Computational Details:

Study of 'Delta Wing in a Square Domain'

• squared domain of length 30
  
• one Wing plane is located at x = 0, y = 0
  
• inflow b.c.'s: constant velocity 1 at the left i.e in between x=-10, y=-7.5 and x=10, y=7.7
• outflow b.c's: unknown at the right  i.e. in between x=20, y=-7.5 and x=20, y=7.7
• Other b.c.'s: zero velocity at the fixed walls
• initial condition at t=0: starting from rest
• viscosity parameter: 1/nu=1,000

• coarse mesh (=level 2): 104 cells, 122 vertices, 556 d.o.f.`s
  

  
  
  

• uniform refinements with exact boundary adaption
• visualization on level 4: 6656 cells, 6800 vertices, 33,568 d.o.f.`s
• computational mesh on level 4: 6656 cells, 6800 vertices, 33,568 d.o.f.`s
• nonconforming nonparametric rotated bilinear fem's (meanvalue version), UPW

• equidistant time stepping for computation with k=0.01
• equidistant time stepping for visualization with k=0.25 (= 1 frame)
• Total time T=30 corresponds to 3,000 time steps
• fractional step theta scheme

• date: 03/19/2004
• simulation by: Raj Kiran Kumar  Murala
  
• visualization by: Raj Kiran Kumar Murala
  
• SUN ULTRA1/140: 5.72 MB, 821 seconds
• GMV data: 143.5 MB
• Software: FEATFLOW1.2 + BOUSS

• 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!