Basis for expectation that economic long range aviation is about to be transformed; design barrier and structure weight penalties; existence of two different values of lift/drag ratio for same aircraft announces that ideal shape for subsonic flight is different from ideal shape for supersonic flight; aerodynamic necessity for variable shape inexorably exists.
Supersonic turning-point
Shell Aviation News
Shell Aviation News ; n 248
1959
4 pages
Article (Journal)
English
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