Page 214 - Practical Design Ships and Floating Structures
P. 214

189

        the case of VLFS, the elastic modes can be considered as the manner as in Ma & Hirayama,  1997. In
        addition,  hydrodynamic  force  and  wave  exciting  force  are  evaluated  directly;  the  motions  and
        deflections can  be  obtained  without  many  difficulties. The  detail  formulations are given  in  our
        previous paper (Hirayama and Ma (1995a), (1 995b))
        In head wave condition, deflection of the structure is mainly caused by vertical bending deformation,
        thus,  the  structure can  be  treated as an  elastic uniform  beam with  two  free  ends.  Then,  vertical
        displacement is expressed as following equation.
                            1;1~1d~Z  8'2
                                    +
                                           +
                                             kz
                                     El
                       pAZ + - - - = q(x,t),             (0 < x < L)            (3)
                             w  ax4  ax4
        where  p is the mass density, A is the sectional area,  11 is the structural damping coefficient, E1 is the
        bending rigidity, k is spring coefficient of foundation. L is beam length. q(x, t) represents external load
        acting at x coordinate. Over-dots denote differentiation with respect to time (t).
        According to the principle of mode superposition, the deflection z can be represented as an aggregation
        of the product of mode function Z, and principal coordinate p, as shown in Eqn. 2.
                               4x7 t) = 2 2, (4 Pr (t)                          (4)
                                             *
                                      r=l
        In this study, we applied the analytic mode functions of beam for Z,. The motion equation of principal
        coordinate of mode pr is un-coupled and could be expressed as following.
        Where Q, brk, % are the generalized mass, structural damping and stiffness of mode, A&, Bt are the
        generalized hydrodynamic  added mass and damping coefficient  respectively.  C& is the generalized
        hydrostatic restoring force coefficient. Finally, the displacement  of beam can be obtained fiom Eqn. 4.
        2.2 Steady Wave Drwt Forces

        The steady drift forces in regular waves are the time averaged mean force due to second order pressure,
        and the forces can be obtained fiom integration the pressure on wetted surface (near field method). On
        the other hand, far field method is also available which is based on momentum theory (Maruo (1960)).
        In that,  the momentums of  fluid  motions in far field are considered in terms of Kochin  functions.
        However, the near field method provides straightforward way in solving the drift forces and the force
        are resolved into each component. Thus, the near field method is applied in this study. By using the
        perturbation approach, the final expression of horizontal drift force is given in Eqn.6 (Pinkster (1980)).
        Here,  the  contribution  of  second  order  potentials  and  hydrostatic  force  due  to  second  order
        displacement  are ignored.



        In which,  ii  is normal vector of the point on wetted surface SO, 6,  is relative wave elevation, x,
        is the motion of CG in space-fixed  coordinate system,  +t  is time differential of velocity potential.
        T('),E(')are first order linear and rotational motion vectors respectively, which satisfied the following
        relation.
                                  p = jp +&I)   )( X
                                        g                                       (7)
        Where,  X  is position vector of the point on wetted surface.
         Once the first order potentials and motions are determined, the drift force will be able to obtained
        according to Eqn.6.  For very large floating structure, the deformation due to elastic mode should be
        included and the results of hydro-elasticity analysis fore-mentioned are utilized.
   209   210   211   212   213   214   215   216   217   218   219