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Thread: Questions about wing loading and CG
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Old 07-01-2005 | 04:22 PM
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WS
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From: St. Catharines, ON,
Default RE: Questions about wing loading and CG
The aerodynamic center would be 25% of the chord located 1/3 the semi-span toward the tip. The CG should be slightly ahead of that point for positive stability.
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