Viscous effects far downstream in a slowly expanding hypersonic nozzle.
KARAMCHETI, K. /STANFORD U., DEPT. OF AERONAUTICS AND ASTRONAUTICS, STANFORD, CALIF./., RASMUSSEN, M. L. /STANFORD U., STANFORD, CALIF./
AIAA Journal ; 4 , 5 ; 807-815
1966
Article (Journal)
Electronic Resource
English
Integral equations for viscous hypersonic nozzle flow
AIAA | 1964
|Hypersonic turbulent transpiration cooling including downstream effects
Engineering Index Backfile | 1966
|NTRS | 1989
|