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dc.contributor.authorDing, H
dc.contributor.authorZhang, Y
dc.contributor.authorSun, C
dc.contributor.authorYang, Y
dc.contributor.authorWen, C
dc.date.accessioned2022-08-26T10:53:13Z
dc.date.issued2022-07-16
dc.date.updated2022-08-25T23:15:53Z
dc.description.abstractAs a clean and energy-saving natural gas purification and separation device, the supersonic separator's internal gas-liquid separation mechanism needs to be explored. However, the complex three-field (gas, droplet, liquid film) two-phase (gas, liquid) supersonic condensation flow challenges the numerical modeling. Most studies are limited to tracking the gas phase and droplets and ignore the effects of liquid film and phase change on droplets and water vapor removal. In the present study, we established a novel Eulerian-Lagrangian method coupled with the Eulerian wall film model to study the three-field behaviors and phase change for the enhancement of separation efficiency in the supersonic separator. The accuracy of the proposed model was validated by three experiments. The gas, droplet, and liquid film behaviors and three-field heat and mass transfers in the supersonic separator are studied using the proposed three-field two-phase flow model. Then, the sensitivity analysis was carried out, which showed the inlet mass flow rate qp,in of the heterogeneous droplets determines the maximum film thickness. For qp, in = 0.001 kg/s, this value is about 85.2 μm. The result also showed a significant improvement in separation efficiency with a proper inlet droplet diameter dp,in, qp,in, and gas pressure pin. For dp,in, qp,in, and pin are selected as 2.2 μm, 0.0015 kg/s, and 3 atm, better separation efficiency can be obtained with droplet removal rate, water vapor removal rate, and dew point depression being optimized to 100%, 57.4%, and 29.1% respectively.en_GB
dc.description.sponsorshipNational Natural Science Foundation of Chinaen_GB
dc.format.extent124833-
dc.identifier.citationVol. 258, article 124833en_GB
dc.identifier.doihttps://doi.org/10.1016/j.energy.2022.124833
dc.identifier.grantnumber51876143en_GB
dc.identifier.grantnumber61873184en_GB
dc.identifier.grantnumber61627803en_GB
dc.identifier.urihttp://hdl.handle.net/10871/130546
dc.identifierORCID: 0000-0002-4445-1589 (Wen, Chuang)
dc.identifierScopusID: 36454182800 (Wen, Chuang)
dc.identifierResearcherID: I-5663-2016 (Wen, Chuang)
dc.language.isoenen_GB
dc.publisherElsevieren_GB
dc.rights© 2022 The Author(s). Published by Elsevier Ltd. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/)en_GB
dc.subjectCondensationen_GB
dc.subjectPhase changeen_GB
dc.subjectDroplet formationen_GB
dc.subjectLiquid filmen_GB
dc.subjectSupersonic flowen_GB
dc.subjectPerformance optimizationen_GB
dc.titleNumerical simulation of supersonic condensation flows using Eulerian-Lagrangian and Eulerian wall film modelsen_GB
dc.typeArticleen_GB
dc.date.available2022-08-26T10:53:13Z
dc.identifier.issn0360-5442
exeter.article-number124833
dc.descriptionThis is the final version. Available on open access from Elsevier via the DOI in this recorden_GB
dc.identifier.journalEnergyen_GB
dc.relation.ispartofEnergy, 258
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/en_GB
dcterms.dateAccepted2022-07-12
rioxxterms.versionVoRen_GB
rioxxterms.licenseref.startdate2022-07-16
rioxxterms.typeJournal Article/Reviewen_GB
refterms.dateFCD2022-08-26T10:51:05Z
refterms.versionFCDVoR
refterms.dateFOA2022-08-26T10:54:15Z
refterms.panelBen_GB


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© 2022 The Author(s). Published by Elsevier Ltd. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/)
Except where otherwise noted, this item's licence is described as © 2022 The Author(s). Published by Elsevier Ltd. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/)