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Compressible

                 «fctf      Navier-Stokes                  Equations

















         12.1  Introduction

         The  compressible  Navier-Stokes  equations  represent  the  highest  level  of  math-
         ematical  modeling  for  describing  aerodynamic  flows  commonly  used  in  engi-
         neering  applications.  These  include:  the  aerodynamic  flow  around  aircraft,  the
         internal  flow  occurring  in  turbomachinery;  the  flow  developing  in  ducts  in  the
         presence  of  heat  transfer;  or  a  combination  of  these  such  as  the  external  aero-
         dynamic  flow  impinging  on  a  wing  leading  edge  surface  heated  by  internal  hot
         air  emanating  from  the  engine  compressor  stages  to  avoid  ice  accumulation.
            The  methods  developed  by the  research  community  for  the  solution  of  these
         equations  for  specific  applications  have  been  building  on  the  advances  made  on
         solving  the  simplified  forms  of  the  equations,  since  the  compressible  Navier-
         Stokes  equations  do  not  introduce  fundamentally  different  flow  characteristics.
         Analysis  of these  equations  shows that  their  types  are  a mix  of  all types  studied
         in  the  previous  chapters.  Since  the  viscous  terms  transform  the  inviscid  first-
         order partial  differential  equations into second-order, the momentum  and  energy
         equations  are  parabolic  in  time  and  space,  but  elliptic  in  space  when  steady
         state  conditions  are  reached.  The  continuity  equation  is,  however,  hyperbolic
         in  space  and  time.  Therefore,  since  the  methods  for  addressing  each  of  these
         issues  have  been  discussed  in  the  previous  chapters,  emphasis  is  placed  on  the
         specific  difficulties  associated  with the  engineering  applications  of the  Reynolds-
         Averaged  compressible  Navier-Stokes  equations  in  this  chapter  (Section  12.2)
         and  their  methods  of  solution.  In  particular,  the  MacCormack  scheme  adapted
         for  viscous  flows  is  discussed  in  Section  12.3,  the  Beam-Warming  method  in
         Section  12.4  and  the  finite-volume  method  in  Section  12.5. Application  on  the
         model  problem  of  Section  11.5, that  is the  sudden  expansion  laminar  duct  flow,
         is discussed  in  Section  12.6  along with  the  detailed  description  of the  computer
         programs  given  in  Appendix  B.
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