ACCEPTED PAPERS - CATEGORY B – STANDBY / POSTERThese papers are standby for oral presentations in case papers are withdrawn from an appropriate session. |
ICAS2014-ST: A. Yaremenko, MAI, Russia NUMERICAL RESEARCH OF MUTUAL INFLUENCE OF X-43A AIRFRAME AND SCRAMJET IN MANEUVERING |
ICAS2014-ST: J. Rumi, Military Institute of Science and Technology, Bangladesh CEASIOM: AN OPEN SOURCE MULTI MODULE CONCEPTUAL AIRCRAFT DESIGN TOOL |
ICAS2014-ST: L. Mo, Delft University of Technology, Netherlands CONCEPTUAL TANKER DESIGN FOR CIVIL OPERATIONS |
ICAS2014-ST: J. Rumi, Military Institute of Science and Technology, Bangladesh DESIGN AND ANALYSIS OF ULTRA-LIGHT WEIGHTED STOL AIRCRAFT |
1 - Aircraft and Systems Integration |
ICAS2014-1.9ST: 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 |
ICAS2014-1.7ST: F Coll, Airbus Military, Spain A400M DASS SYSTEM TEST FLARES TRAJECTORY CALCULATION |
2.1 - Aerodynamics - CFD Methods and Validation |
ICAS2014-2.11ST: R.Z. Nigmatullin, CIAM , Russia; L.V. Terentyeva , CIAM, Russia ANALYSIS OF TONAL NOISE OF LPT BASED ON UNSTEADY GAS FLOW CALCULATIONS |
ICAS2014-11.5ST: S. Alexandrov, TsAGI, Russia VISCOUS HYPERSONIC GAS FLOW CHARACTERISTICS OVER THE DELTA WING WITH BLUNT LEADING EDGES |
ICAS2014-11.5ST: E.J. Fahy, The University of Queensland, Australia LABORATORY AND FLIGHT COMPARISONS OF HAYABUSA WITH ABLATION AND RADIATION EFFECTS |
ICAS2014-2.3ST: 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 |
ICAS2014-2.10ST: L.-J. li, Northwestern Polytechnical University, China NUMERICAL INVESTIGATION OF FLUID FLOW BASED ON ZONAL IDDES METHOD |
ICAS2014-2.3ST: D.S. Ivanyushkin¹, S.A. Takovitskii¹; ¹TsAGI, Russia NOSES OF MINIMAL WAVE DRAG IN SUPERSONIC FLOW |
ICAS2014-2.5ST: 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 |
2.2 - Experimental Aerodynamics |
ICAS2014-3.1ST: 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 |
ICAS2014-3.4ST: 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 |
ICAS2014-3.7ST: 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 |
ICAS2014-3.1ST: G.G. Gadzhimagomedov¹, V.A. Vlasov¹, V.M. Lutovinov¹; ¹Central Aerohydrodynamic Institute, Russia EXAMPLES OF PIV APPLICATIONS TO SUBSONIC FLOWS |
ICAS2014-3.4ST: F.P. Moraleda, UPM, Spain; F.M. Catalano, EESC-USP, Brazil EXPERIMENTAL ANALYSIS OF THE AERODYNAMICS OF POROUS FLAP SIDE-EDGE |
ICAS2014-ST: 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 |
2.3 - Basic Fluid Dynamics and Flow Control |
ICAS2014-3.2ST: 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 |
ICAS2014-5.3ST: L Öster, Saab Aerosystems, Sweden A CFD BENCHMARK STUDY OF FLOW SEPARATION CONTROL WITH PULSATILE JETS ON A HIGH-LIFT AIRFOIL |
ICAS2014-5.3ST: 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 |
2.4 - Applied Aerodynamics |
ICAS2014-4.9ST: C. Breitsamter¹, M. Grawunder¹, R. Reß¹; ¹Technische Universität München, Germany AERODYNAMIC DESIGN OPTIMISATION FOR A HELICOPTER CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
ICAS2014-10.7ST: D.V. Kalinin, CIAM after P.I. Baranova, Russia MULTITHREADED CONTINUOUSLY VARIABLE TRANSMISSION SYNTHESIS FOR NEXT-GENERATION HELICOPTERS |
