Page 194 - Practical Design Ships and Floating Structures
P. 194

169



        where n is the number of mooring lines, xu and yu are the longitudinal and the transversal points of the
        fairlead, T, is the mooring line tension (Ti = f(L3). These expressions, developed  for a single ship
        system, can be used  for a multiple-ship system by  considering the coupling of the ships due to the
        connection hawser in the terms Tu and T,.

        The velocities in both coordinate systems are related by the following expressions:
                                    c+ c = u. cos(ly) - v .sin( y/)
                                                                                (7)
                                     q = u. sin(w) + v .  cos(^)
                                                                                (8)
        where 6 and  17 are the absolute displacement of the ship. The acceleration relation is obtained by the
        time derivative of eqns. 7 and 8. Introducing eqns. 7 and 8 in eqns. 1,2 and 3, the equations of motion
        can be expressed as function of the absolute accelerations, velocities and displacements of the ship as:



        The final expression are extensive and are not included in the text, but can be obtained following the
        steps presented above (see Matter, Sales and Sphaier, 2001)


        3  THE STABILITY ANALYSIS
        The stability analysis consists on the observation of the ship movements around the many possible
        equilibria, the equilibrium positions of the system, for different incidence angles of the current. The
        equations of motions (Eqns.  1, 2 and 3) are expanded in a Taylor's  series around the equilibria and
        linearized. The final expressions are similar to:









        where the tb's are the resultant terms of the linearization. These terms can be obtained analytically as
        shown in Matter et a1 (2001a). The linearized expressions (Eqns.  10, 11 and 12),  can be written as:
                                          x=A,x

        where x  = (q,z, w, 6 7, WIT and q, z and w are respectively the time derivatives of 6, 1;1 and   This is the
        classical eigenvalue problem with x  =  @!e"'.   The eigenvalues d are obtained from the solution of a
        polynomial like:
                                        tan .R =o                              (14)
                                        k=O
        The index n is equal to the number of ships times twice the number of degrees of freedom for a single
        ship. Sometimes, this polynomial  can be  solved  analytically and  then,  it  is possible to  obtain  the
        eigenvalue derivatives in relation to each parameter of the system and perform a more detailed study of
        the  stability, including  a  bifurcation study.  Extending the  study  to  the  offloading operation, the
   189   190   191   192   193   194   195   196   197   198   199