Page 71 - Theory and Design of Air Cushion Craft
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Practical formulae for  predicting air  cushion performance  55

                          5
                                 5
                                                                            45
                        3
                    ~ A)) ]°  =  (2°' r//z s)[l  +  (hj[2t  cos 9 + 2.75 ((//„  -  h s)/t  sin #)~°'  ]}] 05
            N[pJ(p c
                                                                   45  a5
                              X  {h s/[2t  cos 6 + 2.75 ((h b  -  /z s)/t sin 0)~°- ]}  (2.16)
          where m is the flow rate per  unit  air  curtain  length  and  N  the  lift  power  per unit  air
          curtain  area.
            While A. A. West's theory could be applied  to real craft  with a bag and finger skirt,
          the disadvantages  of  this approach would  be as follows:
          •  The assumption  made by West that the bag and finger type skirt may be simplified
             as  a  simple single wall skirt  and  the  air curtain jetted  from  a nozzle  stuck  to  the
             skirt finger does not  agree with  practice.
          •  The theory does not consider the effect  of viscosity of  air as a real fluid. Real flow
             conditions can be illustrated as in Fig. 2.5. Thanks to the viscosity of flow a lot of
             air  will be ingested from  the  atmosphere  into  the  air curtain  to  form  a  combined
             flow,  namely the curtain jet flow ra c which will separate into two curtains, one to the
             atmosphere and another  into the cushion.
          •  The theory does not consider the flow energy losses from nozzles in the bag. Clearly
             this is not reasonable for bag and finger skirts, though it is acceptable for open loop
             designs.
          •  It  is not  reasonable  to assume zero energy loss between the flow streamlines  AA'
             and  BB', i.e. losses in a two-dimensional jet  in  a real fluid as against  an  infinitely
             thin jet.


             2.3  Practical  formulae     for  predicting    air  cushion
                  performance

          The various  theories  described above to predict the static air cushion  performance  of
          craft  over ground,  have disadvantages as follows :
          •  The theory based  on a thin nozzle correlated  with experimental results in the early
             research stage  of hovercraft has precision  at large hover heights (clear  air gap),  but
             is not  realistic for small hovering heights, as is the case of  craft  with bag and  finger
             skirts. This  is because the air curtain jetted  from  under  segments or fingers will be
             distorted  by the proximity  of  the ground  and  the complex geometry  of  the finger
             itself.














          Fig.  2.5  Actual air streamlines  including air viscosity.
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