Flight boundary layer transition measurements on a slender cone at Mach 20
10th Fluid and Plasmadynamics Conference ; 1977 ; Albuquerque , NM , U.S.A.
01.01.1977
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Hypersonic Wind-Tunnel Measurements of Boundary-Layer Transition on a Slender Cone
Online Contents | 2016
|Boundary-Layer Transition on a Film-Cooled Slender Cone
AIAA | 1976
|Boundary layer transition on a film-cooled slender cone
AIAA | 1975
|