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aerodynamic coefficient chaleng with dsmcFoam

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Old   May 17, 2012, 05:53
Default aerodynamic coefficient chaleng with dsmcFoam
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Esmaeil Ahmadiyan
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Hi every body
I am new user in openFoam and tried with dsmcFoam solver
can anybody help me to derive lift , drag and pressure coefficients from this solver ?
I use of forceCoeffs but do not answer
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