Page 63 - Theory and Design of Air Cushion Craft
P. 63

SES  and  ACV  design  47

          directly  by a  small over-pressure of  the  air contained  in the cushion.  Our first aim is
          to understand  what  defines the requirements for cushion air flow and  pressure.
            By  reducing  the  contact  area,  drag  is reduced.  The  air  cushion  interacts  with  the
          water surface in a similar way to the classic potential theory developed by Lamb  [208] in
          the  1930s. In addition, flexible skirts, and the momentum of the cushion air, introduce
          drag components.  Once  the  means  is available  to  estimate  drag  as  well  as  the  static
          forces  on  an air cushion,  stability, trim and  manoeuvrability  can be investigated.
            Skirts  are generally considered  as a separate  element for analysis, though  they can
          influence  craft  performance,  particularly  instabilities  such  as  tuck  under  which may
          lead  to  'plough-in', and  skirt  bounce.
            SES and ACV motions  are complicated by the influence of the air cushion  pressure
          variations on the water surface, and  resulting variations of  dynamic trim. We present
          non-linear  analysis methods  for  solving the  equations  of  motion  in this text, as  this
          approach  gives the most  accurate means for estimation.
            In  the  same  way as for  ships,  it  is often  easier  to  carry  out  model  tests  than  theo-
          retical  analyses, to  determine  some  of  the  design parameters  needed.  SES and  ACV
          model  testing needs  careful  interpretation,  since  responses  which  are  susceptible  to
          different  scaling laws (Froude and Reynolds) both have a significant  effect  on the total
          response.  Recommendations  are discussed in Chapter 9.
            The  Design  Methodology  section  of  this  book  begins with  a  review of  the  basic
          design requirements, including rules and regulations which have to be met. This is fol-
          lowed by a discussion  on the  estimating methods  to determine principal  dimensions.
          Once these have been  estimated,  the craft  can  be developed  first  by designing the  lift
          system, the skirt, the hull structure and propulsion  system. Main engines can then be
          formally  selected,  and  after  optimization  of  the  main  dimensions, consideration  can
          be given to the craft  systems and  controls,  and  internal outfit.
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