Aspects of confluence of 2 streams over region of afterbodies are explained; analysis can be reduced to 3 fundamental problems, development of isobaric mixing zone, separation and reattachment of flow; theoretical results achieved by ONERA (Office Nat d'Etudes et de Recherches Aeronautiques) are presented; several examples of application in regions of hypersonic and supersonic flow.
Investigation of flow over afterbodies of aircraft or rockets
Untersuchungen ueber die Stroemung am Heck von Flugzeugen oder Raketen
Zeitschrift fuer Flugwissenschaften ; 10 , n 7
1962
13 pages
Aufsatz (Zeitschrift)
Deutsch
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