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             differences between  CF and  Cy"' apparent  in  Fig.  2  demonstrate the  importance of  selecting
             favorable hull arrangements.  Indeed, Fig. 2 shows that the ratio,  C,"  / C,-   , approximately varies
             between  2 and 6 within the speed range  considered.  Fig.  2 also shows that the wave-drag  curve,
             CT"'(F) , is  significantly  lower  than  the  curve  CT"'(F)  corresponding  to  the  worst  hull
             arrangements, and even the curve corresponding to the no-interference wave  drag Ci +2Ci, over
             most  of  the  speed  range.   In  fact,  the  curve  C,""'(F)  is  remarkably  close  to  the  curve
             Cp (F) corresponding to the best hull arrangement at every speed, over a broad speed range.
                         40 -
                       3 ::.       - Cw m  t arrangements
                         35 '
                        8 20.
                        8 15.
                         10.
                         05.
                         00  1


                            Figure 2: Wave drag coefficient for different hull arrangements
             The second design problem considered here consists of two steps.  The optimal center and outer hull
             forms are determined independently in the first step using present optimization technique. The center
             and outer hulls of the original wave cancellation multihull ship are used,  respectively, as starting
             baseline hulls in the optimization cycles.  During the optimization process, each hull keeps the same
             displacement as the original design while the wave drag is minimized. There are 76 design variables
             for the center hull  and  64 for the outer hull.  Four design  cycles are required  for each  hull  form
             optimization.

             The optimal center hull (A)  is obtained by minimizing Ci (F) for one Froude number, F=0.5, and the
             optimal center hull (B) is obtained by minimizing Cg(F)for five values of Froude number, F=0.3,
             0,35, 0.4,  0.45,  0.5.  Fig.  3a depicts the predicted  wave-drag-coefficient curves corresponding to
             theoriginal center hull and two optimal center hulls.  Fig. 3a indicates that the wave drag associated
             with the optimal center hull (A)  is reduced tremendously in comparison to the original center hull when
             the Froude number is above 0.4. However, the wave drag is increased slightly at lower Froude

                  1.4                                 1.4
                  1.2                                 1.2
                      +Cw  optid canter hull (A)
                  1.0                                 1.0
                g 0.8                               8 0.8
                -                                   -  0.6
                                                    0
                g 0.6
                  0.4                                 0.4
                  0.2                                 0.2
                  0.0                                 0.0
                   02   025   03   035   04   045   05   055   02   025   03   035   04   045   05   055
                              Froude number                        Froude number
                            Figure 3: Wave drag coefficient for original and optimal hulls
             numbers. Fig.  3a also indicates that the wave drag associated with the optimal center hull  (B) is
             reduced over almost the entire speed range in comparison to the original center hull.  As expected, the
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