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Numerical Simulation as Design Optimization Tool for Gas Turbine Combustion Chambers

[+] Author Affiliations
Digvijay B. Kulshreshtha, Saurabh B. Dikshit

C. K. Pithawalla College of Engineering & Technology, Surat, GJ, India

S. A. Channiwala

S. V. National Institute of Technology, Surat, GJ, India

Paper No. GT2010-22889, pp. 737-746; 10 pages
doi:10.1115/GT2010-22889
From:
  • ASME Turbo Expo 2010: Power for Land, Sea, and Air
  • Volume 2: Combustion, Fuels and Emissions, Parts A and B
  • Glasgow, UK, June 14–18, 2010
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-4397-0 | eISBN: 978-0-7918-3872-3
  • Copyright © 2010 by ASME

abstract

In present study an attempt has been made through CFD approach using CFX 11 to analyze the flow patterns within the combustion liner and through different air admission holes, namely, primary zone, intermediate zone, dilution zone and wall cooling, and from these the temperature distribution in the liner and at walls as well as the temperature quality at the exit of the combustion chamber are predicted. The design optimization is carried out using the CFD results with validation using experimental investigations.

Copyright © 2010 by ASME

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