Integral method for the stagnation region of a hypersonic viscous shock layer with blowing.
DUNN, M. G. /CORNELL AERONAUTICAL LAB., INC., AERODYNAMIC RESEARCH DEPT., BUFFALO, N.Y./., KANG, S.-W.
AIAA Journal ; 6 , 10 ; 2031-2033
1968-01-01
3 pages
Article (Journal)
Electronic Resource
English
Hypersonic merged stagnation shock layers
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