Problem considered is that of finding velocity field in and near throat of given nozzle shape. English translation from Jahrbuch 1942 Luftfahrtforschung.
Flow pattern in converging-diverging nozzle
Nat Advisory Committee Aeronautics -- Tech Memo
National Advisory Committee for Aeronautics -- Technical Memorandums ; Tech Memo 1215
1949
42 pages
Diagrams, Charts, Tables
Report
English
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