Numerical analysis of a swirl stabilized premixed combustor with the flamelet generated manifold approach

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Abstract

In this paper the effectiveness of LES for modeling premixed methane combustion will be investigated in the context of gas turbine modeling. The required reduction of the chemistry is provided by the flamelet generated manifold (FGM) approach of van Oijen (2002). For turbulence-chemistry interactions an algebraic model is used to calculate variations which are used to invoke a pre-assumed pdf, Vreman et al. (2009). The algebraic model has a tunable parameter.
Original languageEnglish
Title of host publicationProceedings of the Direct and Large-Eddy Simulation VIII (DLES8), 7-9 July 2010, Eindhoven, The Netherlands
Editorsxx H. Kuerten et al.
PublisherSpringer
Pages321-326
ISBN (Print)978-90-481-3651-3
DOIs
Publication statusPublished - 2011

Publication series

NameErcoftac Series
ISSN (Print)1382-4309

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