Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/29181
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dc.contributor.authorLi, J-
dc.contributor.authorLiu, H-
dc.contributor.authorLiu, X-
dc.contributor.authorYe, Y-
dc.contributor.authorWang, H-
dc.contributor.authorWang, X-
dc.contributor.authorZhao, H-
dc.contributor.authorYao, M-
dc.date.accessioned2024-06-14T15:08:03Z-
dc.date.available2024-06-14T15:08:03Z-
dc.date.issued2021-01-15-
dc.identifierORCiD: Xinyan Wang https://orcid.org/0000-0002-1988-3742-
dc.identifierORCiD: Hua Zhao https://orcid.org/0000-0002-7876-804X-
dc.identifier.citationLi, J. et al. (2021) 'Development of a simplified n-heptane/methane model for high-pressure direct-injection natural gas marine engines', Frontiers in Energy,15, pp. 405 - 420. doi: 10.1007/s11708-021-0718-3.en_US
dc.identifier.issn2095-1701-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/29181-
dc.description.abstractHigh-pressure direct-injection (HPDI) of natural gas is one of the most promising solutions for future ship engines, in which the combustion process is mainly controlled by the chemical kinetics. However, the employment of detailed chemical models for the multi-dimensional combustion simulation is significantly expensive due to the large scale of the marine engine. In the present paper, a reduced n-heptane/methane model consisting of 35-step reactions was constructed using multiple reduction approaches. Then this model was further reduced to include only 27 reactions by utilizing the HyChem (Hybrid Chemistry) method. An overall good agreement with the experimentally measured ignition delay data of both n-heptane and methane for these two reduced models was achieved and reasonable predictions for the measured laminar flame speeds were obtained for the 35-step model. But the 27-step model cannot predict the laminar flame speed very well. In addition, these two reduced models were both able to reproduce the experimentally measured in-cylinder pressure and heat release rate profiles for a HPDI natural gas marine engine, the highest error of predicted combustion phase being 6.5%. However, the engine-out CO emission was over-predicted and the highest error of predicted NOx emission was less than 12.9%. The predicted distributions of temperature and equivalence ratio by the 35-step and 27-step models are similar to those of the 334-step model. However, the predicted distributions of OH and CH2O are significantly different from those of the 334-step model. In short, the reduced chemical kinetic models developed provide a high-efficient and dependable method to simulate the characteristics of combustion and emissions in HPDI natural gas marine engines.en_US
dc.description.sponsorshipNational Natural Science Foundation of China (Grant Nos. 91941102 and 51922076).en_US
dc.format.extent405 - 420-
dc.format.mediumPrint-Electronic-
dc.languageEnglish-
dc.language.isoen_USen_US
dc.publisherSpringer Natureen_US
dc.rightsCopyright © 2020 Springer Nature. This version of the article has been accepted for publication, after peer review (when applicable) and is subject to Springer Nature’s AM terms of use (see: https://www.springernature.com/gp/open-research/policies/journal-policies), but is not the Version of Record and does not reflect post-acceptance improvements, or any corrections. The Version of Record is available online at: https://doi.org/10.1007/s11708-021-0718-3.-
dc.rights.urihttps://www.springernature.com/gp/open-research/policies/journal-policies-
dc.subjecthigh-pressure direct-injectionen_US
dc.subjectnatural gasen_US
dc.subjectchemical kineticsen_US
dc.subjectcombustion modellingen_US
dc.subjectmarine engineen_US
dc.titleDevelopment of a simplified n-heptane/methane model for high-pressure direct-injection natural gas marine enginesen_US
dc.typeArticleen_US
dc.date.dateAccepted2020-08-06-
dc.identifier.doihttps://doi.org/10.1007/s11708-021-0718-3-
dc.relation.isPartOfFrontiers in Energy Research-
pubs.publication-statusPublished-
pubs.volume15-
dc.identifier.eissn2095-1698-
dc.rights.holderSpringer Nature-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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