Page 102 - Theory and Design of Air Cushion Craft
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Steady drag forces

                33   Air  cushion  wave-making drag       (RJ


             Wave-making drag generated by a pressure distribution is a classical theme of  hydro-
              dynamics, since a ship's hull is generally represented by a surface consisting of  a vary-
             ing  potential  function  which  applies  positive  pressure  in  the  forebody  and  suction
             pressure around  the stern  [8,17].
               The equivalent problem for a hovercraft was addressed  by Newman  and  Poole [18],
             who  derived  a  calculation  method  for  predicting  the  wave-making drag.  They  sim-
             plified  the  air  cushion  to  an  equivalent  rectangular  surface with a uniform  pressure
             distribution  and calculated  the wave-making drag as
                                                   .  7
                                                   PC-'
                                                  [(P w.g)\                      (3.1)
             where
                                        Cl  =  f  (F r  and
             and  R^  is  the  wave-making  drag  due  to  air  cushion,  (N),  p c  the  cushion  pressure
             (N/m  ), B c the cushion beam,  (m), c the cushion length (m), p w  the water mass density
                                          l
                                     4
                                                                             2
                                  2
             (0.10177  -  0.1045)  (N s /m ), g the gravitational acceleration  (9.8066)(m/s ) and  C w
             the wave-making drag coefficient  due to the air cushion  travelling on a waterway with
             infinite depth,  as shown in Fig.  3.2.
               Figure  3.2  shows that  as  cushion  length  is increased,  so  the  primary  hump  at  F r
             approx.  0.56 reduces. Craft with IJB C  in the range 2-A have a significantly  higher drag
             peak  at  F r  approx.  0.33, so thrust margin  at this speed  should also  be checked during
             design.  Figure  3.3 shows the  variation  of  C w  against  IJB C  for  various  F r,  interpreted
             from  Fig.  3.2. It can  be seen that below  IJB C  of  about  6, the primary drag hump  at  F r
             0.56  begins to build up. Figure 3.4 shows plots of  C w vs F r for selected  IJB C,  taken from
             Fig.  3.3.
               It  is important  to  note  here  that  wave-making drag  is proportional  to  p c  and  the
             cushion  width. Craft  drag  can  therefore be  significantly  reduced  by  increasing  craft
             length. This  was used  successfully  by BHC  in stretching the  SR.N6 craft  in the  UK,
             and  the US Navy SES-100 to  SES-200.
               In fact, the wave-making drag  can be defined  as
                                       ^w     ^w     .
                                           =      =  sin  a                      (3.2)
                                      P CS C  W
             where a—a'  is the  average slope  of  the  wave generated by a moving air cushion.  This
             is most suitable for a cushion moving at high F r, generating a wave, rather  longer than
             cushion length.
               Meanwhile, equation  (3.1) can  also  be written as



                                         ~  C^vu


                                                                                    3) --v
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