Experimental study of high-enthalpy shock- tunnel flow. II - Nozzle-flow characteristics.
DUNN, M. G. /CORNELL AERONAUTICAL LAB., INC., AERODYNAMIC RESEARCH DEPT., BUFFALO, N.Y./.
AIAA Journal ; 7 , 9 ; 1717-1724
1969-01-01
8 pages
Article (Journal)
Electronic Resource
English
Influence of Thermal Non-Equilibrium on Nozzle Flow Condition of High Enthalpy Shock Tunnel HIEST
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