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These papers are standby for oral presentation in case papers are withdrawn from an appropriate session.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

 

 

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

THE DEVELOPMENT OF A LOW COST AUTONOMOUS UAV SYSTEM

ICAS 2002-R41 T. Richter, H. Mechler, D. Schmitt: TU Munich, Germany

INTEGRATED PARAMETRIC AIRCRAFT DESIGN

ICAS 2002-R49 H. M. Pasaribu, B. Wijanarko: Institute of Technology Bandung, Indonesia

ANALYSIS OF FLIGHT PERFORMANCE AND STABILITY OF FAMILY OF TRANSPORT AIRPLANE DESIGNS WITH FUSELAGE COMMONALITIES

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

DESIGN ISSUES RELATING TO ULTRALIGHT HELICOPTERS WITH LARGE COMPOUND ROTORS OPERATING IN GROUND EFFECT

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

INTERACTION OF TWO PARALLEL RECTANGULAR JETS

ICAS 2002-R17 J. M. Floryan (1), S. K. Nikumb (2): (1) University of Western Ontario, Canada; (2) National Research Council of Canada, Canada

DESIGN OF SURFACE ROUGHNESS FOR PASSIVE FLOW CONTROL

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

EXPERIMENTAL STUDY OF TURBULENT WAKE FLOW DEVELOPMENT BEHIND A FINITE WING WITH HIGH ANGLE OF ATTACKS

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

IMPROVEMENT OF TRANSONIC AEROFOIL AERODYNAMIC PERFORMANCE

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

THE APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER FLAP AS A FLOW CONTROL ON THE WING FOR REGIONAL AIRCRAFT FAMILY

ICAS 2002-R53 Z. Qiao, A. M. Yang, B. Zhu: Northwestern Polytechnical University, PRC

NUMERICAL SIMULATION OF NAVIER-STOKES EQUATIONS FOR HELICOPTER ROTOR IN FORWARD FLIGHT USING MOVING CHIMERA GRIDS

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

NUMERICAL INVESTIGATION ON THE FLOW CHARACTERISTICS OF A SUPERSONIC JET IMPINGING ON AN AXI-SYMMETRIC DEFLECTOR

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

NORMAL FORCE CALCULATIONS FOR ROCKET-LIKE CONFIGURATIONS

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

BEND/TWIST COUPLING EFFECTS FOR UNSYMMETRICAL & UNBALANCED LAMINATE USED IN AIRCRAFT WING STRUCTURE ANALYSIS

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

AN INVESTIGATION INTO THE EFFECTS OF EXPERIMENTAL ERRORS ON THE CORRELATION BETWEEN FEA AND TEST RESULTS FOR A WELDED FUSELAGE PANEL

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

THE INFLUENCE OF MULTIPLE NESTED LAYER WAVINESS ON COMPRESSION STRENGTH OF CARBON FIBER COMPOSITE MATERIALS

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

AN EXPERIMENTAL METHODOLOGY FOR EVALUATING SURVIVABILITY OF AN AERONAUTICAL CONSTRUCTIONS FROM COMPOSITE MATERIALS

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

ROBUST FLUTTER MARGINS OF A TYPICAL WING SECTION USING WINDTUNNEL EXPERIMENT DATA : A PRELIMINARY STUDY

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

ACTIVE VIBRATION CONTROL OF A SMART PLATE

ICAS 2002-R67 X. Wu, M. D. Raizenne, W. R. Chen, C. Poon, W. Wallace: IAR/NRC, Canada

THIRTY YEARS OF RETROGRESSION AND REAGING

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

NUMERICAL MODEL OF SINGLE MAIN ROTOR HELICOPTER DYNAMICS

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

FLIGHT TRAJECTORIES OPTIMIZATION

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

CONTROL INTEGRATION PROCESS IN AIRCRAFT SYSTEMS DEVELOPMENT

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

ADAPTIVE MODELING AND OPTIMIZATION OF PILOT HELMETS FOR DIFFERENT KINDS OF IMPACTS WITH HARD OBSTACLES

ICAS 2002-R73 N. Rao, A. K. Sinha, R. Kusumo: RMIT University, Australia

A SYSTEM FRAMEWORK FOR THE DESIGN OF AN AVIONICS ARCHITECTURE WITH UPGRADE POTENTIAL – AVIONICS ARCHITECTURE ANALYSIS MODULE

ICAS 2002-R75 G. Sachs, U. Sennes: Technische Universität München, Germany

SPEED CONTROL ISSUES OF 3D TUNNEL/PREDICTOR DISPLAYS

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

HELICOPTER HYDRAULIC SYSTEM (Design, Component Selection, Modular Construction,Integration & Testing)

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

DEVELOPMENT OF ULTRASONIC METHOD OF RADIAL CLEARANCE ASSESSMENT FOR BOLTED JOINTS AT RESTRICTED ACCESS

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

MOTOR CASE FOR ROCKET TRAJECTORY CORRECTION SYSTEM

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

GENERATION OF SU-27 FIGHTER

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