ICAS2014-4.6ST: M.F. Figat¹, A. Kwiek¹, K. Senenko¹; ¹Warsaw University of Technology, Poland AERODYNAMIC DESIGN OF THE STRAKE FOR THE ROCKET PLANE IN TAILLESS CONFIGURATION. |
3.1 - Materials issues, Fatigue and Damage Tolerance |
ICAS2014-ST: I. AHMADI, University of Zanjan, Iran ANALYSIS OF INTER-LAMINAR STRESSES IN COMPOSITE THIN SHELL |
ICAS2014-5.8ST: T. Uhl¹, M. Szwedo, MONIT SHM, Poland; P. Hellstein¹, L. Pieczonka¹; ¹AGH University, Poland IMAGE-BASED STRUCTURAL HEALTH MONITORING OF COMPOSITE STRUCTURES |
ICAS2014-5.8ST: S Denisov, Moscow Aviation Institute, Russia INFLUENCE OF THE ACOUSTIC FIELD SPATIAL STRUCTURE ON THE RESPONSE AND DURABILITY OF THE METAL ISOTROPIC PLATE |
ICAS2014-5.4ST: T. Mileiko, Institute of Solid State Physics of RAS, Russia A NOVEL COMPOSITE MATERIAL FOR TURBINE BLADES |
ICAS2014-5.7ST: 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 |
3.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity |
ICAS2014-6.6ST: 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 |
ICAS2014-6.1ST: R.V. Leonteva, PSC Tupolev, Russia PROCEDURE OF GROUND VIBRATION EXPERIMENTS ON AIRCRAFT WITH SIMULATING FORCES DUE TO ENGINE IMBALANCE AT BLADE LOSS |
4 - Propulsion |
ICAS2014-12.4ST: J. Temis¹, A. Selivanov¹, I. Dzeva¹; ¹Central Institute of Aviation Motors, Russia FLUID-STRUCTURAL ANALYSIS OF A NON-CONTACTING FINGER SEAL |
5.1 - Flight Dynamics and Control (Control & Modelling) |
ICAS2014-8.7ST: 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 |
ICAS2014-8.11ST: 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 |
5.2 - Flight Dynamics and Control (UAV related) |
ICAS2014-9.8ST: H. Hiraguri¹, H. Tokutake¹; ¹Kanazawa University, Japan MODELING OF DUST DEVIL ON MARS AND FLIGHT SIMULATION OF MARS AIRPLANE |
ICAS2014-9.11ST: 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 |
6 - Systems, Subsystems and Equipment |
ICAS2014-10.3ST: V. Bukov, LSC Institute of Aircraft Equipment, Russia A DEMONSTRATOR FOR AVIONICS OF ZERO MAITENANCE EQUIPMENT |
ICAS2014-10.3ST: 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 |
ICAS2014-9.10ST: 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 |
8 - Air Transport System Efficiency |
ICAS2014-11.8ST: J. Rohacs, Rea-Tech Ltd., Hungary DEVELOPING THE MAGLEV ASSISTED AIRCRAFT TAKE-OFF AND LANDING (GABRIEL CONCEPT) |
ICAS2014-11.4ST: K. Zudov¹, V. Vyshinsky¹, M. Kudrov¹; ¹Moscow Institute of Physics and Technology, Russia ON THE FLIGHT OPERATING SAFETY IN THE MOUNTAINOUS ZONE AIRPORT |
9 - Safety and Security |
ICAS2014-ST: P. Mayes, UNSW School of Aviation, Australia DEVELOPMENTS IN ACCIDENT PREVENTION |
ICAS2014-10.10ST: J. Yang¹, D. Yin¹, H. Xie¹; ¹National University of Defense Technology, China A REINFORCEMENT LEARNING BASED UAVS AIR COLLISION AVOIDANCE |
ICAS2014-10.10ST: M. Guillaume, Zurich University of Applied Sciences, Switzerland STRUCTURAL INTEGRITY FOR AGING AIRPLANES |
11 - Operations and Sustainment |
ICAS2014-8.2ST: E. Yoshikawa¹, N. Matayoshi¹; ¹JAXA, Japan DETECTION AND ESTIMATION OF WAKE VORTEX ON ULTRA FAST-SCANNING PULSED-DOPPLER LIDAR |
ICAS2014-5.11ST: A.M. Kachalin, Moscow Aviation Institute, Russia TRAINING OF THE FLIGHT STAFF ON FLIGHT SIMULATORS USING VIDEO CONFERENCE SYSTEMS |
ICAS2014-5.9ST: 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 |