flight System Dynamics, Germany | ||||
10:30 | 11:00 | 11.10.2 |
FE-TO-SPH APPROACH APPLIED TO THE ANALYSIS OF SOFT BODY IMPACT: BIRD STRIKE AND HAIL IMPACT A. Prato¹, M. Anghileri¹, A. Milanese¹, L.M.L. Castelletti¹; ¹Politecnico di Milano, Italy | ||||
11:00 | 11:30 | 11.10.3 |
SUPPRESSION EFFECTIVENESS OF WATER MIST ON ACCIDENTAL AIRCRAFT FIRES A. Yoshida¹, W. Ebina¹, T. Okawa¹; ¹Tokyo Denki University, Japan | ||||
11:30 | 12:00 | 11.10.4 |
USING LINEAR SHAPED CHARGE(LSC) TO FORM BAILOUT EMERGENCY EXIT F. Wenchun¹, S. Wenjuan¹; ¹First Aircraft Institute, China | ||||
12:00 | 12:30 | 11.10.5 |
NOTES TRAINING IN ATM – A NEW APPROACH USING COMPUTER-BASED SIMULATION METHODS: RESEARCH METHODS C.M. Muehlethaler¹, C.P. Knecht¹; ¹Centre for Aviation, Zurich University of Applied Sciences, Switzerland |
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10:00 | 10:30 | 12.10.1 |
FINIT DIFFERENCE MODELS FOR MECHANICS OF CONTINIUA, PROBLEM OF ACCURACY AND DOMAIN OF APPLICABILITY S.K. Godunov, Institute of Mathematics, Siberian Department of Russian Academ, Russia | ||||
10:30 | 11:00 | 12.10.2 |
CFD FOR ROTORCRAFT – RECENT PROGRESS AND NEW CHALLENGES WITH THE GOAHEAD CASE G.N. Barakos¹, R. Steijl¹, M. Woodgate¹; ¹School of Engineering - The University of Liverpool, United Kingdom | ||||
11:00 | 11:30 | 12.10.3 |
EXTREMELY HIGH ORDER AND HIGH RESOLUTION MULTIOPERATORS – BASED SCHEMES FOR CFD APPLICATIONS A.I. Tolstykh, Dorodnicyn Computing Center of Russian Academy of Sciences, Russia | ||||
11:30 | 12:00 | 12.10.4 |
SHOCK WAVE BOUNDARY LAYER INTERACTION PROCESSES. BUFFET CONTROL METHODS I.I. Lipatov¹, R.J. Tugazakov¹, F.T. Vihn¹; ¹TsAGI, Russia | ||||
12:00 | 12:30 | 12.10.5 |
PROTECTION PROBLEM FOR THIN-WALLED COMPOSITE CONSTRUCTIONS OF AIRCRAFT FROM ACTION OF RADIATIONS AND PARTICLES FLUXES A.V. Ostrik, Institute of Problems of Chemical Physics RAS, Russia; V.N. Bakulin, Institute of Applied Mechanics RAS, Russia; A.M. Matveenko, Moscow Aviation Institute, Russia |
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14:00 | 14:30 | 1.11.1 |
INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME C. Galinski, Instytut Lotnictwa, Poland; J. Hajduk, Instytut Techniczny Wojsk Lotniczych, Poland; M. Kalinowski, Politechnika Warszawska, Poland; M. Wichulski¹, L. Stefanek¹; ¹MSP, Poland | ||||
14:30 | 15:00 | 1.11.2 |
A SPECIALIZED UAV FOR SURVEILLANCE IN WINDY, TURBULENT ENVIRONMENT OF THE ANTARCTIC COAST Z.-J. Goraj, Warsaw University of Technology, Poland | ||||
15:00 | 15:30 | 1.11.3 |
DESIGN AND EXPERIMENT OF TWO-ROTORED UAV CYCLOCOPTER C.H. Lee¹, S.Y. Min², J.W. Lee², S.J. Kim¹; ¹Seoul National University, South Korea ;²Korea Aerospace Research Institute, South Korea |
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14:00 | 14:30 | 2.11.1 |
FRAMEWORK FOR LOW-NOISE WIND TURBINE BLADE DESIGN S.S. Rodrigues¹, A.C. Marta¹; ¹LAETA, CCTAE, Instituto Superior Técnico, Universidade de Lisboa, Portugal | ||||
14:30 | 15:00 | 2.11.2 |
