ICAS 2014: TOPICS AND TITLES |
1 - Aircraft and Systems Integration |
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ICAS2014_0001: I. Berlowitz, Israel Aerospace Industries, Israel PASSENGER AIRPLANE CONVERSION TO FREIGHTER |
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ICAS2014_0068: K. Wicke¹, M. Kruse¹, F. Linke¹, V. Gollnick¹; ¹German Aerospace Center (DLR), Germany IMPACT OF INSECT CONTAMINATION ON OPERATIONAL AND ECONOMIC EFFECTIVENESS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY |
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ICAS2014_0073: A. Molina-Cristobal¹, M. Nunez¹, M.D. Guenov¹, T. Laudan², T. Druot²; ¹Cranfield University, United Kingdom; ²Airbus Operations S.A.S, France BLACK-BOX MODEL EPISTEMIC UNCERTAINTY AT EARLY DESIGN STAGE. AN AIRCRAFT POWER-PLANT INTEGRATION CASE STUDY |
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ICAS2014_0074: F Coll, Airbus Military, Spain A400M DASS SYSTEM TEST FLARES TRAJECTORY CALCULATION |
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ICAS2014_0075: R. Ghosh¹, T. Schilling¹, K. Wicke¹; ¹German Aerospace Center, Germany THEORETICAL FRAMEWORK OF SYSTEMS DESIGN FOR THE AIR TRANSPORTATION SYSTEM INCLUDING AN INHERENTLY QUANTITATIVE PHILOSOPHY OF SCENARIO DEVELOPMENT |
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ICAS2014_0089: O. Rand¹, V. Khromov¹; ¹Technion - Israel Institute of Technology, Israel OPTIMUM AND DESIGN TRENDS OF COMPOUND HELICOPTERS |
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ICAS2014_0133: D. Reckzeh, Airbus, Germany MULTIFUNCTIONAL WING MOVEABLES: DESIGN OF THE A350XWB AND THE WAY TO FUTURE CONCEPTS |
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ICAS2014_0175: M. Lengers, Airbus Operations GmbH, Germany INDUSTRIAL ASSESSMENT OF OVERALL AIRCRAFT DRIVEN LOCAL ACTIVE FLOW CONTROL |
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ICAS2014_0180: S. Kachel, Faculty of Mechatronics and Av/Military University of Technology, Poland MULTI-CRITERIAL AERODYNAMIC SYNTHESIS METHOD OF MISSION-ORIENTED AIRCRAFT DESIGN |
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ICAS2014_0202: A.V. Rozhdestvensky¹, O.S. Samsonov¹; ¹“MATI” – Russian State University of Aviation Technology, Russia DESIGN AND OPTIMIZATION OF AIRCRAFT ASSEMBLING BASED ON COMPREHENSIVE SIMULATION OF MANUFACTURING PROCESSES |
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ICAS2014_0203: E. Blanvillain, Airbus Group Innovations, France A HOLISTIC APPROACH TO HYPERSONIC AIRCRAFT DESIGN: ZEHST (ZERO EMISSION HIGH SPEED TECHNOLOGIES) |
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ICAS2014_0246: J. Rumi, Military Institute of Science and Technology, Bangladesh DESIGN AND ANALYSIS OF ULTRA-LIGHT WEIGHTED STOL AIRCRAFT |
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ICAS2014_0247: J. Rumi, Military Institute of Science and Technology, Bangladesh CEASIOM: AN OPEN SOURCE MULTI MODULE CONCEPTUAL AIRCRAFT DESIGN TOOL |
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ICAS2014_0273: M. Chang¹, Z. Zhou¹, R. Wang¹, X.-P. Xu¹; ¹NWPU, China A GENERAL DESIGN METHODOLOGY FOR YEAR-ROUND SOLAR-POWERED STRATOSPHERIC UAVS FROM LOW TO MIDDLE LATITUDES |
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ICAS2014_0299: E. Kroll¹, I. Farbman¹; ¹Technion, Israel LEARNING FROM THE DESIGN METHODOLOGY OF FAMOUS AEROSPACE INNOVATORS |
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ICAS2014_0301: J. Hanjie¹, D. Zhuoyi¹, P. Hongbin¹; ¹The First Aircraft Institute, Aviation Industry Corporation of C, China RESEARCH ON FLYING-PYLON TECHNOLOGY |
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ICAS2014_0314: P.V. Zhuravlev, MAI, Russia APPLICATION OF FLEET CREATION PROBLEMS IN AIRCRAFT PRE-DESIGN |
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ICAS2014_0394: J.P. Fielding¹, A.J. Stewart¹, G.S. Ji¹, G. Rojas¹; ¹Cranfield University, United Kingdom CONCEPTUAL DESIGN OF THREE ALTERNATIVE CONFIGURATIONS OF NEW-GENERATION 19-SEAT BUSH AIRCRAFT |
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ICAS2014_0425: G. La Rocca¹, M. Li¹, P.P.M. van der Linden¹, R.J.M. Elmendorp¹; ¹Delft University of Technology, Netherlands CONCEPTUAL DESIGN OF A PASSENGER AIRCRAFT FOR AERIAL REFUELING OPERATIONS |
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ICAS2014_0428: J. Steelant¹, T. Langener¹; ¹ESA-ESTEC, Netherlands THE LAPCAT-MR2 HYPERSONIC CRUISER CONCEPT |
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ICAS2014_0451: G.A. Popov , Research Institute of Applied Mechanics and Electrodynamics , Russia; V.M. Kulkov¹, V.G. Petukhov¹; ¹Research Institute of Applied Mechanics and Electrodynamics, Russia ANALYSIS FOR POSSIBILITY TO USE SPACE PLATFORM WITH ELECTRIC PROPULSION SYSTEM IN COMBINATION WITH THE LAUNCH VEHICLE FOR AIR LAUNCH |
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ICAS2014_0475: T. Yuhara¹, K. Rinoie, University of Tokyo, Japan; Y. Makino¹; ¹JAXA, Japan CONCEPTUAL DESIGN STUDY ON LH2 FUELED SST - ENVIRONMENTAL IMPACTS REDUCED BY AIRFRAME/PROPULSION SYSTEM INTEGRATION - |
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ICAS2014_0477: L. Mo, Delft University of Technology, Netherlands CONCEPTUAL TANKER DESIGN FOR CIVIL OPERATIONS |
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ICAS2014_0478: K. Fujita, Tohoku University, Japan A PARAMETRIC STUDY OF THE DEPLOYABLE WING AIRPLANE FOR MARS EXPLORATION |
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ICAS2014_0484: R. Zhang¹, H. Du¹, D.-G. Cui, AVIC, China; ¹Chinese Aeronautical Establishment, China OPTIMIZATION DESIGN OF COMPOSITE WING WITH MULTIPLE LOAD CASES AND LARGE SCALE DESIGN VARIABLES |
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ICAS2014_0505: M. Honda¹, K. Yoshida¹; ¹JAXA, Japan D-SEND#2 FLIGHT DEMONSTRATION FOR LOW SONIC BOOM DESIGN TECHNOLOGY |
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ICAS2014_0506: Z. Xu, Beihang University, China; D. Cui, AVIC, China; H. Du, Chinese Aeronautical Establishment, China A RESEARCH ON ACCELERATED SEARCH GENETIC ALGORITHM OPTIMIZATION PLATFORM ORIENTED TO AIRCRAFT AERODYNAMIC DESIGN |
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ICAS2014_0514: A. Dziubinski¹, S. Kuprianowicz¹, K. Surmacz¹, C. Galinski¹, J. Zóltak¹; ¹Instytut Lotnictwa, Poland THE JOINED WING SCALED DEMONSTRATOR RESULTS OF CFD |
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ICAS2014_0520: D. Böhnke¹, B. Nagel¹, V. Gollnick¹; ¹DLR e.V., Germany EXPLICIT MODELING OF TECHNOLOGY IMPROVEMENT OVER TIME IN CONCEPTUAL AIRCRAFT DESIGN |
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ICAS2014_0524: W. Stalewski, INSTITUTE of AVIATION, Poland WING-LOAD CONTROL BASED ON THE \"LEAKY WING\" CONCEPT |
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ICAS2014_0547: A.C. Marta, LAETA, CCTAE, Instituto Superior Técnico, Universidade de Lisboa, Portugal; P.V. Gamboa, Aerospace Sciences Department, Universidade da Beira Interior, Portugal LONG ENDURANCE ELECTRIC UAV FOR CIVILIAN SURVEILLANCE MISSIONS |
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ICAS2014_0551: C. Galinski, Instytut Lotnictwa, Poland; J. Hajduk, Instytut Techniczny Wojsk Lotniczych, Poland; M. Kalinowski, Politechnika Warszawska, Poland; M. Wichulski¹, L. Stefanek¹; ¹MSP, Poland INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME |
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ICAS2014_0600: R.C Munjulury¹, I. Staack¹, A. Abdalla, USP, Brazil; T. Melin¹, C. Jouannet¹, P. Krus¹; ¹Linköping University, Sweden KNOWLEDGE-BASED DESIGN FOR FUTURE COMBAT AIRCRAFT CONCEPTS |
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ICAS2014_0621: I. Staack¹, R.C. Munjulury ¹, T. Melin¹, A. Abdalla, University of São Carlos, Brazil; P. Krus¹; ¹Linköping University, Sweden CONCEPTUAL AIRCRAFT DESIGN MODEL MANAGEMENT DEMONSTRATED ON A 4TH GENERATION FIGHTER |
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ICAS2014_0630: A. Ueno¹, Y. Watanabe¹; ¹JAXA, Japan PROPULSION/AIRFRAME INTEGRATION CONSIDERING LOW DRAG AND LOW SONIC BOOM |
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ICAS2014_0693: Z.-J. Goraj, Warsaw University of Technology, Poland A SPECIALIZED UAV FOR SURVEILLANCE IN WINDY, TURBULENT ENVIRONMENT OF THE ANTARCTIC COAST |
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ICAS2014_0695: A. Yaremenko, MAI, Russia NUMERICAL RESEARCH OF MUTUAL INFLUENCE OF X-43A AIRFRAME AND SCRAMJET IN MANEUVERING |
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ICAS2014_0697: R.B. Jacobs¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States FORMULATION OF AN EXPERIMENT SELECTION METHODOLOGY FOR UNCERTAINTY REDUCTION AND APPLICATION TO ACTIVE FLOW CONTROL |
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ICAS2014_0719: H. Djojodihardjo, Universiti Putra Malysia, Malaysia; M. Anas Bin Abd Bari, Universiti Putra Malaysia, Malaysia CONCEPTUAL DESIGN STUDY OF QUAD-BUBBLE-BUSINESS JET |
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ICAS2014_0725: C.H. Lee¹, S.Y. Min², J.W. Lee², S.J. Kim¹; ¹Seoul National University, South Korea; ²Korea Aerospace Research Institute, South Korea DESIGN AND EXPERIMENT OF TWO-ROTORED UAV CYCLOCOPTER |
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ICAS2014_0740: J. Fuchte¹, T. Pfeiffer¹, P.D. Ciampa¹, B. Nagel¹, V. Gollnick¹; ¹German Aerospace Center, Germany OPTIMIZATION OF REVENUE SPACE OF A BLENDED WING BODY |
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ICAS2014_0750: T. Pfeiffer¹, E. Moerland¹, D. Böhnke¹, B. Nagel¹, V. Gollnick¹; ¹German Aerospace Center, Germany AIRCRAFT CONFIGURATION ANALYSIS USING A LOW-FIDELITY, PHYSICS BASED AEROSPACE FRAMEWORK UNDER UNCERTAINTY CONSIDERATIONS |
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ICAS2014_0752: H. Ishikawa, TOUA Co. Ltd., Japan; N. Tokugawa¹, Y. Ueda, Tokyo Business Service Co. Ltd., Japan; K. Yoshida¹; ¹JAXA, Japan NATURAL LAMINAR FLOW WING DESIGN OF SUPERSONIC TRANSPORT AT HIGH REYNOLDS NUMBER CONDITION |
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ICAS2014_0776: R. Elmendorp¹, R. Vos¹, G. La Rocca¹; ¹TU Delft, Netherlands A CONCEPTUAL DESIGN AND ANALYSIS METHOD FOR CONVENTIONAL AND UNCONVENTIONAL AIRPLANES |
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ICAS2014_0823: H. Choi, Hanyang Univetsity, South Korea AERODYNAMIC ANALYSIS OF THE BWB BUSINESS JET USING DSTRIDUTED PROPULSION SYSTEM |
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ICAS2014_0835: T. Fujikawa, The University of Tokyo, Japan KNOWLEDGE DISCOVERY IN CONCEPTUAL DESIGN OF SPACE PLANES USING MULTI-OBJECTIVE OPTIMIZATION AND DATA MINING |
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ICAS2014_0853: 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 RECENT ADVANCES IN AIRFRAME-PROPULSION CONCEPTS WITH DISTRIBUTED PROPULSION |
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ICAS2014_0879: K.-S. Zhang¹, A. Bakar¹, P.-B. Ji¹, Z.-H. Han¹, X.-P. Li¹; ¹Northwestern Polytechnical University, China MULTIDISCIPLINARY OPTIMIZATION OF TRUSS-BRACED WING LAYOUT |
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ICAS2014_0884: M.D. Guenov¹, M. Nunez¹, A. Molina-Cristobal¹, V.C. Datta¹, A. Riaz¹; ¹Cranfield University, United Kingdom AIRCADIA - AN INTERACTIVE TOOL FOR THE COMPOSITION AND EXPLORATION OF AIRCRAFT COMPUTATIONAL STUDIES AT EARLY DESIGN STAGE |
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ICAS2014_0886: S. Defoort, Onera, France LAPCAT-II: DESIGN OF A COMBINED PROPULSION SYSTEM FOR A HYPERSONIC CRUISER |
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ICAS2014_0887: N. Arai¹, W. Harasani, King Abdulaziz University, Saudi Arabia; K. Hiraoka¹; ¹Tokai University, Japan CONCEPTUAL DESIGN OF SOLAR UAV FOR LONG ENDURANCE |
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ICAS2014_0930: D. Duritsyn¹, A. Ternovoy¹, D. Krivonosova¹, V. Sokolyansky, Central Aerohydrodynamic Institute, TsAGI, Russia; ¹Beriev Aircraft Company, Russia THE BE-200ES FIREFIGHTING AMPHIBIOUS AIRCRAFT EFFECTIVENESS DURING THE FIRE SEASONS 2004÷2011 YEARS IN THE EUROPEAN UNION COUNTRIES |
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ICAS2014_0934: J.R. Kizer¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States SET-BASED DESIGN SPACE EXPLORATION ENABLED BY DYNAMIC CONSTRAINT ANALYSIS |
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ICAS2014_0966: K. Mizobata¹, R. Minato¹, K. Higuchi¹, M. Ueba¹, S. Takagi¹, D. Nakata¹, N. Katsumata¹, K. Higashino¹, N. Tanatsugu¹; ¹Muroran Institute of Technology, Japan DEVELOPMENT OF A SMALL-SCALE SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED |
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ICAS2014_1003: S. Andreev¹, V. Makarov¹, J.P. Fedorchenko¹, N.V. Berseneva¹; ¹CIAM, Russia THE NUMERICAL ANALYSIS OF IMPACT OF CHANGES IN FLIGHT CONDITIONS AND IN ENGINE'S REGIME AT CRUISE ON AIRPLANE'S AERODYNAMIC CHARACTERISTICS |
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ICAS2014_1009: S. Bagassi¹, F. Lucchi¹, F. Persiani¹; ¹University of Bologna, Italy AIRCRAFT PRELIMINARY DESIGN: GENETIC ALGORITHM BASED OPTIMIZATION METHOD |
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ICAS2014_1021: C. Döll¹, B. Paluch¹, A. Guigon¹, D. Fraboulet, CEA Tech, France; ¹ONERA - The French Aerospace Lab, France CONCEPTUAL FEASIBILITY STUDY FOR A FULLY ELECTRICALLY POWERED REGIONAL TRANSPORT AIRCRAFT |
2.1 - Aerodynamics - CFD Methods and Validation |
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ICAS2014_0015: V.V. Riabov, Rivier University, United States THE ANALYSIS OF UNDEREXPANDED JET FLOWS FOR HYPERSONIC AEROTHERMODYNAMIC APPLICATIONS |
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ICAS2014_0040: X.Y. Wang¹, D. Li¹; ¹Northwestern Polytechnical University, China APPLICATION OF SCALE ADAPTIVE SIMULATION BASED ON K-(OMEGA) SST TURBULENCE MODEL |
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ICAS2014_0062: I.A. Gubanova¹, M.A. Gubanova¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia INVERSE METHODS FOR AERODYNAMIC DESIGN USING THE NAVIER-STOKES EQUATIONS |
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ICAS2014_0072: C. Xu¹, C. Bil¹, C.P. Cheung¹; ¹RMIT University, Australia FLUID DYNAMICS ANALYSIS OF A COUNTER ROTATING DUCTED PROPELLER |
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ICAS2014_0076: A.I. Troshin¹, V.V. Vlasenko¹, A.V. Wolkov¹; ¹TsAGI, Russia IMPLEMENTATION OF EARSM TURBULENCE MODEL WITHIN DISCONTINUOUS GALERKIN METHOD |
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ICAS2014_0085: 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 CFD BASED OPTIMIZATION OF HIGH-LIFT DEVICES USING A MESH MORPHING TECHNIQUE |
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ICAS2014_0092: L. Tysell, FOI, Sweden STUDY OF INSTALLATION EFFECTS ON A HIGH-LIFT WING SECTION IN AN OPEN WIND TUNNEL |
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ICAS2014_0094: M.A. Gubanova¹, N.N. Bragin¹, E.S. Perchenkov¹, A.Y. Slitinskaya¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia HIGH-LIFT SYSTEM DESIGN BY NUMERICAL METHODS AND WIND TUNNEL VERIFICATION |
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ICAS2014_0101: Y.M. Ignatkin¹, P.V. Makeev¹, A.I. Shomov¹; ¹Moscow aviation institute, Russia COMPUTATIONAL MODELING OF HELICOPTER'S MAIN AND TAIL ROTOR INTERFERENCE ON THE BASE OF NON-LINEAR BLADE VORTICAL MODEL |
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ICAS2014_0108: 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 LARGE EDDY SIMULATIONS OF TURBULENT FLOWS WITH ADVERSE PRESSURE GRADIENTS |
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ICAS2014_0128: J. Kim, Korea Aerospace Research Institute(KARI), South Korea; K. Kim, Seoul National University, South Korea A DEVELOPMENT AND VERIFICATION OF DENSITY BASED SOLVER USING LU-SGS ALGORITHM IN OPENFOAM |
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ICAS2014_0173: O.V. Karas, TsAGI, Russia EFFICIENT STATIONARY AND NONSTATIONARY AERODYNAMIC CALCULATION ALGORITHMS FOR THE APPLIED AERODYNAMICS PROBLEMS |
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ICAS2014_0176: F. Nicolosi¹, S. Corcione¹, P. Della Vecchia¹; ¹UNIVERSITY OF NAPLES FEDERICO II, Italy COMMUTER AIRCRAFT AERODYNAMIC DESIGN: WIND-TUNNEL TESTS AND CFD ANALYSIS |
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ICAS2014_0181: D.S. Ivanyushkin¹, S.A. Takovitskii¹; ¹TsAGI, Russia NOSES OF MINIMAL WAVE DRAG IN SUPERSONIC FLOW |
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ICAS2014_0220: R.Z. Nigmatullin, CIAM , Russia; L.V. Terentyeva , CIAM, Russia ANALYSIS OF TONAL NOISE OF LPT BASED ON UNSTEADY GAS FLOW CALCULATIONS |
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ICAS2014_0263: D.G. Romano¹, M. Mancini¹; ¹Piaggio Aero Industries S.p.A., Italy AERODYNAMIC OPTIMIZATION OF A GREEN ATF REGIONAL AIRCRAFT IN CRUISE CONDITION |
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ICAS2014_0268: H.H. Huang Hu¹, J.W. Jin Wei¹, F.H.B. Fu Huanbing¹; ¹CADI 611, China RESEARCH ON CORRECTIONS OF CFD SIMULATION TECHNIQUE FOR COMPLEX SHAPED CAVITY FLOW BASED ON THE WIND TUNNEL TEST DATA |
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ICAS2014_0271: C.H. Zhou, Nanjing University of Aeronautics and Astronautics, China A MESH ADAPTATION METHOD FOR SIMULATION OF UNSTEADY FLOWS |
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ICAS2014_0290: X.-P. Li¹, W.-P. Song¹, Z.-H. Han¹; ¹Northwestern Polytechnical Universtity, China NUMERICAL INVESTIGATION OF FUSELAGE-STABILIZER-CONTROL SURFACE INTERFERENCE FOR A HYPERSONIC WAVERIDER VEHICLE |
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ICAS2014_0295: L. Haixu¹, G. Yincheng¹, L. Wenyi¹; ¹Tsinghua University, China NUMERICAL INVESTIGATION OF LIQUID JET INJECTION INTO A SUPERSONIC CROSSFLOW |
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ICAS2014_0300: H. Strüber, Airbus Operations GmbH, Germany; J. Wild, Deutsches Zentrum für Luft- und Raumfahrt, Germany AERODYNAMIC DESIGN OF A HIGH-LIFT SYSTEM COMPATIBLE WITH A NATURAL LAMINAR FLOW WING WITHIN THE DESIREH PROJECT |
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ICAS2014_0310: O. Tretiyakova, MAI, Russia NUMERICAL SIMULATION OF MULTIPLE TURBULENT SUPERSONIC UNDEREXPANDED JETS |
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ICAS2014_0321: S. Bosnyakov¹, I. Kursakov¹, A. Lysenkov¹, S. Mikhaylov¹; ¹TsAGI, Russia NUMERICAL SIMULATION OF UNSTEADY FLOWS AROUND HIGH-LIFT CONFIGURATIONS |
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ICAS2014_0370: M. Sutherland¹, J. Etele¹; ¹Carleton University, Canada URBAN WIND FIELD GENERATION USING LES FOR APPLICATION TO QUADROTOR FLIGHT |
