Experimental study of high-enthalpy shock- tunnel flow. I - Shock-tube flow and nozzle starting time.
DUNN, M. G. /CORNELL AERONAUTICAL LAB., INC., AERODYNAMIC RESEARCH DEPT., BUFFALO, N.Y./.
AIAA Journal ; 7 , 8 ; 1553-1560
1969-01-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Flow Characterization of High Enthalpy Shock Tunnel Based on Shock Stand-Off Distance
British Library Conference Proceedings | 2009
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