Algebraic turbulence model simulations of supersonic open-cavity flow physics

AIAA Journal ◽  
1996 ◽  
Vol 34 (11) ◽  
pp. 2255-2260 ◽  
Author(s):  
Chung-Jen Tam ◽  
Paul D. Orkwis ◽  
Peter J. Disimile
1994 ◽  
Author(s):  
Douglas Dusing ◽  
Curtis Fox ◽  
Chung-Jen Tam ◽  
Paul Orkwis ◽  
Peter Disimile

1967 ◽  
Vol 89 (1) ◽  
pp. 103-108 ◽  
Author(s):  
A. F. Emery ◽  
J. A. Sadunas ◽  
M. Loll

The heat transfer and pressure distribution in a rectangular cavity in a Mach 3 flow were investigated for a rectangular and an inverted-wedge recompression step. Noticeable differences between the results for the two steps were found in the recovery factors, but no real differences were detected in the heat-transfer coefficients or the velocity profiles. Heat-transfer coefficients in the cavity were determined by transient techniques and were found to range from 50 to 110 percent of the flat-plate value just prior to the expansion step.


1997 ◽  
Author(s):  
Chung-Jen Tam ◽  
Paul Orkwis ◽  
Peter Disimile ◽  
Chung-Jen Tam ◽  
Paul Orkwis ◽  
...  

2009 ◽  
Vol 15 (5) ◽  
pp. 336-342 ◽  
Author(s):  
Donghan Geng ◽  
Yu Wang

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