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#1 |
Member
Ovidiu Michiu
Join Date: Apr 2010
Location: Munich, Germany
Posts: 53
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hello forum,
i have a 2d NACA-profile. i'm using the simpleFoam solver and i would like to obtain the lift, drag and momentum coefficients. how can i obtain them? best, Ovidiu |
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#2 |
Member
Ovidiu Michiu
Join Date: Apr 2010
Location: Munich, Germany
Posts: 53
Rep Power: 16 ![]() |
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