Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/111153
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dc.contributorDepartment of Aeronautical and Aviation Engineering-
dc.creatorZhu, J-
dc.creatorZhang, G-
dc.creatorGao, L-
dc.creatorYu, SCM-
dc.date.accessioned2025-02-17T01:37:40Z-
dc.date.available2025-02-17T01:37:40Z-
dc.identifier.issn1070-6631-
dc.identifier.urihttp://hdl.handle.net/10397/111153-
dc.language.isoenen_US
dc.publisherAIP Publishing LLCen_US
dc.rights© 2023 Author(s). Published under an exclusive license by AIP Publishing.en_US
dc.rightsThis article may be downloaded for personal use only. Any other use requires prior permission of the author and AIP Publishing. This article appeared in Zhu, J., Zhang, G., Gao, L., & Yu, S. C. M. (2023). The circulation growth of non-impulsive starting jet. Physics of Fluids, 35(5) and may be found at https://doi.org/10.1063/5.0147768.en_US
dc.titleThe circulation growth of non-impulsive starting jeten_US
dc.typeJournal/Magazine Articleen_US
dc.description.otherinformationAuthor name used in this publication: 朱建玮en_US
dc.description.otherinformationAuthor name used in this publication: 张国庆en_US
dc.description.otherinformationAuthor name used in this publication: 高磊en_US
dc.description.otherinformationAuthor name used in this publication: 余澄文en_US
dc.identifier.spage057102-1-
dc.identifier.epage057102-16-
dc.identifier.volume35-
dc.identifier.issue5-
dc.identifier.doi10.1063/5.0147768-
dcterms.abstractAn analytical model that can be used to predict the circulation growth process for non-impulsive starting jets has been developed by extending the over-pressure correction model for impulsive starting jets. Only the jet velocity function U 0 (t) is needed to obtain the circulation growth process of non-impulsive starting jet. The non-impulsive starting jets generated by nozzle and orifice configurations are performed numerically with two acceleration schemes (represented by two kinds of velocity functions) and different acceleration stage stroke ratios L a D (modifying the acceleration time t a in each velocity function to obtain L a D = 0.05: 0.2: 1.25) to verify the accuracy of the proposed analytical model. The influence of radial velocity distribution in the jet inflow boundary is ignored in the process of constructing this model, but this has been proven to be reasonable. The time-averaged relative error with the growth process of the total circulation predicted by this model is about 11 % to 26 %, which is smaller than the 44 % to 88 % obtained by the classical slug model. For the range of L a D from 0.05 to 1.25, the relative error with the prediction of the total circulation at the end of the acceleration stage is from 4 % to 28 %, as compared to the 39 % to 96 % for the slug model.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationPhysics of fluids, May 2023, v. 35, no. 5, 057102, p. 057102-1 - 057102-16-
dcterms.isPartOfPhysics of fluids-
dcterms.issued2023-05-
dc.identifier.scopus2-s2.0-85159125000-
dc.identifier.eissn1089-7666-
dc.identifier.artn057102-
dc.description.validate202502 bcch-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Othersen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextFunding Military Commission Equipment Development Department, Equipment Advance Research Field Fund; State Administration of Science, Technology and Industry for National Defense, PRCen_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryVoR alloweden_US
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