ACCEPTED PAPERS - CATEGORY B These papers are standby for oral presentation in case papers are withdrawn from an appropriate session. Full papers appear in the congress CD-Rom proceedings where these are available
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1. Integration and Multidisciplinary Matters |
ICAS 2002-R16 J. P. Fielding, H. Smith: Cranfield University, UK DEVELOPMENT OF ENVIRONMENTALLY-FRIENDLY TECHNOLOGIES AND CONFIGURATIONS FOR SUBSONIC JET TRANSPORTS |
ICAS 2002-R35 M. T. Lee, W-Y. Chang, C-C. Yang, K-W. Lin, Y-F. Tsai, C-R. Wu, F-B. Hsiao: National Cheng Kung University, Taiwan |
ICAS 2002-R41 T. Richter, H. Mechler, D. Schmitt: TU Munich, Germany |
ICAS 2002-R49 H. M. Pasaribu, B. Wijanarko: Institute of Technology Bandung, Indonesia |
ICAS 2002-R50 A. Pistek: Brno University of Technology, Czech Republic DEVELOPMENT OF A NEW GENERATION OF AIRCRAFT FOR PILOT TRAINING |
ICAS 2002-R70 Z. M. Zain: Mara University of Technology, Malaisia |
ICAS 2002-R74 G. Renaud, G. Shi: IAR/NRC, Canada EVALUATION AND IMPLEMENTATION OF MULTIDISCIPLINARY DESIGN OPTIMIZATION STRATEGIES |
ICAS 2002-R76 H. A. P. Blom, S. H. Stroeve, M. H. C. Everdij, M. N. J. van der Park: National Aerospace Laboratory, Amsterdam, the Netherlands HUMAN COGNITION PERFORMANCE MODEL BASED EVALUATION OF SAFE SPACING IN AIR TRAFFIC |
2. Aerodynamics |
ICAS 2002-R1 H. Acar: Istanbul Technical University, Turkey THE EFFECT OF THE ANGLE OF THE INCLINED FLAT PLATE ON THE DEFLEXION OF A PLANE WALL JET |
ICAS 2002-R15 D. Erdem (1), V. Ath (2): (1) Istanbul Technical University, Turkey; (2) Civil Aviation School, Kayseri, Turkey |
ICAS 2002-R17 J. M. Floryan (1), S. K. Nikumb (2): (1) University of Western Ontario, Canada; (2) National Research Council of Canada, Canada |
ICAS 2002-R20 D. I. Greenwell: QinetiQ plc, UK AN ENGINEERING MODEL OF DELTA WING VORTEX BREAKDOWN |
ICAS 2002-R21 E. Hansen: Bombardier Aerospace, Canada FAST AND ACCURATE SURFACE AND GRID CREATION ON A COMPLETE AIRCRAFT FOR A CARTESIAN GRID BASED EULER SOLVER |
ICAS 2002-R23 H. Hamdani, M. Nauman, K. Parvez: National University of Sciences & Technology, Pakistan SEPARATION CONTROL BY ALTERNATING TANGENTIAL BLOWING/SUCTION AT MULTIPLE SLOTS |
ICAS 2002-R24 F. B. Hsiao (1), C-Z. Cheng (1), W-J. Liu (1), C-C. Hsu (2): (1) National Cheng Kung University, Taiwan; (2) Air Force Aeronautic Technique School, Kaohsiung, Taiwan |
ICAS 2002-R25 X. Huang: IAR/NRC, Canada CENTRE-BODY AND LEADING-EDGE BEVEL EFFECTS ON DELTA WING AERODYNAMICS AT HIGH INCIDENCE |
ICAS 2002-R29 E. Tarhan (1), E. Oktay (1), M. S. Kavsaoglu (2): (1) ROKETSAN, Missile Industries, Inc., 06780 Ankara Turkey; (2) Middle East Technical University, Turkey SOLUTION OF AIRFOIL-FLAP CONFIGURATIONS BY USING CHIMERA GRID SYSTEM |
ICAS 2002-R3 C. B. Allen: University of Bristol, UK AN UNSTEADY FLOW-SOLVER WITH ALGEBRAIC GRID MOTION FOR AEROELASTIC SIMULATIONS |
ICAS 2002-R30 M. S. Kavsaoglu, G. Durmus: , MULTI BLOCK NAVIER STOKES SOLUTIONS OF LOW ASPECT RATIO RECTANGULAR FLAT WINGS IN COMPRESSIBLE FLOW |
