Paper emphasizes great potential value of flight testing as means of conducting research into problems of high speed flight and shows that there is still much to be done if one is to understand fully all that occurs even at comparatively modest Mach numbers (up to, say, 0.85); compresssibility effects on drag and on lift; stability and control. (See also - discussion p 503-12)
Flight research at high subsonic speeds
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 52 , n 452
1948
21 pages
Article (Journal)
English
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