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Analysis of Gas Turbine Combustor Exhaust Emissions:Effects of Transient Inlet Air Pressure

dc.rights.licensehttp://creativecommons.org/licenses/by/4.0 - Atribuciónes_MX
dc.contributor.authorFERNANDO ZENAIDO SIERRA ESPINOSAes_MX
dc.contributor.authorJUAN CARLOS GARCIA CASTREJONes_MX
dc.contributor.authorJOSE ALFREDO RODRIGUEZ RAMIREZes_MX
dc.coverage.spatialMEX - Méxicoes_MX
dc.date2024
dc.date.accessioned2024-01-22T16:31:04Z
dc.date.available2024-01-22T16:31:04Z
dc.identifier.issndigital: 2194-4296, impreso: 2194-4288
dc.identifier.urihttp://riaa.uaem.mx/handle/20.500.12055/4398
dc.descriptionGas turbine combustors are often subjected to combustion instabilities because of variability of operating conditions, affecting components, and altering exhaust emissions. Herein, the analysis focuses on simulating numerically the non-premixed combustion as unsteady flamelet combustion and detailed kinetic mechanism. The goal is analyzing exhaust gases under unsteady inlet airflow conditions to define operation guidelines. The numerical approach is validated using data from the literature for nonperturbed cases. Three periodical perturbations of different amplitude show differences with the nonperturbed case. Besides emission of exhaust gases, the temperature field is sensitive to airflow inlet conditions. According to the simulation results, a strong dependence of temperature and pressure in primary and dilution zones of combustor exists on the inlet air pressure condition. Emissions of flue gases like CO and NOx respond to combustor thermal behavior showing high sensitivity to inlet air pressure as well. Results indicate that moderate pressure oscillations may derive into flashback effects.es_MX
dc.formatpdf - Adobe PDFes_MX
dc.languageeng - Ingléses_MX
dc.publisherWiley-VCH GmbHes_MX
dc.relation.ispartofEnergyTechnologyes_MX
dc.relation.ispartofseries1es_MX
dc.relation.haspart10es_MX
dc.relation.urihttps://onlinelibrary.wiley.com/doi/full/10.1002/ente.202301093es_MX
dc.rightsopenAccess - Acceso Abiertoes_MX
dc.subject7 - INGENIERÍA Y TECNOLOGÍAes_MX
dc.subject.other33 - CIENCIAS TECNOLÓGICASes_MX
dc.titleAnalysis of Gas Turbine Combustor Exhaust Emissions:Effects of Transient Inlet Air Pressurees_MX
dc.typearticle - Artículoes_MX
uaem.unidadCentro de Investigación en Ingeniería y Ciencias Aplicadas (CIICAp)- Instituto de Investigación en Ciencias Básicas y Aplicadas (IICBA) - Centro de Investigación en Ingeniería y Ciencias Aplicadas (CIICAp)- Instituto de Investigación en Ciencias Básicas y Aplicadas (IICBA)es_MX
dc.type.publicationacceptedVersiones_MX
dc.audienceresearchers - Investigadoreses_MX


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  • Colección Revistas de Investigación [240]
    Artículos publicados por investigadores de la UAEM en revistas de investigación, sean éstas de la UAEM o de otras instituciones nacionales o extranjeras.

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