Computational Details:

'Delta Wing in a Square Domain'

• squared domian length30
• one wing plane is  located at x=0,y=0
• inflow b.c.'s: constant velocity 1 at the left bottom edge i.e in between x=-10, y=-7.5 and x=10, y=7.7
• outflow b.c's: unknown at the right top edge 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 1): 129 cells, 148 vertices, 683 d.o.f.`s
  

  
  
  

• uniform refinements with exact boundary adaption
• visualization on level 4: 8256 cells, 8408 vertices, 41,584 d.o.f.`s
• computational mesh on level 4: 8256 cells, 8408 vertices, 41,584 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: 05/13/2004
• simulation by: Katneni Ajay Kumar
• visualization by:Katneni Ajay Kumar
• SUN ULTRA1/140: 6.93 MB,  42529 seconds
• GMV data: 1289 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!