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Investigation of collection efficiency of round-nozzle impactors at different atmospheric pressures and temperatures

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dc.contributor.authorPark, Chun-Woo-
dc.contributor.authorKim, Gyuho-
dc.contributor.authorYook, Se-Jin-
dc.contributor.authorAhn, Kang-Ho-
dc.date.accessioned2021-06-22T20:03:40Z-
dc.date.available2021-06-22T20:03:40Z-
dc.date.created2021-01-21-
dc.date.issued2015-05-
dc.identifier.issn0921-8831-
dc.identifier.urihttps://scholarworks.bwise.kr/erica/handle/2021.sw.erica/18377-
dc.description.abstractA simulation approach for predicting the collection efficiency of inertial impactors was developed by calculating particle trajectories in a Lagrangian reference frame. When numerically predicted collection efficiencies of the electrical low-pressure impactor (ELPI) were compared with the experimental data found in the literature, the agreement was good and the relative difference in cut-off size was less than 12%. Then, balloon-borne impactors having nominal cut-off sizes of 1 mu m, 2.5 mu m, and 10 mu m were designed, and their collection efficiencies were predicted using the present simulation approach. When volumetric sampling flow rate of air introduced to the single-stage round-nozzle impactors was fixed at varying altitude, the cut-off sizes were predicted to decrease from 0.98 mu m, 2.47 mu m, and 9.86 mu m at sea level to 0.47 mu m (by 52.0%), 1.70 mu m (by 31.2%), and 7.62 mu m (by 22.7%) at 16-km-altitude, respectively. When volumetric sampling flow rate was adjusted, the cut-off sizes of the single-stage round-nozzle impactors were estimated to remain almost unchanged with the variation of less than 5.1%, 7.3%, and 10.6%, respectively, at varying altitude in troposphere. (C) 2015 The Society of Powder Technology Japan. Published by Elsevier B.V. and The Society of Powder Technology Japan. All rights reserved.-
dc.language영어-
dc.language.isoen-
dc.publisherElsevier BV-
dc.titleInvestigation of collection efficiency of round-nozzle impactors at different atmospheric pressures and temperatures-
dc.typeArticle-
dc.contributor.affiliatedAuthorAhn, Kang-Ho-
dc.identifier.doi10.1016/j.apt.2015.02.014-
dc.identifier.scopusid2-s2.0-84931563019-
dc.identifier.wosid000356240900023-
dc.identifier.bibliographicCitationAdvanced Powder Technology, v.26, no.3, pp.868 - 873-
dc.relation.isPartOfAdvanced Powder Technology-
dc.citation.titleAdvanced Powder Technology-
dc.citation.volume26-
dc.citation.number3-
dc.citation.startPage868-
dc.citation.endPage873-
dc.type.rimsART-
dc.type.docTypeArticle-
dc.description.journalClass1-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalWebOfScienceCategoryEngineering, Chemical-
dc.subject.keywordPlusINERTIAL IMPACTORS-
dc.subject.keywordPlusPARTICLE-
dc.subject.keywordPlusTROPOSPHERE-
dc.subject.keywordPlusINLET-
dc.subject.keywordAuthorInertial impactor-
dc.subject.keywordAuthorCollection efficiency-
dc.subject.keywordAuthorStokes number-
dc.subject.keywordAuthorBalloon-borne-
dc.subject.keywordAuthorELPI-
dc.identifier.urlhttps://www.sciencedirect.com/science/article/pii/S092188311500045X?via%3Dihub-
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