Basic performance and flow characteristics of variable density tunnel; problems of model support and of special mounting systems for wind tunnel tests at Mach Numbers close to 1; Lockheed "Bump " method of testing through transonic region; calibration, operation, and data reduction procedures required for obtaining and interpreting experimental data.
High-speed testing in southern California cooperative wind tunnel
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 15 , n 2
1948
20 pages
Bibliography
Article (Journal)
English
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Southern California cooperative wind tunnel
Engineering Index Backfile | 1945
Southern California cooperative wind tunnel
Engineering Index Backfile | 1945
High-speed wind tunnel testing
TIBKAT | 1965
|Wind Tunnel Testing of High Speed Propellers
British Library Conference Proceedings | 1997
|