Experimental study of axially-symmetric base flow with turbulent initial boundary layer at M sub infinity equals 2.42
3rd Fluid and Plasma Dynamics Conference ; 1970 ; Los Angeles , CA , U.S.A.
1970-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flow with M/infinity/equals 1 past thin airfoils
AIAA | 1970
|Flow with M/infinity/equals 1 past thin airfoils
NTRS | 1970
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