Detailed measurements have been taken of the three-dimensional velocity field within the vaneless diffuser of a backswept low speed centrifugal compressor using hot-wire anemometry. A 16 percent below and an 11 percent above design flow rate were used in the present study. Results at both flow rates show how the blade wake mixes out more rapidly than the passage wake. Strong secondary flows inherited from the impeller at the higher flow rate delay the mixing out of the circumferential velocity variations, but at both flow rates these circumferential variations are negligible at the last measurement station. The measured tangential/radial flow angle is used to recommend optimum values for the vaneless space and vane angle for design of a vaned diffuser.
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October 1995
Research Papers
Off-Design Flow Measurements in a Centrifugal Compressor Vaneless Diffuser
A. Pinarbasi,
A. Pinarbasi
Department of Mechanical Engineering, University of Cumhuriyet, Sivas, Turkey
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M. W. Johnson
M. W. Johnson
Department of Mechanical Engineering, University of Liverpool, Liverpool, United Kingdom
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A. Pinarbasi
Department of Mechanical Engineering, University of Cumhuriyet, Sivas, Turkey
M. W. Johnson
Department of Mechanical Engineering, University of Liverpool, Liverpool, United Kingdom
J. Turbomach. Oct 1995, 117(4): 602-608 (7 pages)
Published Online: October 1, 1995
Article history
Received:
February 4, 1994
Online:
January 29, 2008
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Citation
Pinarbasi, A., and Johnson, M. W. (October 1, 1995). "Off-Design Flow Measurements in a Centrifugal Compressor Vaneless Diffuser." ASME. J. Turbomach. October 1995; 117(4): 602–608. https://doi.org/10.1115/1.2836574
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