A study of hypersonic swept shock wave/turbulent boundary layer interactions using a conical Navier-Stokes code
AlAA 4th International Aerospace Planes Conference ; 1992 ; Orlando , FL
01.01.1992
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Shock-Wave/Boundary Layer Interactions at Hypersonic Speeds by an Implicit Navier-Stokes Solver
British Library Conference Proceedings | 1993
|Hypersonic Crossing Shock-Wave-Turbulent-Boundary-Layer Interactions
Online Contents | 1993
|