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Three-Dimensional Effects in Supersonic and Transonic Compressor Rotors: An Experimental and Computational Study PUBLIC ACCESS

[+] Author Affiliations
K. D. Broichhausen, H. E. Gallus

Technical University Aachen, West Germany

Paper No. 82-GT-276, pp. V001T01A092; 10 pages
doi:10.1115/82-GT-276
From:
  • ASME 1982 International Gas Turbine Conference and Exhibit
  • Volume 1: Turbomachinery
  • London, England, April 18–22, 1982
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7956-6
  • Copyright © 1982 by ASME

abstract

A computation method for the three-dimensional rotational flow through transonic and supersonic rotors is described and discussed by means of a comparison with experimental results. The computation treats subsonic and supersonic flows with different algorithms. The compression shocks are calculated as real three-dimensional discontinuities on the basis of the Rankine-Hugoniot-equations. The experimental data result from measurements in transonic and supersonic compressor rotors. A comparison of the data shows to what extent these three-dimensional effects are covered by the described theory.

Copyright © 1982 by ASME
Topics: Compressors , Rotors
This article is only available in the PDF format.

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