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       The so called flux vectors E and Fare evaluated in the n+l time level. Newton's  linearization
       procedure provides the flux vectors in the time level n:




       Substituting  (15)  into  equation  (14),  grouping  AQ  terms  on  the  left-hand  side  of  (14),  and
       approximating partial derivatives by  central differences, it  is possible  to write down  the following
       equation:
                    (I + At(6.A" -6,MF)+  At(6,,B" - 8,M;)bQ"  = -At(6$"  + 6,,F")   (16)
       where
                      E" =E: -E" "9
                      F" = F;" - Fvn





                      6<( )=  *         , 6,( )= ( )Z,J+I  -( It.J-1
                            ( )S+l,J  -(  ),-I.,
                                                     2
       Equation (1 6) is a penta-diagonal system of algebraic equations that solution can be improved by
       convenient approximated factorization - Beam and Warming (1978).  The left-hand side of (24) below,
       after proper factorization of (16), presents only rand derivatives in separate terms. Therefore, the
       numerical scheme of solution can be split into two steps. The first equation is solved for all interior
       grid points;  then, the second equation is solved for all interior grid points using the previous values of
       f- In each step, the resulting block tridiagonal system of algebraic equations is solved by application of
       Thomas algorithm (Anderson, Tannehill and Pletcher, 1984).

                        {Z + &(S, A - SsM6 ))" f " = (RHS)"               (17)


                          + A&B   - 6,pn  AQ~ fn
                                            =
                        where   (RH.)" =-~t(6~~ +6,~                       (18)
       Central  difference  schemes  require  artificial  dissipation  to  improve  stability  - Pulliam  (1980).
       Artificial dissipation suppresses high  frequency  oscillations and  controls the odd-even  uncoupling
       inherent to central difference schemes.  The Von-Neumann  linear stability analysis applied to  the
       Beam-Warming central difference scheme shows that some artificial dissipation is required to improve
       stability.
                           (I + At6.A"  - At6.M;  + Df'P = (RHS)' + D'"
                                                                           (1 9)
                           (I + &6,,B" - At6,,M; + D:)bQ''  = f"
       where
                0:) = -&,AU'V,A.,J; DF = -&iAtJ-'V,A,,&  0(4) -&&l?J-'[(V,A,p  +(V,,A,)ZbP
                                                     =
       3.2 Grid Generclrion

       An algebraic grid generator using the multi-suface method - Fletcher (1988) - is used to generate the
       grid points over and around the ship hull (body fitted grid).  The grid is locally orthogonal to the body
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