Compressible laminar boundary layer on a cone at high angle of attack
CHANG, P. K. /CATHOLIC U. OF AMERICA, WASHINGTON, D.C./., SMITH, R. A.
AIAA Journal ; 8 , 11 ; 1921-1927
1970
Aufsatz (Zeitschrift)
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
|