Authors demonstrate that under given incident flow conditions, forces on airfoil depend only on characteristics of trailing vortex sheet, i.e., on potential flow due to this sheet at considerable downstream distance. Brief English abstract from Luftfahrtforschung v 20 n 2 Feb 27 1943 p 48-56. (Abstract Sec)
Theory of lifting wing
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 47 , n 390
1943
Article (Journal)
English
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Cancellation zone in supersonic lifting wing theory
AIAA | 1986
|Engineering Index Backfile | 1961
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