Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/111056
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dc.contributorDepartment of Mechanical Engineeringen_US
dc.contributorDepartment of Civil and Environmental Engineeringen_US
dc.contributorSchool of Fashion and Textilesen_US
dc.creatorZhao, Fen_US
dc.creatorZeng, Len_US
dc.creatorBai, Hen_US
dc.creatorAlam, Men_US
dc.creatorWang, Zen_US
dc.creatorDong, Yen_US
dc.creatorTang, Hen_US
dc.date.accessioned2025-02-17T01:36:57Z-
dc.date.available2025-02-17T01:36:57Z-
dc.identifier.issn1070-6631en_US
dc.identifier.urihttp://hdl.handle.net/10397/111056-
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 Fuwang Zhao, Lingwei Zeng, Honglei Bai, Md. Mahbub Alam, Zhaokun Wang, You Dong, Hui Tang; Vortex-induced vibration of a sinusoidal wavy cylinder: The effect of wavelength. Physics of Fluids 1 August 2024; 36 (8): 087163 and may be found at https://doi.org/10.1063/5.0219753.en_US
dc.titleVortex-induced vibration of a sinusoidal wavy cylinder : the effect of wavelengthen_US
dc.typeJournal/Magazine Articleen_US
dc.description.otherinformationAuthor name used in this publication: 赵福旺en_US
dc.description.otherinformationAuthor name used in this publication: 曾令伟en_US
dc.description.otherinformationAuthor name used in this publication: 白宏磊en_US
dc.description.otherinformationAuthor name used in this publication: 王兆坤en_US
dc.description.otherinformationAuthor name used in this publication: 董优en_US
dc.description.otherinformationAuthor name used in this publication: 唐辉en_US
dc.identifier.spage087163-1en_US
dc.identifier.epage087163-17en_US
dc.identifier.volume36en_US
dc.identifier.issue8en_US
dc.identifier.doi10.1063/5.0219753en_US
dcterms.abstractWhile considerable research has addressed flow around stationary sinusoidal wavy cylinders, studies on vortex-induced vibration (VIV) of elastic-supported wavy cylinders still remain limited. This study aims to address this gap through a series of water tunnel experiments, focusing on the effects of the cylinder's spanwise wavelength. Three typical spanwise wavelengths (λ* = 1.8, 3.6, and 6.0) are considered, with the first and third identified as the optimal for reducing fluid forces (lift forces by over 90%) in previous stationary cylinder studies. The cylinder oscillates transversally at a range of reduced velocities Ur = 3.0–12.0, corresponding to the Reynolds numbers (1.5–7.0) × 103. Results indicate that, compared with a smooth cylinder, the λ* = 1.8 cylinder experiences reduced oscillation throughout the VIV regime, while the cylinders with λ* = 3.6 or 6.0 undergo enhanced oscillation over a broader lock-in range. The oscillation of the wavy cylinders with λ* = 3.6 or 6.0 tend to occur at a higher Ur, leading to an extension of the lower branch. Frequency analysis shows that, despite affecting vibration amplitude, the wavy surface retains typical VIV features. These results reveal a notable dependence of fluid forces and force-displacement phase lag on the cylinder's wavelength. Finally, we provide a detailed discussion of the phase-averaged and time-averaged flow structures from the time-resolved particle image velocimetry measurement. Overall, this study addresses the research gap concerning the impact of wavelength on the behavior of elastically supported wavy cylinders, providing significant insights for the development of practical strategies for VIV suppression and enhancement.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationPhysics of fluids, Aug. 2024, v. 36, no. 8, 087163, p. 087163-1 - 087163-17en_US
dcterms.isPartOfPhysics of fluidsen_US
dcterms.issued2024-08-
dc.identifier.scopus2-s2.0-85202863468-
dc.identifier.eissn1089-7666en_US
dc.identifier.artn087163en_US
dc.description.validate202502 bcchen_US
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Others-
dc.description.fundingSourceOthersen_US
dc.description.fundingTextLaboratory of Aerodynamic Noise Control; National Natural Science Foundation of Chinaen_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryVoR alloweden_US
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