Numerical method for obtaining solution to inverse problem of flow behind given detached shock to any desired accuracy; cases of zero and small incidence; particular attention devoted to analysis of sonic and subsonic region of flow field.
Theoretical investigation of flow field about blunt-nosed bodies in supersonic flight
J Aero/Space Sciences
Journal of the Aero/Space Sciences ; 25 , n 12
1958
10 pages
Article (Journal)
English
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