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August 8, 2005, 06:30 |
lift coefficient in vof
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#1 |
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hi users I am using fluent to calculate lift coefficient over an airfoil with free surface .what is the ideal no of cells reqiured, when i used 2 lakh the and used lift monitor lift did not converge to a const. value till 30 seconds.If anyone has any suggestion to make please do reply .
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