POSTERS |
ICAS 2000-P1.1: P. Berry, Linköping University Constraint Analysis on a Solar Powered Aircraft |
ICAS 2000-P1.2: H. D.Froning Jr., Flight Unlimited TB 20, a Low Cost Tool for in-flight Teaching
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ICAS 2000-P1.3: H. D. La Roche, La Roche Consulting Dynaero & OneraLa Roche Consulting, Switzerland Winggrid At Transonic Speeds: Impact On Performance, Challenges To Solve
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ICAS 2000-P1.4: M. G. Maunsell, Aircraft laboratory, University of São Paulo, São Carlos Engineering School, Brazil. The Developement Of An Unconventional Vtol Vehicle
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ICAS 2000-P1.5: B. L. Nagabhushan, Saint Louis University Sequential Dispensing Concepts for Impact Pattern Control
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ICAS 2000-P1.6: V. Broz, CTU in Prague An Experimental System for the Measurement of Flow Velocity Vector
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ICAS 2000-P1.7: H. Dimitrescu, INCAS Moving Wall Effect in Dynamic Stall
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P1.8: D. Erdem, Istanbul Technical University An Experimental Study on Offset Jets
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ICAS 2000-P2.4: J. Haider, Pakistan International Airlines, Pakistan Design Of Wingtip Vortex Turbine
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ICAS 2000-P2.5: J. D. Hammond, British Aerospace Airbus Ltd., UK Rapid Wind Tunnel Model Manufacture And Model Change Techniques
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ICAS 2000-P2.6: M. G. Lambourne, Aircraft Research Association Ltd., UK The Ara Second-Generation Esp System
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ICAS 2000-P2.7: J. R. Potts, W. J. Crowther, Fluid Mechanics Research Group, School of Engineering, University of Manchester, UK
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ICAS 2000-P3.1: E. M. Belo, EESC-USP, Dpt. De Engenharia Mecanica Spill over Effects in Active Vibration Suppression Systems
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ICAS 2000-P3.2: B. Wang (1, 2), Q. Yang (2), (1) Xi’an Aircraft Design & Research Institute, Xi’an, PRC (2) Northwestern Polytechnical University, Xi’an, PRC A Study Of Option Of Material Fatigue Property Description For Fatigue Life Prediction
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ICAS 2000-P3.3: J. G. Damilano, J. L. F. Azevedo, Instituto de Aeronáutica e Espaço, Centro Técnico Aeroespacial, CTA/IAE/ASE, Brazil A Detailed Study Of Panel Flutter Stability For The First Brazilian Satellite Launcher Main Fairing
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ICAS 2000-P3.4: V. Koldaev, J. L. F. Azevedo, Instituto de Aeronautica e Espaco, CTA/IAE/ASE-N, Brazil Numerical Solution Of Aeroelastic Problem In Unsteady Motion Of Parachute System
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ICAS 2000-P4.1: D. Hanus, Czech Technical University in Prague, Department of Automotive and Aerospace Engineering, Czech Republic New Design Method Of Inlets And Outlet Nozzles Of Turboprop Engines
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ICAS 2000-P4.2: E. Khalifa, SNECMA Improving Jet Engine Control Thanks to the New Control Techniques
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ICAS 2000-P4.3: H. D. Kim, The Queen's Univ. of Belfast Computations of the Plume Interference Effects at Mach 2.0
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ICAS 2000-P4.4: D. A. Perigo, N.Qin, Cranfield University, UK A Numerical Investigation Of The Flows In And Around Annular-Plug Nozzle Configurations
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ICAS 2000-P5.1: Z. Dzygadlo, G. Kowaleczko, Military University of Technology, Warsaw, Poland Non-Linear Ground Resonance Of A Helicopter
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ICAS 2000-P5.2: F. Cai, X. Gao, J. Gao, Electronic Engineering Department, Northwestern Polytechnical University, Xi'an, PRC Bearing-Corrected Guidance With Incomplete Target Information For Over The Shoulder
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ICAS 2000-P5.3: M. Krawczyk (1), W. Blajer (2), J. A. Goszczyski (1),, (1) Institute of Aviation, Poland (2) Technical University of Radom, Poland The Application Of Inverse Simulation Techniques To The Modelling Of Spatial Manoeuvres
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ICAS 2000-P5.4: U. La Roche, Switzerland, La Roche Consulting Dynaero & Onera Prototype Design And Tests Of A Commercial Ul-Aircraft Equipped With Winggrid Wingtips
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ICAS 2000-P5.5: D. Sindel, Istanbul Technical University Impact of Helicopter Dynamics to Rescue Operations
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ICAS 2000-P5.6: R. Szabolcsi, L. Pokoradi, J. Bera, ’Miklós Zrínyi’ National Defense University, Hungary Robust Control Law Synthesis For High Manoeuvrable Aircraft
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ICAS 2000-P5.7: Z. Zagdanski, Air Force Institute of Technology Long Term Simulation of Flight Dynamics of a Structurally Rigid Aeroplane in Terms of Aeroelasticity
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ICAS 2000-P6.1: Y. B. Seo, J. W. Choi, Pusan National University, Korea A Novel Eigenstructure Assignment Method For Stochastic Dynamic Systems
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ICAS 2000-P7.1: R. Shaoming, Yin Yang City, PRC Using the Robot to Detect the Characteristic Curve of Stick Force with Displacement in the Airplane Assembly Line
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ICAS 2000-P8.1: J. Bera, L. Pokoradi, R. Szabolcsi, Miklós Zrínyi National Defense University, Hungary Investigation Of The Helicopter Noise
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ICAS 2000-P9.1: M. Cowrie, British Aerospace Systems & Equipment The Base Terrain Awareness and Warning System - TAWS
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ICAS 2000-P9.2: J. M. Hedo, Universitad Politecnica de Madrid Emergency Evacuation of Narrow-Body, Wide-Body and Unconventional Transport Airplanes
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ICAS 2000-P11.1: H. Lobentanzer, DaimlerChrysler Research and Technology, Frankfurt, Germany Customer Driven Development Of Aircraft Cabin And Subsystem Concepts
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