Numerical Investigations of Hypersonic Boundary-Layer Stability for a Blunt Flat Delta Wing
AIAA Aviation Forum ; 2023 ; San Diego, Calif.; Online
Fluid dynamics ; Volume 1 of 3 ; 285-309
2023
Aufsatz (Konferenz)
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
|