Compressibility shocks accompanying local or total supersonic flows lead to pronounced flow separations which result in unusually high energy losses on airplane wings, vanes, and in diffusers; phenomena investigated experimentally and theoretically. English translation from Technische Berichte v 10 n 2 1943.
Separation of flow due to compressibility shock
Nat Advisory Committee Aeronautics -- Tech Memo
1947
6 pages
3 Supp Sheets
Report
English
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The separation of flow due to compressibility shock
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