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An Experimental Investigation of a Vortex Flow Cascade FREE

[+] Author Affiliations
Tang Yan-Ping, Chen Mao-Zhang

Beijing Institute of Aeronautics and Astronautics, Beijing, China

Paper No. 88-GT-265, pp. V001T01A095; 7 pages
doi:10.1115/88-GT-265
From:
  • ASME 1988 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Amsterdam, The Netherlands, June 6–9, 1988
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7918-4
  • Copyright © 1988 by ASME

abstract

A new type of compressor cascade, called the vortex flow cascade (shortly VFC), has been developed in the paper. The VFC is made up of the normal compressor cascade (shortly NCC) with NACA-65-0010 profile and vortex generator. Experiments are conducted for researching the effects of a large scale streamwise control vortex on the flow structure inside cascade passage. The results are encouraging. Based on the present investigation the vortical flow pattern and loss mechanism of VFC have been discussed.

Copyright © 1988 by ASME
This article is only available in the PDF format.

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