Nonequilibrium Viscous Shock-Layer Heat Transfer with Arbitrary Surface Catalycity

2005 ◽  
Vol 42 (2) ◽  
pp. 193-200 ◽  
Author(s):  
George R. Inger ◽  
Richard L. Baker
1977 ◽  
Vol 99 (2) ◽  
pp. 307-313 ◽  
Author(s):  
J. C. Adams

An analysis technique applicable to the problem of leeward vortex-induced heat transfer on a sharp cone at high angles of incidence under hypersonic laminar flow conditions is presented. The analysis, a three-dimensional hypersonic viscous shock layer approach in conjunction with a numerical solution procedure, is shown to be both applicable and accurate based on comparisons of heat-transfer distributions, surface pressure distributions, and leeward meridian flow-field profile measurements taken in a hypersonic wind tunnel. Detailed calculations of the embedded vortex flow field on the leeward side of the cone are presented in such a manner as to clearly portray exactly how embedded vortex flow influences local heating rates.


1993 ◽  
Author(s):  
ROOP GUPTA ◽  
SUDHEER NAYANI ◽  
KAM-PUI LEE ◽  
ERNEST ZOBY

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