Experimental flowfield visualization of a high alpha wing at Mach 1.62
25th AIAA Aerospace Sciences Meeting ; 1987 ; Reno , NV , U.S.A.
01.01.1987
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Turbulent-heat-transfer measurements at mach number of 1.62
Engineering Index Backfile | 1955
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