Page 100 - Theory and Design of Air Cushion Craft
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                       Steady             drag         forces









             3.1 Introduction


          ACVs  and  SESs  create  drag  forces  as  they  move  over  the  water  surface.  The  most
          important drag components are those due to friction with immersed components  such
          as sidewalls, skirt, propellers, rudders and  other appendages;  and  wave-making drag
          from  the  moving cushion pressure field and  sidewalls. In  addition, momentum  drag
          due  to  acceleration  of  the  air  used  for the  supporting  air cushion, and  aerodynamic
          profile drag of  the ACV or  SES become important components  at higher speeds.
            In  this  chapter  we  will  outline  the  theory  behind  these  drag  components  and
          describe methods for their estimation.



             3.2  Classification of  drag components


          The  method  of  calculating drag  forces  on  an  ACV or  SES is similar to  that  for  pre-
          dicting the drag  of  a planing hull  or  a  sea plane before  take-off.  ACVs and  SES also
          generate spray drag, skirt friction  drag and  skirt inertia drag in addition to the water
          drag components  associated with a normal ship. For this reason drag calculations are
          more complicated  than for other marine  craft.
            Based upon  calculation methods for predicting the drag of a planing hull, the prin-
          cipal author and  colleagues at MARIC have developed a methodology  for predicting
          the drag for ACV/SES which may be summarized as  follows:
          •  First  of  all we obtain  the total  drag  from  model  tests in a towing tank  and  some
             other  main components  of  drag  by means  of  reliable and  practical  methods, e.g.
             according to  the Reynolds analogue theory to  obtain  the test results in wind tun-
             nels for predicting  air  profile  drag.
          •  Then  the  residual  drag  of  models  can  be  determined  by  deducting  the  main
             components  of  drag  which can  be calculated  individually, from  the  total  drag  of
             the model measurements.

          According  to  Froude's  analogue theory we can  define  the  residual  drag  of  full-scale
          ships  from  that  of  models;  consequently  the  total  drag  for  a  full-scale ship  can  be
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