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A strange problem in supersonic NS simulation

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Old   December 11, 2014, 04:23
Smile A strange problem in supersonic NS simulation
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Ying Zhuying
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Hello,everyone!
Recently, I have a strange problem in supersonic NS simulation with SU2. It is a 2Ma 2D wedge. Turbulence model is SA. I set farfield, NS_wall, outlet boundary condition. The pressure contour of result shows strange at the two junctions place --farfield and NS_wall, outlet and NS_wall.
Below is my grid and SU2 configuration file, contour of the result.
Appreciate any reply!
Attached Images
File Type: gif P_Contour.gif (33.4 KB, 30 views)
File Type: gif Ma_Contour.gif (39.8 KB, 20 views)
File Type: gif T_Contour.gif (28.0 KB, 18 views)
Attached Files
File Type: txt wedge_turb_2Ma.txt (9.4 KB, 16 views)
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Old   December 26, 2014, 06:00
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szhuang
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Quote:
Originally Posted by zylanboluo View Post
Hello,everyone!
Recently, I have a strange problem in supersonic NS simulation with SU2. It is a 2Ma 2D wedge. Turbulence model is SA. I set farfield, NS_wall, outlet boundary condition. The pressure contour of result shows strange at the two junctions place --farfield and NS_wall, outlet and NS_wall.
Below is my grid and SU2 configuration file, contour of the result.
Appreciate any reply!
I have the same problem, if you have solved this problem , can you tell me ? thank you .
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Old   December 29, 2014, 13:02
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Frederik
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It looks like you are simulating a bump instead of a wedge; you might want to recheck your boundary conditions...
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Old   December 29, 2014, 20:29
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The boundary condition is set as: the lower boundary--wall; the upper and left boundary--farfield; the right boundary--outlet.
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Old   December 30, 2014, 09:44
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Frederik
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Originally Posted by zylanboluo View Post
The boundary condition is set as: the lower boundary--wall; the upper and left boundary--farfield; the right boundary--outlet.
Exactly... shouldn't you use a symmetry/slipwall if you want to simulate a wedge instead of a bump (there's a difference between the two).
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