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Prediction of Gas Turbine Combustor-Liner Temperature PUBLIC ACCESS

[+] Author Affiliations
Yousef S. H. Najjar, Riad M. Droubi

King Abdulaziz University, Jeddah, Saudi Arabia

Paper No. 87-GT-177, pp. V003T06A025; 6 pages
doi:10.1115/87-GT-177
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

Broadening of fuel specifications decreases the hydrogen content and increases the aromatics and final boiling point. The cumulative effect will be an increase in soot formation hence flame radiation which affects flame tube durability.

In this work an analytical study is made where empirical formulae are developed for luminosity, radiation and convection at idle and full load conditions. These equations predict combustor liner temperature with high degree of agreement with previous experimental work.

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

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