POSTERS
Abstracts of papers appearing in the congress CD-Rom proceedings are linked to this list

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

 

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

 

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

 

ICAS 2000-P1.5: B. L. Nagabhushan, Saint Louis University

Sequential Dispensing Concepts for Impact Pattern Control

 

ICAS 2000-P1.6: V. Broz, CTU in Prague

An Experimental System for the Measurement of Flow Velocity Vector

 

ICAS 2000-P1.7: H. Dimitrescu, INCAS

Moving Wall Effect in Dynamic Stall

 

P1.8: D. Erdem, Istanbul Technical University

An Experimental Study on Offset Jets

 

ICAS 2000-P2.4: J. Haider, Pakistan International Airlines, Pakistan

Design Of Wingtip Vortex Turbine

 

ICAS 2000-P2.5: J. D. Hammond, British Aerospace Airbus Ltd., UK

Rapid Wind Tunnel Model Manufacture And Model Change Techniques

 

ICAS 2000-P2.6: M. G. Lambourne, Aircraft Research Association Ltd., UK

The Ara Second-Generation Esp System

 

ICAS 2000-P2.7: J. R. Potts, W. J. Crowther, Fluid Mechanics Research Group, School of Engineering, University of Manchester, UK

Disc-Wing Aerodynamics

 

ICAS 2000-P3.1: E. M. Belo, EESC-USP, Dpt. De Engenharia Mecanica

Spill over Effects in Active Vibration Suppression Systems

 

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

 

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

 

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

 

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

 

ICAS 2000-P4.2: E. Khalifa, SNECMA

Improving Jet Engine Control Thanks to the New Control Techniques

 

ICAS 2000-P4.3: H. D. Kim, The Queen's Univ. of Belfast

Computations of the Plume Interference Effects at Mach 2.0

 

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

 

ICAS 2000-P5.1: Z. Dzygadlo, G. Kowaleczko, Military University of Technology, Warsaw, Poland

Non-Linear Ground Resonance Of A Helicopter

 

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

 

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

 

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

 

ICAS 2000-P5.5: D. Sindel, Istanbul Technical University

Impact of Helicopter Dynamics to Rescue Operations

 

ICAS 2000-P5.6: R. Szabolcsi, L. Pokoradi, J. Bera, ’Miklós Zrínyi’ National Defense University, Hungary

Robust Control Law Synthesis For High Manoeuvrable Aircraft

 

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

 

ICAS 2000-P6.1: Y. B. Seo, J. W. Choi, Pusan National University, Korea

A Novel Eigenstructure Assignment Method For Stochastic Dynamic Systems

 

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

 

ICAS 2000-P8.1: J. Bera, L. Pokoradi, R. Szabolcsi, Miklós Zrínyi National Defense University, Hungary

Investigation Of The Helicopter Noise

 

ICAS 2000-P9.1: M. Cowrie, British Aerospace Systems & Equipment

The Base Terrain Awareness and Warning System - TAWS

 

ICAS 2000-P9.2: J. M. Hedo, Universitad Politecnica de Madrid

Emergency Evacuation of Narrow-Body, Wide-Body and Unconventional Transport Airplanes

 

ICAS 2000-P11.1: H. Lobentanzer, DaimlerChrysler Research and Technology, Frankfurt, Germany

Customer Driven Development Of Aircraft Cabin And Subsystem Concepts