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. Goey, de

doi:10.1007/978-94-007-2482-2_51

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. Goey, de

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

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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 language	English
Title of host publication	Proceedings of the Direct and Large-Eddy Simulation VIII (DLES8), 7-9 July 2010, Eindhoven, The Netherlands
Editors	xx H. Kuerten et al.
Publisher	Springer
Pages	321-326
ISBN (Print)	978-90-481-3651-3
DOIs	https://doi.org/10.1007/978-94-007-2482-2_51
Publication status	Published - 2011

Publication series

Name	Ercoftac Series
ISSN (Print)	1382-4309

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10.1007/978-94-007-2482-2_51

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Cardoso de Souza, T., Bastiaans, R. J. M., Geurts, B. J., & Goey, de, L. P. H. (2011). Numerical analysis of a swirl stabilized premixed combustor with the flamelet generated manifold approach. In X. H. Kuerten et al. (Ed.), Proceedings of the Direct and Large-Eddy Simulation VIII (DLES8), 7-9 July 2010, Eindhoven, The Netherlands (pp. 321-326). (Ercoftac Series). Springer. https://doi.org/10.1007/978-94-007-2482-2_51

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title = "Numerical analysis of a swirl stabilized premixed combustor with the flamelet generated manifold approach",

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.",

author = "{Cardoso de Souza}, T. and R.J.M. Bastiaans and B.J. Geurts and {Goey, de}, L.P.H.",

year = "2011",

doi = "10.1007/978-94-007-2482-2_51",

language = "English",

isbn = "978-90-481-3651-3",

series = "Ercoftac Series",

publisher = "Springer",

pages = "321--326",

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booktitle = "Proceedings of the Direct and Large-Eddy Simulation VIII (DLES8), 7-9 July 2010, Eindhoven, The Netherlands",

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}

Cardoso de Souza, T, Bastiaans, RJM , Geurts, BJ & Goey, de, LPH 2011, Numerical analysis of a swirl stabilized premixed combustor with the flamelet generated manifold approach. in X H. Kuerten et al. (ed.), Proceedings of the Direct and Large-Eddy Simulation VIII (DLES8), 7-9 July 2010, Eindhoven, The Netherlands. Ercoftac Series, Springer, pp. 321-326. https://doi.org/10.1007/978-94-007-2482-2_51

Numerical analysis of a swirl stabilized premixed combustor with the flamelet generated manifold approach. / Cardoso de Souza, T.; Bastiaans, R.J.M.; Geurts, B.J. et al.
Proceedings of the Direct and Large-Eddy Simulation VIII (DLES8), 7-9 July 2010, Eindhoven, The Netherlands. ed. / xx H. Kuerten et al. Springer, 2011. p. 321-326 (Ercoftac Series).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

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N2 - 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.

AB - 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.

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BT - Proceedings of the Direct and Large-Eddy Simulation VIII (DLES8), 7-9 July 2010, Eindhoven, The Netherlands

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Cardoso de Souza T, Bastiaans RJM , Geurts BJ , Goey, de LPH. Numerical analysis of a swirl stabilized premixed combustor with the flamelet generated manifold approach. In H. Kuerten et al. X, editor, Proceedings of the Direct and Large-Eddy Simulation VIII (DLES8), 7-9 July 2010, Eindhoven, The Netherlands. Springer. 2011. p. 321-326. (Ercoftac Series). doi: 10.1007/978-94-007-2482-2_51

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

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