3.35 For the system shown in Fig. 3.49, x and y denote, res pectively, the absolute dis placements of the mass m and the end Q of the dashpot c. (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 trans- mitted to the support at P, when the end Q is subjected to the harmonic motion y(1) = Y cos ot. %3D APT R3 HARMONICALLY EXCITED VIBRATION (1) = Y cos ot k2 FIGURE 3.49
3.35 For the system shown in Fig. 3.49, x and y denote, res pectively, the absolute dis placements of the mass m and the end Q of the dashpot c. (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 trans- mitted to the support at P, when the end Q is subjected to the harmonic motion y(1) = Y cos ot. %3D APT R3 HARMONICALLY EXCITED VIBRATION (1) = Y cos ot k2 FIGURE 3.49
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Transcribed Image Text:3.35 For the system shown in Fig. 3.49, x and y denote, res pectively, the absolute dis placements
of the mass m and the end Q of the dashpot c. (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 trans-
mitted to the support at P, when the end Q is subjected to the harmonic motion
y(1) = Y cos wt.
346
CHAPT R3 HARMONICALLY EXCITED VIBRATION
(1) = Y cos wt
C1
k,
m
FIGURE 3.49
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