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ICAS2014_0402: R.V. Bulbovich¹, V.V. Pavlogradskiy¹, V.V. Palchikovskiy¹; ¹Perm National Research Polytechnic University, Russia THE PROCEDURE OF LINER IMPEDANCE EDUCTION BY FINITE ELEMENT METHOD |
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ICAS2014_0407: F. Nicolosi¹, P. Della Vecchia¹, D. Ciliberti ¹, V. Cusati¹; ¹University of Naples Federico II, Italy DEVELOPMENT OF NEW PRELIMINARY DESIGN METHODOLOGIES FOR REGIONAL TURBOPROP AIRCRAFT BY CFD ANALYSES |
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ICAS2014_0417: A.N. Zamyatin¹, M.A. Grigoryev¹, V.V. Rogozin¹, A.I. Zhelannikov, TsAGI, Russia; ¹GFRI, Russia MATHEMATICAL MODEL OF AIRCRAFT WAKE VORTICES DEVELOPMENT FOR TAKE-OFF/LANDING PHASES FOR WAKE VORTEX SAFETY SYSTEMS |
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ICAS2014_0468: L.T.L.C. Paolicchi¹, W.F.N. Santos¹; ¹National Institute for Space Research (INPE), Brazil MACH NUMBER EFFECT ON THE FLOWFIELD STRUCTURE OF HYPERSONIC GAP FLOWS |
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ICAS2014_0472: Y.I. Khlopkov, Central Aerohydrodynamic Institute, Russia; A.Y. Khlopkov¹, Z.Y. Myo Myint¹, T.V. Vyong¹; ¹Moscow Institute of Physics and Technology, Russia MONTE CARLO METHODS IN APPLIED MATHEMATICS AND COMPUTATIONAL AERODYNAMICS |
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ICAS2014_0499: K. Anisimov¹, E. Kazhan¹, A. Lysenkov¹; ¹TsAGI, Russia COMPUTATIONAL METHOD FOR STEADY FLOW (RANS) USING ZONAL APPROACH AND ITS IMPLEMENTATION EXPERIENCE FOR SOLUTION OF TASK OF INTERFERENCE ENGINE AND AIRFRAME |
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ICAS2014_0532: L.-J. li, Northwestern Polytechnical University, China NUMERICAL INVESTIGATION OF FLUID FLOW BASED ON ZONAL IDDES METHOD |
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ICAS2014_0549: B.-G. Mi¹, H. Zhan¹, B. Wang¹; ¹Northwestern Polytechnical University, China COMPUTATIONAL INVESTIGATION OF SIMULATION ON THE DYNAMIC DERIVATIVES OF FLIGHT VEHICLE |
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ICAS2014_0560: 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 NUMERICAL INVESTIGATION ON ENGINE INLET DISTORTION UNDER CROSSWIND FOR A COMMERCIAL TRANSPORT AIRCRAFT |
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ICAS2014_0566: A. Rumyantsev¹, V. Silantyev¹; ¹FSUE “SibNIA named after S.A. Chaplygin”, Russia NUMERICAL AND EXPERIMENTAL STUDY OF A FLOW OVER STRAIGHT AND SWEPT HIGH-LIFT WINGS |
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ICAS2014_0573: V.A. Levin, Institute of mechanics MSU, Russia THE STUDY OF NONQUILIBRIUM GAS-DYNAMIC PROCESSES IN THE FLOW AROUND BODIES IN THE WIND TUNNEL IT-2M TSAGI |
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ICAS2014_0589: S.S. Rodrigues¹, A.C. Marta¹; ¹LAETA, CCTAE, Instituto Superior Técnico, Universidade de Lisboa, Portugal FRAMEWORK FOR LOW-NOISE WIND TURBINE BLADE DESIGN |
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ICAS2014_0599: K.A. Makarov¹, A.A. Pavlenko¹; ¹TsAGI, Russia NUMERICAL INVESTIGATION OF AN AILERON HINGE MOMENTS AND EFFECTIVENESS ON A HIGH LIFT WING AIRFOIL |
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ICAS2014_0616: V. Skarolek¹, K. Miyaji¹; ¹Yokohama National University, Japan UNSTEADY FLOW OVER A SD7003 AIRFOIL AT LOW REYNOLDS NUMBERS USING A HIGH-ORDER ACCURATE FLUX RECONSTRUCTION SCHEME |
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ICAS2014_0619: V.V. Gorsky¹, V.G. Resh¹; ¹MIC NPO MASHINOSTROYENIA, Russia THE STUDY OF CARBON MATERIAL’S AEROTHERMOCHEMICAL DESTRUCTION IN COMBUSTION PRODUCTS OF LIQUID-PROPELLANT ROCKET ENGINES |
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ICAS2014_0622: A.S. Batrakov¹, A.N. Kusyumov¹, G. Barakos, The University of Liverpool, United Kingdom; ¹KNRTU-KAI, Russia SIMULATION OF FLOW AROUND FUSELAGE OF HELICOPTER USING ACTUATOR DISC THEORY |
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ICAS2014_0634: E.V. Larina¹, I.A. Kryukov¹, I.E. Ivanov¹; ¹Moscow Aviation Institute (National Research University), Russia NUMERICAL SIMULATION OF HIGH-SPEED SEPARATION FLOW IN THE AEROSPACE PROPULSION SYSTEMS |
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ICAS2014_0642: A.A. Aksenov, TESIS, Russia; A.A. Dyadkin ¹, S.P. Rybak ¹, T.V. Simakova ¹; ¹RSC Energia, Russia NUMERICAL SOLVING PROBLEMS OF SPACECRAFT DESIGN |
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ICAS2014_0667: A.M. Molchanov, Moscow Aviation Institute, Russia NUMERICAL SIMULATIONT OF GAS AND MULTIPHASE SUPERSONIC JETS WITH NON-EQUILIBRIUM PROCESSES |
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ICAS2014_0687: M.M. Dubinina¹, M.Y. Sorokin¹; ¹PJSC “Ulyanovsk instrument manufacturing design bureau”, Russia INFLUENCE NUMERICAL SCHEMES TO ESTIMATE ERROR OF AIR PRESSURE PROBE |
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ICAS2014_0707: C.-J. WU¹, L.-L. ZHU¹; ¹School of Aeronautics and Astronautics, DUT, China NUMERICAL SIMULATION OF SELF-PROPELLED FLYING OF A THREE-DIMENSIONAL BIRD WITH FLAPPING WINGS |
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ICAS2014_0738: M. Sueki¹, T. Mizukaki¹; ¹Tokai University, Japan NUMERICAL ANALYSIS OF SHOCK WAVES BEHAVIOR AROUND AERODYNAMIC DECELERATOR FOR MARS PLANETARY PROBE |
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ICAS2014_0739: 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 CFD-BASED COLLABORATIVE DESIGN OPTIMIZATION USING ECFD |
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ICAS2014_0774: L.I. Garipova¹, A.N. Kusyumov¹, G.N. Barakos, The University of Liverpool, United Kingdom; ¹KNRTU-KAI, Russia CFD MODELING OF 2D AEROFOIL DYNAMIC STALL |
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ICAS2014_0788: H. Takano¹, K. Fukuda¹; ¹Tokai University, Japan NUMERICAL INVESTIGATION OF FLOW AROUND AN AIRFOIL WITH UNSTEADY MOVING |
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ICAS2014_0796: A. Stephan¹, F. Holzäpfel¹, T. Misaka, Tohoku University, Institute of Fluid Science, Japan; ¹Deutsches Zentrum für Luft- und Raumfahrt (DLR), Germany SIMULATION OF AIRCRAFT WAKE VORTICES DURING LANDING WITH DECAY ENHANCING OBSTACLES |
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ICAS2014_0818: K. Kondo, Tokyo University of Science, Japan COMPUTATIONAL COMPARATIVE STUDY FOR DESIGN OF LOW REYNOLDS NUMBER AIRFOIL |
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ICAS2014_0839: J.H. Lee, Chungnam National University, Russia; L. Kartovitskiy¹, A. Tsipenko¹; ¹Moscow Aviation Institute (National Research University), Russia NUMERICAL AND EXPERIMENTAL INVESTIGATION OF NON-STATIONARY PROCESSES IN SUPERSONIC GAS EJECTOR |
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ICAS2014_0842: D. Sasaki, Kanazawa Institute of Technology, Japan; K. Nakahashi, JAXA, Japan RAPID LARGE-SCALE CARTESIAN MESHING FOR AERODYNAMIC COMPUTATIONS |
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ICAS2014_0848: E.J. Fahy, The University of Queensland, Australia LABORATORY AND FLIGHT COMPARISONS OF HAYABUSA WITH ABLATION AND RADIATION EFFECTS |
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ICAS2014_0851: J.Y. Huh¹, K.H. Kim¹, S.Y. Jung, Agency for Defense Development, South Korea; ¹Seoul National University, South Korea MESHLESS METHOD FOR SIMULATION OF COMPRESSIBLE REACTING FLOW |
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ICAS2014_0874: K. Matsushima¹, I. Yamamichi¹, N. Tokugawa, JAXA, Japan; ¹University of Toyama, Japan AERODYNAMIC DESIGN METHOD FOR SUPERSONIC SLENDER BODY USING AN INVERSE PROBLEM |
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ICAS2014_0888: Y. Fukushima, Institute of Fluid Science, Tohoku University, Japan EFFICIENT JET NOISE PREDICTION USING SYNTHETIC EDDY METHOD AND BLOCK-STRUCTURED CARTESIAN MESH |
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ICAS2014_0894: S. Alexandrov, TsAGI, Russia VISCOUS HYPERSONIC GAS FLOW CHARACTERISTICS OVER THE DELTA WING WITH BLUNT LEADING EDGES |
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ICAS2014_0908: S. Watanabe¹, S. Kuchi-ishi¹, K. Murakami¹, A. Hashimoto¹, H. Kato¹, K. Yasue¹, H. Saiki², J. Ogino²; ¹JAXA, Japan; ²Ryoyu Systems Co., Ltd., Japan DAHWIN - DIGITAL/ANALOG-HYBRID WIND TUNNEL - FOR INNOVATIVE EFD/CFD INTEGRATION |
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ICAS2014_0913: N.-A Sidenko, Research-and-development center “CENTRE COMPOSITE” Joint Venture, Latvia COMPUTER MODELLING TECHNIQUE AERODYNAMIC CHARACTERISTICS MODELLING OF THE STAND WITH LONG-RANGE LARGE DIAMETER AIR JET |
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ICAS2014_0918: T. Sulaiman¹, S. Sekimoto¹, T. Nonomura², M. Anyoji², K. Fujii²; ¹University of Tokyo, Japan; ²ISAS / JAXA, Japan DBD PLASMA ACTUATOR MULTI-OBJECTIVE DESIGN OPTIMIZATION AT REYNOLDS NUMBER 63,000 : STROUHAL NUMBER EFFECT |
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ICAS2014_0929: M. Hayashi, University of São Paulo, Brazil ON THE USE OF THE ADJOINT METHOD TO COMPUTE NON--GEOMETRIC SENSITIVITIES |
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ICAS2014_0933: 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 AERODYNAMIC INTERFERENCE OF WINGTIP AND WING DEVICES ON BWB MODEL |
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ICAS2014_0940: K. Surmacz, Institute of Aviation, Poland DYNAMICS OF A VORTEX RING AROUND A MAIN ROTOR HELICOPTER |
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ICAS2014_0953: O. Kotsur¹, G. Scheglov, BMSTU, Russia; P. Leyland¹; ¹EPFL, Switzerland VERIFICATION OF MODELLING OF FLUID-STRUCTURE INTERACTION (FSI) PROBLEMS BASED ON EXPERIMENTAL RESEARCH OF BLUFF BODY OSCILLATIONS IN FLUIDS |
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ICAS2014_0964: C.W. Skaleski, Instituto Tecnológico de Aeronáutica, Brazil; F.I.K. Odaguil¹, J.H.A. Azevedo¹, L.S.M. Lima¹, R.A.S. Cardoso¹, P.H. Iscold, Universidade Federal de Minas Gerais, Brazil; ¹Embraer, Brazil CFD – BASED STUDY ON GOLDSCHMIED PROPULSION CONCEPT APPLICATION FOR DRAG REDUCTION |
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ICAS2014_0970: C.J. Atkin, City University, United Kingdom CONVERGENCE OF CALCULATED TRANSITION LOCI DURING COMPUTATIONAL ANALYSIS OF TRANSONIC AEROFOILS AND INFINITE SWEPT WINGS |
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ICAS2014_1010: T. Wan¹, Y.S. Chen¹; ¹Tamkang University, Taiwan ON THE OPTIMIZATION OF BLENDED WING BODY AIRCRAFT CONFIGURATION VIA THE SURROGATE MODELING METHOD |
2.2 - Experimental Aerodynamics |
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ICAS2014_0098: V.N. Kovrizhina¹, E.S. Shapoval, FSUE TsAGI, Russia; G.M. Zharkova¹; ¹Khristianovich Institute of Theoretical and Applied Mechanics, Russia PROBLEMS AND ACHIEVEMENTS IN PANORAMIC SHEAR STRESS DIAGNOSTICS BY LIQUID CRYSTALS |
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ICAS2014_0113: M. Samardzic¹, Z. Anastasijevic ¹, D. Marinkovski ¹, J. Isakovic, Tehnikum Taurunum-College of Applied Engineering Studies, Serbia; ¹Military Technical Institute (VTI), Serbia MEASUREMENT OF THE CROSS-COUPLING DERIVATIVES DUE TO PITCHING IN THE HIGH REYNOLDS NUMBER BLOWDOWN WIND TUNNEL |
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ICAS2014_0124: V.I. Birukov¹, N.N. Bragin¹, M.F. Garifulin¹, S.I. Skomorokhov¹, V.V. Yanin¹; ¹TsAGI, Russia INVESTIGATION OF UNSTEADY FLOW ON A HIGH ASPECT RATIO WING |
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ICAS2014_0138: D. Vukovic¹, D. Curcic¹, D. Marinkovski¹, D. Damljanovic¹, M. Samardžic¹, A. Vitic¹; ¹Vojnotehnicki institut, Serbia LIVING WITH SUPERSONIC STARTING LOADS IN THE T-38 TRISONIC WIND TUNNEL OF VTI |
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ICAS2014_0162: D. Damljanovic¹, B. Rasuo, Faculty of Mechanical Engineering University of Belgrade, Serbia; S. Mandic¹, D. Vukovic¹, J. Isakovic, College of Applied Engineering Studies, Serbia; ¹Military Technical Institute (VTI), Serbia USABILITY OF COMPARATIVE EXPERIMENTAL - NUMERICAL SUPERSONIC TEST CASES WITH THE HB REFERENCE MODEL |
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ICAS2014_0190: S.A. Glazkov¹, A.R. Gorbushin¹, I.A. Kursakov¹; ¹Central Aerohydrodynamic Institute, Russia FIN AND REAR STINGS SUPPORT EFFECTS ON THE FLOW AROUND THE AIRCRAFT MODEL |
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ICAS2014_0230: T. Ukai¹, Y. Saito¹, K. Miyakoshi¹, T. Yamaguchi¹, K. Ohtani¹, S. Obayashi¹; ¹Institute of Fluid Science, Japan LONG RISE-TIME PRESSURE SIGNATURE THROUGH JET TURBULENCE IN A LABORATORY-SCALE EXPERIMENT |
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ICAS2014_0302: S.M. Roux¹, G.I. Mahmood¹, J.P. Meyer¹; ¹University of Pretoria, South Africa FLOW FIELD AROUND DIMPLED SHORT PIN-FINS IN A STAGGERED ARRAY |
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ICAS2014_0354: V.V. Petronevich¹, Y.V. Kartashev¹, A.R. Gorbushin¹, K.D. Bukharov¹; ¹FSUE, Russia REALIZATION OF A CONTINUOUS BALANCE TESTING PROCEDURE IN A COMPRESSOR-DRIVEN TRANSONIC WIND TUNNEL |
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ICAS2014_0362: J. Ertveldt¹, J. Schoukens¹, R. Pintelon¹, S. Vanlanduit¹; ¹Vrije Universiteit Brussel, Belgium DESIGN AND VALIDATION OF A FORCED MOTION VARIABLE STIFFNESS AEROELASTIC WIND TUNNEL APPARATUS (AATB) |
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ICAS2014_0374: A.P. Kiselev¹, V.A. Kuzminsky¹, D.S. Sboev¹; ¹TsAGI, Russia THE LAMINAR-TURBULENT TRANSITION ZONE IN 2D AND 3D BOUNDARY LAYERS WITH EMPHASIS ON EFFECT OF FREE STREAM TURBULENCE |
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ICAS2014_0376: G.G. Gadzhimagomedov¹, V.A. Vlasov¹, V.M. Lutovinov¹; ¹Central Aerohydrodynamic Institute, Russia EXAMPLES OF PIV APPLICATIONS TO SUBSONIC FLOWS |
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ICAS2014_0399: M.A. Brutyan¹, A.V. Petrov¹, A.V. Potapchik¹; ¹TsAGI, Russia APPLICATION OF LIGHT SCATTERING EFFECT IN AERODYNAMIC EXPERIMENT |
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ICAS2014_0503: L.G. Wang¹, B.F. Song¹, W.Q. Yang¹, P. Fu¹; ¹Northwestern Polytechnical University, China EXPERIMENTAL CHARACTERIZATION OF A FLEXIBLE MEMBRANE FLAPPING-WING IN FORWARD FLIGHT |
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ICAS2014_0519: R. Bur¹, V. Brion¹, P. Molton¹; ¹ONERA, France AN OVERVIEW OF RECENT EXPERIMENTAL STUDIES CONDUCTED IN ONERA S3CH TRANSONIC WIND TUNNEL |
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ICAS2014_0528: M. Motomatsu, Graduate school of Tokai University, Japan; Y. Inada, Tokai University, Japan EFFECT OF ELASTICITY IN THE BIRD-LIKE PRIMARY FEATHER WING ON THE FLIGHT STABILITY |
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ICAS2014_0536: Y.-H. Kim, Emirates Aviation University, United Arab Emirates; K.P. Garry, Cranfield University, Germany THE EFFECT OF A SYNTHETIC JET ON THE PRESSURE DISTRIBUTION OF A FLAT PLATE |
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ICAS2014_0542: T.I. Saeed¹, J.F. Morrison¹, M.S. Mughal¹; ¹Imperial College London, United Kingdom ROUGHNESS EFFECTS ON SWEPT-WING CROSSFLOW TRANSITION IN MODERATE FREE-STREAM TURBULENCE |
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ICAS2014_0601: B. Li¹, B. Song¹, L. Wang¹; ¹Northwestern Polytechnical University , China A THREE-DIMENSIONAL FLAPPING WING MECHANISM FOR WIND TUNNEL EXPERIMENTS |
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ICAS2014_0606: F.P. Moraleda, UPM, Spain; F.M. Catalano, EESC-USP, Brazil EXPERIMENTAL ANALYSIS OF THE AERODYNAMICS OF POROUS FLAP SIDE-EDGE |
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ICAS2014_0618: F. Peng¹, S. Bifeng¹, W. Liguang¹; ¹Northwestern Polytechnical University, China AN EXPERIMENTAL STUDY ON THE INFLUENCE OF PASSIVE DEFORMATION TO LIFT AND THRUST GENERATION IN FLEXIBLE FLAPPING WING |
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ICAS2014_0640: 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 FLOW STRUCTURE IN THE BASE REGION OF RE-ENTRY VEHICLE WITH SUPERSONIC BRAKING PLUMES IMPINGING WITH LANDING SURFACE |
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ICAS2014_0694: E. Koopmans¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands EXPERIMENTAL RESEARCH ON FLOW SEPARATION CONTROL USING SYNTHETIC JET ACTUATORS |
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ICAS2014_0727: A.C. Avelar¹, E. Basso¹, J.B.P. Falcão Filho¹, P.G.M. Romero, Intituto Tecnológico de Aeronáutica, Brazil; J.J.L. Hsu¹; ¹Instituto de Aeronautica e Espaço, Brazil INVESTIGATION OF THE FLOW PATTERNS ON A SOUNDING ROCKET FORE-BODY SECTION |
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ICAS2014_0741: X.J. Zhao¹, Y.H. Ma¹, W.Z. Xiao¹; ¹China Academy of Aerospace Aerodynamics, China COMPRESSIBLE BOUNDARY LAYER HEAT FLUX MEASUREMENT USING EMBEDDED THERMOCOUPLES |
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ICAS2014_0756: B. Barbieri, University of Pretoria, South Africa EXPERIMENTAL INVESTIGATION OF ENDWALL FLOW FIELD, HEAT TRANSFER IN A LINEAR TURBINE BLADE CASCADE WITH CONTOURED ENDWALL |
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ICAS2014_0802: Y.Y. Zheng, University of New South Wales, Australia PIV INTRODUCED EXPERIMENTAL INVESTIGATION OF COUNTERFLOW EJECTION ON BLUNT BODY MOVING WITH SUPERSONIC SPEED |
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ICAS2014_0872: E.R. Gowree¹, C.J. Atkin¹; ¹City University London, United Kingdom INCOMPRESSIBLE TURBULENT FLOW AT THE LEADING EDGE OF SWEPT WINGS |
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ICAS2014_0898: 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 HYPERSONIC FLOWFIELD AND HEAT FLUX PECULIARITIES ON THE NEW SPACE LAUNCHER WITH WINGED REUSABLE FIRST STAGE. |
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ICAS2014_0912: M.V. Ustinov¹, A.A. Uspensky¹, A.Y. Urusov¹, D.A. Rusianov¹; ¹TsAGI, Russia LAMINAR-TURBULENT TRANSITION CONTROL BY DIELECTRIC BARRIER DISCHARGE. THEORY AND EXPERIMENT |
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ICAS2014_0914: A.I. Ivanov¹, E.V. Streltsov¹; ¹TsAGI, Russia CONTROLLED BOUNDARY LAYER ON THE SOLID WALLS OF WIND TUNNELS: NEW APPROACH TO THE BOUNDARY INTERFERENCE PROBLEM |
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ICAS2014_0993: S.N. Tolkachev¹, V.N. Gorev¹, V.V. Kozlov¹; ¹ITAM SB RAS, Russia THE ROLE OF LOCALIZED ROUGHNESS ON THE LAMINAR-TURBULENT TRANSITION ON THE OBLIQUE WING |
2.3 - Basic Fluid Dynamics and Flow Control |
