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Experimental Investigations of Pressure Drop in the Combustion Chamber of Gas Turbine FREE

[+] Author Affiliations
Marek Dzida, Krzysztof Kosowski

Technical University of Gdańsk, Poland

Paper No. 89-GT-247, pp. V003T06A001; 4 pages
doi:10.1115/89-GT-247
From:
  • ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications
  • Toronto, Ontario, Canada, June 4–8, 1989
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7915-3
  • Copyright © 1989 by ASME

abstract

In bibliography we can find many methods of determining pressure drop in the combustion chambers of gas turbines, but there is only very few data of experimental results.

This article presents the experimental investigations of pressure drop in the combustion chamber over a wide range of part-load performances (from minimal power up to take-off power). Our research was carried out on an aircraft gas turbine of small output. The experimental results have proved that relative pressure drop changes with respect to fuel flow over the whole range of operating conditions. The results were then compared with theoretical methods.

Copyright © 1989 by ASME
This article is only available in the PDF format.

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