Series solutions for shock tube laminar boundary layer and test time.
KING, W. S. /AEROSPACE CORP., LABS. DIV., EL SEGUNDO, CALIF./., MIRELS, H. /AEROSPACE CORP., LABS., DIV., AERODYNAMICS AND HEAT TRANSFER DEPT., EL SEGUNDO, CALIF./.
AIAA Journal ; 4 , 5 ; 782-789
1966
Article (Journal)
Electronic Resource
English
Laminar sidewall boundary layer in a dusty-gas shock tube
TIBKAT | 1986
|Shock tube test time limitation due to turbulent-wall boundary layer
Engineering Index Backfile | 1964
|