ICAS 2002-R33 K. H. Kim (2), C. Kim (1), O. Rho (1), K. Lee (2): (1) Seoul National University, 151-742, Seoul, Korea; (2) Sejong-Lockheed Martin Aerospace Research Center, Korea THE STUDY OF MONOTONICITY OF AUSM-TYPE SCHEMES IN SHOCK DISCONTINUITIES |
ICAS 2002-R38 L. Haiye: Turin Polytechnic University, Italy A SIMPLE AND NONLINEAR AERODYNAMIC MODELING FOR DELTA WITH WITH LEV BREAKDOWN INVOLVED |
ICAS 2002-R39 E. Ly, J. Nakamichi: NAL, Japan TIME-LINEARISED TRANSONIC SMALL DISTURBANCE CODE INCLUDING ENTROPY AND VORTICITY EFFECTS |
ICAS 2002-R40 R. Marsilio, D. Grillo: Turin Polytechnic University, Italy IMPLEMENTATION AND VALIDATION OF THE SPALART-ALLMARAS TURBULENCE MODEL FOR HIGH SPEED FLOWS |
ICAS 2002-R43 J. J. Miau: National Cheng Kung University, Taiwan NORMAL AND SIDE FORCES AMPLIFICATION BY LATERAL JET ISSUED FROM AN OGIVE CYLINDER |
ICAS 2002-R44 M. A. Moelyadi: Institute of Technology Bandung, Indonesia |
ICAS 2002-R46 R. K. Nangia (1), M. E. Palmer (1), C. P. Tilmann (2): (1) Nangia Aero Research Associates, UK; (2) Wright-Patterson AFB, OHIO, USA ON DESIGN OF UNCONVENTIONAL HIGH ASPECT RATIO "JOINED-WING" TYPE AIRCRAFT |
ICAS 2002-R48 T. Xu (1), X. -C. Cal (2), M. Paraschivoiu (1): (1) University of Toronto, Canada; (2) University of Colorado, Boulder, USA ILU PRECONDITIONED MULTI-MODEL FORMULATION FOR COMPRESSIBLE FLOWS ON 3D UNSTRUCTURED MESHES |
ICAS 2002-R5 A. Bengin: Faculty of Mechanical Engineering, Yugoslavia AN ALGORITHM FOR THE CALCULATION OF AERODYNAMIC WING-PROPELLER INTERACTION |
ICAS 2002-R52 P. Edi: Indonesian Aerospace, Indonesia |
ICAS 2002-R53 Z. Qiao, A. M. Yang, B. Zhu: Northwestern Polytechnical University, PRC |
ICAS 2002-R59 W. Sang, F. Li, E. Qin: Northwestern Polytechnical University, PRC NUMERICAL SIMULATION OF THE STORE SEPARATION USING UNSTRUCTURED CARTESIAN GRID |
ICAS 2002-R6 E. Berton, D. Favier, C. Maresca, M. Nsi Mba: CNRS/ University of Méditerranée, France CENTRIFUGAL AND 3D EFFECTS ON THE NEAR TIP SECTION OF ROTATING BLADE |
ICAS 2002-R60 S. Sankaran (1), R. M. Rajeswara (1), T. N. V. Satyanarayana (1), N. Satyanarayana (1), K. Visvanathan (1), R. B. Kotapati (2): (1) ISRO, Sriharikota, India; (2) Arizona State University, USA |
ICAS 2002-R68 S. Yarusevych (1), J. G. Kawall (2), P. Sullivan (1): (1) University of Toronto, Canada; (2) Ryerson University INFLUENCE OF ACOUSTIC EXCITATION ON AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBERS |
ICAS 2002-R69 Y. Qian (1), H. Sobieczky (2): (1) Beijing University of Aeronautics and Astronautics, PRC; (2) DLR German Aerospace Research Center, Göttingen, Germany WAVERIDER DESIGN WITH PARAMETRIC FLOW QUALITY CONTROL BY INVERSE METHOD OF CHARACTERISTICS |
ICAS 2002-R7 E. D. V. Bigarelli, J. L. F. Azevedo: CTA/ITA, Brazil |
ICAS 2002-R79 J. Yin, P. Pilidis: Cranfield University, UK INFLUENCE OF INLET PROFILE ON HIGH-BPRTURBOFAN PERFORMANCE USING A RADIALPROFILE MAP |
3. Materials and Structures |
ICAS 2002-R10 D. H. Chester: Israel Aircraft Industries Ltd., Israel PRE-STRESSED SYMMETRIC COMPOSITE BEAMS IN AIRCRAFT - ANALYSIS AND DESIGN IMPLICATIONS |