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ICAS2014_0037: L Öster, Saab Aerosystems, Sweden A CFD BENCHMARK STUDY OF FLOW SEPARATION CONTROL WITH PULSATILE JETS ON A HIGH-LIFT AIRFOIL |
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ICAS2014_0184: T. Atobe, Japan Aerospace Exploration Agency, Japan OBLIQUE MODE ENHANCEMENT BY LONGITUDINAL WALL OSCILLATION IN 2D CHANNEL FLOW |
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ICAS2014_0199: G.N. Dudin, Central Aerohydrodynamic Institute (TsAGI), Russia THE FLOW IN THE PLANE OF SYMMETRY OF THE DELTA WING IN THE REGIME OF STRONG VISCOUS-INVISCID INTERACTION. |
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ICAS2014_0204: I.V. Egorov, TsAGI, Russia INFLUENCE OF SMALL SPATIAL PERTURBATIONS OF SUPERSONIC FLOW VELOCITY ON THE HEAT FLUX TO THE CYLINDER SURFACE |
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ICAS2014_0289: A.V. Fedorov¹, V.G. Soudakov¹, I.V. Egorov¹, A.A. Sidorenko², Y. Gromyko², D. Bountin²; ¹TsAGI, Russia; ²ITAM SB RAS and NSU, Russia LAMINAR FLOW CONTROL OF A HIGH-SPEED BOUNDARY LAYER BY LOCALIZED WALL HEATING OR COOLING |
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ICAS2014_0303: S.L. Chernyshev¹, A.P. Kuryachii¹, S.V. Manuilovich ¹, D.A. Rusyanov¹, M.D. Gamirullin¹; ¹Central Aerohydrodynamic Institute, Russia THEORETICAL MODELING OF THE ELECTROGASDYNAMIC METHOD OF LAMINAR FLOW CONTROL ON A SWEPT WING |
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ICAS2014_0323: P.A. Polivanov¹, A.A. Sidorenko¹, A.A. Maslov¹; ¹ITAM SB RAS, Russia ARTIFICIAL TURBULIZATION OF THE SUPERSONIC BOUNDARY LAYER BY DIELECTRIC BARRIER DISCHARGE |
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ICAS2014_0341: L.-H. Feng¹, J.-J. Wang¹, K.-S. Choi, University of Nottingham, United Kingdom; ¹Beijing University of Aeronautics and Astronautics, China A NOVEL CONCEPTIONS OF PLASMA GURNEY FLAP |
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ICAS2014_0355: P.V. Chuvakhov, Central Aerohydrodynamic Institute (TsAGI), Russia INVESTIGATION OF HEAT FLUX AND EFFUSION/FILM COOLING EFFICIENCY OVER A SHARP CONE SURFACE AT HIGH SUPERSONIC SPEEDS |
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ICAS2014_0379: X. XU¹, Z. ZHOU¹, R. WANG¹; ¹Northwestern Polytechnical University, China THE EFFICIENCY ANALYSIS OF GUST ALLEVIATION BASED ON ACTIVE FLOW CONTROL |
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ICAS2014_0440: K. Okabayashi¹, T. Matsue², M. Asai², H. Naito¹; ¹Japan aerospace exploration agency, Japan; ²Tokyo metropolitan university, Japan RANS MODELING FOR FLOWS ON RIBLETS BASED ON EXPERIMENTAL DATA |
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ICAS2014_0479: N. Morimoto¹, S. Aso¹, Y. Tani¹; ¹Kyushu University, Japan REDUCTION OF AERODYNAMIC HEATING AND DRAG WITH OPPOSING JET THROUGH EXTENDED NOZZLE IN HIGH ENTHALPY FLOW |
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ICAS2014_0521: V.I. Sakharov¹, V.V. Shtapov¹, E.B. Vasilevskiy¹, B.E. Zhestkov¹; ¹TsAGI, Russia A BLUNTED CONE IN A SUPERSONIC HIGH-ENTHALPY NONEQUILIBRIUM UNDEREXPANDED AIR JET |
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ICAS2014_0544: S.M. Drozdov, TsAGI, Russia TO THE NON-UNIQUENESS PROBLEM OF HYPERSONIC STEADY-STATE FLOW ON THE BLUNTED BODIES LEADING AGE. |
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ICAS2014_0571: F. Maksimov, Institute of Computer Aided Design, Russian Academy of Sciences, Russia EXISTENCE CRITERIA OF NON-VISCOUS VORTICAL STRUCTURES IN SHOCK LAYERS OF CONICAL GAS FLOWS |
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ICAS2014_0575: A.L. Stasenko¹, G.V. Molleson¹; ¹TsAGI, Russia PHYSICS PHENOMENA ACCOMPANIED STREAMLINING OF A BODY BY THE GAS-PARICLE SUPERSONIC JET |
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ICAS2014_0577: M.L. Combrinck, Flamengro, a Div of Armscor SOC Ltd, South Africa; L.N. Dala, Council for Scientific and Industrial Research, South Africa EULERIAN DERIVATIONS OF NON-INERTIAL NAVIER-STOKES EQUATIONS |
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ICAS2014_0610: Y.-L. Ba¹, C. Pan¹, J.-J. Wang¹; ¹Beijing University of Aeronautics and Astronautics, China SEPARATED LAMINAR SHEAR LAYER TRANSITION OVER A TWO-DIMENSIONAL BUMP |
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ICAS2014_0675: V.I. Shalaev, Moscow Institute of Physics and technology, Russia SINGULARITIES IN LAMINAR BOUNDARY LAYER AND FLOW STRUCTURE NEAR SINK PLANE ON CONICAL BODIES |
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ICAS2014_0689: M.P. Brandão, ITA, Brazil AERODYNAMICS VIA AEROACOUSTICS – THE CASE FOR CIRCULATION CAPTURE |
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ICAS2014_0696: A. Shmilovich¹, Y. Yadlin¹, E. Whalen¹; ¹The Boeing Company, United States COMPUTATIONAL EVALUATION OF FLOW CONTROL FOR ENHANCED CONTROL AUTHORITY OF A VERTICAL TAIL |
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ICAS2014_0769: I.I. Lipatov¹, A.A. Prihodko, Dnepropetrovsk State University, Ukraine; R.Y. Tugazakov¹, T.W. Fam, MIPT, Russia; ¹TsAGI, Russia NUMERICAL MODELING OF THE BUFFET ONSET IN 2-D AND 3-D FLOWS |
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ICAS2014_0857: Y. Lee¹, S.H. Park¹, H.B. Chang¹, Y.H. Cho, Seyon Engineering & System Co., South Korea; ¹Korea Aerospace University, South Korea DYNAMIC CHARACTERISTICS OF THE THRUST VECTORING CONTROL BY HIGHLY COMPRESSIBLE COANDA EFFECTS |
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ICAS2014_0877: L. Wang¹, R. Hu¹, L. Li¹, S. Fu¹; ¹Tsinghua University, China DETACHED-EDDY SIMULATION OF FLOW PAST A BACKWARD-FACING STEP WITH A HARMONIC ACTUATION |
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ICAS2014_0944: A. Esmaeili¹, J.M.M. Sousa¹; ¹IDMEC - Instituto Superior Tecnico, Portugal INFLUENCE OF WING ASPECT RATIO ON PASSIVE STALL CONTROL AT LOW REYNOLDS NUMBER USING SINUSOIDAL LEADING EDGES |
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ICAS2014_0987: L.M.B.C Campos¹, F.S. Cunha¹; ¹Instituto Superior Técnico, Universidade de Lisboa, Portugal ON THE INTERAL STRUCTURAL OF SHOCK WAVE IN RELAXING GAS |
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ICAS2014_1001: H. Xu¹, S. Sherwin¹, P. Hall, Department of Mathematics, Imperial College London, United Kingdom; ¹Department of Aeronautics, Imperial College London, United Kingdom TRANSMISSION COEFFICIENT OF TOLLMIEN-SCHLICHTING WAVES UNDERGOING SMALL INDENTATION/HUMP DISTORTION |
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ICAS2014_1002: C. Thomas¹, P. Hall¹, C. Davies, Cardiff University, United Kingdom; ¹Imperial College, United Kingdom THE EFFECTS OF NONLINEARITY ON CROSSFLOW RECEPTIVITY |
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ICAS2014_1012: T. Bobarykina, ITAM SB RAS, Russia INVESTIGATION OF THE OPTICAL PULSING DISCHARGE IN THE SUPERSONIC AIR FLOW |
2.4 - Applied Aerodynamics |
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ICAS2014_0024: A. Hövelmann¹, C. Breitsamter¹; ¹Technische Universität München, Germany EXPERIMENTAL INVESTIGATIONS ON VORTEX FLOW PHENOMENA OF A DIAMOND WING CONFIGURATION |
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ICAS2014_0030: V.V. Riabov, Rivier University, United States INTERFERENCE BETWEEN BODIES IN HYPERSONIC RAREFIED-GAS FLOWS |
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ICAS2014_0048: K. Isogai, Japan Aerospace Exploration Agency, Japan SUBSONIC AND TRANSONIC FLOW SIMULATION FOR A WING OSCILLATING IN YAW AND SIDESLIP |
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ICAS2014_0051: J. Young¹, J.C.S. Lai¹; ¹University of New South Wales, Australia EFFECT OF ANGLE OF ATTACK KINEMATICS ON PASSIVE FLAPPING FOIL POWER GENERATION |
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ICAS2014_0057: L.L.M. Veldhuis¹, T. Sinnige¹; ¹Delft University of Technology, Netherlands THE EFFECT OF PYLON TRAILING EDGE BLOWING ON THE PERFORMANCE AND NOISE PRODUCTION OF A PROPELLER |
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ICAS2014_0084: N.V. Voevodenko¹, L.G. Ivanteeva¹, V.J. Lunin¹; ¹TsAGI, Russia NUMERICAL INVESTIGATIONS ON THE SLENDER AXISYMMETRIC BODIES AERODYNAMICS IN WIDE RANGE OF MACH NUMBERS AND ANGLES OF ATTACK FROM 0° TO 180° |
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ICAS2014_0087: A. Kuzmin¹, A. Ryabinin¹; ¹St. Petersburg State University, Russia TRANSONIC AIRFOILS, WINGS, AND PROJECTILES ADMITTING ANOMALOUS BEHAVIOR OF AERODYNAMIC COEFFICIENTS |
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ICAS2014_0125: K. Szilder, Aerospace, National Research Council, Canada THREE-DIMENSIONAL NUMERICAL SIMULATION OF ICE ACCRETION USING A MORPHOGENETIC APPROACH |
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ICAS2014_0163: M.F. Figat¹, A. Kwiek¹, K. Senenko¹; ¹Warsaw University of Technology, Poland AERODYNAMIC DESIGN OF THE STRAKE FOR THE ROCKET PLANE IN TAILLESS CONFIGURATION. |
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ICAS2014_0195: T. Ikeda¹, T. Atobe¹, Y. Konishi², H. Nagai², K. Asai²; ¹Japan Aerospace Exploration Agency, Japan; ²Tohoku University, Japan NUMERICAL STUDY OF WIND-TUNNEL ACOUSTIC RESONANCE INDUCED BY TWO-DIMENSIONAL AIRFOIL FLOW AT LOW REYNOLDS NUMBER |
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ICAS2014_0207: A. Viviani, Second University of Naples, Italy; G. Pezzella, Italian Aerospace Research Center, Italy HYPERSONIC AERODYNAMIC APPRAISAL OF WINGED BLUNT, RATHER SHARP AND SPATULED BODY RE-ENTRY VEHICLES |
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ICAS2014_0214: S.Y. Soloviev, KSRC, Russia INTERACTION OF KARMAN VORTICES WITH LONGITUDINAL VORTEX SYSTEMS IN FLOWS AROUND BODIES |
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ICAS2014_0228: N. Tokugawa, Japan Aerospace Exploration Agency, Japan; T. Osada, Gakushuin University, Japan; Y. Ueda, Tokyo Business Service Co. Ltd., Japan; H. Ishikawa, TOUA Co. Ltd., Japan NATURAL LAMINAR FLOW DESIGN OF FUSELAGE NOSE FOR SMALL SUPERSONIC CIVIL TRANSPORT |
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ICAS2014_0233: K. Szilder, National Research Council, Canada THE INFLUENCE OF ICE ACCRETION ON THE AERODYNAMIC PERFORMENCE OF A UAS AIRFOIL |
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ICAS2014_0249: M. Principi, City University London, United Kingdom; S. Prince, Cranfield University, United Kingdom FEASIBILITY ASSESSMENT OF SPINNING CYLINDER LIFT FOR REMOTE FLIGHT IN MARS AND TITAN ATMOSPHERES |
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ICAS2014_0260: 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 COMPUTATIONAL ANALYSIS FOR FLAPPING WING BY COUPLED CFD AND CSD SOLUTIONS |
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ICAS2014_0275: Y.I. Khlopkov¹, S.L. Chernyshev¹, Z.Y. Myo Myint², A.Y. Khlopkov²; ¹Central Aerohydrodynamic Institute, Russia; ²Moscow Institute of Physics and Technology, Russia HYPERSONIC AEROTHERMODYNAMICS INVESTIGATION FOR AEROSPACE SYSTEM |
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ICAS2014_0298: H. Strüber, Airbus Operations GmbH, Germany THE AERODYNAMIC DESIGN OF THE A350 XWB-900 HIGH LIFT SYSTEM |
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ICAS2014_0387: A.L. Bolsunovsky¹, N.P. Buzoverya¹, I.L. Chernyshev¹, V.G. Sudokov¹, A.V. Voyevodin¹; ¹TsAGI, Russia NOVEL CONFIGURATION OF A BUSINESS JET WITH A DROP-SHAPED FUSELAGE |
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ICAS2014_0388: A.L. Bolsunovsky¹, N.P. Buzoverya¹, I.L. Chernyshev¹, B.I. Gurevich¹, A.P. Tsyganov¹; ¹TsAGI, Russia ARRANGEMENT AND AERODYNAMIC STUDIES FOR LONG-RANGE AIRCRAFT IN “FLYING WING” LAYOUT |
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ICAS2014_0389: A.L. Bolsunovsky¹, N.N. Bragin¹, N.P. Buzoverya¹, I.L. Chernyshev¹, A.K. Ivanyushkin¹, S.I. Skomorohov¹; ¹TsAGI, Russia AERODYNAMIC STUDIES ON LOW-NOISE AIRCRAFT WITH UPPER ENGINE INSTALLATION |
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ICAS2014_0390: A.L. Bolsunovsky¹, N.P. Buzoverya¹, S.I. Skomorohov¹; ¹TsAGI, Russia INVESTIGATION OF ADAPTIVE WING BENEFITS FOR TRANSPORT AIRCRAFT |
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ICAS2014_0420: J.D.M. Botha,, University of the Witwatersrand, South Africa; L. Dala, CSIR, South Africa; S. Schaber, Airbus, Germany OPTIMISATION OF A NOVEL TRAILING EDGE CONCEPT FOR A HIGH LIFT DEVICE |
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ICAS2014_0449: D.I. Ignatyev¹, A.N. Khrabrov¹; ¹TsAGI, Russia MODEL OF THE UNSTEADY AERODYNAMIC CHARACTERISTICS AT HIGH AOA WITH NONLINEAR DEPENDENCY IN ANGULAR RATE |
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ICAS2014_0453: A.A. Gubanov¹, D.Y. Gusev¹; ¹Central Aerohydrodynamic Institute n.a. Prof. N.E. Zhukovsky, Russia POTENTIAL USE OF WAVERIDER AND BUSEMANN BIPLANE IN AERODYNAMIC DESIGN OF HIGH-SPEED VEHICLES WITH AIR-BREATHING ENGINES |
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ICAS2014_0456: H. Nagai¹, K. Isogai¹, N. Uda¹, K. Ono¹; ¹Kyushu University, Japan INVESTIGATION OF AIRFOIL FOR AN INSECT-SIZED FLAPPING WING |
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ICAS2014_0462: M. Cristofaro¹, Y. Wang, China Academy of Aerospace Aerodynamics, China; A. Da Ronch¹; ¹University of Southampton, United Kingdom TOWARDS COMPUTATIONAL FLIGHT DYNAMICS OF A PASSENGER JET AIRCRAFT |
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ICAS2014_0481: W. Yang¹, B. Song¹, W. Song¹, L. Wang¹, P. Fu¹, J. Xu¹; ¹Northwestern Polytechnical University, China AERODYNAMIC RESEARCH OF FLEXIBLE FLAPPING WING BY COMBINING DIC AND CFD APPROACHES |
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ICAS2014_0482: S. Lee, Hanyang University, South Korea STUDY ON PERFORMANCE AND FLOW CHARACTERISTICS FOR EMBEDDED DISTRIBUTED PROPULSION SYSTEM |
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ICAS2014_0483: M.H. Ryu, Hanyang Univ./Department of Mechanical Engineering, South Korea; L.S. Cho, Hansung Univ./Department of Mechanical Systems Engineering, South Korea; J.S. Cho, Hanyang Univ./School of Mechanical Engineering, South Korea INVESTIGATION OF THE TIP CLEARANCE EFFECT IN A COUNTER-ROTATING DUCTED FAN FOR VTOL UAV |
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ICAS2014_0518: 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 QUASI-ANALYTICAL AERODYNAMIC METHODS FOR PROPULSIVE FUSELAGE CONCEPTS |
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ICAS2014_0563: D.V. Kalinin, CIAM after P.I. Baranova, Russia MULTITHREADED CONTINUOUSLY VARIABLE TRANSMISSION SYNTHESIS FOR NEXT-GENERATION HELICOPTERS |
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ICAS2014_0576: A.B. Miller¹, Y.F. Potapov¹, A.L. Stasenko¹; ¹TsAGI, Russia EXPERIMENTAL AND THEORETICAL INVESTIGATIONS OF AIRCRAFT ICING IN THE CASE OF CRYSTAL AND MIXED-PHASE FLOWS |
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ICAS2014_0597: W.S. Hinman¹, C.T. Johansen¹, C.J. Arisman¹, W.C. Galuppo¹; ¹University of Calgary, Canada NUMERICAL INVESTIGATION OF LAMINAR NEAR WAKE SEPARATION ON CIRCULAR CYLINDERS AT SUPERSONIC VELOCITIES |
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ICAS2014_0637: F.M. Catalano, University of Sao Paulo, Brazil MISSION ADAPTIVE WING-LET OPTIMIZATION FOR REDUCTING VORTEX DRAG |
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ICAS2014_0652: P.S. Palar, The University of Tokyo, Japan MULTI OBJECTIVE OPTIMIZATION OF TRANSONIC AIRFOIL USING CST METHODOLOGY WITH GENERAL AND EVOLVED SUPERCRITICAL CLASS FUNCTION |
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ICAS2014_0663: K. Bogdanski¹, W. Krusz¹, M. Rodzewicz¹, M. Rutkowski¹; ¹Warsaw University of Technology, Poland DESIGN AND OPTIMIZATION OF LOW SPEED DUCTED FAN FOR A NEW GENERATION OF JOINED WING AIRCRAFT |
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ICAS2014_0686: C. Breitsamter¹, M. Grawunder¹, R. Reß¹; ¹Technische Universität München, Germany AERODYNAMIC DESIGN OPTIMISATION FOR A HELICOPTER CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
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ICAS2014_0691: K.A. Jamison, Council of Scientific and Industrial Research, South Africa TRANSONIC STORE SEPARATION ANALYSES USING MODERN DESIGN OF EXPERIMENTS AND QUANTITATIVE GRADING OF RESULTS |
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ICAS2014_0700: B. Goliszek, Warsaw University of Technology, Poland DESIGN AND OPTIMAZATION OF THE WING WITH VERY HIGH LIFT POSSIBILITIES. |
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ICAS2014_0732: Y. Tani¹, K. Miyazaki¹, S. Aso¹, H. Ura², T. Ito²; ¹Kyushu University, Japan; ²JAXA, Japan AERODYNAMIC NOISE REDUCTION FOR HIGH LIFT DEVICES USING MORPHING FLAP CONCEPT |
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ICAS2014_0735: W. Yamazaki, Nagaoka University of Technology, Japan; K. Kusunose, Japan Aerospace Exploration Agency, Japan INNOVATIVE SUPERSONIC TRANSPORT CONFIGURATION BY BIPLANE WING / TWIN-BODY FUSELAGE |
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ICAS2014_0751: M. Figat, Warsaw University of Technology, Poland AERODYNAMIC DESIGN OF FLYING WING WITH EMPHASIS ON HIGH WING LOADING |
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ICAS2014_0763: S. Taishi, Tokyo Metropolitan University, Japan DEVELOPMENT OF AERODYNAMIC DESIGN PROCESS FOR REUSABLE WINGED SPACE VEHICLE USING OPENVSP |
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ICAS2014_0939: J. Versteegh, University of the Witwatersrand, South Africa LEE-SIDE FLOW SIMULATIONS OF CRUCIFORM WING-BODY CONFIGURATIONS AT INCOMPRESSIBLE MACH NUMBERS |
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ICAS2014_0969: L. Manfriani¹, M. Righi¹; ¹ZHAW, Switzerland AERODYNAMIC MODELLING OF A REFUELLING BOOM |
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ICAS2014_1013: V.F. Chirkashenko¹, V.M. Fomin¹, A.M. Kharitonov ¹, V.F. Volkov¹; ¹ITAM SB RAS, Russia CONTROL OF SONIC BOOM LEVEL BY CRYOGENIC ACTION ON THE PROCESS OF FLOW AROUND THE AIRCRAFT |
3.1 - Materials issues, Fatigue and Damage Tolerance |
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ICAS2014_0020: Y.-H. CHEN¹, Y. YUAN¹; ¹Beijing Institute of Aeronautical Materials, China PREPARATION, CHARACTERIZATION AND APPLICATION OF ABRASION-RESISTANT HYBRID COATINGS ON POLYCARBONATE TRANSPARENCIES |
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ICAS2014_0120: B.E. Vasilyev¹, L.A. Magerramova¹; ¹CIAM, Russia HIGH TEMPERATURES TURBINE BLADES DAMAGE PREDICTION TAKING INTO ACCOUNT LOADING HISTORY DURING A FLIGHT CYCLE |
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ICAS2014_0143: Z. Sun¹, Z. Guo¹, G. Liu¹; ¹AVIC Xi’an Aero-engine (Group) LTD., China ANALYSIS AND COUNTERMEASURE ON AERO-ENGINE BLADE DEFECT |
