Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/90961
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dc.contributorDepartment of Industrial and Systems Engineering-
dc.creatorYin, T-
dc.creatorZhang, G-
dc.creatorDu, J-
dc.creatorTo, S-
dc.date.accessioned2021-09-03T02:35:41Z-
dc.date.available2021-09-03T02:35:41Z-
dc.identifier.urihttp://hdl.handle.net/10397/90961-
dc.language.isoenen_US
dc.publisherInstitute of Electrical and Electronics Engineersen_US
dc.rightsThis work is licensed under a Creative Commons Attribution 4.0 License. For more information, see https://creativecommons.org/licenses/by/4.0/en_US
dc.rightsThe following publication T. Yin, G. Zhang, J. Du and S. To, "Nonlinear Analysis of Stability and Rotational Accuracy of an Unbalanced Rotor Supported by Aerostatic Journal Bearings," in IEEE Access, vol. 9, pp. 61887-61900, 2021 is available at https://doi.org/10.1109/ACCESS.2021.3075051en_US
dc.subjectAerodynamicsen_US
dc.subjectAerostatic bearingsen_US
dc.subjectFinite element analysisen_US
dc.subjectMathematical modelen_US
dc.subjectNonlinear analysisen_US
dc.subjectNumerical stabilityen_US
dc.subjectOrificesen_US
dc.subjectRotational accuracyen_US
dc.subjectRotorsen_US
dc.subjectVibrationsen_US
dc.subjectWhirl stabilityen_US
dc.titleNonlinear analysis of stability and rotational accuracy of an unbalanced rotor supported by aerostatic journal bearingsen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage61887-
dc.identifier.epage61900-
dc.identifier.volume9-
dc.identifier.doi10.1109/ACCESS.2021.3075051-
dcterms.abstractThis paper presents the nonlinear analysis of stability and dynamic rotational accuracy of an unbalanced rotor supported by aerostatic journal bearings. A finite element method is utilized with the Runge-Kutta fourth order method to solve the transient Reynolds equation and the rotor dynamics equations simultaneously for the dynamic response analysis of the rotor. The dynamic behavior of the rotor center is analyzed under different rotor masses. It is shown that the dynamic responses of the rotor strongly depend on the rotor mass. The periodic, multi-periodic or quasi-periodic motions are observed as the rotor mass changes. Under a given operating speed, the mass at which the resonance occurs is studied and its relationship with the mass of the rotor at the threshold of instability is found for the first time. The influences of supply pressure, bearing clearance, orifice diameter and eccentric distance on the rotational accuracy, the resonance and instability threshold are also investigated. The result of this study can provide guidance for designing aerostatic bearing rotor systems with required running accuracy and stability.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationIEEE access, 2021, v. 9, p. 61887-61900-
dcterms.isPartOfIEEE access-
dcterms.issued2021-
dc.identifier.scopus2-s2.0-85104571157-
dc.identifier.eissn2169-3536-
dc.description.validate202109 bcvc-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Scopus/WOSen_US
dc.description.pubStatusPublisheden_US
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