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Computer Predictions of Erosion Damage in Gas Turbines PUBLIC ACCESS

[+] Author Affiliations
A. F. Abdel Azim El-Sayed

Zagazig University, Zagazig, Egypt

A. Brown

Royal Military College of Science, Swindon, Wilts, UK

Paper No. 87-GT-127, pp. V003T05A004; 8 pages
doi:10.1115/87-GT-127
From:
  • ASME 1987 International Gas Turbine Conference and Exhibition
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Anaheim, California, USA, May 31–June 4, 1987
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7925-2
  • Copyright © 1987 by ASME

abstract

In this article an iterative procedure is presented for estimating erosion in axial gas turbine blades. The procedure is applied to a two stage turbine and the erosion is estimated for a 12,000 hour engine running time. The effect of the erosion on engine performance is estimated through changes in pressure coefficient distribution around a blade section.

Copyright © 1987 by ASME
This article is only available in the PDF format.

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