ICAS 2002-R11 D. Cui (1), Z. Li (1), Y. Xiu (1), J. He (2): (1) Beijing University of Aeronautics & Astronautics, PRC; PRC Aviation Industry Corp., PRC; (2) China Aero Information Center, Beijing, PRC |
ICAS 2002-R14 A. Dabayeh: IMP Group Ltd, Canada EXTENSION OF REPAIR LIFETIME FOR THE CP140 BY COLD WORKING OF FATIGUED HOLES |
ICAS 2002-R18 J. Shah, A. Gibson, M. Price: Queen’s University of Belfast, Belfast, UK |
ICAS 2002-R2 F. F. Afagh: Carleton University, Canada INTEGRATED ACTIVE FIBRES IN VIBRATION CONTROL OF HELICOPTER BLADES |
ICAS 2002-R32 Z. M. Khan: National University of Sciences and Technology, Pakistan |
ICAS 2002-R34 J. Laliberte (1), C. Poon (1), P. V. Straznicky (2): (1) National Research Council, Canada; (2) Carleton University, Canada NUMERICAL MODELLING OF LOW-VELOCITY IMPACT DAMAGE IN FIBRE-METAL-LAMINATES |
ICAS 2002-R36 T. M. Lee: RMIT University, Australia SIGNAL SUBSPACE IDENTIFICATION & NOISE REDUCTION OF FLIGHT TEST DATA WITH TRUNCATED SINGULAR VALUE DECOMPOSITION |
ICAS 2002-R42 I. R. Memon (1), X. Zhang (2), D. Cui (2): (1) National University of Science and Technology, Pakistan; (2) Beijing University of Aeronautics and Astronautics, Beijing, PRC FATIGUE LIFE PREDICTION OF 3-D PROBLEMS BY DAMAGE MECHANICS WITH SPECTRUM LOADING |
ICAS 2002-R47 C. P. Pagwiwoko: University of Science Malaysia, other DYNAMIC MODELING AND TIME DOMAIN SIMULATION OF NON-LINEAR FLUTTER WITH THE EXISTENCE OF FREE-PLAY MECHANISM |
ICAS 2002-R54 B. Rasuo: University of Belgrade, Yugoslavia |
ICAS 2002-R61 C. D. Mcmahon, M. L. Scott: RMIT University, Australia INNOVATIVE TECHNIQUES FOR THE FINITE ELEMENT ANALYSIS AND OPTIMISATION OF COMPOSITE STRUCTURES |
ICAS 2002-R63 H. Y. Sutarto, A. S. Rianto , S. Zaki, L. Gunawan: Bandung Institute of technology, Indonesia |
ICAS 2002-R65 Y. Yaman (1), T. Caliskan (1), V. Nalbantoglu (2), E. Prasad (3), D. Waechter (3): (1) Middle East Technical University, Turkey; (2) ASELSAN Electronics Industries, Ankara, Turkey; (3) Sensor Technology Limited, Ontario, Canada |
ICAS 2002-R67 X. Wu, M. D. Raizenne, W. R. Chen, C. Poon, W. Wallace: IAR/NRC, Canada |
4. Propulsion |
ICAS 2002-R4 J. Bayandor: RMIT University, Australia PARAMETRIC BASED AERODYNAMIC DESIGN OF PERFORMANCE ENHANCING BLADING SYSTEMS |
ICAS 2002-R57 M. A. Rosen: Ryerson University, Canada EXERGY BASED LOSS ANALYSIS OF A TURBOJET OVER A FLIGHT CYCLE |
ICAS 2002-R64 J. Syms: IAR/NRC, Canada VALIDATION OF ANALYTIC TOOL FOR SUBSCALE PROPELLER TESTS |
5. Flight Dynamics and Control |
ICAS 2002-R12 D. Cvetkovic (1), I. Kostic (1), C. Mitrovic (1), A. Bengin (1), D. Radakovic (2): (1) Faculty of Mechanical Engineering, Yugoslavia; (2) Federal Bureau for Measures and Precious Metals, Belgrade, Yugoslavia |
ICAS 2002-R19 Z. Goraj (1), A. Olejnik (2): (1) Warsaw University of Technology, Poland; (2) Military University of Technology, Warsaw, Poland EXTREME LOADS OF A TRAINER JET FOLLOWING A SUDDEN DEFLECTION OF CONTROL SURFACE |
ICAS 2002-R22 H. Muhammad: Institute of Technology of Bandung, Indonesia AERODYNAMIC MODEL IDENTIFICATION OF THE N-250 AIRCRAFT BASED ON FLIGHT |
