Hypersonic transition studies on a slender cone at small angles of attack.
HENDERSON, A., JR. /NASA, LANGLEY RESEARCH CENTER, AERO-PHYSICS DIV., FLOW ANALYSIS SECTION, HAMPTON, MADDALON, D. V. /NASA, LANGLEY RESEARCH CENTER, AERO-PHYSICS DIV., HAMPTON, VA./
AIAA Journal ; 6 , 1 ; 176-177
1968
Article (Journal)
Electronic Resource
English
Hypersonic Slender Body Theory for All Angles of Attack
AIAA | 1992
|Viscous hypersonic flow past slender cone
Engineering Index Backfile | 1967
|