s-omega model for hypersonic folw for Mach>10 -- CFD Online Discussion Forums

September 27, 2007, 10:45	s-omega model for hypersonic folw for Mach>10	#1
margarita Guest Posts: n/a	Hi, I have the problem with turbulence modeling up for hypersonic flow with high Mach value( >10). I try to use Baldwin-Lomax and k-omega model, but it doesn't work. I try also k-eps and S-A, the same problem. I would like to use s-omega model, proposed by David C. Wilcox in his book "Turbulence modeling for CFD (2006)". Thank you in advance for your help. Margarita.

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