aerodynamic coefficient chaleng with dsmcFoam
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
I used it in previous versions of dsmcfoam (localMfp, localCf etc.). But now it is not there..
Any suggestion from your side
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