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Engineering, 15.10.2019 01:20 noeltan12031

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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