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September 8, 2012, 04:37 |
Appropriate LES cyclic mesh
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#1 |
Member
Hugh Ingham
Join Date: Aug 2012
Posts: 35
Rep Power: 14 |
Hi foamers,
I am conducting a LES simulation of a supersonic turbulent round jet and have some questions concerning my mesh. My domain is a converging-diverging nozzle protruding into the free-stream. I have reduced my domain to a 1/8th pipe and am using cyclic boundary conditions on the two side faces. However I have created my grid by sweeping a structured 2-D mesh through a wedge, which means that now at the centre-line I have a sharp point with very high aspect ratio cells. How do I best deal with the mesh at the centreline? I have subdivided the domain so that I have used tet prisms close to the centre axis and matched them with quad cells used for everywhere else. The mesh is shown below: meshpic.jpg Foam mesh.jpg mesh shot.jpg Am I restricted in the cells I choose because I am running LES? Is what I have done reasonable? Any help would be really appreciated. Thanks, Hugh |
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September 10, 2012, 03:14 |
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#2 |
Member
Hugh Ingham
Join Date: Aug 2012
Posts: 35
Rep Power: 14 |
Could anyone help me with this?
Thanks in advance |
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Tags |
les grid, les model, structured mesh |
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