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Analytical and Experimental Determination of Tip Clearance Effects in a High Work Turbine Rotor PUBLIC ACCESS

[+] Author Affiliations
Jong-Shang Liu, George Minkkinen, Riccardo Bozzola

Textron Lycoming, Stratford, CT

Paper No. 91-GT-197, pp. V001T01A074; 6 pages
doi:10.1115/91-GT-197
From:
  • ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Orlando, Florida, USA, June 3–6, 1991
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7898-9
  • Copyright © 1991 by ASME

abstract

Analytical and experimental investigations were conducted to study important tip clearance flow phenomena, such as leakage vortex, flow underturning, and the effect of clearance flow on blade loading and losses. A three-dimensional Navier-Stokes code was modified to include a tip clearance model. A recently designed transonic high-work turbine rotor was used as a test case. Detailed measurements were made at rotor inlet and exit planes and compared to analytical results. The comparisons included important design features, such as exit total pressure and flow angle. For tip clearance calculation, the agreement with data was improved in the near-tip region compared to calculation without tip clearance. The clearance flow phenomena, leakage vortex, flow underturning, changing of blade loading, and loss distribution were predicted.

Copyright © 1991 by ASME
This article is only available in the PDF format.

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