In relating test results obtained from wind tunnels to results from actual flight tests, corrections must be made to allow for aeroelastic effects and the effect of Reynolds' number differences. Using data from Concorde and airbus tests, an attempt is made to define what degree of accuracy may be expected from aerodynamic coefficients derived from wind tunnel measurements. (Author)
Critical Analysis of Comparisons Between Flight Test Results and Wind Tunnel Test Predictions in Subsonic and Supersonic Transport Aircraft
1976
56 pages
Report
No indication
English
In-flight tuning: Wind tunnel test results and flight test preparation
Tema Archive | 2011
|In-Flight Tuning: Wind Tunnel Test Results and Flight Test Preparation
British Library Conference Proceedings | 2011
|