An Attempt of Large Eddy Simulation (LES) for Combustor Modeling

Authors

  • Lei-Yong Jiang Gas Turbine Laboratory, Aerospace Research Center, the National Research Council of Canada, 1200 Montreal Road, M-10, Ottawa, Ontario, K1A 0R6, Canada.
  • Ian Campbell Gas Turbine Laboratory, Aerospace Research Center, the National Research Council of Canada, 1200 Montreal Road, M-10, Ottawa, Ontario, K1A 0R6, Canada.

DOI:

https://doi.org/10.9734/bpi/rder/v12/5303D

Keywords:

Large eddy simulation, turbulence modeling, combustion, combustor modeling, gas turbine, thermal boundary

Abstract

An attempt of large eddy simulation (LES) in a model combustor is performed, and a number of critical issues, such as grid size, incoming flow, wall boundary, physical sub-model and result sampling, are discussed. The computed results are compared with comprehensive experimental measurements, and illustrate that the mean axial velocity and temperature distributions inside the combustion chamber can be fairly well predicted by LES. However, for LES to become an accurate and cost-affordable tool for advanced combustion system development, some basic issues remain to be addressed and more validation studies are required. In addition, considerable computing power is needed in order to catch both low and high frequencies of flow motion in actual turbulent combustion systems.  

Published

2021-05-29

How to Cite

Lei-Yong Jiang, & Ian Campbell. (2021). An Attempt of Large Eddy Simulation (LES) for Combustor Modeling. Recent Developments in Engineering Research Vol. 12, 174–191. https://doi.org/10.9734/bpi/rder/v12/5303D