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ICAS2014_0174: S. Vasiliev¹, A. Artemiev¹, S. Jurgenson¹; ¹MAI, Russia X-RAY COMPUTER TOMOGRAPHY INVESTIGATION FOR POLYMER COMPOSITE MATERIAL UNDER THE STATIC LOAD |
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ICAS2014_0187: Y. Morimoto¹, N. Kishimoto¹; ¹Setsunan Univ., Japan RELATIONSHIP BETWEEN POROSITY INSIDE CFRP SPECIMEN AND RESOLUTION OF MICRO X-RAY CT |
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ICAS2014_0216: V.V. Konovalov¹, A.A. Sviridov¹; ¹TsAGI, Russia SMALL CRACKS IN ALUMINUM STRUCTURES UNDER STATIC AND CYCLIC LOADING |
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ICAS2014_0225: Y.S. Borovskaya¹, M.A. Glebova¹, V.I. Grishin¹; ¹TsAGI, Russia DEFINITION OF THE BOLT SHEARING LOAD IN MULTIPLE-ROWMETAL COMPOSITE JOINTS |
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ICAS2014_0226: Y.I. Dudarkov¹, E.A. Levchenko¹, M.V. Limonin¹; ¹TsAGI, Russia SOME LAMINATE DEFORMATIONS FEATURES |
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ICAS2014_0244: A. Groth¹, N. Kashaev¹, N. Huber¹; ¹Helmholtz-Zentrum Geesthacht, Germany INTRODUCING RESIDUAL STRESSES IN THIN ALUMINIUM STRUCTURES BY LASER GENERATED TEMPERATURE FIELDS |
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ICAS2014_0262: F. Zhang, Beijing Aeronautical Technology Research Center, China HEAVY SPECTRA UNDER OPERATIONAL LOADS CAN REDUCE LIFE BUT NOT FATIGUE SCATTER FACTOR |
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ICAS2014_0386: J. Lu¹, N. Kashaev¹, N. Huber¹; ¹Helmholtz-Zentrum Geesthacht, Germany DAMAGE TOLERANCE IMPROVEMENT OF LASER BEAM WELDED FUSELAGE STRUCTURES VIA CRENELLATIONS |
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ICAS2014_0392: V.S. Pisarev¹, S.I. Eleonsky¹, A.V. Chernov¹; ¹TsAGI, Russia RESIDUAL STRESS CHARACTERIZATION IN ORTHOTROPIC PLATE BY COMBINING HOLE-DRILLING METHOD AND SPECKLE INTERFEROMETRY |
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ICAS2014_0413: L. Pieczonka¹, A. Klepka¹, S. Pavlopoulou², W.J. Staszewski¹, C. Soutis²; ¹AGH University, Poland; ²Manchester University, United Kingdom NONLINEAR ACOUSTICS FOR HEALTH MONITORING OF COMPOSITE SCARF REPAIRS |
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ICAS2014_0416: T. Uhl¹, M. Szwedo, MONIT SHM, Poland; P. Hellstein¹, L. Pieczonka¹; ¹AGH University, Poland IMAGE-BASED STRUCTURAL HEALTH MONITORING OF COMPOSITE STRUCTURES |
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ICAS2014_0457: S Denisov, Moscow Aviation Institute, Russia INFLUENCE OF THE ACOUSTIC FIELD SPATIAL STRUCTURE ON THE RESPONSE AND DURABILITY OF THE METAL ISOTROPIC PLATE |
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ICAS2014_0489: M. Kintscher¹, S. Geier¹, H.P. Monner¹, M. Wiedemann¹; ¹DLR, Germany INVESTIGATION OF MULTI-MATERIAL LAMINATES FOR SMART DROOP NOSE DEVICES |
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ICAS2014_0510: B. Zhang, Beijing Institute of Aeronautical Materials, China EFFECT OF SURFACE COATING ON RECRYSTALLIZATION OF SINGLE CRYSTAL SUPERALLOY |
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ICAS2014_0512: C. Liu¹, B. Zang¹, X. Chen¹, C. Tao¹, D. Liu¹; ¹Beijing Institute of Aeronautical Materials, China FAILURE ANALYSIS ON REAR GEARBOX OUTPUT GEAR OF HELICOPTER |
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ICAS2014_0534: D. Micheli¹, R. Pastore¹, A. Vricella¹, R.-B. Morles¹, M. Marchetti¹; ¹Sapienza University, Italy SYNTHESYS OF RADAR ABSORBING MATERIALS FOR STEALTH AIRCRAFT BY USING NANOMATERIALS AND EVOLUTIONARY COMPUTATION |
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ICAS2014_0569: L.B. Getsov, NPO CKTI, Russia; A.S. Semenov¹, S.G. Semenov¹, E.A. Tikhomirova, JSK Klimov, Russia; ¹Saint-Petersburg State Polytechnical University, Russia EXPERIMENTS AND FAILURE CRITERIA FOR SINGLE CRYSTAL ALLOYS OF GAS TURBINE ENGINE UNDER STATIC AND THERMOCYCLIC LOADING |
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ICAS2014_0579: I. AHMADI, University of Zanjan, Iran ANALYSIS OF INTER-LAMINAR STRESSES IN COMPOSITE THIN SHELL |
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ICAS2014_0611: A.V. Pankov¹, I.G. Khlebnikova¹; ¹TsAGI, Russia CONSIDERATION OF THE SERVICE LIFE TAKING INTO ACCOUNT A LOT OF ONE-TYPE STRESSED UNIT ELEMENTS |
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ICAS2014_0625: Z. Ni, Shanghai Aircraft Design and Research Institute, China A NEW 3D PROGRESSIVE DAMAGE MODEL FOR COMPOSITE LAMINATES |
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ICAS2014_0631: G. Komarov¹, S. Bukharov¹, A. Lebedev¹; ¹MATI, Russia THERMOPLASTIC COMPOSITE AIRCRAFT STRUCTURE REPAIR METHODOLOGY |
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ICAS2014_0635: I. Sen¹, R.C. Alderliesten¹, R. Bendictus¹; ¹Delft University of Technology, Netherlands APPROXIMATE FUNCTION FOR FATIGUE CRACK PROPAGATION IN A DESIGN OPTIMISATION PROCEDURE FOR FIBRE METAL LAMINATES |
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ICAS2014_0638: J. Liu¹, P. Staron¹, D. Schnubel¹, N. Schell¹, N. Huber¹, N. Kashaev¹; ¹Helmholtz-Zentrum Geesthacht, Germany THE COOLING GRADIENT AND MICROSTRUCTURE CONTROL IN LASER BEAM WELDED TIAL ALLOY ASSISTED BY TEMPERATURE FIELD SIMULATION |
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ICAS2014_0645: Z. Chen, Nanjing University of Aeronautics and Astronautics, China MICROSTRUCTURE AND EVOLUTION OF PORES DURING THE DENSIFICATION CYCLES OF ZRC DOPED CARBON/CARNON COMPOSITES |
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ICAS2014_0678: S. Khosoussi¹, M. Mondali, , Islamic Azad University, Science and Research Branch, Iran; A. Abedian¹; ¹Sharif University of Technology, Iran AN ANALYTICAL SOLUTION TO THE ELASTIC-PLASTIC BEHAVIOR OF METAL MATRIX COMPOSITES UNDER TENSILE LOADING |
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ICAS2014_0692: B. Alem¹, A. Abedian¹; ¹Sharif university of technology, Iran FATIGUE DAMAGE DETECTION IN LARGE THIN WALL PLATE BASED ON ULTRASONIC GUIDED WAVE BY USING A PIEZOELECTRIC SENSOR NETWORK |
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ICAS2014_0713: M.-Q. Cong, Nanjing University of Aeronautics and Astronautics, China EFFECT OF Y ON MICROSTRUCTURE AND TENSILE PROPERTIES OF AS-CAST MG2SI/MG-ZN-SI COMPOSITES |
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ICAS2014_0782: J. Temis¹, K. Azmetov¹, A. Fakeev¹; ¹Central Institute of Aviation Motors, Russia PROBLEM OF LOW CYCLE FATIGUE OF TURBOMACHINES |
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ICAS2014_0794: N. Banerji¹, P. Leyland¹, S. Haussener¹; ¹Ecole Polytechnique Fédérale de Lausanne, Switzerland CHARACTERISING INTERNAL HEAT TRANSFER IN THERMAL PROTECTION SYSTEMS |
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ICAS2014_0795: 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 IMPROVED METHODS FOR MODELLING IMPERFECTIONS FOR BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELLS |
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ICAS2014_0819: M.H. Safaei, Iran DAMAGE IDENTIFICATION USING FIBRE BRAGG GRATING SENSORS EMBEDDED WITHIN A COMPOSITE PLATE |
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ICAS2014_0845: I. Ovchinnikov, Bauman Moscow State Technical University, Russia OWN SPECTRUM BANDS OF MECHANICAL SYSTEMS |
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ICAS2014_0860: T. Mileiko, Institute of Solid State Physics of RAS, Russia A NOVEL COMPOSITE MATERIAL FOR TURBINE BLADES |
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ICAS2014_0866: A. Balakirev¹, B. Bolotov¹, A. Golovkin¹, M. Nikhamkin¹, N. Sazhenkov¹, L. Voronov¹, I. Konev¹; ¹Perm National Research Polytechnic University, Russia EXPERIMENTAL EVALUATION OF THE EFFICIENCY OF GAS TURBINE ENGINE PARTS DAMPING WITH DRY FRICTION DAMPERS USING LASER VIBROMETER |
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ICAS2014_0905: I.C.J. Barbosa¹, M.A.R. Loja¹; ¹GI-MOSM/ISEL, IDMEC/LAETA , Portugal DESIGN OF A LAMINATED COMPOSITE MULTI-CELL STRUCTURE SUBJECTED TO TORSION |
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ICAS2014_0906: 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 NOVEL METAL MATRIX/CARBON COMPOSITES FOR AIRSPACE APPLICATIONS |
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ICAS2014_0907: T.V. Larionova, St.Petersburg State Polytechnical University, Russia; B.-S. You, Korea Insitute of Materials Science, South Korea RAPID SOLIDIFIED MG-CA-ZN ALLOYS WITH MICROALLOYING OF LA, ND, Y, ZR |
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ICAS2014_0919: V.I. Kleptsov, Beriev Aircraft Company, Russia THE PRINCIPLES OF FATIGUE APPROVAL FOR TRANSPORT AIRCRAFT AFTER ITS PRINCIPAL STRUCTURE ELEMENTS MODIFICATION |
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ICAS2014_0931: V.I. Korolkov, Voronezh State Technical University, Russia METHOD DISTURBANCES IN THE LIMIT DEFORMATIONS IN THE CROSS-SECTION WING IS |
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ICAS2014_1018: A.C. Orifici, RMIT University, Australia CONTROL OF COMPOSITE MATERIAL CRACK BRANCHING FOR IMPROVED FRACTURE TOUGHNESS |
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ICAS2014_1044: P. Panin¹, N. Nochovnaya¹, D. Kablov¹, E. Alexeev¹; ¹FSUE VIAM, Russia LOW-COST TITANIUM ALLOYS FOR TITANIUM-POLYMER LAYERED COMPOSITES |
3.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity |
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ICAS2014_0052: 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 FOD CHARACTERISTICS OF TITANIUM METAL MATRIX COMPOSITE (TMC) TO APPLY AIRCRAFT LANDING GEAR STRUCTURE |
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ICAS2014_0053: A.I. Danilin, Samara State Aerospace University, Russia OPTIMALITY CRITERIA FOR STRUCTURAL DESIGN OF AIRFRAMES WITH DYNAMIC REQUIREMENTS |
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ICAS2014_0088: K. Seywald¹, F. Hellmundt¹, A. Wildschek¹, F. Holzapfel, TUM, Germany; ¹Airbus Group Innovations, Germany AIRWORTHINESS INVESTIGATION OF A HIGHLY NONPLANAR FLEXIBLE WING CONCEPT |
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ICAS2014_0102: I. Ruiz Juretschke¹, B. Villalta Oliveira¹, R. Bancalero Santolaya¹; ¹Airbus Defense and Space, Spain LOADS MODEL FLIGHT TEST VALIDATION BY MEANS OF INNOVATIVE, PHOTOGRAMMETRY BASED, DEFORMATION MEASUREMENT TECHNIQUE. |
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ICAS2014_0111: Q. Sun¹, Y.J. Liu¹, R.H. Jin¹; ¹School of Aeronautics, Northwestern Polytechnical University, China NUMERICAL SIMULATION OF BIRD STRIKE IN AIRCRAFT LEADING EDGE STRUCTURE USING A NEW DYNAMIC FAILURE MODEL |
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ICAS2014_0139: M. Zichenkov¹, F. Ishmuratov¹; ¹TsAGI, Russia NONLINEARITIES AND UNCERTAINTIES OF AEROELASTICITY CHARACTERISTICS IN AIRCRAFT DESIGN AND CERTIFICATION |
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ICAS2014_0140: S. Kuzmina¹, F. Ishmuratov¹, O. Karas¹, A. Chizhov¹; ¹TsAGI, Russia DYNAMIC RESPONSE OF AN AIRPLANE ELASTIC STRUCTURE IN TRANSONIC FLOW |
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ICAS2014_0141: Q. Xiong, CASIC, China; D.-G. Cui, AVIC, China AEROELASTIC OPTIMIZATION OF COMPOSITE WING BASED ON IMPROVED ADAPTIVE GENETIC ALGORITHM |
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ICAS2014_0142: F.-F. Wang, AMECO, China; D.-G. Cui, AVIC, China AN ENGINEERING ANALYSIS METHOD OF POST-BUCKLING FOR COMPOSITE STIFFENED PANELS |
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ICAS2014_0151: G.A. Amiryants¹, V.P. Kulesh¹, V.A. Malyutin¹, A.V. Chedrik¹; ¹Central aerohydrodynamic institute - TsAGI, Russia AEROELASTIC ANALYSIS OF THE ADAPTIVE WING WIND TUNNEL DEMONSTRATOR OF THE SADE PROJECT |
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ICAS2014_0167: J. Cecrdle, Aeronautical Research and Test Institute (VZLU), Czech Republic UPDATING OF AIRCRAFT STRUCTURE DYNAMIC MODEL TO GROUND VIBRATION TEST RESULTS |
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ICAS2014_0317: Y.H. Ma¹, H.X. Zhu¹, J. Hong¹; ¹Beihang University, China STRUCTURE DESIGN AND MECHANICAL SIMULATION ON THE SC-MR SUPPORT FOR ROTOR SYSTEM |
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ICAS2014_0324: G. Liseykin¹, M. Bogatyrev¹, M. Pronin¹, V. Smyslov¹; ¹TsAGI, Russia STRUCTURAL NONLINEARITIES SIMULATION ON THE FLUTTER ELECTROMECHANICAL MODELING TEST BENCH |
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ICAS2014_0325: Y.A. Azarov¹, G.V. Liseykin¹, M.A. Pronin¹, O.A. Orlova¹; ¹TsAGI, Russia FLUTTER CALCULATIONS AND TRANSONIC WIND TUNNEL TESTING OF DYNAMICALLY SCALED MODEL OF THE HIGH-ASPECT-RATIO WING |
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ICAS2014_0333: B. Plaumann¹, D. Krause¹; ¹TUHH, Institute PKT, Germany A METHODICAL APPROACH FOR DYNAMIC SYSTEM ANALYSIS & SYNTHESIS IN THE DIMENSIONING OF VARIANT LIGHTWEIGHT CABIN INTERIOR |
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ICAS2014_0363: J. Ertveldt, Vrije Universiteit Brussel - Dept. MECH, Belgium ON-LINE MONITORING AND FLUTTER SPEED PREDICTION BASED ON IDENTIFICATION OF A TIME-VARYING SYSTEM |
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ICAS2014_0408: X.-Z. Gao¹, Z.-X. Hou¹, Z. Guo¹, X.-Q. Chen¹; ¹National University of Defense Technology, China DESIGN AND PERFORMANCE TEST OF A TWIN-FUSELAGE CONFIGURATION SOLAR-POWERED UAV |
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ICAS2014_0423: M.-C. Meijer, University of the Witwatersrand, South Africa AEROELASTIC PREDICTION FOR MISSILE FINS IN SUPERSONIC FLOWS |
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ICAS2014_0435: T. Ungwattanapanit¹, H. Baier¹; ¹TU München, Germany POSTBUCKLING ANALYSIS AND OPTIMIZATION OF STIFFENED FUSELAGE PANELS UTILIZING VARIABLE-STIFFNESS LAMINATES |
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ICAS2014_0460: R. Seemann¹, B. Plaumann¹, J. Oltmann¹, D. Krause¹; ¹TUHH, Institute PKT, Germany FE-MODELLING GUIDELINES FOR THE DIMENSIONING OF AIRCRAFT CABIN INTERIOR UNDER STATIONARY DYNAMIC LOADS |
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ICAS2014_0463: Y. Wang¹, A. Da Ronch², M. Ghandchi-Therani², F. Li¹; ¹China Academy of Aerospace Aerodynamics, China; ²University of Southampton, United Kingdom ADAPTIVE FEEDFORWARD CONTROL DESIGN FOR GUST LOADS ALLEVIATION AND LCO SUPPRESSION |
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ICAS2014_0492: 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 MULTI-TERRAIN IMPACT SIMULATIONS OF A CRASHWORTHY COMPOSITE HELICOPTER SUBFLOOR |
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ICAS2014_0496: W. Qian¹, G. Yang², G. Zheng², G. Zhang¹; ¹Shenyang Aircraft Design & Research Institute, China; ²Institute of Mechanics, Chinese Academy of Science, China NUMERICAL SIMULATION AND WIND TUNNEL TESTING OF FLUTTER ABOUT AN ALL- MOVABLE HORIZONTAL TAIL AT TRANSONIC SPEEDS |
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ICAS2014_0497: D. XUE¹, B.-F. SONG¹, W.-Q. YANG¹; ¹Northwestern Polytechnical University, China RESEARCH ON LONG PERIODICAL STRUCTURAL DEFORMATION OF FLEXIBLE FLAPPING WING IN FLIGHT |
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ICAS2014_0555: M. Halle¹, F. Thielecke¹; ¹TUHH/FST, Germany FLIGHT LOADS ESTIMATION USING LOCAL MODEL NETWORKS |
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ICAS2014_0623: R. Adhy Sasongko, Institut Teknologi Bandung, Indonesia A STUDY ON THE EFFECT OF WEAPON INSTALLATION TO AEROELASTIC CHARACTERISTIC OF FIGHTER AIRCRAFT WING |
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ICAS2014_0644: A. Pistek, Brno Univerzity of Technology, Czech Republic ANALYTICAL METHOD FOR LIMIT LOAD CAPACITY CALCULATION OF THIN WALLED AIRCRAFT STRUCTURES |
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ICAS2014_0651: A. Shanygin¹, M. Zichenkov¹, I. Kondakov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia MAIN BENEFITS OF PRO-COMPOSITE LAYOUTS FOR WING AND FUSELAGE PRIMARY STRUCTURE UNITS |
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ICAS2014_0655: H. Dastoom Laatleyli, Sharif University of Technology, Dep. of Aerospace Eng., Iran NONLINEAR STABILITY ANALYSIS OF CARBON NANOTUBES BASED ON TIMOSHENKO BEAM THEORY AND MODIFIED COUPLE STRESS THEORY |
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ICAS2014_0658: E. Dubovikov¹, V. Fomin¹; ¹TsAGI, Russia STRENGTH ANALYSIS TECHNIQUE FOR HIGH LOADED ELEMENTS OF COMPOSITE AIRFRAMES |
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ICAS2014_0681: E.L. Jansen¹, H. Abramovich, Technion, I.I.T., Israel; R. Rolfes¹; ¹Leibniz Universitaet Hannover, Germany THE DIRECT PREDICTION OF BUCKLING LOADS OF SHELLS UNDER AXIAL COMPRESSION USING VCT - TOWARDS AN UPGRADED APPROACH |
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ICAS2014_0684: R. Wiranegara¹, A. Turan¹; ¹University of Manchester, United Kingdom A SIMPLE APPROACH TO COMPUTATIONAL AEROELASTICITY OF NASA ROTOR 67 |
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ICAS2014_0701: V. Soloshenko, Moscow Aviation Institute (National Research University), Russia CONCEPTUAL DESIGN OF CIVIL AIRPLANE COMPOSITE WINGBOX STRUCTURES |
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ICAS2014_0702: M. Rodzewicz¹, D. Glowacki¹; ¹Warsaw University of Technology, Poland INVESTIGATIONS INTO LOAD SPECTRA OF LIGHT-WEIGHT UAV’S |
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ICAS2014_0711: T.H.L. Pinto, UFVJM - ICT, Brazil; R.G.A. da Silva, ITA, Brazil; G.R. Begnini, Embraer, Brazil COMPARATIVE STUDY OF SYSTEM IDENTIFICATION METHODS APPLIED TO AEROELASTIC MODELS TESTED IN WIND TUNNEL |
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ICAS2014_0755: Z.W. Liu ¹, Z.X. Hou¹, J.T. Zhang¹, X.Z. Gao¹; ¹National University of Defense Technology, China THE VERY FLEXIBLE AIRCRAFTS AND ALBATROSS FLIGHT |
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ICAS2014_0771: Y.T. Zuo¹, Z.H. Gao¹, G. Chen, Xi’ an Jiaotong University, China; ¹Northwestern Polytechnical University, China EFFICIENT AERO-STRUCTURAL DESIGN OPTIMIZATION BASED ON HIGH-FIDELITY METHODS |
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ICAS2014_0784: F. Yang, Shanghai Aircraft Design and Research Institute of COMAC, China; J. Xie, Civil Aviation University of China, China AEROELASTIC RESPONSE SIMULATION FOR DIFFERENT EXCITATION TECHNIQUES IN FLIGHT FLUTTER TEST OF MODERN CIVIL |
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ICAS2014_0786: G. Romeo¹, F. Danzi¹, E. Cestino¹; ¹Politecnico di Torino, Italy MULTI-OBJECTIVE OPTIMIZATION OF THE COMPOSITE WING BOX OF SOLAR POWERED HALE UAV |
