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Questions about ReTheta & Gamma setup in airfoil calculation

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Old   December 4, 2018, 21:53
Default Questions about ReTheta & Gamma setup in airfoil calculation
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Dear all,

I am calculating the NACA 64312 airfoil. The freestream velocity is 50m/s, the turbulent intensity is 1%. I use the Komega SSTLM transition model for calculation and my setup for U, k and Rethetat are shown in the attached figures. Unfortunately, the calculation fails. There may be some errors in
my setup. Could anyone help me? Thank you.



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