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July 14, 2023, 11:21
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Supersonic Shock Train Simulation
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#1 |
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New Member
Ashwin
Join Date: Jul 2023
Posts: 9
Rep Power: 2  |
Hello, I'm trying to simulate a shock train formed in a rectangular duct under supersonic conditions by referring a research paper.
Boundary Conditions - Pressure Inlet - Total Pressure= 310,000 Pa, Static Pressure= 16,535 Pa Total Temp = 289K Pressure Outlet - Static Pressure = 99,000 Pa. Density based solver, Ive tried k-epsilon and k-w sst. However, when I run the simulation, I'm unable to get a convergent solution and I am unable to replicate the results of the research paper. If anyone has done a similar simulation, could you please guide me? Thanks |
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December 7, 2023, 07:52
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#2 |
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New Member
Wenbin Bai
Join Date: Dec 2023
Posts: 1
Rep Power: 0 |
Can you produce the residual curves?
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| Tags |
| convergence, shock train, supersonic inlet |
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