Numerical solutions are presented for supersonic perfect gas flow; full inviscid equations are used and conditions at shock wave prescribed; body shapes and surface pressure distributions are obtained.
Calculation of supersonic flow past bodies supporting shock waves shaped like elliptic cones
NASA -- Tech Note
1959
30 pages
Report
Englisch
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Supersonic flow past slender bodies of elliptic cross-section
TIBKAT | 1955
|Supersonic flow past large-angle pointed cones.
AIAA | 1972
|