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Computational Details:

"Rotating propeller in a box for a low Reynolds number" Back to >>Rotating propeller in a box for a low Reynolds number<<


Description of the flow problem
Description of the spatial discretization
Description of the temporal discretization
Computer requirements
Mathematical details




Description of the flow problem

  • diameter of square: 0.6
  • length/width of propeller : 0.5/0.1
  • rotational speed of propeller : 0.5*PI
  • Dirichlet b.c.'s on propeller surface (= differentiation of the propeller speed)
  • Dirichlet b.c.'s for right inflow with horizontal speed -1
  • natural b.c.'s on the three outlets
  • other b.c.'s: zero velocity at walls of the square
  • initial condition at t=0: starting from rest
  • viscosity parameter: 1/nu=100




Description of the spatial discretization

  • coarse mesh (=level 1): 1 square !!!
  • equidistantly refined tensor product mesh of the square EVERYWHERE and for ALL TIME STEPS !!!
  • computation and visualization on level 8: 16,384 cells, 16,641 vertices, 82,432 d.o.f.`s
  • nonconforming nonparametric rotated bilinear fem's (meanvalue version), UPW




Description of the temporal discretization

  • equidistant time stepping for computation with k=0.00111112
  • equidistant time stepping for visualization with k= 0.02 (= 1 frame)
  • Total time T=5 seconds corresponds to 4,500 time steps
  • fractional step theta scheme




Computer requirements

  • date: 04/15/98
  • simulation by: S.Turek
  • visualization by: S.Turek
  • SUN ULTRA 45/250: 13 MB, 269,537 seconds
  • AVS data: 750 MB
  • Software: FEATFLOW1.1 + CC2D_MOVBC




Mathematical details

  • For more details about numerical and algorithmic aspects see the `Mathematical Background' in the FEATFLOW manual or visit our paper archive for much more details.
  • The problem-specific data for the applied software version including parameter files and input data can be downloaded here!




Please send any comments and suggestions to: featflow@featflow.de