Page 293 - Introduction to Naval Architecture
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278                VIBRATION, NOISE AND SHOCK

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          The period becomes T d = &r/ [(A/M) - (^/2JW) ]° , frequency being
        l/T d , where/i is a damping coefficient such that damping force equals
        ju (velocity).
          Successive amplitudes decay according to the equation


          As the damping increases the number of oscillations about the mean
        position will reduce until finally the body does not overshoot the
        equilibrium position at all. The system is then said to be dead beat.


        Regular forced vibrations
        Free vibrations can occur when for instance, a structural member is
        struck an instantaneous blow. More generally the disturbing force will
        continue to be applied to the system for a longish period and will itself
        fluctuate in amplitude. The simplest type of disturbing force to assume
        for analysis purposes is one with constant amplitude varying sinusoi-
        dally with time. This would be the case where the ship is in a regular
        wave system. The differential equation of motion, taking x as the
        displacement at time t, becomes:




        The solution of this equation for x is the sum of two parts. The first
        part is the solution of the equation with no forcing function. That is,
        it is the solution of the damped oscillation previously considered. The
        second part is an oscillation at the frequency of the applied force. It
        is x = B sm(a)t - y).
          After a time the first part will die away leaving the oscillation in the
        frequency of the forcing function. This is called a. forced oscillation. It is
        important to know its amplitude, B, and the phase angle, y. These can
        be shown to be:










        In these expressions A is called the tuning factor and is equal to
                0-5
        a)/ (k/M)  . That is the tuning factor is the ratio of the frequency of the
        applied force to the natural frequency of the system. Since k represents
        the stiffness of the system, F 0/k is the displacement which would be
        caused by a static force F 0. The ratio of the amplitude of the dynamic
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