Off-Design Flow Measurements in a Centrifugal Compressor Vaneless Diffuser

[+] Author and Article Information
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 117(4), 602-608 (Oct 01, 1995) (7 pages) doi:10.1115/1.2836574 History: Received February 04, 1994; Online January 29, 2008


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.

Copyright © 1995 by The American Society of Mechanical Engineers
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In