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ASSIGNOMENTI 7. Considering a un-swept wing modeled by 3 horseshoes, the control points are at 1/4...


ASSIGNOMENTI 7. Considering a un-swept wing modeled by 3 horseshoes, the control points are at 1/4 chord points of middle lin
ASSIGNOMENTI 7. Considering a un-swept wing modeled by 3 horseshoes, the control points are at 1/4 chord points of middle line on each segment, please deduct the aerodynamics influence matrix A. (x,y,z) 3 (x2,Y,Z) (x,Y,)
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