A numerical study of supersonic viscous cone flow at high angle of attack
14th Aerospace Sciences Meeting ; 1976 ; Washington , DC , U.S.A.
01.01.1976
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Laminar boundary layer on cone in supersonic flow at large angle of attack
Engineering Index Backfile | 1953
|Laminar boundary layer on cone in supersonic flow at large angle of attack
Engineering Index Backfile | 1952
|