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Overtip Pressure Measurements in a Cold-Flow Turbine Rig FREE

[+] Author Affiliations
R. C. Kingcombe, I. M. Smith, R. V. Steeden

Royal Aerospace Establishment, Pyestock, Farnborough, Hampshire, UK

Paper No. 90-GT-312, pp. V001T01A097; 8 pages
doi:10.1115/90-GT-312
From:
  • ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Brussels, Belgium, June 11–14, 1990
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7904-7
  • Copyright © 1990 by ASME

abstract

In shroudless axial turbines the flow over the tips of the rotor blades is complex and accounts for significant loss of efficiency. In order to investigate the structure of this overtip flow, a row of high frequency response miniature pressure transducers was mounted in the casing of a cold flow turbine rig in the region swept by the rotor tips.

Copyright © 1990 by ASME
This article is only available in the PDF format.

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