EFFICIENT JET NOISE PREDICTION USING SYNTHETIC EDDY METHOD AND BLOCK-STRUCTURED CARTESIAN MESH Y. Fukushima, Institute of Fluid Science, Tohoku University, Japan | ||||
15:00 | 15:30 | 2.11.3 |
RESEARCH ON CORRECTIONS OF CFD SIMULATION TECHNIQUE FOR COMPLEX SHAPED CAVITY FLOW BASED ON THE WIND TUNNEL TEST DATA H.H. Huang Hu¹, J.W. Jin Wei¹, F.H.B. Fu Huanbing¹; ¹CADI 611, China |
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14:00 | 14:30 | 3.11.1 |
SINGULARITIES IN LAMINAR BOUNDARY LAYER AND FLOW STRUCTURE NEAR SINK PLANE ON CONICAL BODIES V.I. Shalaev, Moscow Institute of Physics and technology, Russia | ||||
14:30 | 15:00 | 3.11.2 |
PHYSICS PHENOMENA ACCOMPANIED STREAMLINING OF A BODY BY THE GAS-PARICLE SUPERSONIC JET A.L. Stasenko¹, G.V. Molleson¹; ¹TsAGI, Russia | ||||
15:00 | 15:30 | 3.11.3 |
EXISTENCE CRITERIA OF NON-VISCOUS VORTICAL STRUCTURES IN SHOCK LAYERS OF CONICAL GAS FLOWS F. Maksimov, Institute of Computer Aided Design, Russian Academy of Sciences, Russia |
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14:00 | 14:30 | 4.11.1 |
MULTI OBJECTIVE OPTIMIZATION OF TRANSONIC AIRFOIL USING CST METHODOLOGY WITH GENERAL AND EVOLVED SUPERCRITICAL CLASS FUNCTION P.S. Palar, The University of Tokyo, Japan |
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14:00 | 14:30 | 5.11.1 |
INNOVATIVE TECHNOLOGIES AND VIDEO CONFERENCE SYSTEMS IN TECHNOLOGICAL PROCESS OF AIRCRAFT ENGINE PRODUCTION A.M. Kachalin, Moscow Aviation Institute, Russia | ||||
14:30 | 15:00 | 5.11.2 |
UAV BASED ADVANCED MONITORING SYSTEM: FLEET AND LOGISTIC SYSTEM SIZING BY OBJECT-BASED MODEL AND MONTE-CARLO SIMULATION S. Chiesa¹, M. Fioriti¹, R. Fusaro¹; ¹Politecnico di Torino, Italy | ||||
15:00 | 15:30 | 5.11.3 |
COMPUTING SIMULATION FOR FIRE-FIGHTING HELICOPTER OPERATION ANALYSIS I.V. Borisov, Southern Federal University, Taganrog Institute of Technology, Russia; A.V. Tsipenko, Moscow Aviation Institute, Russia |
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14:00 | 14:30 | 6.11.1 |
WAKE VORTEX ENCOUNTER LOADS. FLIGHT TESTS AND NUMERICAL SIMULATIONS M.A. Torralba¹, J. Cerezo¹, S. Claverías¹, M. Reyes¹, H. Climent¹, C. Suñer¹, M. Karpel, Technion-Israel Institute of Technology, Israel; ¹Airbus Defence and Space, Spain | ||||
14:30 | 15:00 | 6.11.2 |
OPTIMALITY CRITERIA FOR STRUCTURAL DESIGN OF AIRFRAMES WITH DYNAMIC REQUIREMENTS A.I. Danilin, Samara State Aerospace University, Russia | ||||
15:00 | 15:30 | 6.11.3 |
NONLINEAR STABILITY ANALYSIS OF CARBON NANOTUBES BASED ON TIMOSHENKO BEAM THEORY AND MODIFIED COUPLE STRESS THEORY H. Dastoom Laatleyli, Sharif University of Technology, Dep. of Aerospace Eng., Iran |
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14:00 | 14:30 | 7.11.1 |
NUMERICAL INVESTIGATION ON THE CORRELATION BETWEEN SHOCK STRUCTURE AND THRUST PERFORMANCE IN AN OVEREXPANDED NOZZLE H.A. Choi¹, H.D. Kam, Hanwha Corp., South Korea; J.S. Kim¹; ¹Pukyong National University, South Korea | ||||
14:30 | 15:00 | 7.11.2 |
EFFECT OF TEMPERATURE ON FLOW CHARACTERISTICS IN SUPERSONIC IMPINGING JET USING RANS/ILES HIGH RESOLUTION METHOD L.A. Benderskiy, CIAM, Russia | ||||
