REDWING_1
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by Mike Walters Mike Walters

Feasibility calculations for a small UAV wing. 1084mm total span. CNC carbon center section.
 
Total Span: 1078.00 mm
Wing Area: 31.55 dm²
 
CG@22.50%: 175.04 mm
Wing Load: 50.71 g/dm²
 
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