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Old 01-26-2007 | 08:27 AM
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Lorance66
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From: Mechanicsburg, PA
Default locating CG
Can anyone help me figure out how to calculate the CG for a forward swept wing aircraft?

I am speaking about a wing similar to an X-29 but with no tail. I think maybe the standard formula for CG may work for this type of wing, am I correct?

thanks

Brad

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