15:00 | 15:30 | 7.11.3 |
INVESTIGATION OF SYNTHETIC JETS EFFICIENCY ON SEPARATION FLOW IN DIFFUSERS OF DIFFERENT GEOMETRY WITH RANS/ILES-METHOD D.A. Lyubimov¹, I.V. Potekhina¹; ¹CIAM, Russia |
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14:00 | 14:30 | 8.11.1 |
ADAPTIVE CONTROL OF AEROELASTIC SYSTEMS: AN IMMERSION AND INVARIANCE APPROACH A. Mannarino¹, P. Mantegazza¹; ¹Politecnico di Milano, Italy | ||||
14:30 | 15:00 | 8.11.2 |
L1 ADAPTIVE CONTROLLER DESIGN FOR GUST LOAD ALLEVIATION E. Capello¹, G. Guglieri¹, F. Quagliotti¹; ¹Politecnico di Torino, Italy | ||||
15:00 | 15:30 | 8.11.3 |
CONSTRAINED PREDICTIVE STRATEGIES FOR FLIGHT CONTROL SYSTEMS G. Franzè, DIMES- Università della Calabria, Italy; M. Mattei, DIII- Seconda Università di Napoli, Italy; V. Scordamaglia, DIIES - Università di Reggio Calabria, Italy |
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14:00 | 14:30 | 9.11.1 |
AUTONOMOUS TARGETED FLIGHT OF A ROTARY-WING MICRO AERIAL VEHICLE IN INDOOR, GPS-DENIED ENVIRONMENTS S. Potyagaylo¹, O. Rand¹; ¹Technion, Israel | ||||
14:30 | 15:00 | 9.11.2 |
AN APPLICATION OF DIGITAL IMAGE PROCESSING FOR UAV’S AUTOMATIC LANDING SYSTEM AID M.P. Degrande¹, E.E.T. Moreira¹, E.M. Belo¹; ¹Escola de Engenharia de São Carlos - Universidade de São Paulo, Brazil | ||||
15:00 | 15:30 | 9.11.3 |
NAVIGATION FOR VERTICAL PRECISION LANDING BASED ON OPTICAL TRACKING OF A SPATIAL RETROREFLECTIVE MARKER ARRAY P. Hartmann¹, C. Ben¹, D. Moormann¹; ¹RWTH Aachen, Germany |
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14:00 | 14:30 | 10.11.1 |
AUTOMATION IN FUTURE AIR TRANSPORT: A SCENARIO-BASED APPROACH TO THE DEFINITION OF OPERATIONAL REQUIREMENTS N.P. Randt, Technical University of Munich, Germany; S. Wolf, Munich Airport, Germany | ||||
14:30 | 15:00 | 10.11.2 |
A BIBLIOMETRICS APPLICATION FOR EVALUATING CONTRIBUTION OF A RESEARCH INSTITUTE TO SCIENCE H. Nakamura¹, Y. Kajikawa, Tokyo Institute of Technology, Japan; S. Suzuki¹; ¹The University of Tokyo, Japan | ||||
15:00 | 15:30 | 10.11.3 |
AIMING AND MISSING IN MULTIPLE DIMENSIONS D.K. Howarth, MEE Inc., United States |
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14:00 | 14:30 | 11.11.1 |
ENHANCED AND SYNTHETIC VISION SYSTEMS DEVELOPMENT BASED ON INTEGRATED MODULAR AVIONICS S.Y. Zheltov¹, Y.V. Vizilter¹, O.V. Vygolov¹; ¹State Research Institute of Aviation Systems (FGUP “GosNIIAS”), Russia | ||||
14:30 | 15:00 | 11.11.2 |
SAFETY ASPECT OF MISSION SUPPORT DISPLAY FOR HIGH-DEMAN DAERIAL WORK K. Funabiki¹, H. Tsuda¹, G. Tsuchiya¹; ¹JAXA, Japan | ||||
15:00 | 15:30 | 11.11.3 |
EMERGENCY LANDING SITE LOCATION USING AERIAL IMAGE SEGMENTATION T. Levora¹, O. Bruna¹, P. Paces¹; ¹Czech Technical University in Prague, Czech Republic |
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14:00 | 14:30 | 12.11.1 |
PRESENTATION OF HORIZON 2020 PROGRAMME R. Burger, EC, France | ||||
14:30 | 15:00 | 12.11.2 |
EREA AND FUTURE SKY J. Kaspar, EREA, Czech Republic | ||||
15:00 | 15:30 | 12.11.3 |
OVERVIEW AND RESULTS OF FP7 PROJECT AFLONEXT M. Fischer, Airbus, Germany |