Engineering, 18.11.2019 23:31, joannachavez12345

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

Answers: 2

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