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udf for 3d wing

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Old   October 8, 2004, 09:13
Default udf for 3d wing
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Hi everybody.

I'm studing a 3d tapered, swirled wing and I need to obtain the evolution of lift and drag along wing span. I think that the solution is to write a Udf that takes in account lift and drag section to section, according to the current air direction. CAn someone help me to write this UDF or to redirect me to a UDF on-line library?

Thanks. Giorgio
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