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Calculate aerodynamic coefficients with openfoam using only opensource programs |
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May 20, 2016, 12:26 |
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#21 |
New Member
Join Date: Feb 2016
Posts: 28
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Hi everyone,
I am following the same procedure than Xwang in the first post. I am wondering if someone found an answer for the 4th point which is the issue of how to stop simulations? The only tool I have to define the convergence uses the residuals. But when I reach 1e-6 for each variable it does not mean I reach convergence... Is there already something implemented to define a convergence criterion using lift and drag coefficients? Regards, mqsim |
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