Page 150 - Theory and Design of Air Cushion Craft
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Effect  of various factors on drag  133


















                                  2         3         4         5
                                          v(m/s)

           Fig. 3.48  Influence of cushion length/beam  ratio on total drag of craft models in different test tanks.  1: tests in
           MARIC pj(  =  20; 2: same model, thicker skirt, different tank; 3: as 2, pj(  =  15.7; 4: as 3, but in MARIC tank.

                         fl(x9.8N)
                                                      r

                                                    /
                       10
                              A  \             //

                                           ^ ^^
                                                         if
                                                                 "^
                                                           i
                              •  '      Vr~~''         ^-| i i i i i i n i i
                                                        _\
                                                         \
                                                         W      n
                                                   t t
                                                 (mm)  (X9.8N)  (r/min)
                                               -   60   87.8  10000
                            /            -— O -—  40    87.8  10000

                          /              —A---    20    87.8  10000





           Fig. 3.49  Influence of  inner draft of sidewalls (on total  drag of  SES model on still water.



           Effect  of  air flow  rate
           It  is probable  that  the  air  flow  coefficient  Q  magnitude  will  not  affect  the take-off
          performance  of  hovercraft  (except  too  small  values  of  Q)  when  the  skirt  has  been
          carefully  designed, because of  the  good wave-yielding performance for flexible skirts.
           However,  craft  drag  at  post-hump  speeds  will be  closely  related  to  Q. Therefore,  the
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