Heat transfer and boundary layer growth for ultra high Reynolds number compressible turbulent boundary layers for a radiatively driven hypersonic wind tunnel
40th AIAA Aerospace Sciences Meeting & Exhibit ; 2002 ; Reno , NV , U.S.A.
2002-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Radiatively Driven Hypersonic Wind Tunnel
Online Contents | 1995
|Radiatively driven hypersonic wind tunnel
AIAA | 1995
|Radiatively driven hypersonic wind tunnel
AIAA | 1994