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

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Samenvatting

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.
Originele taal-2Engels
TitelProceedings of the Direct and Large-Eddy Simulation VIII (DLES8), 7-9 July 2010, Eindhoven, The Netherlands
Redacteurenxx H. Kuerten et al.
UitgeverijSpringer
Pagina's321-326
ISBN van geprinte versie978-90-481-3651-3
DOI's
StatusGepubliceerd - 2011

Publicatie series

NaamErcoftac Series
ISSN van geprinte versie1382-4309

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