NASA NTRS · 19950019657
Numerical Calculations of Shock-Wave/Boundary-Layer Flow Interactions
Abstract
The paper presents results of calculations for 2-D supersonic turbulent compression corner flows. The results seem to indicate that the newer, improved kappa-epsilon models offer limited advantages over the standard kappa-epsilon model in predicting the shock-wave/boundary-layer flows in the 2-D compression corner over a wide range of corner angles and flow conditions.
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Huang, P. G., Liou, W. W.. 1994-08-01. Numerical Calculations of Shock-Wave/Boundary-Layer Flow Interactions. https://ntrs.nasa.gov/citations/19950019657
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