Laminar boundary-layer separation and near-wake flow for a smooth blunt body at supersonic and hypersonic speeds.
GRANGE, J.-M., KLINEBERG, J. M., LEES, L. /CALIFORNIA INST. OF TECH., PASADENA, CALIF./.
AIAA Journal ; 5 , 6 ; 1089-1096
1967-01-01
8 pages
Article (Journal)
Electronic Resource
English
Near wake of a blunt body at hypersonic speeds
AIAA | 1965
|Near wake of a blunt body at hypersonic speeds
AIAA | 1964
|