I need help in udf ,please.
:confused:I want to have Numerical simulation of 0012 airfoil in fluent .But only a section of the wall of the 0012 airfoil is changing like cosine curve,that is only the y coordinate of this section is changing. Could you tell me how to achieve it? I had
to try to use the udf,but i didn't know how to achieve it. Thank you for your help. |
nobody?i need help.............
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Could you explain you problem clearly. Is airfoil moving or stationary? What do you mean by only section of airfoil is moving.
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You want change a solid wall geometry and hence deform the grid?
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