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Old 01-09-2008, 04:52 PM
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Default WINGSPAN AND WING ROOT TO PRODUCE LIFT AT WHAT SPEED WITH A WEIGHT OF

What I would love to know would be if there is a calculation for lift. Is there a calculation for how much lift you can get for any given wingspan and chord and root and wing area with also drag factor. The reason is I want to design and build something very specific and unique can anyone help