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Old   October 26, 2009, 08:31
Red face About compressible flow at low mach
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hit
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Dear CFD friends,

now,I have a question about calculation of compressible flow at low mach,But I can not get a good result.I can not find reasons. Calculation condition as follows:
[1]stream flow Mach number M=0.01
[2]Rey=6e4
[3]space: MUSCL method
Roe average method
[4]time: LUSGS method
[5]Laminar flow method(Compressible flow Code is used)

By these conditions,for example,If Roe-average method is used at very low Mach number(Mach number M=0.01) by Compressible flow Code,Can I get good result?
Thanks
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