Page 193 - Practical Ship Design
P. 193

Powering I                                                           159


         when the viscous or frictional components respectively of the model resistance are
         subtracted from the model total resistance to establish the respective residuary
         resistance coefficients, with the further change caused by the multiplication of the
         ship friction coefficient by the form factor being of lesser significance.
           An example with some figures may help to make the difference clear. A ship of

           L = 330 m, V = 300,000 m3, 15 knot speed, F, = 0.136  (V = volume of
                    displacement)

         was tested using a model with the following particulars:
           I  = 7 m, F, = 0.136, speed = 1.127 ds
           K from test = 0.33
           model R,  = 6.856 x lo6  ship R,  = 2.14 x lo9
           Ctm        = 4.309 x
           Cfm        = 3.203 x
           AC         = 0.10  10-~
            Car       = 0.05 x

         By the ITTC’57 method:
           Cr         = (4.309 - 3.203) x   = 1.106 x
           ct-\       = 1.39  10-~

            Ct,       = (1.39 + 0.10 + 1.106 + 0.05) x   = 2.646 x
           Proportion of frictional resistance   = (Cf\ + AC)/C,,
                                            = (1.39 + 0.10y2.646
                                            = 56%
         By the ITTC’78 method:
           Cr         = (4.309 - 1.33 x 3.203) x   = 0.05 x lo-’
            cv\       = (1.33 x 1.39 + 0.10) x   = 1.949 x
            Ct,       = (1.949 + 0.05 + 0.05) x   = 2.049 x
           Proportion of viscous resistance   = 1.949/2.049
                                            = 95%
         Apart from the change in the proportion of frictional/viscous resistance, the very
         large reduction in C,,, from 2.646 x   to 2.049 x   or 29% should be noted.
         This change in value is of course tied to the K value of 0.33 used in this example, a
         figure which appears to agree with Holtrop and Mennen’s formula given in 86.9.
           Although most tank authorities appear to have adopted the new method, others
         are sticking to the use of ITTC’57. Designers can only hope that there will shortly
         be an end to the succession of changes and variety of methods used by tanks which
         have caused them so much difficulty in the last two decades.
           This hope may, however, be a little premature as a  1993 R.I.N.A. paper by
         C.W.B.  Grigson  “An  accurate  smooth  friction  line  for  use  in  performance
   188   189   190   191   192   193   194   195   196   197   198