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ICAS2014_0789: L.C. de Oliveira¹, R. Degenhardt¹, T. Klimmek¹; ¹DLR, Germany AEROELASTIC BEHAVIOR OF COMPOSITE WINGS IN POSTBUCKLING REGIME |
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ICAS2014_0797: Q.Y. Chen, COMAC, China NUMERICAL ANALYSIS OF TRANSONIC FLUTTER OF SUPERCRITICAL AIRFOIL OF A BUSINESS JET |
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ICAS2014_0849: L. Chen¹, Z.Q. Dou¹; ¹Shang Aircraft Design and Research Institute, China THE FLUTTER MODEL CHARACTERISTIC STUDY AND WIND-TUNNEL TEST FOR WING-MOUNTED CIVIL AIRCRAFT |
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ICAS2014_0859: R.V. Leonteva, PSC Tupolev, Russia PROCEDURE OF GROUND VIBRATION EXPERIMENTS ON AIRCRAFT WITH SIMULATING FORCES DUE TO ENGINE IMBALANCE AT BLADE LOSS |
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ICAS2014_0861: M.A. Arbelo, PFH - Private University of Applied Sciences, Germany BUCKLING OF IMPERFECTION SENSITIVE SHELL STRUCTURES: NUMERICAL MODELS TO PREDICT LESS CONSERVATIVE KNOCK-DOWN FACTORS |
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ICAS2014_0881: 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 WAKE VORTEX ENCOUNTER LOADS. FLIGHT TESTS AND NUMERICAL SIMULATIONS |
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ICAS2014_0942: J.A. Corman¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States ASSESSING STRUCTURAL TECHNOLOGY PERFORMANCE FOR THE HYBRID WING BODY THROUGH PROBABILISTIC WEIGHT ESTIMATION |
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ICAS2014_0947: M.M. Entezari¹, M. Mohammadi-Amin¹, M.M. Alishahi, Shiraz University, Iran; ¹Astronautics Research Institute, Iran NUMERICAL SIMULATION AND PARAMETRIC STUDY OF SUPERSONIC WING FLUTTER |
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ICAS2014_0955: S. Dähne¹, T. Bach¹, C. Hühne¹; ¹Germen Aerospace Center (DLR), Germany STEPS TO FEASIBILITY FOR LAMINAR WING DESIGN IN A MULTIDISCIPLINARY ENVIRONMENT |
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ICAS2014_0960: V.K. Svyatodukh¹, D.E. Lopanitsyn¹, A.S. Ustinov¹; ¹TsAGI, Russia AIRLINERS CONTROL SYSTEMS AUTOMATION FUNCTIONS ENCHANCEMENT IN BEHALF OF AIRPLANE STRUCTURAL STRENGTH |
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ICAS2014_0976: S. Perino¹, J. Bayandor¹; ¹Virginia Tech, United States A RAPID ANALYSIS METHODOLOGY FOR EARTH ENTRY VEHICLE DEVELOPMENT |
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ICAS2014_0992: A Deivasigamani¹, J.M. McCarthy¹, S.J. John¹, S. Watkins¹, F. Coman, FCST Pty. Ltd., Australia; ¹RMIT University, Australia PROXIMITY EFFECTS OF PIEZOELECTRIC ENERGY HARVESTERS IN FLUID FLOW |
4 - Propulsion |
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ICAS2014_0014: 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 MECHANISM OF FLAMEHOLDING IN PLASMA-ASSISTED SUPERSONIC COMBUSTOR |
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ICAS2014_0035: W. Dong¹, J.J. Zhu¹, M. Zheng¹, R. Wang¹; ¹Shanghai Jiao Tong University, China NUMERICAL STUDY OF ICE ACCRETION ON ROTATING AERO-ENGINE CONE |
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ICAS2014_0036: A.R. Wadia, GE Aviation, United States EXPERIMENTAL AND NUMERICAL INVESTIGATION OF LOADING LEVELS AND DISTRIBUTIONS ON LOW PRESSURE TURBINE PERFORMANCE |
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ICAS2014_0078: F. Haselbach¹, A. Newby¹, R. Parker¹; ¹Rolls-Royce, United Kingdom CONCEPTS AND TECHNOLOGIES FOR THE NEXT GENERATION OF LARGE CIVIL AIRCRAFT ENGINES |
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ICAS2014_0093: A.L. Kartashev¹, M.A. Kartasheva¹; ¹South Ural State University, Russia PROFILING OF OPTIMAL ANNULAR NOZZLES WITH POLYPHASE WORKING MEDIUM |
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ICAS2014_0095: N.N. Ledovskaya, Central Institute of Aviation Motors, Russia VARIATION OF UNSTEADY FLOW PATTERN IN COMPRESSORS PRECEDING THE LOSS OF GASDYNAMIC STABILITY. EXPERIMENT. |
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ICAS2014_0104: S.V. Pankov¹, V.I. Mileshin¹, V.N. Korzhnev¹; ¹Central Institute of Aviation Motors, Russia NUMERICAL AND EXPERIMENTAL INVESTIGATIONS BYPASS-FLOW FANS FOR AN ADVANCED CIVIL AIRCRAFT ENGINE |
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ICAS2014_0105: R. Schnell¹, G. Ashcroft¹; ¹DLR, Germany GEOMETRIC VARIABILITY AND ITS INFLUENCE ON STEADY AND UNSTEADY FAN AERODYNAMIC PERFORMANCE |
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ICAS2014_0119: Y.A. Ravikovich¹, Y.I. Ermilov¹, A.O. Pugachev¹, A.A. Matushkin¹, D.P. Kholobtsev¹; ¹MAI, Russia PREDICTION OF OPERATIONAL CHARACTERISTICS OF FLUID-FILM AND GAS BEARINGS FOR HIGH-SPEED TURBOMACHINERY USING COMPUTATIONAL FLUID DYNAMICS |
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ICAS2014_0160: V. Avrashkov, MAI, Russia; M. Boucheze¹, S. Balland¹; ¹MBDA-France, France DESIGN OF SUPERSONIC EJECTION SYSTEM FOR HIGH SPEED COMBUSTION INVESTIGATION AND RESULTS OF WIDE RANGE COMBUSTION CHAMBER TESTS |
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ICAS2014_0169: S.A. Takovitskii, TsAGI, Russia SUPERSONIC NOZZLE THRUST AUGMENTATION |
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ICAS2014_0192: A. Salnikov, CIAM, Russia STRENGTH RELIABILITY OF TURBINE ROTOR ENSURING BASED ON MULTIDISCIPLINARY OPTIMIZATION |
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ICAS2014_0193: L. Magerramova, Central Institute of Aviation Motors, Russia BIMETALLIC BLISK DESIGN FOR HIGH TEMPERATURE TURBINES OF GAS TURBINE ENGINE OF DIFFERENT APPLICATION |
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ICAS2014_0198: F.D. Golberg¹, O.S. Gurevich¹, A.A. Petukhov¹; ¹CIAM, Russia IMPROVING CONTROL RELIABILITY AND QUALITY OF AIRCRAFT ENGINES BY MEANS THE SOFTWARE «VIRTUAL ENGINE» |
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ICAS2014_0209: V. Kopchenov¹, S. Batura¹, L. Bezgin¹, N. Titova¹, A. Starik¹; ¹CIAM, Russia ANALYSIS OF THE PREDICTION ABILITY OF REACTION MECHANISMS FOR CFD MODELING OF THE COMBUSTION IN HIGH VELOCITY ENGINES |
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ICAS2014_0217: L.S. Yanovskiy¹, V.V. Raznoschikov¹, A.V. Baykov¹, I.S. Averkov¹; ¹Central Institute of Aviation Motors named after P.I. Baranova, Russia TRANSPORT AIRCRAFT WITH HIGH FUEL EFFICIENCY WITH \"ELECTROCHEMICAL\" GAS TURBINE ENGINE BASED ON SOFC |
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ICAS2014_0218: O. Gurevich¹, A. Gulienko¹, U. Schurovskiy¹; ¹CIAM, Russia DEMONSTRATION SYSTEMS OF THE “ELECTRIC” GAS TURBINE ENGINE |
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ICAS2014_0219: L.S. Yanovskiy¹, A.V. Baykov¹, I.S. Averkov¹; ¹Central Institute of Aviation Motors named after P.I. Baranov, Russia FUNDAMENTALS OF THE THEORY OF AVIATION \\\"ELECTROCHEMICAL\\\" GAS TURBINE ENGINES WITH SOLID OXIDE FUEL CELLS |
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ICAS2014_0227: N.A. Zlenko¹, S.V. Mikhaylov¹, A.V. Shenkin¹; ¹TsAGI, Russia CONSTRUCTION AND USE OF IMITATING MODEL IN THE PROCESS OF MULTI-CRITERIA OPTIMIZATION OF THE SEPARATE-FLOW NOZZLE |
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ICAS2014_0231: A.V. Shenkin¹, A.P. Mazurov¹, A.P. Bykov¹; ¹TsAGI, Russia AERODYNAMIC DESIGN OF SINGLE-EXPANSION-RAMP NOZZLE FOR AIRCRAFT WITH SUPERSONIC CRUISE SPEED OF FLIGHT |
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ICAS2014_0236: L. Bezgin¹, V. Kopchenov¹, N. Titova¹, A. Starik¹; ¹CIAM, Russia MECHANISMS OF POLLUTANT FORMATION IN THE H2 - FUELLED COMBUSTOR OF HIGH VELOCITY AIR-BREATHING ENGINE: MODELING STUDY |
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ICAS2014_0252: A.D. Nepomnyashchiy, Central Institute of Aviation Motors, Russia TURBULENCE MEASUREMENTS IN A FLOW PART OF TURBOMACHINES USING A HIGH-FREQUENCY PRESSURE PROBE |
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ICAS2014_0253: V.D. Venediktov, Central Institute of Aviation Motors, Russia ABOUT APPROACHES TO RESEARCH OF FLAT LPT CASCADES AT LOW RE NUMBERS |
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ICAS2014_0255: I.I. Ivanov¹, B.S. Blinnik¹; ¹Central Institute of Aviation Motors, Russia DYNAMIC LOADS ACTING ON ENGINE FRAME ELEMENTS AFTER FAN BLADE OUT EVENT STUDY |
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ICAS2014_0272: V.G. Nesterenko¹, A.A. Matushkin¹, V.V. Nesterenko¹; ¹MAI, Russia IMPROVEMENT OF THE DESIGN AND METHODS OF DESIGNING CRITICAL COMPONENTS OF GAS FLOW PATH OF MODULAR AIRCRAFT GAS TURBINE |
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ICAS2014_0278: R.C. Chang¹, S. Tan¹; ¹China University of Science and Technology, Taiwan EVALUATIONS OF PROBLEM AREAS ON CAUSES OF EXCESSIVE FUEL CONSUMPTION FOR TURBOFAN ENGINES |
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ICAS2014_0280: V.A. Stepanov¹, A.Y. Makarov¹, V.P. Maslov¹; ¹CIAM, Russia EXPERIMENTAL STUDY OF SYNTHETIC JETS FOR THE CONTROL OF FLOWS SEPARATION IN THE ENGINE'S DUCTS |
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ICAS2014_0294: B.-W. Wang, NUDT, China AERODYNAMIC CHARACTERISTICS OF ANNULAR WING AND THE IMPACT ON THE PERFORMANCE OF DUCTED FAN |
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ICAS2014_0296: K. Yang¹, Q.Y. Tu¹, Y.H. Cai¹; ¹Northwestern Polytechnical University, China PERFORMANCE ANALYSIS OF BALL BEARING CONTROLS FOR ENGINE OPERATING SYSTEM |
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ICAS2014_0308: A.A. Savelyev¹, S.V. Mikhaylov¹, N.A. Zlenko¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia AERODYNAMIC INLET DESIGN FOR CIVIL AIRCRAFT NACELLE |
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ICAS2014_0313: A. Shiryaeva, TsAGI, Russia TECHNOLOGY AND CODE FOR NUMERICAL SIMULATION OF DIFFERENT COMBUSTION TYPES IN HIGH-SPEED VISCOUS GAS TURBULENT FLOWS |
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ICAS2014_0345: E. Kozharinov, Central Institute of Aviation Motors, Russia RELIABILITY IMPROVEMENT OF ACCESSORY GEARBOX BEVEL DRIVES |
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ICAS2014_0373: L.A. Benderskiy¹, D.A. Lyubimov¹; ¹CIAM, Russia INVESTIGATION OF FLOW PARAMETERS AND NOISE OF SUBSONIC AND SUPERSONIC JETS USING RANS/ILES HIGH RESOLUTION METHOD |
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ICAS2014_0375: L.A. Benderskiy, CIAM, Russia EFFECT OF TEMPERATURE ON FLOW CHARACTERISTICS IN SUPERSONIC IMPINGING JET USING RANS/ILES HIGH RESOLUTION METHOD |
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ICAS2014_0384: A. Placzek, Onera, France AEROELASTIC DAMPING PREDICTIONS FOR MULTISTAGE TURBOMACHINERY APPLICATIONS |
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ICAS2014_0391: P. Ryabov, CIAM, Russia RESEARCH OF EFFICIENCY OF THE MID-FLIGHT POWER PLANT BASED ON THE HYBRID ENGINES FOR ADVANCED AIRLINERS |
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ICAS2014_0396: A.I. Lanshin¹, A.S. Polev¹; ¹CIAM, Russia ANALYSIS OF TRENDS AND FORECAST OF GTE DEVELOPMENT FOR SUBSONIC CIVIL AIRCRAFT |
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ICAS2014_0397: A.I. Lanshin¹, Y.V. Fokin¹, I.V. Osipov¹, V.V. Gavrilov¹; ¹CIAM, Russia PERSPECTIVE OF SMALL GAS TURBINE ENGINES DEVELOPMENT |
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ICAS2014_0404: O. Gurevich¹, A. Lukovnikov¹, A. Gulienko¹, V. Zakharchenko¹, I. Kovalenko¹, P. Suntsov¹; ¹CIAM, Russia ANALYSIS OF POSSIBILITIES TO APPLY ELECTRIC TECHNOLOGIES FOR HELICOPTER PROPULSION SYSTEM |
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ICAS2014_0448: P. Beaumier, Onera, France A LOW ORDER METHOD FOR CO-AXIAL PROPELLER AND ROTOR PERFORMANCE PREDICTION |
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ICAS2014_0461: M.J. Ivanov¹, V.K. Mamaev¹, G.B. Zhestkov¹; ¹Central Institute of Aviation Motors, Russia THERMODYNAMICALLY COMPATIBLE THEORY OF HIGH TEMPERATURE TURBOJET ENGINES |
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ICAS2014_0485: Y. Khaletskiy¹, V. Mileshin¹; ¹Central Institute of Aviation Motors, Russia COMPARISON OF DUCTED AND UNDUCTED COUNTER ROTATING FAN MODEL NOISE |
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ICAS2014_0501: O. Verseux¹, Y. Sommerer¹; ¹Airbus Operation SAS, France NEW CHALLENGES FOR ENGINE NACELLE COMPARTMENTS PRESSURE AND THERMAL LOADS MANAGEMENT WITH AIRCRAFT ENGINE EVOLUTION |
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ICAS2014_0509: F.A. Slobodkina¹, V.V. Malinin¹, A.I. Tarasov, Lulka RDC, Russia; ¹Gubkin Russian State University of Oil and Gas, Russia NUMERICAL MODELING OF FLOW IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS |
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ICAS2014_0511: J.-H. Xu¹, W.-P. Song¹, W.-Q. Yang¹; ¹Northwestern Polytechnical University, China A STUDY ON AERODYNAMIC DESIGN OF HIGH-EFFICIENCY PROPELLERS AT HIGH-ALTITUDE |
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ICAS2014_0517: A.C. Marta, LAETA, CCTAE, Instituto Superior Técnico, Universidade de Lisboa, Portugal; S. Shankaran, Fluid Mechanics Lab, Global Research Center, General Electric, United States ON THE OPTIMAL LOCATION OF BLEED PORTS FOR GAS TURBINE COOLING |
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ICAS2014_0546: D.A. Lyubimov¹, I.V. Potekhina¹; ¹CIAM, Russia INVESTIGATION OF SYNTHETIC JETS EFFICIENCY ON SEPARATION FLOW IN DIFFUSERS OF DIFFERENT GEOMETRY WITH RANS/ILES-METHOD |
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ICAS2014_0548: M.B. Guzairov¹, I.A. Krivosheev¹, D.A. Akhmedzyanov¹, A.E. Kishalov¹, K.V. Markina¹; ¹Ufa State Aviation Technical University, Russia NUMERICAL INVESTIGATION OF CHARACTIRISTICS OF DUAL-CIRCUIT NOZZLES WITH CONSIDERING THE EXTERNAL FLOW |
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ICAS2014_0590: O. Marakueva, Baltic State Technical University, Russia AERODYNAMIC DESIGN AND OPTIMIZATION OF BLADE CONFIGURATION IN AN INLET STAGE OF AN AIRCRAFT ENGINE COMPRESSOR |
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ICAS2014_0605: S. ChenB. SongH. Wa ANALYSIS OF PROPULSION AND ENERGY SYSTEM’S INFLUENCE ON THE PERFORMANCE OF HIGH ALTITUDE AIRSHIP |
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ICAS2014_0609: K. Prashant¹, R. Bhaskar¹; ¹Indian Institute of Technology Bombay, India USING WAVES TO SIMULATE DISTORTION IN INTERNAL FLOWS IN AN AXIAL FLOW FAN |
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ICAS2014_0612: A. Mirzoyan¹, A. Evstigneev¹; ¹Central Institute of Aviation Motors (CIAM), Russia STUDIES ON POSSIBLE UNIFICATION OF ENGINES FOR ADVANCED SMALL AND MEDIUM SUPERSONIC CIVIL AEROPLANES |
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ICAS2014_0614: S.G. Rebrov, FSUE Keldysh Research Centre, France; P.V. Kholodov, Moscow Aviation Institute, Russia; G.R. Yakhina, Ecole Centrale de Lyon, France NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF LASER IGNITION IN COMBUSTION CHAMBERS |
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ICAS2014_0628: M. MAKIDA¹, H. YAMADA¹, K. SHIMODAIRA¹; ¹Japan Aerospace Exploration Agency, Japan DETAILED RESEARCH ON RICH-LEAN TYPE SINGLE SECTOR AND FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT ENGINE |
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ICAS2014_0632: A.A. Rossikhin¹, Y.D. Khaletskiy, Central Institute of Aviation Motors , Russia; V.I. Mileshin¹; ¹Central Institute of Aviation Motors, Russia FAR-FIELD FAN NOISE ESTIMATION WITH THE APPLICATION OF 3D AEROACOUSTIC CALCULATION |
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ICAS2014_0716: H.D. Schwartz¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States MODEL FORM UNCERTAINTY REPRESENTATION TO ENABLE MULTIFIDELITY DESIGN OF ADVANCED CONCEPTS |
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ICAS2014_0744: P.C. Vratny¹, P. Forsbach¹, A. Seitz¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany INVESTIGATION OF UNIVERSALLY ELECTRIC PROPULSION SYSTEMS FOR TRANSPORT AIRCRAFT |
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ICAS2014_0746: A. Zubko¹, I. Zubko¹, V. Kritsky¹; ¹Lyulka Design Bureau, Russia IMPLEMENTATION OF HIGH STRENGTH COMPOSITE CERAMIC MATERIALS FOR PRODUCING TRIBOTECHNICAL PARTS OF GAS TURBINE ENGINES AS CONSTRUCTIONAL NANO-STRUCTURED MATERIALS |
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ICAS2014_0770: 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 PROGRESS TOWARDS ADAPTIVE AIRCRAFT ENGINE NACELLES |
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ICAS2014_0779: J. Temis¹, A. Selivanov¹, I. Dzeva¹; ¹Central Institute of Aviation Motors, Russia FLUID-STRUCTURAL ANALYSIS OF A NON-CONTACTING FINGER SEAL |
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ICAS2014_0780: G. Veresnikov, IPU, Russia RECOVERY OF HIGH-SPEED AND THROTTLE CHARACTERISTICS TURBOJET ENGINE BASED ON THE EMPIRICAL DATA |
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ICAS2014_0791: N. Kapyrin, MAI (Moscow Aviation Institute), Russia DESIGNING GAS TURBINE CONTROL SYSTEMS AT DIFFERENT LEVELS OF ABSTRACTION |
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ICAS2014_0820: A.V. Lukovnikov¹, O.D. Selivanov¹, P.A. Ryabov¹, Y.A. Ezrokhi¹, S.M. Kalensky¹; ¹CIAM, Russia THE HYBRID PROPULSION SYSTEMS FOR THE ADVANCED AIRCRAFT |
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ICAS2014_0825: I. Brailko¹, V. Mileshin¹, A. Rossikhin¹; ¹Central Institute of Aviation Motors, Russia ASSESSMENT OF AERODYNAMIC AND ACOUSTIC CHARACTERISTICS OF COUNTER-ROTATING OPEN ROTORS |
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ICAS2014_0847: M. Danilov¹, M. Frantsuzov¹, N. Kukshinov¹; ¹Central Institute of Aviation Motors, Russia HEAT FLUX LEVEL DETERMINATION IN MODEL COMBUSTION CHAMBER OF HIGH-SPEED RAMJET ENGINE |
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ICAS2014_0856: Y.M. Tsirkunov¹, D.A. Romanyuk¹, S.V. Panfilov¹; ¹Baltic State Technical University, Russia COMPUTATIONAL SIMULATION OF TWO-PHASE GAS-PARTICLE FLOW IN AN INLET “ROTOR-STATOR” STAGE OF A TURBOJET ENGINE COMPRESSOR |
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ICAS2014_0869: 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 PHYSICAL INSIGHT INTO FUEL MIXING ENHANCEMENT WITH BACKWARD-FACING STEP FOR SCRAMJET ENGINES VIA MULTI-OBJECTIVE DESIGN OPTIMIZATION |
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ICAS2014_0871: S.V. Kharkovskiy ¹, R.Z. Nigmatullin¹, V.S. Kinzburskiy¹, V.V. Starodubtsev¹; ¹CIAM, Russia MULTIDISCIPLINARY ANALYSIS OF HIGH AND LOW PRESSURE TURBINES ON TRANSITIVE MODES IN THE FLIGHT CYCLE |
