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1.5  Aerodynamics  of  Ground-Based  Vehicles                          37



         of  turbulence  models  (Chapter  3,  [15,16]).  Much  work  remains  to  be  done  in
         the  calibration  and  tailoring  of turbulence  models  for  vehicle  application  before
         results  of  consistent  accuracy  can  be  obtained.
            The direct  numerical  simulation  (DNS)  is the  next  approach  employed  in  the
         application  of CFD  to  vehicle aerodynamics  (see Fig.  1.35). The  accuracy  of  the
         results obtained  with this approach  is about  the accuracy  of the results  obtained
         with  the  RANS  approach;  that  is, drag  prediction  is  within  five  percent.  With
         almost  10 6  grid  points  for  a  half  model,  DNS  has  been  able  to  discriminate  the
         effect  of  several  aerodynamic  devices  (spoilers,  flaps)  on  the  drag  and  lift  of  a
         sports  car  (Fig.  1.36).  Grid  generation  (Chapter  9)  is said  to  require  only  three
         days,  and  CPU-time  for  a  single  configuration  requires  between  10 to  20  hours
         on  a  supercomputer.
            The  other  approach  used  in  applying  CFD  to  vehicle  aerodynamics  is to  use
         zonal  methods  in  which  the  near  field  calculations  performed  with  the  Navier-
         Stokes  equations  are  patched  to  the  rest  of  the  flowfield  calculations  obtained
         with  inviscid  flow  and  boundary-layer  equations.
            CFD  is  also  useful  in  calculating  internal  flows  such  as  in  ducts  connected
         to the  radiator  and  air  conditioning  units. Another  interesting  area  is the  venti-
         lation  and  heat  balance  of the  passenger  compartment.  The  internal  flow  calcu-
         lations  are  not  in  general  performed  to  the  same  accuracy  required  in  the  drag
         calculations,  but  the  requirements  for  these  calculations  cannot  be  relaxed  too
         much  since  the  internal  flow  produces  its  own  drag  component.























            0.1



             10°  20*  30°  40°  50°   60°  70°  80°  90°
                                           a
         Fig.  1.35.  Drag  versus  rear  slant  angle  a  computed  with  a  DNS  code  and  compared  to
         measurements  at  the  same  Reynolds  number  [29].
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