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.
01.01.1970
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
|Wedge and cone theory for m infinity equals infinity.
AIAA | 1965
|