Shock wave transport effects on hypersonic leading edge flow.
GARVINE, R. W. /GENERAL ELECTRIC CO., MISSILE AND SPACE DIV., SPACE SCIENCES LAB., THEORETICAL FLUID
AIAA Journal ; 4 , 10 ; 1856-1858
1966
Article (Journal)
Electronic Resource
English
Blunt-leading-edge problem in hypersonic flow
Engineering Index Backfile | 1963
|THE BLUNT-LEADING-EDGE PROBLEM IN HYPERSONIC FLOW
AIAA | 1963
|