Three-Dimensional Approximate Viscous Shock Layer Method for Hypersonic Flow over Blunt-Nosed Bodies
41st Aerospace Sciences Meeting and Exhibit
2003-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Approximate Viscous Shock Layer Technique for Calculating Hypersonic Flows About Blunt-Nosed Bodies
Online Contents | 1994
|