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Flow Separation in GE frame 9 Compressor CFD simulation

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Old   October 23, 2017, 14:54
Question Flow Separation in GE frame 9 Compressor CFD simulation
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i man
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Has anybody simulated GE frame 9 Compressor? I had simulated this 17th stages compressor with the CFX; when I used a coarse mesh with y+=30 and k-w turbulence model, there is no problem in convergence and everything in CFD-POST is fine. But when it comes to simulating with a fine mesh, y+=1 and SST turbulence model; Inlet mass decreases and post-process show a big region of flow separation near the leading edge close to the hub. Can anybody give me any tips?
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Old   October 27, 2017, 11:35
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Typically, certain flow effects are not captured on coarse mesh. They are smeared over the cell volume. Separation at the hub is a problem. Try to eliminate/isolate the problem and simulate the stage with different boundary conditions (reduce discharge pressure, or mass for example). See if the separation is still present.

Frankly, I do not have experience with that particular frame.

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