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[Sponsors] |
December 15, 2006, 10:01 |
Cm calculations
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#1 |
Guest
Posts: n/a
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Hi,
1) I would like to know how to calculate cm for the airfoil i'm working with? 2) To calculate cl or cd it's only needed Force Global X or Global Y obtained from the calculator icon? 3) The Force Global Z must be 0? thanks in advance Andres, |
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