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Calculate Lift and Drag Coefficients CL and CD

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June 13, 2012, 06:20		#9
malhar New Member Malhar Malushte Join Date: May 2012 Posts: 16 Rep Power: 14	hello every1, i am also new to openfoam. i have done similar sim ulation for flow acrodss a cylinder. i get drag n lift forces correctly, i.e accor ding to vortex shedding i am getting variation in lift forces. but the coeff of drag n lift Cd n Cl, i am getting them constant throughout. i am unable ti digest this contrasting behavour. please guide me thr this. thanks n regards malhar.

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