Considering a un-swept wing
modeled by 3 horseshoes, the
control points are at 1/4 chord...
Engineering, 24.10.2019 16:43 brandonkelly104
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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