Flow field study about a hemispherical cylinder in transonic and lowsupersonic Mach number range
13th Aerospace Sciences Meeting ; 1975 ; Pasadena , CA , U.S.A.
01.01.1975
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flow field about hemisphere-cylinder body at Mach number of 7.3
Engineering Index Backfile | 1962
|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
|