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The Effect of the Reynolds Number on the Three-Dimensional Flow in a Straight Compressor Cascade FREE

[+] Author Affiliations
Václav Cyrus

The National Research Institute for Machine Design (SVÚSS), Prague, Czechoslovakia

Paper No. 88-GT-269, pp. V001T01A096; 9 pages
doi:10.1115/88-GT-269
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 straight compressor cascade of aspect ratio 2 was tested in a low speed tunnel within Reynolds number Re1 = 45 000 – 150 000 and inlet flow angle α1 = 35° – 48°. The profile of the blade was NACA 65-12-10. The purpose of the paper was to obtain data on three–dimensional flow in a straight cascade at low Reynolds numbers. Some experimental results on secondary flow have been made into simple correlation relations.

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

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