For the system shown in Fig. 3.49, (x) and (y) denote, respectively, the absolute displacements of the
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For the system shown in Fig. 3.49, \(x\) and \(y\) denote, respectively, the absolute displacements of the mass \(m\) and the end \(Q\) of the dashpot \(c_{1}\).
(a) Derive the equation of motion of the mass \(m\),
(b) find the steady-state displacement of the mass \(m\), and
(c) find the force transmitted to the support at \(P\), when the end \(Q\) is subjected to the harmonic motion \(y(t)=Y \cos \omega t\).
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