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LOWEST STABILITY BOUNDARY ON FLOW OF CONCENTRIC ROTATING CYLINDERS

dc.citation.epage1532en_US
dc.citation.issue5en_US
dc.citation.spage1527en_US
dc.citation.volume20en_US
dc.citation.woscount0
dc.contributor.authorLin, H. C.en_US
dc.contributor.authorYang, W. M.en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.date.accessioned2014-12-08T15:06:59Z
dc.date.available2014-12-08T15:06:59Z
dc.date.issued2010-05-01en_US
dc.description.abstractIn this study, we numerically investigate the lowest instability boundary of nonaxisymmetric Taylor vortex flow (TVF) for different axial wavenumbers. The variation in the axial wavenumber of a supercritical TVF can affect the instability of the flow, because the wavelength of a Taylor vortex is constant only when the flow is axisymmetrical. When the nonaxisymmetric TVF is transformed to a wavy vortex flow (WVF), the instability boundary is changed with the variation in the axial wavenumber. We carry out an instability analysis of the nonaxisymmetric TVF between two concentric rotating cylinders, which have a radius ratio of 0.88.en_US
dc.identifier.doi10.1142/S0218127410026678en_US
dc.identifier.issn0218-1274en_US
dc.identifier.journalINTERNATIONAL JOURNAL OF BIFURCATION AND CHAOSen_US
dc.identifier.urihttp://dx.doi.org/10.1142/S0218127410026678en_US
dc.identifier.urihttps://ir.lib.nycu.edu.tw/handle/11536/5465
dc.identifier.wosnumberWOS:000279882400019
dc.language.isoen_USen_US
dc.subjectInstabilityen_US
dc.subjectTaylor vortexen_US
dc.subjectwavy vortexen_US
dc.subjectTaylor-Couette flowen_US
dc.subjectChebyshev methoden_US
dc.titleLOWEST STABILITY BOUNDARY ON FLOW OF CONCENTRIC ROTATING CYLINDERSen_US
dc.typeArticleen_US

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