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ICAS2014_0902: I.V. Eremkin¹, I.N. Shirokov¹; ¹Moscow Aviation Institute (National Research University), Russia THE STUDIES OF CONSTRUCTION ELEMENTS OF SCRAMJET ENGINE CONDUCTED BY ON UNIVERSAL MODEL AERODYNAMIC FACILITY |
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ICAS2014_0904: V.M. Abashev¹, A.G. Prudnikov¹, E.E. Son¹; ¹Moscow Aviation Institute, Russia MODERN RESEARCH AREAS OF SOLID HYPERSONIC RAMJET ENGINES |
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ICAS2014_0928: A. Startsev¹, Y. Fokin¹, E. Steshakov¹; ¹Central Inst of Aviation Motors, Russia CFD DESIGN AND ANALYSIS OF A COMPACT SINGLE-SPOOL COMPRESSOR FOR A HEAVY TRANSPORT HELICOPTER'S POWERPLANT |
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ICAS2014_0948: H.A. Choi¹, H.D. Kam, Hanwha Corp., South Korea; J.S. Kim¹; ¹Pukyong National University, South Korea NUMERICAL INVESTIGATION ON THE CORRELATION BETWEEN SHOCK STRUCTURE AND THRUST PERFORMANCE IN AN OVEREXPANDED NOZZLE |
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ICAS2014_0974: A.A. Inozemtsev¹, L.B. Polatidi¹, I.L. Andreychenko¹; ¹Aviadvigatel OJSC, Russia LIFE VALIDATION STRATEGY |
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ICAS2014_0977: A. Mahallati, National Research Council of Canada, Canada GEOMETRIC AND FLOW PARAMETERS EFFECTING THE AERO-THERMAL PERFORMANCE OF TURBOFAN FORCED MIXERS |
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ICAS2014_0978: A. Mahallati, National Research Council of Canada, Canada AERODYNAMIC DESIGN OF HIGH PERFORMANCES INTER-TURBINE TRANSITION DUCTS |
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ICAS2014_1007: T. Popova¹, M. Drobysh¹, A. Lanshin¹, V. Lomazov¹; ¹CENTRAL INSTITUTE of AVIATION MOTORS, Russia DEVELOPMENT OF KEY TECHNOLOGIES FOR MICRO REGENERATIVE GAS TURBINES |
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ICAS2014_1023: E.E. Iglesias¹, H. Millwater¹; ¹University of Texas at San Antonio, United States SENSITIVITY ANALYSIS OF TURBINE ENGINE SUSTAINMENT |
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ICAS2014_1024: A.R. Wadia, GE Aviation, United States TECHNOLOGIES FOR THE NEXT ENGINE GENERATION |
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ICAS2014_1025: J. Henne, MTU, Germany GEARING UP FOR HIGH VOLUME GTFTM PRODUCTION |
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ICAS2014_1026: V. Mileshin, CIAM, Russia CHALLENGES IN FAN AND HIGH PRESSURE COMPRESSOR DEVELOPMENT |
5.1 - Flight Dynamics and Control (Control & Modelling) |
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ICAS2014_0033: A. Fujimori¹, S. Oh-hara¹; ¹University of Yamanashi, Japan ITERATIVE LEARNING IDENTIFICATION AGAINST NON-ZERO INITIAL STATES AND ESTIMATION OF AERODYNAMIC DERIVATIVES |
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ICAS2014_0060: A. Mannarino¹, P. Mantegazza¹; ¹Politecnico di Milano, Italy ADAPTIVE CONTROL OF AEROELASTIC SYSTEMS: AN IMMERSION AND INVARIANCE APPROACH |
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ICAS2014_0114: Y. Lee¹, Y. Kim¹, G. Moon², B.-E. Jun²; ¹Seoul National University, South Korea; ²Agency for Defense Development, South Korea BOOST-PHASE MISSILE ATTITUDE CONTROLLER DESIGN USING HIGHER-ORDER SLIDING MODES |
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ICAS2014_0115: N. Yoshitani, TEIKYO UNIVERSITY, Japan A TIME SERIES MODEL OF ANGLE OF ATTACK AND PITCH RATE FOR A WIDE RANGE OF ALTITUDE AND VELOCITY |
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ICAS2014_0121: A.A. Dementyev¹, Y.I. Didenko¹, N.B. Lysenkova¹; ¹TsAGI, Russia PRINCIPLES OF THE AUTOMATED CONTROL FOR THE CIVIL AIRCRAFT, WHICH PROVIDE FLIGHT SAFETY |
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ICAS2014_0122: A.A. Bondarenko¹, V.I. Zhelonkin¹, M.V. Zhelonkin¹, O.I. Tkachenko¹; ¹TSAGI, Russia TRAINING TECHNIQUE TO EXERCISE AT SIMULATOR THE DIFFICULT FLIGHT STAGES |
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ICAS2014_0134: M. Dobrovinsky¹, J. Z. Ben-Asher¹; ¹Technion, Israel CRUISE FLIGHT THROTTLE OPTIMIZATION BY APPROXIMATE DYNAMIC PROGRAMMING |
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ICAS2014_0152: A.V. Nebylov, State University of Aerospace Instrumentation, Russia FLIGHT CONTROL SYSTEMS FOR WIG-CRAFT |
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ICAS2014_0165: A.V. Efremov¹, A.V. Koshelenko¹, M.S. Tjaglik¹, A.S. Tjaglik¹; ¹Moscow aviation institute, Russia THE WAYS FOR IMPROVEMENT OF AGREEMENT BETWEEN IN-FLIGHT AND GROUND-BASED SIMULATION FOR EVALUATION OF HANDLING QUALITIES AND PILOT TRAINING |
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ICAS2014_0166: T.A. Tikhomirova¹, G.T. Fedorenko¹; ¹FGUP GosNIIAS, Russia FAST ANALYSIS OF THE NATURAL EDGE LANDMARKS FOR AUTONOMOUS NAVIGATION |
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ICAS2014_0201: R. Rodríguez Robles¹, J. Pérez Serrano¹; ¹Airbus Military, Spain SLOSHING MECHANICAL MODEL FOR STABILITY AND HANDLING QUALITIES EVALUATION OF THE C295 AIRCRAFT WITH THE OSD SYSTEM |
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ICAS2014_0210: O.N. Korsun, State Institute of Aviation Systems, Russia; B.K. Poplavsky, Gromov Flight Research Institute, Russia APPROACHES FOR FLIGHT TESTS AIRCRAFT PARAMETER IDENTIFICATION |
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ICAS2014_0232: T. Langener¹, S. Erb¹, J. Steelant¹; ¹ESA, Netherlands TRAJECTORY SIMULATION AND OPTIMIZATION OF THE LAPCAT-MR2 HYPERSONIC CRUISER CONCEPT |
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ICAS2014_0237: E. Capello¹, G. Guglieri¹, F. Quagliotti¹; ¹Politecnico di Torino, Italy L1 ADAPTIVE CONTROLLER DESIGN FOR GUST LOAD ALLEVIATION |
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ICAS2014_0256: H. Abbasi, National Research Council Canada, Canada NON-INTRUSIVE FLIGHT TEST INSTRUMENTATION TECHNOLOGIES |
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ICAS2014_0270: T. Goetzendorf-Grabowski, Warsaw University of Technology, Poland STABILITY PROBLEMS OF THREE SURFACE CONFIGURATION |
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ICAS2014_0277: M. Naruoka, Japan Aerospace Exploration Agency, Japan FLIGHT DATA CLASSIFIER FOR EFFECTIVE AIRCRAFT PERFORMANCE ANALYSIS |
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ICAS2014_0306: R. Verhoeven¹, R. Dalmau², X. Prats², N. de Gelder¹; ¹NLR, Netherlands; ²UPC, Spain REAL-TIME AIRCRAFT CONTINUOUS DESCENT TRAJECTORY OPTIMIZATION WITH ATC TIME CONSTRAINTS USING DIRECT COLLOCATION METHODS |
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ICAS2014_0319: 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 EVALUATIONS OF FLYING QUALITIES FOR A NEW AND AN AGING TRANSPORT AIRCRAFT IN SEVERE ATMOSPHERIC TURBULENCE |
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ICAS2014_0329: M.N. Krasilshchikov¹, D.A. Kozorez¹, K.I. Sypalo, Central Aerohydrodynamic Institute, Russia; ¹Moscow Aviation Institute (National Research University), Russia DEVELOPMENT OF HIGH SPEED FLYING VEHICLE ON-BOARD INTEGRATED NAVIGATION, CONTROL AND GUIDANCE SYSTEM |
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ICAS2014_0412: G. Franzè, DIMES- Università della Calabria, Italy; M. Mattei, DIII- Seconda Università di Napoli, Italy; V. Scordamaglia, DIIES - Università di Reggio Calabria, Italy CONSTRAINED PREDICTIVE STRATEGIES FOR FLIGHT CONTROL SYSTEMS |
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ICAS2014_0415: I. Grishin¹, A. Khrabrov¹, A. Kolinko¹, M. Sidoryuk¹, A. Vyalkov¹; ¹TsAGI, Russia WIND TUNNEL INVESTIGATION OF CRITICAL FLIGHT REGIMES USING DYNAMICALLY SCALED ACTIVELY CONTROLLED MODEL IN 3 DOF GIMBAL |
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ICAS2014_0421: Y. Liu¹, Z. Gao¹; ¹Northwestern Polytechnical University, China AN EVALUATING MODEL FOR CONTROL EFFECTOR SUPERIORITY BASED ON PERFORMANCE REQUIREMENTS |
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ICAS2014_0427: M.-G. Seo¹, C.-H. Lee², M.-J. Tahk¹, J.-I. Lee², B.-E. Jun²; ¹KAIST, South Korea; ²Agency for Defense Development, South Korea CONTROL INPUT BLENDING LOGIC WITH AERODYNAMIC CONTROL AND REACTION JET CONTROL |
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ICAS2014_0438: A. Andreeva-Mori¹, K. Kobayashi¹, M. Shindo¹; ¹Japan Aerospace Exploration Agency, Japan EVALUATION OF SATELLITE IMAGERY INTEGRATION IN OPTIMAL AIRCRAFT OPERATION PLANNING FOR DISASTER RELIEF |
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ICAS2014_0442: A.N. Khrabrov¹, D.A. Kravchenko¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia COMPUTATIONAL INVESTIGATION OF UNSTEADY AERODYNAMIC CHARACTERISTICS OF A MODERN AIRLINER |
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ICAS2014_0447: A.M. Shmatkov¹, A.E. Utemov¹, Y.N. Zhelnin, TsAGI, Russia; F.L. Chernousko¹; ¹IPMech RAS, Russia NUMERICAL CALCULATION OF OPTIMAL 3D-TRAJECTORIES FOR THE MANEUVERABLE AIRCRAFT |
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ICAS2014_0464: M. Zhang¹, M. Cristofaro², Y. Wang, China Academy of Aerospace Aerodynamics, China; A. Da Ronch², A. Rizzi¹; ¹Royal Institute of Technology, Sweden; ²University of Southampton, United Kingdom INVESTIGATING THE PIAGGIO AVANTI DESIGN USING CEASIOM |
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ICAS2014_0487: A.V. Efremov¹, S.A. Popov¹, I.A. Nikitchenko¹, A.V. Koshelenko¹, Y.V. Tiumentzev¹; ¹Moscow aviation institute, Russia AERODYNAMICS AND FLIGHT DYNAMICS PROBLEMS OF HIGH SPEED VEHICLES AND WAYS FOR THEIR SOLUTION |
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ICAS2014_0526: Y.Q. Dong¹, L.D. Zhang¹, J.L. Ai¹; ¹Fudan University, China ATTITUDE PROTECTION FOR SIDE STICK-OPERATED AIRCRAFT - THE CLASSIC APPROACH |
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ICAS2014_0530: M.V. Egorchev¹, D.S. Kozlov¹, Y.V. Tiumentsev¹; ¹Moscow Aviation Institute (MAI), Russia NEURAL NETWORK ADAPTIVE SEMI-EMPIRICAL MODELS FOR AIRCRAFT CONTROLLED MOTION |
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ICAS2014_0552: M. Lis¹, A. Dziubinski¹, C. Galinski¹, G. Krysztofiak¹, P. Ruchala¹, K. Surmacz¹; ¹Instytut Lotnictwa, Poland PREDICTED FLIGHT CHARACTERISTICS OF THE INVERTED JOINED WING SCALED DEMONSTRATOR |
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ICAS2014_0561: O.N. Korsun, State Institute of Aviation Systems, Russia; V.P. Harkov, Experimental Enterprise Nauka-Soft, Russia ENERGY APPROACH FOR AIRCRAFT VELOCITY OPTIMAL CONTROL DESIGN |
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ICAS2014_0562: A.E. Sagalakov¹, A.S. Filatyev¹; ¹Central Aerohydrodynamic institute (TsAGI), Russia NEW PERIODIC SOLUTIONS IN THE AIRCRAFT MAXIMUM RANGE PROBLEM |
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ICAS2014_0588: V.V. Rogozin¹, S.A. Zuev¹, M.A. Grigoryev¹, L.E. Zaichik², Y.P. Yashin²; ¹GFRI, Russia; ²TsAGI, Russia REFINEMENT OF THE MODEL OF PILOT PERCEPTION OF AIRCRAFT MOTION IN UPSET CONDITIONS UTILIZING FLIGHT TESTS RESULTS |
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ICAS2014_0591: N. Abramov¹, M. Bommanahal², S. Chetty², M. Goman¹, E. Kolesnikov¹, P.V.S. Murthy²; ¹De Montfort University, United Kingdom; ²CSIR-National Aerospace Laboratories, India FLIGHT ENVELOPE EXPANSION VIA ACTIVE CONTROL SOLUTIONS FOR A GENERIC TAILLESS AIRCRAFT |
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ICAS2014_0664: C. Roos¹, G. Hardier¹, C. Döll¹; ¹ONERA/DCSD, France A COMPARISON OF TECHNIQUES TO GET SPARSE RATIONAL APPROXIMATIONS FOR LINEAR FRACTIONAL REPRESENTATIONS |
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ICAS2014_0671: S. Kannokkada¹, N.K. Sinha¹; ¹Indian Institute of Technology Madras, India EFFECT OF AERODYNAMIC UNCERTAINTIES ON HIGH-ALPHA SPIN |
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ICAS2014_0734: W. Lee, Seoul Nat'l Univ., South Korea PERFORMANCE OF SWITCHING TYPE DATABASE REFERENCED NAVIGATION ALGORITHM USING TERRAIN HEIGHT AND GRAVITY ANOMALY |
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ICAS2014_0742: S.W. Shim¹, B.-G. Park², B.-J. Jeon¹, M.-J. Tahk¹, H.H. Kwon²; ¹KAIST, South Korea; ²LIG Nex1, South Korea EXTENDED KALMAN FILTER DESIGN USING BEARING AND TIME-TO-GO MEASUREMENT FOR A HOMING MISSILE GUIDANCE |
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ICAS2014_0745: A.G. Bushgens¹, L.E. Zaychik¹, A.N. Khrabrov¹, I.I. Grishin¹, P.A. Desyatnik¹, V.V. Biryukov, FRI, Russia; ¹TsAGI, Russia UPSET RECOVERING SIMULATION TO ENHANCE FLIGHT SAFETY BY ON-GROUND PILOT TRAINING |
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ICAS2014_0777: V. Ovcharenko , Moscow Aviation Institute (State Technical University), Russia; E. Egorova, Russian Aircraft Corporation \, Russia IDENTIFICATION OF THE AERODYNAMIC COEFFICIENTS OF THE MULTIROLE MANEUVERABLE AIRCRAFT BASED ON UNSTEADY FLIGHT |
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ICAS2014_0787: H.-H. Kwon¹, M.-W. Seo¹, D.-S. Jang¹, H.-L. Choi¹; ¹KAIST, South Korea SUM-OF-SQUARES BASED STABILITY ANALYSIS FOR SKID-TO-TURN MISSILES WITH THREE-LOOP AUTOPILOT |
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ICAS2014_0815: S.G. Bazhen SIMULATION OF ON-BOARD MODEL OF AIRLINER TO EVALUATE CAPABILITY OF TRAJECTORIES AND FLIGHT SAFETY |
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ICAS2014_0893: A. Kwiek, Warsaw University of Technology, Poland STUDY ON CONTROL AND STABILITY OF THE ROCKET PLANE TO SPACE TOURISM |
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ICAS2014_0901: D. Rohacs, REA-TECH, Hungary; M. Voskuijl, Delft University of Technology, Netherlands; N. Siepenkötter, RWTH Aachen, Germany 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. |
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ICAS2014_0920: A.S. Filatyev¹, O.V. Yanova¹, N.N. Ryabukha, Gromov Flight Research Institute (FRI), Russia; ¹Central Aerohydrodynamic Institute (TsAGI), Russia THROUGH OPTIMIZATION OF A WINGED BOOSTER TRAJECTORY OF REUSABLE AEROSPACE SYSTEM AND PECULIARITIES OF ITS FLIGHT TRY-OUT |
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ICAS2014_0921: A.S. Filatyev¹, A.A. Golikov¹; ¹Central Aerohydrodynamic Institute, Russia NEW FEATURES OF UNGUIDED BODY REENTRY WITH SUBCIRCULAR VELOCITY AND PECULIARITIES OF ITS SIMULATION |
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ICAS2014_0951: M. Ulinowicz¹, J. Narkiewicz¹; ¹Warsaw University of Tchnology, Poland AIRCRAFT PARAMETER IDENTIFICATION USING GENTIC ALGORITHMS |
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ICAS2014_0959: S.G. Bazhenov¹, V.S. Korolyov¹, E.L. Kulida², V.G. Lebedev²; ¹Central Aerohydrodynamic Institute (TsAGI), Russia; ²Institute of Control Sciences n.a. V.A. Trapeznikov, Russia ABOUT AIRCRAFT STABILITY DURING WING-IN-GROUND EFFECT FLIGHT |
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ICAS2014_0990: L.M.B.C. Campos, Instituto Superior Técnico, Portugal; J.M.G. Marques, Universidade Lusófona de Humanidades e Tecnologias, Portugal ON THE COMPENSATION AND DAMPING OF ROLL INDUCED BY WAKE VORTICES |
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ICAS2014_1005: S.P. Kostukov, Beriev Aircraft Company, Russia SYNTHESIS OF AIRCRAFT MOTION CONTROL LAWS USING AGGREGATIVE CONTROLLER ANALYTICAL DESIGN PROCEDURE DURING AUTOMATIC IN-FLIGHT REFUELING |
5.2 - Flight Dynamics and Control (UAV related) |
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ICAS2014_0099: H. Hiraguri¹, H. Tokutake¹; ¹Kanazawa University, Japan MODELING OF DUST DEVIL ON MARS AND FLIGHT SIMULATION OF MARS AIRPLANE |
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ICAS2014_0123: Z.-X. Yao, SADRI, China AERODYNAMIC MODEL IDENTIFICATION FROM FLIGHT DATA FOR A NOVEL CONCEPT SCALED UAV |
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ICAS2014_0189: C. Park¹, H.J. Kim¹, Y. Kim¹; ¹Seoul National University, South Korea REAL-TIME LEADER-FOLLOWER UAV FORMATION FLIGHT BASED ON MODIFIED NONLINEAR GUIDANCE |
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ICAS2014_0259: W. Shi¹, Z. Yuan¹, L. Zhang¹; ¹AVIC Chengdu Aircraft Design & Research Institute, China AUTOMATED CONTROL STRATEGY FOR HALE UAV FLAMEOUT LANDING AND ITS FLIGHT SIMULATION STUDY |
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ICAS2014_0285: G. Di Francesco¹, G. Scapaticci¹, M. Mattei¹; ¹Seconda Università di Napoli, Italy TRANSITION CONTROL AND REDUNDANCY MANAGEMENT FOR A TILT ROTOR UAV USING GENETIC ALGORITHMS |
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ICAS2014_0316: H.-I. Lee¹, B.-Y. Lee¹, D.-W. Yoo¹, G.-H. Moon¹, M.-J. Tahk¹; ¹KAIST, South Korea DYNAMICS MODELING AND ROBUST CONTROLLER DESIGN OF THE MULTI-UAV TRANSPORTATION SYSTEM |
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ICAS2014_0433: H. Djojodihardjo¹, M. Anas Bin Abd Bari¹; ¹Universiti Putra Malaysia, Malaysia KINEMATIC AND UNSTEADY AERODYNAMIC MODELLING OF FLAPPING BI- AND QUAD-WING ORNITHOPTER |
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ICAS2014_0441: Y. Inada, Tokai University, Japan FLEXIBLE FORMATION SHAPE CONTROL BASED ON THE LOCAL INTERACTION AMONG AIR VEHICLES |
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ICAS2014_0495: M. Rieck¹, M. Richter¹, M. Bittner¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, Germany GENERATION OF INITIAL GUESSES FOR OPTIMAL CONTROL PROBLEMS WITH MIXED INTEGER DEPENDENT CONSTRAINTS |
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ICAS2014_0507: R. Wang¹, Z. Zhou¹, X. Zhu, Institute of UAV, Northwestern Polytechnical University, China; X. Xu¹; ¹Science and Technology on UAV Laboratory, Northwestern Polytechn, China FLIGHT DYNAMICS OF HIGHLY FLEXIBLE SOLAR-POWERED UAV BASED ON GEOMETRICALLY NONLINEAR INTRINSIC BEAM |
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ICAS2014_0527: Y.Q. Dong¹, X.Z. YANG¹, J.L. AI¹; ¹Fudan University, China RESEARCH ON ENEMY AIRCRAFT BANK ANGLE ESTIMATION FOR AUTONOMOUS AIR COMBAT |
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ICAS2014_0529: J. Wang¹, B. Song¹, L. Wang¹; ¹School of Aeronautics,Northwestern Polytechnical Unversity, China L1 ADAPTIVE ATTITUDE CONTROLLER FOR A TAIL-SITTER MAV IN HOVER FLIGHT |
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ICAS2014_0567: S. Potyagaylo¹, O. Rand¹; ¹Technion, Israel AUTONOMOUS TARGETED FLIGHT OF A ROTARY-WING MICRO AERIAL VEHICLE IN INDOOR, GPS-DENIED ENVIRONMENTS |
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ICAS2014_0574: S. Bassolillo¹, E. D'Amato¹, I. Notaro¹, L. Blasi¹; ¹Second University of Naples - DIII, Italy A MULTI-OBJECTIVE GENETIC ALGORITHM FOR A MAXIMUM COVERAGE FLIGHT TRAJECTORY OPTIMIZATION IN A CONSTRAINED ENVIRONMENT |
