Boundary layer acoustic measurements in transitional and turbulent flow at M infinity equals 4.0
4th Aerodynamic Testing Conference ; 1969 ; Cincinnati , OH , U.S.A.
1969-01-01
Conference paper
Electronic Resource
English
Wedge and cone theory for m infinity equals infinity.
AIAA | 1965
|Wedge and cone theory for m infinity equals infinity.
NTRS | 1965
|Flow with M/infinity/equals 1 past thin airfoils
AIAA | 1970
|Flow with M/infinity/equals 1 past thin airfoils
NTRS | 1970
|