Finite-difference analysis of the three-dimensional turbulent boundary layer on a sharp cone at angle of attack in a supersonic flow
10th Aerospace Sciences Meeting ; 1972 ; San Diego , CA , U.S.A.
01.01.1972
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Investigation of Boundary Layer Transition in Three-Dimensional Supersonic Flow over Sharp Cone
British Library Conference Proceedings | 2011
|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
|