Computational Details:

Study of 'Delta Wing in Square Domain'

• squared domain of length 30
• one wing is located at (0,0)  connecting the vertices (-0.5,0),(0.5,-0.5),(0,0),(0.5,0.5)
• inflow : constant velocity 1 at the left  i.e in between x=-10, y= -7.5 and x=-10, y=7.7
• outflow : 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 1): 124 cells, 142 vertices, 656 d.o.f.`s
  

  
  
  

• uniform refinements with exact boundary adaption
• visualization on level 4: 7,936 cells, 8,080 vertices, 39,968 d.o.f.`s
• computational mesh on level 4: 7,936 cells, 8,080 vertices, 39,968 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: 03/15/2004
• simulation by :Madamanchi Dharmendra Mani
• visualization by: Madamanchi Dharmendra Mani
• SUN ULTRA1/140: 7.38 MB, 45,682 seconds
• GMV data: 1,377 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!