Page 200 - Practical Ship Design
P. 200

166                                                            Chapter 6


                (1 + x) =  ship-model  correlation factor, if not already included in
                          Pe(naked) (see 56.2)
                A=        additional resistance of appendages expressed as a fraction of
                          the naked resistance (bilge keels, stabilisers, bow thrust tunnels,
                          twin rudders, shaft brackets, bossings, etc.; see also 57.3).

             (ii) Quasi-propulsive eficiency qd
             This is made up of the open water propeller efficiency qo, the relative rotative
             efficiency qr, and the hull efficiency qh.
                qd = qo  qr  qh                                                (6.21)

             qh in turn is made up from the thrust deduction and wake factors as follows:
                     1-t
                qh =-                                                          (6.22)
                     1 - w,

              where
                                         T-R
                t = thrust deduction factor = -                                (6.23)
                                           T
              and
                                         v -v,
                w, = Taylor wake fraction = -                                 (6.23a)
                                           V
              T = thrust and R = resistance
              V = ship speed and V, = speed of advance.

                An approximate value of qd, derived by Emerson is
                            -
                         NJL
                qd =K--                                                        (6.24)
                         10000

              where N is propeller RPM and K is a constant, originally given as 0.83, but which
              should probably be increased to 0.84 for single-screw ships with today’s more
              efficient propellers. (See 57.5 for a discussion about this formula.)

              (iii) Delivered horsepower Pd

              This is the power at the propeller and is given by the formula

                    ‘e(]>
                Pd =-                                                          (6.25)
                      qd
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