Section presents data on aerodynamic characteristics of revolution for angle of attack range of zero to almost 90° throughout supersonic and hypersonic flight regimes; basic theories governing pressure distributions on bodies of revolution and in their surrounding flow fields are evaluated. (Available, Superintendent of Documents, U S Government Printing Office, Washington, D.C.)
Handbook of supersonic aerodynamics -- Section 8, bodies of revolution
U S Bur Naval Weapons NAVWEPS Report
1961
335 pages
Report
English
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