Book Description

Contents: Conclusions of the FMP Symposium in Valloire (1975) and Progress on Ground/Fight Correlation; Progress in Wind Tunnel Test Techniques and in the Corrections and Analysis of the Results; Ground/Flight Correlation on the Space Shuttle Orbiter from Re-Entry to Landing; Ground/Flight Correlation on the Alpha-Jet Experimental Aircraft with a Transonic Wing; Flight and Wind-Tunnel Correlation of Boundary-Layer Transition on the AEDC Transition Cone; Experimental Investigations of Transport Aircraft Low Speed Engine Interference Effects and Flight Test Correlation; Comparison of Prediction, Wind Tunnel and Flight Test Data for the Canadair Challenger Turbofan Aircraft; Lessons from Tornado Afterbody Development; The Use of Free-Flight Models for the Prediction of Departure Control; Comparison of Flight and Wind Tunnel Buffeting Measurements on the SAAB 105 Aircraft; Some Measurements of Buffeting on a Flutter Model of a Typical Strike Aircraft; Correlation Aspects of Analytical Wind Tunnel and Flight Test Results for a Hingeless Rotor Helicopter; Dynamic Structural Aeroelastic Stability Testing of the XV-15 Tilt Rotor Research Aircraft; Structural Aspects of Ground/Flight Correlation on the Variable Sweep Wing Aircraft Tornado; Real-Time Flutter Analysis of an Active Flutter-Suppression System on a Remotely Piloted Research Aircraft; Flight Flutter Testing with Emphasis on the Tip Vane Method.