Numerical Analysis of a Swirl Stabilized Premixed Combustor with the Flamelet Generated Manifold approach

T. Cardoso de Souza, R.J.M. Bastiaans, B.J. Geurts, L.P.H. de Goey

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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 publicationDirect and Large-Eddy Simulation VIII
    EditorsHans Kuerten, Bernard Geurts, Vincenzo Armenio, Jochen Fröhlich
    Place of PublicationDordrecht
    PublisherSpringer
    Pages321-326
    Number of pages6
    ISBN (Electronic)978-94-007-2482-2
    ISBN (Print)978-94-007-2481-5
    DOIs
    Publication statusPublished - 2011
    Event8th ERCOFTAC Workshop on Direct and Large-Eddy Simulation VIII, DLES 2010 - Eindhoven University of Technology, Eindhoven, Netherlands
    Duration: 7 Jul 20109 Jul 2010
    Conference number: 8

    Publication series

    NameERCOFTAC series
    PublisherSpringer
    Volume15
    ISSN (Print)1382-4309

    Workshop

    Workshop8th ERCOFTAC Workshop on Direct and Large-Eddy Simulation VIII, DLES 2010
    Abbreviated titleDLES
    Country/TerritoryNetherlands
    CityEindhoven
    Period7/07/109/07/10

    Keywords

    • Axial velocity
    • Algebraic model
    • Progress variable
    • Dynamic smagorinsky model
    • Reaction progress variable

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