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Transonic flow, 2D compressor blade

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Old   August 15, 2022, 13:17
Default Transonic flow, 2D compressor blade
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Panov Dmitrii
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Hi all,
I am trying to calculate transonic flow around the 2D compressor blade. And i'm stuck: solver crashing or solution don't convergence. I tried roSimpleFoam and roPimpleFoam. Are there better solvers for such type of transonic flow? I will also be grateful if someone can share experience in calculating the transonic flow in a compressor using standard OpenFOAM solvers.
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Old   August 15, 2022, 13:33
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Domenico Lahaye
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Convergence of rhoS/PimpleFoam is indeed delicate.

We found boundary condition settings crucial.

How are you setting boundary conditions for pressure, density and temperature on the inlet and outlet patches?
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Old   August 18, 2022, 05:37
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Panov Dmitrii
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Hello, Domenico
Thank you for your reply and a fresh look at the problem. I changed the fixed values BC to total pressure and velocity direction and now everything works. I jast tried to get solution for stall rigion. This is validation case so i will share results when will get.
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Old   August 18, 2022, 08:02
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Wonderful! Well done! I look forward to seeing your results.
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