A numerical study of supersonic flow over a compression corner with different incoming boundary-layer profiles
21st Fluid Dynamics, Plasma Dynamics and Lasers Conference ; 1990 ; Seattle , WA , U.S.A.
1990-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Study of Wave Trains in Supersonic Flow over a Compression Corner (AIAA 2016-0049)
British Library Conference Proceedings | 2016
|