Crossing shock wave turbulent boundary layer interactions - Variableangle and shock generator length geometry effects at Mach 3
30th Aerospace Sciences Meeting and Exhibit ; 1992 ; Reno , NV , U.S.A.
1992-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Hypersonic crossing shock-wave/turbulent-boundary-layer interactions
Tema Archiv | 1993
|