Page 229 - Process Modelling and Simulation With Finite Element Methods
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216        Process Modelling and Simulation with Finite Element Methods


                                     Re=-  PUD
                                            P

          This dimensionless  parameter  rolls the  influences  of  the  fluid  density  p, inlet
          velocity U, the diameter D, and viscosity p into one parameter that describes the
          dynamic  similarity  of  the  flow.  Thus  changes  in  the  pipe  diameter  for fully
          developed  flow  are  not  classed  as  geometric  variation,  but  rather  the  more
          common parametric variation.
             Just  as  in  the  last  chapter  where  examples  of  simulations  were  given  for
          stationary models and for transient models, in this chapter we will give examples
          of stationary geometric continuation and transient geometric continuation.  In the
          former, distinct models are solved with slightly different domains and  therefore
          different meshes.  Therefore the solutions are incompatible  (different degrees of
          freedom) from one geometric parameter  value to the next.  If the old solution is
          to be taken as the initial guess for new geometry, then mapping the old solution
          to the new domain in a consistent fashion must be done.  In the examples given
          here, the system of PDEs for the stationary models are linear, so the solution can
          be determined  directly in one FEM step.  Thus mapping  old  solutions onto the
          new  geometry  has  no  additional  value.   The  transient  problem,  however,
         involves  a problem  in  a  shrinking  domain  with  a  moving  front.  The domain
          changes after each time step, so the mapping of the solution at the old time step
          onto the  new  domain  is essential  to the model.  Consequently,  after each time
          step, re-meshing  must  be done as  well.  One class of  problem  where  this  is a
          crucial step is the free boundary problem.  Film flows and jet flows, for instance,
          are cases where the position of the boundary is intimately related to the solution
          of  the  velocity  field.  The  boundaries  should  be  located  wherever  the  stress
         balances are satisfied.
             The 2-D incompressible,  laminar Navier-Stokes  equations  can be solved by
          several standard means (finite difference, finite element, spectral element, lattice
          Boltzmann,  and  multigrid  techniques)  and  have  been  implemented  in  standard
          simulation  engines  commercially  with  fixed  boundary  conditions  and  complex
         geometries.  Standard computational fluid dynamics packages have two standard
         engines:  (1) the grid generator  to cater for complex geometry, and (2) the PDE
         engine, which can solve more general systems of transport equations that include
         the pressure  as in  the Navier-Stokes  equations  as a Lagrange  multiplier  for the
         continuity  equation.  These two  steps  are typically  conducted separately.  The
         grid  is  generated  initially,  and  thereafter  many  simulations  are  conducted.
         FEMLAB is no different in this respect.
             This paradigm for computational  fluid dynamics  does not  deal particularly
         well  with  free boundary  problems.  An iterative  scheme  for coupling  the flow
         solution  to  grid  generation  could  be  envisaged,  but  automation  with  standard
         packages  is  difficult  to  implement.  Ruschak  [l] described the  now  standard
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