Numerical Study of Film Cooling Scheme on a Blunt-Nosed Body in Hypersonic Flow
41st AIAA Thermophysics Conference
01.01.2009
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Study of Hypersonic Leeward Flow over a Blunt Nosed Delta Wing
Online Contents | 1995
|Numerical study of hypersonic leeward flow over a blunt nosed delta wing
Tema Archiv | 1995
|