Mathematics, 12.02.2020 03:08 anonymous174
See illustrated as the half of the wing and its loading during flight. The information about the wing geometry, the wing material, and the loadings are given. You can assume that the cross-section of the wing is consistent along the span length, and that the only deformation is bending. Calculate and plot the wing deflection as a function of the span (0 < z < b/2).
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See illustrated as the half of the wing and its loading during flight. The information about the win...
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