A Numerical Investigation on the Volute/Diffuser Interaction due to the Axial Distortion at Impeller Exit
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Abstract A numerical simulation is performed on a single stage centrifugal compressor using the commercially available CFD software, CFX-TASCflow. The steady flow is obtained by circumferentially averaging the exit fluxes of the impeller. Three runs are made at design condition and off-design conditions. The predicted performance is in agreement with experimental data. The flow details inside the stationary components are investigated, resulting in a flow model describing the volute/diffuser interaction at design and off-design conditions. The recirculation and twin vortex structure are found to explain the volute loss increase at lower and higher mass flows, respectively.
2001 ◽
Vol 123
(3)
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pp. 475-483
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2011 ◽
Vol 189-193
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pp. 2362-2365
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2012 ◽
Vol 516-517
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pp. 634-637
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2012 ◽
Vol 256-259
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pp. 2543-2547
2012 ◽
Vol 232
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pp. 284-287
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2015 ◽
Vol 8
(3)
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pp. 347
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