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dc.contributor.authorGövert, Simon
dc.contributor.authorMira, Daniel
dc.contributor.authorKok, Jim B. W.
dc.contributor.authorVázquez, Mariano
dc.contributor.authorHouzeaux, Guillaume
dc.contributor.otherBarcelona Supercomputing Center
dc.date.accessioned2018-03-05T12:03:05Z
dc.date.available2018-03-05T12:03:05Z
dc.date.issued2018-03
dc.identifier.citationGövert, S. [et al.]. The Effect of Partial Premixing and Heat Loss on the Reacting Flow Field Prediction of a Swirl Stabilized Gas Turbine Model Combustor. "Flow, Turbulence and Combustion", Març 2018, vol. 100, núm. 2, p. 503-534.
dc.identifier.issn1386-6184
dc.identifier.urihttp://hdl.handle.net/2117/114802
dc.description.abstractThis work addresses the prediction of the reacting flow field in a swirl stabilized gas turbine model combustor using large-eddy simulation. The modeling of the combustion chemistry is based on laminar premixed flamelets and the effect of turbulence-chemistry interaction is considered by a presumed shape probability density function. The prediction capabilities of the presented combustion model for perfectly premixed and partially premixed conditions are demonstrated. The effect of partial premixing for the prediction of the reacting flow field is assessed by comparison of a perfectly premixed and partially premixed simulation. Even though significant mixture fraction fluctuations are observed, only small impact of the non-perfect premixing is found on the flow field and flame dynamics. Subsequently, the effect of heat loss to the walls is assessed assuming perfectly premixing. The adiabatic baseline case is compared to heat loss simulations with adiabatic and non-adiabatic chemistry tabulation. The results highlight the importance of considering the effect of heat loss on the chemical kinetics for an accurate prediction of the flow features. Both heat loss simulations significantly improve the temperature prediction, but the non-adiabatic chemistry tabulation is required to accurately capture the chemical composition in the reacting layers.
dc.description.sponsorshipThe research leading to these results has received funding through the People Program (Marie Curie Actions) of the European Union’s Seventh Framework Program (FP7, 2007-2013) for the project COPA-GT (grant agreement No. FP7-290042) as well as the European Union’s Horizon 2020 Program (2014-2020) and the Brazilian Ministry of Science, Technology and Innovation through Rede Nacional de Pesquisa (RNP) under the HPC4E Project (grant agreement No. 689772). Furthermore, computer resources and technical assistance has been provided by the Red Española de Supercomputación (RES) (grant numbers FI-2015-1-0002, FI-2015-3-0013, FI-2016-1-0001).
dc.format.extent32 p.
dc.language.isoeng
dc.publisherSpringer Verlag
dc.rightsAttribution-NonCommercial-NoDerivs 4.0 Spain
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subjectÀrees temàtiques de la UPC::Energies
dc.subject.lcshTurbulent flow
dc.subject.otherTurbulent combustion
dc.subject.otherPartial premixing
dc.subject.otherHeat loss effects
dc.subject.otherTabulated chemistry
dc.titleThe Effect of Partial Premixing and Heat Loss on the Reacting Flow Field Prediction of a Swirl Stabilized Gas Turbine Model Combustor
dc.typeArticle
dc.subject.lemacTurbulència atmosfèrica
dc.identifier.doi10.1007/s10494-017-9848-4
dc.description.peerreviewedPeer Reviewed
dc.relation.publisherversionhttps://link.springer.com/article/10.1007/s10494-017-9848-4
dc.rights.accessOpen Access
dc.description.versionPostprint (published version)
dc.relation.projectidinfo:eu-repo/grantAgreement/EC/H2020/689772/EU/HPC for Energy/HPC4E
upcommons.citation.publishedtrue
upcommons.citation.publicationNameFlow, Turbulence and Combustion
upcommons.citation.volume100
upcommons.citation.number2
upcommons.citation.startingPage503
upcommons.citation.endingPage534
dc.identifier.pmid30069142


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Except where otherwise noted, content on this work is licensed under a Creative Commons license: Attribution-NonCommercial-NoDerivs 3.0 Spain