It is demonstrated that mixed subsonic-supersonic flows about two-dimensional bodies can be calculated where not only transition from subsonic to supersonic but also transition from supersonic to subsonic takes place continuously, that is, without pressure jump. English translation from ZWB Forschungsbericht n 1794 Aug 7 1943.
Calculation of compressible flows with local regions of supersonic velocity
Nat Advisory Committee Aeronautics -- Tech Memo
1947
13 pages
7 Supp Plates
Report
Englisch
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