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ICAS2014_0586: R.K. Rangel, BRVANT / BRV UAV& Flight Systems , Brazil; K.H. Kienitz¹, M.P. Brandão¹; ¹Technological Institute of Aeronautics - ITA, Brazil DEVELOPMENT OF A MULTI-PURPOSE UAV WITH BIO-INSPIRED FEATURES |
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ICAS2014_0587: S. Chiesa¹, S.C. Aleina¹, G.A. Di Meo¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy AUTONOMOUS TAKE-OFF AND LANDING FOR UNMANNED AIRCRAFT SYSTEM: RISK AND SAFETY ANALYSIS |
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ICAS2014_0659: P. Czekalowski, Institute of Aviation, Poland; K.-S. Sibilski¹, A. Zyluk¹; ¹Air Force Institute of Technology, Poland APPLICATION OF ARTIFICIAL NEURAL NETWORK IN MODELING OF ENTOMOPTER DYNAMICS |
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ICAS2014_0730: Y. Nagao¹, K. Uchiyama¹; ¹Nihon University, Japan FORMATION FLIGHT OF FIXED-WING UAVS USING ARTIFICIAL POTENTIAL FIELD |
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ICAS2014_0731: V.V. Golubev¹, W. MacKunis¹; ¹ERAU, United States ON UAV ROBUST NONLINEAR CONTROL IN PRESENCE OF PARAMETRIC UNCERTAINTIES |
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ICAS2014_0765: G.H. Moon¹, D.W. Yoo¹, B.Y. Lee¹, H.I. Lee¹, M.J. Tahk¹; ¹KAIST, South Korea MULITLE TASK ASSIGNMENT FOR COOPERATIVE TRANSPORT SYSTEM WITH GROUP BUYING APPROACH |
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ICAS2014_0826: N. K. SINHA, IIT-Madras, India CONCEPTUAL DESIGN OF AIRCRAFT FOR OPTIMAL MANEUVERS |
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ICAS2014_0837: Y.I. Jenie, Delft University of Technology, Faculty of Aerospace Engineering, Netherlands HARDWARE IMPLEMENTATION OF COOPERATIVE AUTONOMOUS COLLISION AVOIDANCE STRATEGY FOR UNMANNED AERIAL VEHICLES |
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ICAS2014_0838: Z. Lei¹, H. Kawamura¹; ¹Tokyo University of Science, Suwa, Japan DESIGN AND FLIGHT TEST OF A SOLAR-POWERED UNMANNED AIR VEHICLE FOR LONG ENDURANCE |
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ICAS2014_0840: E. Miles, University of Pretoria, South Africa; B.A. Broughton, Incomar Aeronautic, South Africa OPTIMAL CONTROL SURFACE MIXING OF A RHOMBOID WING UAV |
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ICAS2014_0850: P. Hartmann¹, C. Ben¹, D. Moormann¹; ¹RWTH Aachen, Germany NAVIGATION FOR VERTICAL PRECISION LANDING BASED ON OPTICAL TRACKING OF A SPATIAL RETROREFLECTIVE MARKER ARRAY |
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ICAS2014_0915: M.P. Degrande¹, E.E.T. Moreira¹, E.M. Belo¹; ¹Escola de Engenharia de São Carlos - Universidade de São Paulo, Brazil AN APPLICATION OF DIGITAL IMAGE PROCESSING FOR UAV’S AUTOMATIC LANDING SYSTEM AID |
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ICAS2014_1011: J. Dadashi, Virginia Polytechnic Institute and State University, United States IDENTIFICATION AND TRACKING CONTROL OF FLAPPING MOTIONS IN ROBOTIC BATS |
6 - Systems, Subsystems and Equipment |
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ICAS2014_0080: L. Hu, Nanjing Engineering Institute of Aircraft Systems,AVIC, China RESEARCH ON INTEGRATION OF VAPOR CYCLE/LIQUID-COOLED REFRIGERATION SYSTEM FOR HELICOPTERS |
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ICAS2014_0100: M. Mirzaee¹, M. Sam kan, Sattari University, Iran; S. Behroozifar¹; ¹University of Science and Applied of SAMAPARAN, Iran DADF ( DIGITAL AUTOMATIC DIRECTION FINDER ) |
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ICAS2014_0146: A.E. Ananenkov¹, A.V. Konovaltsev¹, V.M. Nuzhdin¹, V.V. Rastorguev¹, V.N. Skosyrev, Moscow State Technical University, Russia; ¹Moscow Aviation Institute, Russia MULTI-FUNCTIONAL AERODROME CONTROL RADAR BY USPR TECHNOLOGY |
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ICAS2014_0148: G.A. Chuyanov¹, V.V. Kosyanchuk¹, N.I. Selvesyuk¹, E.Y. Zybin¹; ¹State Research Institute of Aviation Systems, Russia ADVANCED AVIONICS EQUIPMENT ON THE BASIS OF SECOND GENERATION INTEGRATED MODULAR AVIONICS |
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ICAS2014_0208: H. Inokuchi¹, M. Furuta¹, T. Inagaki¹; ¹JAXA, Japan HIGH ALTITUDE TURBULENCE DETECTION USING AN AIRBORNE DOPPLER LIDAR |
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ICAS2014_0243: S.A. Gafurov¹, A.B. Prokofiev¹, E.V. Shakhmatov ¹; ¹Samara State Aerospace University (National Research University), Russia REDUCTION OF VIBROACOUSTIC LOAD IN AVIATION COMBINED PUMPS |
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ICAS2014_0254: E.E. Kitanina, Saint-Petersburg State Technical University, Russia; D.A. Bondarenko, EADS RTO SK LLC, Russia; D. Morrison, Airbus Operations Ltd, United Kingdom AIR EVOLUTION IN FUEL FLOW UNDER DECREASED PRESSURE CONDITIONS: EXPERIMENTAL STUDIES AND ENGINEERING CODE DEVELOPMENT |
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ICAS2014_0261: R. Trott, EADS Innovation Works Germany, Germany OPTIMIZATION OF ADSORPTION-BASED DEHUMIDIFICATION DEVICES FOR FUEL-TANK INERTING APPLICATIONS |
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ICAS2014_0274: O.V. Zayats¹, V.Y. Tugaenko¹, V.P. Khvostikov, Ioffe Physico-Technical Institute, Russia; ¹S.P. Korolev Rocket And Space Corporation \\\\\\\\, Russia UAV REMOTE POWER SUPPLY SYSTEM BY LASER RADIATION |
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ICAS2014_0343: A. Lupidi¹, S. Lischi¹, F. Berizzi¹, M. Martorella¹, F. Cuccoli¹; ¹CNIT - RaSS, Italy POLARIMETRIC AVIONIC WEATHER RADAR FOR INCREASING FLIGHT SAFETY AND EFFICIENCY |
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ICAS2014_0395: A. Shinkafi¹, C. Lawson¹, R. Seresinhe¹, D. Quaglia¹, I. Madani¹; ¹Cranfield University, United Kingdom AN INTELLIGENT ICE PROTECTION SYSTEM FOR NEXT GENERATION AIRCRAFT TRAJECTORY OPTIMISATION |
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ICAS2014_0398: R. Seresinhe¹, C. Lawson¹, A. Shinkafi¹, D. Quaglia¹, I. Madani¹; ¹Cranfield University, United Kingdom AIRFRAME SYSTEMS POWER OFF-TAKE MODELLING IN MORE-ELECTRIC LARGE AIRCRAFT FOR USE IN TRAJECTORY OPTIMISATION |
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ICAS2014_0437: E. Efimov¹, T. Shevgunov¹, A. Valaytite¹, E. Sadovskaya¹; ¹Moscow Aviation Institute (National Research University), Russia ARTIFICIAL NEURAL NETWORK BASED SIGNAL PROCESSING FOR PERSPECTIVE ONBOARD SYSTEMS |
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ICAS2014_0455: I. Notaro¹, M. Ariola, Università di Napoli Parthenope-DI, Italy; E. D'Amato¹, M. Mattei¹; ¹Seconda Università degli Studi di Napoli-DIII, Italy HW VS SW SENSOR REDUNDANCY: FAULT DETECTION AND ISOLATION OBSERVER BASED APPROACHES FOR INERTIAL MEASUREMENT UNITS |
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ICAS2014_0498: Q. Yuwu¹, Z. Ning¹, Z. Xingmin¹; ¹Xi’an Aero-engine ( Group ) Ltd., China THE EFFECT OF THE HUMIDITY ON THE CORRECTION COEFFICIENT OF THE SONIC THERMOCOUPLE USED IN AVIATION |
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ICAS2014_0557: V. Bukov, LSC Institute of Aircraft Equipment, Russia A DEMONSTRATOR FOR AVIONICS OF ZERO MAITENANCE EQUIPMENT |
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ICAS2014_0641: M. Ciminello¹, P. Bettini², S. Ameduri¹, E. Guerreschi², G. Cuneo²; ¹CIRA, Italy; ²Politecnico di Milano, Italy EXPERIMENTAL VALIDATION OF A SENSORIZED RING BASED ON OPTICAL FIBER FOR STRAIN MONITORING OF MORPHING STRUCTURE |
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ICAS2014_0669: G. Di Rito¹, R. Galatolo¹, E. Denti¹, F. Schettini¹; ¹Università di Pisa - Dip. di Ingegneria Civile ed Industriale, Italy DYNAMIC NOTCH FILTERING CONTROL FOR FAULT-TOLERANT ACTUATORS OF FLY-BY-WIRE HELICOPTERS |
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ICAS2014_0672: E. Richter, EADS Deutschland GmbH, Germany; D. Krause, Otto-Von-Guericke University, Germany DEVELOPMENT OF A SOLID PROPELLANT GAS GENERATOR (SPGG) SYSTEM FOR FIRE SUPPRESSION IN AVIATION - DESIGN OF AN INJECTOR |
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ICAS2014_0676: S.V. Semenov¹, M.S. Nikhamkin¹, O.V. Korepanova², Y.A. Berendorf²; ¹Perm National Research Polytechnic University, Russia; ²OJSC “Aviadvigatel”, Russia EXPERIMENTAL INVESTIGATION OF ROTOR DYNAMICS IN AIRCRAFT ENGINE WITH TWO-AXIS STIFFNESS ANISOTROPY OF SUPPORTS |
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ICAS2014_0699: S. Ameduri¹, L. Pellone¹, N. Favaloro¹, M. Ciminello¹; ¹Centro Italiano Ricerche Aerospaziali, Italy AN UAV LANDING GEAR SYSTEM ACTUATED THROUGH SMA ACTIVE ELEMENTS |
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ICAS2014_0709: K. Shiomi, ENRI, Japan; S. Aoyama, IRT Corp., Japan DEVELOPMENT OF PASSIVE SURVEILLANCE RADAR |
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ICAS2014_0747: I. Ogoltsov¹, S. Samsonovich¹, A. Selivanov¹, A. Alekseenkov¹; ¹Moscow Aviation Institute (National Research University), Russia NEW DEVELOPMENTS OF ELECTRICALLY POWERED ELECTROHYDRAULIC AND ELECTROMECHANICAL ACTUATORS FOR THE MORE ELECTRIC AIRCRAFT |
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ICAS2014_0767: R. Malakhov, The Moscow Aviation Institute (National Research University), Russia GAN POWER AMPLIFIER FOR ON-BOARD DIGITAL ANTENNA ARRAY |
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ICAS2014_0846: Konstantin K. Veremeenko, Moscow Aviation Institute (National Research University), Russia ON A CONCEPT OF CREATION OF AN AIRPORT ADVANCED SURFACE MOVEMENT AND GROUND CONTROL SYSTEM |
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ICAS2014_0891: T. Strobl¹, S. Storm¹, M. Kolb¹, J. Haag¹, M. Hornung, Technical University of Munich, Germany; ¹Airbus Group Innovations, Germany DEVELOPMENT OF A HYBRID ICE PROTECTION SYSTEM BASED ON NANOSTRUCTURED HYDROPHOBIC SURFACES |
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ICAS2014_0897: F. Schettini¹, E. Denti¹, G. Di Rito¹, R. Galatolo¹; ¹Università di Pisa, Dip. di Ingegneria Civile e Industriale, Italy SIMULATION OF AN ALL-ELECTRIC FLIGHT CONTROL SYSTEM FOR THE EVALUATION OF POWER CONSUMPTION |
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ICAS2014_0899: 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 INTEGRATED ONBOARD NETWORKING FOR IMA2G |
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ICAS2014_0936: P Nevoret, Safran / Messier-Bugatti-Dowty, France RECENT ADVANCES IN ELECTRICAL LANDING GEAR SYSTEMS |
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ICAS2014_0937: Y. Sheynin¹, E. Suvorova¹, A. Syschikov¹, B. Sedov¹, N. Matveeva¹, D. Raszhivin¹; ¹SUAI, Russia TOOLSET FOR ONBOARD NETWORKS DESIGN AND CONFIGURATION |
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ICAS2014_0950: C.Y. Nakashima¹, L. Tobaldini Neto¹; ¹Embraer, Brazil HEAT EXCHANGER THERMAL STRATIFICATION MODEL |
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ICAS2014_0984: N. Matveeva, Saint-Petersburg State University of Aerospace Instrumentation, Russia METHOD OF SEARCHING FOR ROUTES WITH DELAY AND JITTER LIMITATION |
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ICAS2014_0986: C.Y. Nakashima, Embraer, Brazil MODELING, SIMULATION AND VALIDATION OF A BLEED SYSTEM MODEL |
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ICAS2014_0995: A.A. Afonin¹, A.S. Sulakov¹, G.G. Yamashev¹; ¹MAI, Russia ABOUT THE CONCEPT OF STRAPDOWN VECTOR AEROGRAVIMETRIC MEASUREMENTS |
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ICAS2014_1000: O. Kreerenko, Beriev Aircraft Company, Russia; E. Kreerenko, Southern Federal University , Russia COMBINED SYNTHESIS OF CONTROL LAWS OF THE AIRCRAFT BRAKING ON THE RUNWAY DURING LANDING |
7 - Systems Engineering and Supply Chain |
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ICAS2014_0049: T. WangY. YanL. NUMERICAL SIMULATIONS AND EXPERIMENTS ON THE INJECTION MOLDING OF AIRCRAFT TRANSPARENCIES |
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ICAS2014_0097: D.K. Howarth, MEE Inc., United States AIMING AND MISSING IN MULTIPLE DIMENSIONS |
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ICAS2014_0194: A. Reysset¹, M. Budinger¹, J.-C. Maré¹; ¹Institut Clément Ader, France MISSION PROFILES ANALYSIS: GUIDELINES TO AIRCRAFT ACTUATORS NEW TECHNOLOGY SPECIFICATION |
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ICAS2014_0239: N.P. Randt, Technical University of Munich, Germany; S. Wolf, Munich Airport, Germany AUTOMATION IN FUTURE AIR TRANSPORT: A SCENARIO-BASED APPROACH TO THE DEFINITION OF OPERATIONAL REQUIREMENTS |
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ICAS2014_0309: N.N. Shabrov¹, A.K. Kuzin¹, S.G. Orlov¹, B.N. Chetverushkin², M.V. Iakobovski²; ¹St. Petersburg State Polytechnical University, Russia; ²Institute for Mathematical Modeling of RAS, Russia VIRTUAL PROTOTYPING MODELING IN THE CAVE 3D ENVIRONMENT |
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ICAS2014_0358: I.V. Koverninskiy¹, A.V. Kan¹; ¹FSUE GosNIIAS, Russia UNIFIED TOOLS OF DEVELOPMENT OF THE ONBOARD EQUIPMENT BASED ON THE INTEGRATED MODULAR AVIONICS |
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ICAS2014_0515: H. Nakamura¹, Y. Kajikawa, Tokyo Institute of Technology, Japan; S. Suzuki¹; ¹The University of Tokyo, Japan A BIBLIOMETRICS APPLICATION FOR EVALUATING CONTRIBUTION OF A RESEARCH INSTITUTE TO SCIENCE |
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ICAS2014_0594: W. CHENG¹, C. XING¹, H. ZHANG¹, Y. WU¹; ¹Aviation Industry Development Research Center of China (ADR), China RESEARCH ON TECHNOLOGY READINESS ASSESSMENT MODEL FOR SYSTEM OF SYSTEMS |
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ICAS2014_0646: I. Svadkovskiy¹, L. Zhemuranova¹; ¹CIAM, Russia USING THE VIRTUAL REALITY SYSTEM IN THE DEVELOPMENT OF AIRCRAFT ENGINE |
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ICAS2014_0668: F. De Crescenzio¹, F. Lucchi¹, N. Mezannar¹, F. Persiani¹; ¹University of Bologna, Italy USING BCIS (BRAIN COMPUTER INTERFACES) TO EVALUATE EMOTIONAL PERCEPTION OF PASSENGER CABIN DESIGN IN VIRTUAL ENVIRONMENTS |
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ICAS2014_0717: K.N. Gatian¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States QUANTITATIVE FIDELITY MANAGEMENT AND SELECTION OF PHYSICS-BASED MULTIDISCIPLINARY DESIGN ENVIRONMENTS |
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ICAS2014_0875: G.S. Schwening¹, A.M. Abdalla¹; ¹Escola de Engenharia de São Carlos - Universidade de São Paulo, Brazil SELECTION OF AGRICULTURAL AIRCRAFT USING AHP AND TOPSIS METHODS IN FUZZY ENVIRONMENT |
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ICAS2014_0910: V. Zdanevich¹, A. Mazin¹; ¹Southern Federal University, Russia DEVELOPMENT TRENDS OF AMPHIBIAN'S SHAPE. |
8 - Air Transport System Efficiency |
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ICAS2014_0028: M.M. van Lith , TU Delft , Netherlands; H.G. Visser¹, H.S. Hosseini¹; ¹TU Delft, Netherlands MODELING AN OPERATIONS CONCEPT FOR COMMERCIAL AIR-TO-AIR REFUELING BASED ON A VEHICLE ROUTING PROBLEM FORMULATION |
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ICAS2014_0032: R. Mori, Electronic Navigation Research Institute, Japan OPTIMAL PUSHBACK TIME WITH EXISTING UNCERTAINTIES AT BUSY AIRPORT |
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ICAS2014_0154: R.M. Arnaldo Valdés¹, V.F. Gomez Comendador¹, R. Barragán, CRIDA, Spain; L. Perez¹; ¹UPM, Spain EUROPEAN AIR NAVIGATION SERVICE PROVIDERS’ EFFICIENCY EVALUATION THROUGH DATA ENVELOPMENT ANALYSIS (DEA) |
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ICAS2014_0159: K. Kageyama, ENRI, Japan; B. Park, KOTI, South Korea VALIDATION AND SIMULATION STUDY OF THE ARRIVAL MERGING PROCEDURE MODEL |
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ICAS2014_0229: R. Barragan, CRIDA, Spain; J.A. Perez Castan¹, M. Sadornil¹, F. Saez Nieto¹, J. Crespo¹, R. Arnaldo¹, C. Cuerno¹; ¹UPM, Spain OPTIMISED ALGORITHMS FOR EXTENDED ARRIVAL MANAGERS |
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ICAS2014_0250: S.M. Malaek¹, F. Enayatollahi¹, J. Parastari, Civil Aviation Technology College, Iran; ¹Sharif University of Technology, Iran TERMINAL HOLDING TIME OPTIMIZATION BY DYNAMIC CDA ROUTING ALGORITHM |
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ICAS2014_0351: K. Zudov¹, V. Vyshinsky¹, M. Kudrov¹; ¹Moscow Institute of Physics and Technology, Russia ON THE FLIGHT OPERATING SAFETY IN THE MOUNTAINOUS ZONE AIRPORT |
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ICAS2014_0393: A. Tezuka, Waseda University, Japan 4D TRAJECTORY BASED OPERATION IN HIGH DENSITY TERMINAL CONTROL AREA CONSIDERING THE UNCERTAINTY OF WEATHER FORECAST DATA |
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ICAS2014_0450: M. Dupeyrat¹, S. Aubry¹, H. Hesselink², S. Loth, DLR, Germany; A. Remiro, ISDEFE, Spain; P. Schmollgruber¹, R. Verbeek², C. Welman²; ¹ONERA, France; ²NLR, Netherlands EVALUATION OF OPERATIONS ON AN AIRPORT WITH A CIRCULAR RUNWAY |
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ICAS2014_0486: D. Nieuwenhuisen, National Aerospace Laboratory, Netherlands 4D TRAJECTORY MANAGEMENT SUPPORT IN THE C-SHARE PROJECT |
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ICAS2014_0522: F. Morscheck, DLR, Germany ANALYSES ON A CIVIL AIR TO AIR REFUELING NETWORK IN A TRAFFIC SIMULATION |
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ICAS2014_0556: J. Crespo¹, C. Cuerno¹, R.M. Arnaldo¹, J. Saez Nieto¹, M. Sadornil¹, J. Pérez¹, R. Barragan, CRIDA, Spain; ¹Technical University of Madrid (UPM), Spain A COMPARISON OF THE TWO ARRIVAL TRAFFIC SYNCHRONIZATION CONCEPTS ENVISIONED FOR NEXTGEN AND SESAR. |
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ICAS2014_0564: N. Grevtsov¹, A. Dymchenko¹; ¹TsAGI, Russia APPLICATION OF SUBOPTIMAL 4-D NAVIGATION ALGORITHMS FOR FLIGHT PLANNING AND CONTROL CONSIDERING WEATHER CONDITIONS |
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ICAS2014_0617: S. Lehner¹, K. Kölker¹, K. Lütjens¹; ¹German Aerospace Center (DLR), Germany EVALUATING TEMPORAL INTEGRATION OF EUROPEAN AIR TRANSPORT |
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ICAS2014_0714: T. Iijima¹, N. Matayoshi¹, E. Yoshikawa¹; ¹JAXA, Japan DEVELOPMENT AND EVALUATION OF LOW-LEVEL TURBULENCE ADVISORY DISPLAY FOR AIRCRAFT OPERATION |
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ICAS2014_0724: Y. Matsuno, The University of Tokyo, Japan STOCHASTIC CONFLICT-FREE 4D TRAJECTORY OPTIMIZATION IN THE PRESENCE OF UNCERTAINTY |
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ICAS2014_0743: A. Harada¹, T. Kozuka¹, Y. Miyazawa¹, N.K. Wickramasinghe², M. Brown², Y. Fukuda²; ¹Kyushu University, Japan; ²ENRI Japan, Japan ANALYSIS OF AIR TRAFFIC EFFICIENCY USING DYNAMIC PROGRAMMING TRAJECTORY OPTIMIZATION |
