Flow field study about a hemispherical cylinder in transonic and lowsupersonic Mach number range
13th Aerospace Sciences Meeting ; 1975 ; Pasadena , CA , U.S.A.
1975-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Separated trailing-edge flow at a transonic Mach number
AIAA | 1983
|Separated trailing-edge flow at a transonic Mach number
NTRS | 1983
|Separated trailing-edge flow at a transonic Mach number
AIAA | 1982
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