=+Let us consider the free-free system of Figure 3.7, which could be representative of the fundamental behaviour

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=+Let us consider the free-free system of Figure 3.7, which could be representative of the fundamental behaviour of bending vibration for an airplane in flight. Take M = 8m as the fuselage mass, m the wing lumped mass (including engines) and k as the stiffness between the vertical displacements of the fuselage and the vertical displacement of the wing lumped

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