Numerical Investigations of Hypersonic Boundary-Layer Stability for a Blunt Flat Delta Wing
AIAA AVIATION 2023 Forum
01.01.2023
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
|