Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/114405
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dc.contributorDepartment of Mechanical Engineering-
dc.creatorWang, F-
dc.creatorChan, TL-
dc.date.accessioned2025-08-01T03:44:12Z-
dc.date.available2025-08-01T03:44:12Z-
dc.identifier.isbn978-1-990800-00-9-
dc.identifier.urihttp://hdl.handle.net/10397/114405-
dc.language.isoenen_US
dc.publisherAvestia Publishingen_US
dc.rightsPosted with permission of the author.en_US
dc.rightsThe following publication Wang, F., & Chan, T. L. (2022). A New One-equation Turbulence Model based on the Combined Standard k-ε and k-ω Turbulence Models for Benchmark Flow Configurations, 145 is available at https://avestia.com/MHMT2022_Proceedings/files/paper/ICMFHT/ICMFHT_145.pdf.en_US
dc.subjectBenchmark flowsen_US
dc.subjectCFDen_US
dc.subjectOne- and two-equation turbulence modelsen_US
dc.subjectThird-order velocity gradientsen_US
dc.subjectTurbulence modellingen_US
dc.titleA new one-equation turbulence model based on the combined standard k-ε and k-ω turbulence models for benchmark flow configurationsen_US
dc.typeConference Paperen_US
dc.identifier.spage145-1-
dc.identifier.epage145-8-
dc.identifier.doi10.11159/icmfht22.145-
dcterms.abstractA new one-equation turbulence model based on the two-equation standard k-ε and Wilcox's k-ω turbulence models is proposed and developed for validating the benchmark flow configurations. The desirable features of both these two-equation turbulence models are combined into the new one-equation turbulence model in the complete form without neglecting the third-order velocity gradient term than simply assuming that equal coefficients in the diffusion terms. This new one-equation turbulence model is used to simulate for different benchmark flow configurations including the flow over a flat plate at zero pressure gradient, the bump-in-channel flow, the backward facing step flow and the NASA wall-mounted hump separated flow. The numerical results are fully validated and compared with the results of the experimental dataset, the one- and two-equation turbulence models, and the high-accuracy NASA codes (i.e., CFL3D and FUN3D). The new one-equation turbulence model is proved to be more accurate when compared with the one-equation Wray-Agarwal and two-equation shear stress transport (SST) k-ω turbulence models for the benchmark flow configurations.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationProceedings of the 7th World Congress on Momentum, Heat and Mass Transfer (MHMT'22), April 07 - 09, 2022, Virtual Conference, 145, p. 145-1 - 145-8-
dcterms.issued2022-
dc.relation.conferenceWorld Congress on Momentum, Heat and Mass Transfer [MHMT]-
dc.identifier.artn145-
dc.description.validate202508 bcch-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumbera3814een_US
dc.identifier.SubFormID51188en_US
dc.description.fundingSourceRGCen_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryPublisher permissionen_US
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