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Engineering, 16.11.2019 21:31 lareynademividp0a99r

Considering a un-swept wing modeled by 3 horseshoes, the control points are at 1/4 chord points of middle line on each segment, deduct the aerodynamics influence matrix

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Considering a un-swept wing modeled by 3 horseshoes, the control points are at 1/4 chord points of m...
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