ICAS 2002-R26 M. Huzmezan: University of British Columbia, Canada RECONFIGURABLE CONTROL OF AN EXPERIMENTAL UNMANNED AIR VEHICLE (UAV) |
ICAS 2002-R31 S. Khan: Pakistan Air Force, Pakistan |
6. Systems, Subsystems and Equipments |
ICAS 2002-R28 H. Kannemans, H. W. Jentink: NLR, Netherlands A METHOD TO DERIVE THE USAGE OF HYDRAULIC ACTUATORS FROM FLIGHT DATA |
ICAS 2002-R37 H. H. T. Liu, A. De Ruiter: Toronto University, Canada |
ICAS 2002-R45 S. Mondoloni, M. Paglione, S. Green: CSSI Inc., FAA WHJTC, NASA Ames TRAJECTORY MODELING ACCURACY FOR AIR TRAFFIC MANAGEMENT DECISION SUPPORT TOOLS |
ICAS 2002-R55B Rogers: , TORQUE CONTROL SYSTEM BASED ON COMPOUND CONTROL STRATEGIES FOR AERODYNAMIC LOAD SIMULATOR |
ICAS 2002-R71 C. Mitrovic, I. Kosti C, D. Cvetkovi C, A. Bengin: University of Belgrade, Yugoslavia |
ICAS 2002-R73 N. Rao, A. K. Sinha, R. Kusumo: RMIT University, Australia |
ICAS 2002-R75 G. Sachs, U. Sennes: Technische Universität München, Germany |
ICAS 2002-R77 G. Villero, L. Borello: Turin Polytechnic University, Italy PROPOSALS AND COMPARATIVE EVALUATION OF SYNTHETIC NONLINEAR MODELS IN FLIGHT CONTROLS SIMULATION |
ICAS 2002-R78 S. Viswanath, R. Nagarajan: Hindustan Aeronautics Ltd, India |
ICAS 2002-R80 X. Zhu (1), S. Shen (2): (1) Civil Aviation Flight College, PRC; (2) Beijing University of Aeronautical and Astronautical, PRC APPLICATION OF FAULT DIAGNOSIS EXPERT SYSTEM FOR AIRCRAFT ELECTRIC POWER SYSTEM |
7. Design, Development, Manufacturing |
ICAS 2002-R13 : Cvetkovic, Belgrade University, Yugoslavia Algorithm for Automatic Generation of the Technical Documentation of Helicopter Composite Tail Rotor Blades in TIS |
ICAS 2002-R27 S. Kainikara: RMIT University, Australia SYSTEM APPROACH TO IDENTIFY AEROSPACE RESEARCH CAPABILITIES AT UNIVERSITY |
ICAS 2002-R51 A. Pistek: Brno University of Technology, Czech Republic MATRIX FORMULATION OF WING LOADING DISTRIBUTION |
ICAS 2002-R55A Rogers: , PREDICTING CURE KINETICS FOR A NON-ISOTHERMAL CURE PROCESS WITH A CONVENTIONAL ISOTHERMAL DSC TECHNIQUE. |
ICAS 2002-R58 T. B. Ryzhova: Central Aerohydrodynamic Institute (TsAGI), Russian Federation |
ICAS 2002-R62 D. A. Barlow (1), M. L. Scott (2), G. Clayton (1): (1) Hawker de Havilland, Victoria, Australia; (2) RMIT University, Australia CALCULATING THE COST OF A CARBON FIBRE COMPOSITE STRUCTURE FROM WITHIN A FINITE ELEMENT MODEL |
ICAS 2002-R9 S. Boguslavsky (1), A. Cherevatsky (2) , H Dayan (2), M.Shabtai (1), F.Olevsky (1): (1) Israel Military Industries, Israel; (2) Shafir Production Systems, Israel |
8. Aircraft Operations |
ICAS 2002-R66 W. Ti: Chinese Flight Test Establishment, PRC FLIGHT TEST MANAGEMENT AND COMMAND GUIDANCE SYSTEM FOR FLIGHT TEST |
ICAS 2002-R72 M. A. Pogossyan, M. P. Simonov, G. I. Zagainov, A. Z. Tarasov: Sukhoi Aircraft Design Bureau, Russian Federation |
ICAS 2002-R8 L. M. B. C. Campos, J. M. G. Marques: IST, Portugal ON THE CALCULATION OF COLLISION PROBABILITIES AS AN ASSURANCE OF SAFE SEPARATION BETWEEN AIRCRAFT |
ICAS 2002-R22/1 L. Janicek: Institute of Aerospace Engineering, Czech Republic TECHNOLOGICAL TRENDS IN SIMULATION TECHNOLOGY IN AVIATION & PILOT TRAINIG |