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May 21, 2020, 18:09
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Inlet Profile for Supersonic Flow
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#1 |
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New Member
Join Date: May 2020
Posts: 7
Rep Power: 7  |
How can I implement an inlet profile for a 2D supersonic flow? I am running a compressible, RANS-SA Mach 5 flow in SU2 v6.2 and would like to use an inlet profile to impose an incoming boundary layer. However, I am using a supersonic inlet and the SU2 Laminar Backward-facing Step tutorial uses a normal inlet. Can I implement an inlet profile if I am using a supersonic inlet?
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May 21, 2020, 18:46
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#2 |
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Senior Member
Pedro Gomes
Join Date: Dec 2017
Posts: 467
Rep Power: 15 |
No, you would have to modify some code for that.
Also the supersonic inlet is purely convective, it does not account for diffusion terms. |
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