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New Member
Join Date: Feb 2014
Posts: 9
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Dear all,
I am working on a CFD problem for flow over airfoil which is having a ramp motion. I have calculated Cl, Cd and Cm. Now, I am trying to trying to calculate Pressure-Coefficient at different angle of attacks. Please help me how can I do the same in Fluent. Waiting for all your responses. |
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