An investigation of separated flow about a hemisphere-cylinder at incidence in the Mach number range from 0.6 to 1.5
15th Aerospace Sciences Meeting ; 1977 ; Los Angeles , CA , U.S.A.
01.01.1977
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flow field about hemisphere-cylinder body at Mach number of 7.3
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