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(Solved): ok An airplane wing is modeled as a 3 DoF lumped- mass system. Derive the flexibility matrix ...
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An airplane wing is modeled as a 3 DoF lumped- mass system. Derive the flexibility matrix and the EoM of the wing by assuming that all A? = A, (EI); = EI, 4? = l 4? As(EDA (ED O (a) www A. (ED (20)
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