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Experimental and Computational Study of a Radial Compressor Inlet FREE

[+] Author Affiliations
Jay M. Koch, Peter N. Chow

Dresser-Rand, Olean, NY

Brad R. Hutchinson, Steve R. Elias

Advanced Scientific Computing, Waterloo, ON, Canada

Paper No. 95-GT-082, pp. V001T01A014; 10 pages
doi:10.1115/95-GT-082
From:
  • ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Houston, Texas, USA, June 5–8, 1995
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7878-1
  • Copyright © 1995 by ASME

abstract

Flow field measurements and flow visualization for a quarter scale model of a radial compressor inlet are presented for varying flow rates and inlet profiles. Non-uniform inlet profiles are created using a 90° bend directly upstream of the inlet. Experimental results are compared with the CFD analysis from a commercial 3-D Navier Stokes code. The experimental and computational results show good agreement, even in regions of reverse flow. The results from this study show CFD analysis can be used with confidence to predict the performance of radial compressor inlets.

Copyright © 1995 by ASME
Topics: Compressors
This article is only available in the PDF format.

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