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aerodynamic coefficient chaleng with dsmcFoam

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May 17, 2012, 05:53	aerodynamic coefficient chaleng with dsmcFoam	#1
e.ahmadiyan New Member Esmaeil Ahmadiyan Join Date: Sep 2011 Posts: 26 Rep Power: 15	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 thanks

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