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ICAS2014_0761: 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 THE NETWORK FLOW ENVIRONMENT: SLOT ALLOCATION MODEL EVALUATION WITH CONVECTIVE NOWCASTING |
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ICAS2014_0844: Y. Nakamura, Electronic Navigation Research Institute, Japan; N. Takeichi¹, K. Fukuoka¹; ¹Nagoya University, Japan A SELF-SEPARATION ALGORITHM USING SPEED CONTROL FOR WIDTH-LIMITED HIGH DENSITY AIR CORRIDOR |
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ICAS2014_0876: G. Enea, Engility Corporation, United States; G. McDonald¹, J. Bronsvoort¹; ¹AirServices Australia, Australia TRAJECTORY PREDICTION PERFORMANCE COMPARISON TOWARDS EFFICIENT TIME-BASED METERING OPERATIONS |
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ICAS2014_0952: Pan Weijun¹, Qiu Wenbin¹, Kang Rui¹; ¹Civil Aviation Flight University of China, China BALANCED ALLOCATION ON ARRIVAL AIR TRAFFIC FLOW |
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ICAS2014_0971: J. Rohacs, Rea-Tech Ltd., Hungary DEVELOPING THE MAGLEV ASSISTED AIRCRAFT TAKE-OFF AND LANDING (GABRIEL CONCEPT) |
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ICAS2014_0979: J. Mercer, San Jose State University / NASA Ames Research Center, United States DIFFEREING AIR TRAFFIC CONTROLLER RESPONSES TO SIMILAR TRAJECTORY PREDICTION ERRORS |
9 - Safety and Security |
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ICAS2014_0012: P.M. Politano, The Citadel, United States; R.O. Walton, Embry-Riddle Aeronautical University - Worldwide, Germany GENDER RELATED PERCEPTIONS, STRESS, ANXIETY, DEPRESSION, AND PERSONALITY CHARACTERISTICS: FEMALES ON THE FLIGHT DECK |
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ICAS2014_0041: P. Mayes, UNSW School of Aviation, Australia DEVELOPMENTS IN ACCIDENT PREVENTION |
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ICAS2014_0047: F. Wenchun¹, S. Wenjuan¹; ¹First Aircraft Institute, China USING LINEAR SHAPED CHARGE(LSC) TO FORM BAILOUT EMERGENCY EXIT |
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ICAS2014_0066: L.P. Ruiz-Calavera¹, S. Cid-Arroyo¹, L. Benitez-Montañes¹; ¹Airbus Defense and Space, Spain SPINNER SHED ICE ENGINE INGESTION ASSESSMENT METHODOLOGY |
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ICAS2014_0107: G.T. Andreev¹, V.V. Bogatyrev¹; ¹TsAGI, Russia INVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI |
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ICAS2014_0183: S.Y. Zheltov¹, Y.V. Vizilter¹, O.V. Vygolov¹; ¹State Research Institute of Aviation Systems (FGUP “GosNIIAS”), Russia ENHANCED AND SYNTHETIC VISION SYSTEMS DEVELOPMENT BASED ON INTEGRATED MODULAR AVIONICS |
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ICAS2014_0205: L. Malysheva, Moscow State Technical University of Civil Aviation, Russia EXTREME INFLUENCE OF ENVIRONMENT AND RISKS OF THE FLIGHT SAFETY DEGRADATION DUE TO THE CHANGE OF THE A/C T/O-AND-L PERF |
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ICAS2014_0235: G. Lu, Chengdu Aircraft Design & Research Institute, China THE TRANSFORM PRINCIPLE AND MODEL FOR AIRCRAFT MTTR IN THREE-DIMENSIONAL DIGITAL DESIGN CONDITION |
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ICAS2014_0241: A. Prato¹, M. Anghileri¹, A. Milanese¹, L.M.L. Castelletti¹; ¹Politecnico di Milano, Italy FE-TO-SPH APPROACH APPLIED TO THE ANALYSIS OF SOFT BODY IMPACT: BIRD STRIKE AND HAIL IMPACT |
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ICAS2014_0305: D.-Y. Wang¹, Y.-L. Fu¹, X.-Y. Qi¹; ¹Beihang University, China RESEARCH ON A PROGNOSTIC AND HEALTH MONITORING APPROACH FOR EMAS IN THE FLIGHT CONTROL SYSTEM |
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ICAS2014_0318: D.A. Aggromito¹, R. Thomson, CRC-ACS, Australia; J. Wang, DSTO, Australia; B. Chen¹, W. Yan¹; ¹Monash University, Australia USING A BIODYNAMIC MODEL TO INVESTIGATE THE EFFECTS OF BODY-BORNE EQUIPMENT ON FORCES EXPERIENCED IN A SIMULATED HELICOPTER CRASH |
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ICAS2014_0414: M. Guillaume, Zurich University of Applied Sciences, Switzerland STRUCTURAL INTEGRITY FOR AGING AIRPLANES |
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ICAS2014_0419: S.S. Silva¹, H. Cho¹, R.J. Hansman¹; ¹MIT, United States HUMAN FACTORS STUDIES OF AN ADS-B BASED TRAFFIC ALERTING SYSTEM FOR GENERAL AVIATION |
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ICAS2014_0480: A. Yoshida¹, W. Ebina¹, T. Okawa¹; ¹Tokyo Denki University, Japan SUPPRESSION EFFECTIVENESS OF WATER MIST ON ACCIDENTAL AIRCRAFT FIRES |
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ICAS2014_0688: A.D. Mironov¹, A.Y. Nakvasin¹; ¹GROMOV FLIGHT RESEARCH INSTITUTE (LII GROMOV), Russia DEVELOPMENT AND FLIGHT RESEARCH OF NON-INTRUSIVE AIRBORNE SYSTEM OF PILOT PSYCHOPHYSIOLOGICAL STATUS MONITORING |
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ICAS2014_0723: H. Tsuda¹, K. Funabiki¹, H. Shirouzu¹, K. Tawada, Shimadzu co., Japan; T. Toshida, NEC co., Japan; ¹JAXA, Japan FLIGHT TESTS OF SYNTHETIC TERRAIN AND FLIR IMAGES ON HELMET-MOUNTED DISPLAY |
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ICAS2014_0758: C. Wang¹, L. Drees¹, F. Holzapfel¹; ¹Technische Universität München - Inst. of Flight System Dynamics, Germany INCIDENT PREDICTION USING SUBSET SIMULATION |
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ICAS2014_0813: J.O. Entzinger¹, T. Uemura¹, S. Suzuki¹; ¹The University of Tokyo, Japan MENTAL EFFORT AND SAFETY IN CURVED APPROACHES |
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ICAS2014_0833: C.M. Muehlethaler¹, C.P. Knecht¹; ¹Centre for Aviation, Zurich University of Applied Sciences, Switzerland NOTES TRAINING IN ATM – A NEW APPROACH USING COMPUTER-BASED SIMULATION METHODS: RESEARCH METHODS |
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ICAS2014_0882: T. Levora¹, O. Bruna¹, P. Paces¹; ¹Czech Technical University in Prague, Czech Republic PATH PLANNING FOR ULTRALIGHTS UNDER EMERGENCY CONDITIONS |
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ICAS2014_0885: T. Levora¹, O. Bruna¹, P. Paces¹; ¹Czech Technical University in Prague, Czech Republic EMERGENCY LANDING SITE LOCATION USING AERIAL IMAGE SEGMENTATION |
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ICAS2014_0892: J. Yang¹, D. Yin¹, H. Xie¹; ¹National University of Defense Technology, China A REINFORCEMENT LEARNING BASED UAVS AIR COLLISION AVOIDANCE |
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ICAS2014_0925: E. Norde¹, J.M. Hospers¹, E. van der Weide¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands AIRCRAFT ICING IN FLIGHT: EFFECTS OF IMPACT OF SUPERCOOLED LARGE DROPLETS |
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ICAS2014_0949: A. De Marco¹, J. D\'Auria¹; ¹University of Naples Federico II, Italy COLLISION RISK STUDIES WITH 6DOF FLIGHT SIMULATIONS WHEN AERODROME OBSTACLE STANDARDS CANNOT BE MET |
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ICAS2014_0965: K. Funabiki¹, H. Tsuda¹, G. Tsuchiya¹; ¹JAXA, Japan SAFETY ASPECT OF MISSION SUPPORT DISPLAY FOR HIGH-DEMAN DAERIAL WORK |
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ICAS2014_0973: I. Jankovics, Budapest University of Technology and Economics, Hungary SUBJECTIVE FACTORS IN CONTROLLERS' DECISIONS |
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ICAS2014_0999: A.G. Kuznetsov¹, L.N. Aleksandrovskaya¹, V.N. Masur¹; ¹JSC Moscow Institute of Electromechanics & Automatics, Russia METHOD OF REQUIREMENTS CONFIRMATION TO AIRCRAFT AUTOMATIC LANDING SAFETY AT MATHEMATICS SIMULATION STAGE |
10 - Challenge of the Environment |
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ICAS2014_0031: H.M.J Kuijpers, TU Delft , Netherlands; H.G. Visser, TU Delft, Netherlands NOISE ABATEMENT PATH PLANNING USING VIRTUAL FORCES |
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ICAS2014_0034: A. Waitschat¹, V. Pommier-Budinger, Institut Supérieur de l\'Aéronautique et de l\'Espace , France; F. Thielecke¹; ¹Hamburg University of Technology, Germany HYDRAULIC SYSTEM NOISE REDUCTION BY A COMBINED CONSIDERATION OF FLUID BORNE NOISE AND STRUCTURE BORNE NOISE |
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ICAS2014_0149: A.M. Savel’ev¹, V.A. Skibin¹, A.M. Starik¹; ¹Central Institute of Aviation Motors, Russia EVALUATION OF EMISSION CHARACTERISTICS OF GAS TURBINE ENGINES USING ALTERNATIVE FUELS |
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ICAS2014_0150: V.E. Kozlov¹, A.M. Starik¹, N.S. Titova¹; ¹Central Institute of Aviation Motors, Russia MODELING STUDY OF POLLUTANT FORMATION IN HOMOGENEOUS METHANE AND SYNGAS FUELED COMBUSTOR |
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ICAS2014_0158: A.A. Okhapkin, Central Aerohydrodynamic Institute, Russia PERFORMANCE ASSESSMENT OF ALTERNATIVE FUELS AT THE AIR TRANSPORTATION SYSTEM LEVEL |
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ICAS2014_0315: V.N. Zhuravlev, Moscow Aviation Institute, Russia COMPARATIVE ANALYSIS OF RUSSIAN AND WESTERN APPROACHES TO THE PROBLEM OF ALTERNATIVE FUEL USAGE IN AVIATION |
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ICAS2014_0338: G. Serafino, Università degli studi di trieste; Selex ES, Italy MULTI-OBJECTIVE TRAJECTORY OPTIMIZATION TO REDUCE AIRCRAFT EMISSIONS IN CASE OF UNFORESEEN WEATHER EVENTS |
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ICAS2014_0356: M. Richter¹, M. Bittner¹, M. Rieck¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TUM, Germany A NON-COOPERATIVE BI-LEVEL OPTIMAL CONTROL PROBLEM FORMULATION FOR NOISE MINIMAL DEPARTURE TRAJECTORIES |
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ICAS2014_0400: 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 ECOLOGICAL OPTIMIZATION OF JET AIRCRAFT FLIGHTS IN VIEW OF CONTRAILS AND CONTRAIL CIRRUS FORMATION |
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ICAS2014_0558: K.V. Pushkin, Moscow Aviation Institute (National Research University), MAI, Russia CONTROLLED HYDROGEN GENERATOR AND ADDITIONAL SOURCE OF ELECTRICAL CURRENT FOR INDEPENDENT OXYGEN-HYDROGEN POWER PLANTS |
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ICAS2014_0581: Z. Ilic¹, B. Rasuo, University of Belgrade, Faculty of Mechanical Engineering, Serbia; M. Jovanovic¹, S. Jovicic¹; ¹Technical Test Center , Serbia IMPACT OF IRREGULARITIES IN THE PISTON ENGINE OPERATION ON THE INFLIGHT VIBRATION LEVEL |
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ICAS2014_0584: A. Johanning¹, D. Scholz¹; ¹Hamburg University of Applied Sciences, Germany CONCEPTUAL AIRCRAFT DESIGN BASED ON LIFE CYCLE ASSESSMENT |
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ICAS2014_0704: M. Micallef¹, K. Chircop¹, D. Zammit-Mangion¹, A. Sammut¹, M. Xuereb¹, A. Muscat, Qu Aero Ltd., Malta; ¹University of Malta, Malta A QUASI-REAL-TIME GROUND-BASED TRAJECTORY OPTIMIZATION TOOL FOR GREENER OPERATIONS |
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ICAS2014_0917: M.A. Lobanova, Baltic State Technical University, Russia A STUDY OF FLOW AND INITIAL STAGE OF WATER CONDENSATION IN THE TWO-PHASE JET-VORTEX WAKE BEHIND A CRUISE AIRCRAFT |
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ICAS2014_0958: W.A. Chishty, National Research Council Canada, Canada PERFORMANCE AND EMISSIONS CHARACTERISTICS OF ALTERNATIVE AVIATION FUELS |
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ICAS2014_0988: C. Legendre, Free Field Technologies, Belgium; L.M.B.C. Campos, Instituto Superior Tecnico, Portugal ON SOUND ABSORPTION BY AN ACOUSTIC LINER WITH BIAS FLOW |
11 - Operations and Sustainment |
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ICAS2014_0063: A.N. Petrov, Gromov Flight Research Institute, Russia DEVELOPMENT OF INSTRUCTIONS FOR CONTINUING AIRWORTHINESS AND AIRCRAFT LOGISTIC SUPPORT ANALYSIS |
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ICAS2014_0071: C. Bil¹, R. Hadgraft¹, P. Ruamtham¹; ¹RMIT University, Australia AEROSPACE ENGINEERING: INVESTIGATING STUDENT PERCEPTIONS AND INDUSTRY REALITIES |
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ICAS2014_0179: A.Z. Bagerman¹, I.P. Leonova¹, A.V. Konopatova¹; ¹Krylov State Research Centre, Russia PLANNING OF AN EXPENDITURE OF THE RESOURSE OF GAS TURBINE ENGINE IN OPERATION |
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ICAS2014_0185: E. Yoshikawa¹, N. Matayoshi¹; ¹JAXA, Japan WAKE VORTEX OBSERVATION CAMPAIGN BY ULTRA FAST-SCANNING LIDAR IN NARITA AIRPORT, JAPAN |
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ICAS2014_0186: E. Yoshikawa¹, N. Matayoshi¹; ¹JAXA, Japan DETECTION AND ESTIMATION OF WAKE VORTEX ON ULTRA FAST-SCANNING PULSED-DOPPLER LIDAR |
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ICAS2014_0240: A.A. Fedotov, Moscow Aviation Institute (National Research University), Russia MODELING AND OPTIMIZING OF BONDED PATCH REPAIRS FOR POLYMER COMPOSITE STRUCTURES |
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ICAS2014_0381: A.M. Kachalin, Moscow Aviation Institute, Russia TRAINING OF THE FLIGHT STAFF ON FLIGHT SIMULATORS USING VIDEO CONFERENCE SYSTEMS |
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ICAS2014_0382: A.M. Kachalin, Moscow Aviation Institute, Russia INNOVATIVE TECHNOLOGIES AND VIDEO CONFERENCE SYSTEMS IN TECHNOLOGICAL PROCESS OF AIRCRAFT ENGINE PRODUCTION |
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ICAS2014_0411: Y. Buryak¹, S. Zheltov¹; ¹State Institute of Aviation Systems, Russia SECURING THE SUPPLY CHAIN OF INDUSTRIAL PRODUCTS ON THE BASIS OF THE USE OF MODERN INFORMATION TECHNOLOGIES |
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ICAS2014_0543: B. Rasuo¹, G. Djuknic¹; ¹University of Belgrade, Serbia IMPROVEMENT OF THE AIRCRAFT GENERAL OVERHAUL PROCEDURE |
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ICAS2014_0550: X. Chen¹, H. Ren¹, C. Bil¹; ¹RMIT, Australia THE INFLUENCE OF SHM TECHNIQUES ON SCHEDULED MAINTENANCE OF AIRCRAFT COMPOSITE STRUCTURES |
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ICAS2014_0593: M. Schmidt¹, K.O. Plötner¹, A. Seitz¹, A.T. Isikveren¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany PROFIT-BASED NETWORK LEVEL EVALUATION OF AIRCRAFT BLOCK TIMES |
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ICAS2014_0639: N. Matayoshi, JAXA, Japan DYNAMIC WAKE VORTEX SEPARATION COMBINING WITH TRAFFIC OPTIMIZATION |
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ICAS2014_0710: N. Matayoshi¹, T. Iijima¹, E. Yoshikawa¹, T. Ushio, Osaka University, Japan; ¹JAXA, Japan DEVELOPMENT OF LOW-LEVEL TURBULENCE ADVISORY SYSTEM FOR AIRCRAFT OPERATION |
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ICAS2014_0733: S. Chiesa¹, M. Fioriti¹, R. Fusaro¹; ¹Politecnico di Torino, Italy UAV BASED ADVANCED MONITORING SYSTEM: FLEET AND LOGISTIC SYSTEM SIZING BY OBJECT-BASED MODEL AND MONTE-CARLO SIMULATION |
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ICAS2014_0736: E. Fouladi¹, N. Shadaab¹, A. Abedian¹, A.K. Tanara, Graduate School of Management and Economics, Sharif University, Iran; ¹Department of Aerospace Engineering, Sharif University, Iran AGING AIRCRAFT COST ANALYSIS USING SYSTEM DYNAMICS MODELING |
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ICAS2014_0841: I.V. Borisov, Southern Federal University, Taganrog Institute of Technology, Russia; A.V. Tsipenko, Moscow Aviation Institute, Russia COMPUTING SIMULATION FOR FIRE-FIGHTING HELICOPTER OPERATION ANALYSIS |
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ICAS2014_1022: F. Quagliotti, Politecnico di Torino, Italy DOCTORAL PROGRAMS AND TRAINING: EUROPEAN PERSPECTIVES |
12 - Host nation |
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ICAS2014_1030: S.K. Godunov, Institute of Mathematics, Siberian Department of Russian Academ, Russia FINIT DIFFERENCE MODELS FOR MECHANICS OF CONTINIUA, PROBLEM OF ACCURACY AND DOMAIN OF APPLICABILITY |
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ICAS2014_1031: G.N. Barakos¹, R. Steijl¹, M. Woodgate¹; ¹School of Engineering - The University of Liverpool, United Kingdom CFD FOR ROTORCRAFT – RECENT PROGRESS AND NEW CHALLENGES WITH THE GOAHEAD CASE |
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ICAS2014_1032: A.I. Tolstykh, Dorodnicyn Computing Center of Russian Academy of Sciences, Russia EXTREMELY HIGH ORDER AND HIGH RESOLUTION MULTIOPERATORS – BASED SCHEMES FOR CFD APPLICATIONS |
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ICAS2014_1033: I.I. Lipatov¹, R.J. Tugazakov¹, F.T. Vihn¹; ¹TsAGI, Russia SHOCK WAVE BOUNDARY LAYER INTERACTION PROCESSES. BUFFET CONTROL METHODS |
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ICAS2014_1034: 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 PROTECTION PROBLEM FOR THIN-WALLED COMPOSITE CONSTRUCTIONS OF AIRCRAFT FROM ACTION OF RADIATIONS AND PARTICLES FLUXES |
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ICAS2014_1035: D.A. Sobolev, Institute for the History of Science and Technology, Russia THE CONTRIBUTION OF DIFFERENT COUNTRIES TO AIRPLANE DEVELOPMENT AND MANUFACTURE- PART I. INVENTION OF AIRPLANE |
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ICAS2014_1036: Y.V. Kuzmin, Institute for the History of Science and Technology, Russia THE CONTRIBUTION OF DIFFERENT COUNTRIES TO AIRPLANE DEVELOPMENT AND MANUFACTURE - PART II. HOW MANY AIRPLANES WERE THERE? |
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ICAS2014_1037: V.V. Lebedev, Institute for History for Science and Technology, Russia FIRST AIRFIELDS OF SAINT PETERSBURG - FIRST AIRFIELDS OF RUSSIA |
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ICAS2014_1038: R. Burger, EC, France PRESENTATION OF HORIZON 2020 PROGRAMME |
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ICAS2014_1039: J. Kaspar, EREA, Czech Republic EREA AND FUTURE SKY |
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ICAS2014_1040: M. Fischer, Airbus, Germany OVERVIEW AND RESULTS OF FP7 PROJECT AFLONEXT |
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ICAS2014_1041: F.R. van der Linden, Smithsonian National Air and Space Museum, United States CREATING THE MODERN AIRLINER: U.S. GOVERNMENT AND BUSINESS, 1918-2014 |
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ICAS2014_1042: G. Bridel, Switzerland FROM ST. PETERSBURG TO ZURICH: AERONAUTICAL AND SCIENTIFIC MILESTONES FROM SWISS PERSPECTIVES AROUND THE NAMES BERNOULLI |
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ICAS2014_1043: M. Kanevsky, Russia WAKE VORTEX FLIGHT SAFETY SYSTEM: CURRENT STATUS AN PERSPECTIVES |