Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/111081
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dc.contributorDepartment of Mechanical Engineeringen_US
dc.creatorZhu, Jen_US
dc.creatorWang, Hen_US
dc.creatorZeng, Len_US
dc.date.accessioned2025-02-17T01:37:13Z-
dc.date.available2025-02-17T01:37:13Z-
dc.identifier.issn1070-6631en_US
dc.identifier.urihttp://hdl.handle.net/10397/111081-
dc.language.isoenen_US
dc.publisherAIP Publishing LLCen_US
dc.rights© 2024 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 Jing Zhu, Hanfeng Wang, Lingwei Zeng; Control of the flow around a finite-height square cylinder with slot blowing near its free-end side edges. Physics of Fluids 1 February 2024; 36 (2): 025146 and may be found at https://dx.doi.org/10.1063/5.0187959.en_US
dc.titleControl of the flow around a finite-height square cylinder with slot blowing near its free-end side edgesen_US
dc.typeJournal/Magazine Articleen_US
dc.description.otherinformationAuthor name used in this publication: 朱静en_US
dc.description.otherinformationAuthor name used in this publication: 王汉封en_US
dc.description.otherinformationAuthor name used in this publication: 曾令伟en_US
dc.identifier.spage025146-1en_US
dc.identifier.epage025146-16en_US
dc.identifier.volume36en_US
dc.identifier.issue2en_US
dc.identifier.doi10.1063/5.0187959en_US
dcterms.abstractThis paper describes an active control technique that uses symmetric downward slot blowing from the free-end side edges of a finite-height square cylinder to suppress the aerodynamic forces. The width (d) of the tested cylinder is 40 mm and the aspect ratio H/d is 5. The Reynolds number based on the oncoming flow velocity U∞ and d is 2.67 × 104. The tested blowing ratio Cb (=Ub/U∞, where Ub is the blowing velocity at the slot exit) ranges from 0 to 4, and two typical included angles of θ = 5° and 45° are considered. The experimental results indicate that free-end slot blowing effectively suppresses the aerodynamic forces on the cylinder. The maximum reduction in the aerodynamic forces occurs with θ = 5° and Cb = 3.0, whereupon the mean drag, fluctuating drag, and fluctuating lateral force are reduced by 6.80%, 48.52%, and 69.38%, respectively. Furthermore, slot blowing control introduces a strong downward entrainment into the near wake of the cylinder, weakening its spanwise vortex shedding. This successfully converts the alternating spanwise vortex shedding into symmetric shedding, especially near the free end from which the downward blowing issues.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationPhysics of fluids, Feb. 2024, v. 36, no. 2, 025146, p. 025146-1 - 025146-16en_US
dcterms.isPartOfPhysics of fluidsen_US
dcterms.issued2024-02-
dc.identifier.scopus2-s2.0-85186067271-
dc.identifier.eissn1089-7666en_US
dc.identifier.artn025146en_US
dc.description.validate202502 bcchen_US
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Others-
dc.description.fundingSourceOthersen_US
dc.description.fundingTextNational Nature Science Foundation of China; Hunan Provincial Natural Science Foundation of Chinaen_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryVoR alloweden_US
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