Transonic 2-D Stage (turbomachinery case) #2301
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safdarianebi
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Are you defining two boundary conditions on the same boundary? |
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I am trying to simulate a 2-D transonic turbomachinery stage. And, the inlet mach number is equal to 1.2. I am using MARKER_GILES and MARKER_SUPERSONIC_INLET boundary conditions. My simulation converges perfectly, but the final result is not satisfying as inflow mach number is 0.4.
I don't know what is wrong, and I would be grateful if you could help me solve this problem.
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