The Influence of the Relative Number of Impingement and Effusion Cooling Holes on Gas Turbine Combustor Wall Heat Transfer

El-Jummah, AM, Nazari, A, Andrews, GE orcid.org/0000-0002-8398-1363 et al. (1 more author) (2017) The Influence of the Relative Number of Impingement and Effusion Cooling Holes on Gas Turbine Combustor Wall Heat Transfer. In: Proceedings of 13th International Conference On Heat Transfer, Fluid Mechanics and Thermodynamics (HEFAT2017). 13th International Conference On Heat Transfer, Fluid Mechanics and Thermodynamics (HEFAT2017), 17-19 Jul 2017, Portoroz, Slovenia. , pp. 190-195.

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Authors/Creators:
Dates:
  • Published: 17 July 2017
  • Accepted: 5 June 2017
  • Published (online): 17 July 2017
Institution: The University of Leeds
Academic Units: The University of Leeds > Faculty of Engineering (Leeds) > School of Chemical & Process Engineering (Leeds)
Depositing User: Symplectic Publications
Date Deposited: 10 Aug 2017 10:38
Last Modified: 10 Aug 2017 10:49
Published Version: https://edas.info/showManuscript.php?m=1570346304&...
Status: Published

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