Page 300 - Introduction to Naval Architecture
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VIBRATION, NOISE AND SHOCK                 285

        Formulae for ship vibration

        The formulae for uniform beams suggests that for the ship an
        approximation will be given by a formula of the type:






          Assuming the hull is made of various grades of steel, for which E is
        effectively constant, this can be represented by:







        where 7 a is the moment of inertia of the midships section.
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          This formulation was first proposed by Schlick . Suggestions for the
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        value of the constant for different ship types have been made  but these
        can only be very approximate because of the many variables involved in
        ships. The most important are:

          (1) Mass and stiffness distribution along the length.
          (2) Departure from ordinary simple theory due to shear deflection
              and structural discontinuities.
          (3) Added mass.
          (4) Rotary inertia.


        Shear deflection
        Simple bending theory assumes that when a beam is bent sections
        which were plane and perpendicular to the neutral axis before bending
        remain so after. For this condition there can be no shear stress in the
        beam. The influence of shear stresses is two-fold:


          (1) The stress is no longer simply proportional to the distance from
              the neutral axis.
          (2) Additional deflection of the beam occurs, the shear deflection.


        To illustrate the effects of shear consider again the massless beam
        carrying a mass Mat its centre. If the beam has a solid rectangular cross
        section the deflection due to shear alone is given by BMgl/WbdG, where
        b and d are the breadth and depth of the beam and G is the Modulus of
        rigidity.
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