dc.contributor.authorZhang, G. Q.
dc.contributor.authorJi, L. C.
dc.contributor.authorHu, X.
dc.date.accessioned2017-06-07T09:35:38Z
dc.date.available2017-06-07T09:35:38Z
dc.date.issued2017
dc.identifier.citationZhang, G. Q., Ji, L. C., & Hu, X. (2017). Vortex-induced vibration for an isolated circular cylinder under the wake interference of an oscillating airfoil: Part II. Single degree of freedom. Acta Astronautica, 133, 311-323.en_US
dc.identifier.issn0094-5765en_US
dc.identifier.urihttp://hdl.handle.net/10220/42617
dc.description.abstractThe vortex-induced vibration behind an isolated cylinder under the wake interference of an oscillating airfoil at different oscillating frequencies and amplitudes have been studied numerically. Our previous research [11] mainly focused on the two degree of freedom vibration problem, several types of the phase portraits of the displacement have been newly found, including the "half -8″ and "cone-net" types as reduced velocity increases. At present, we have continued the research to the single degree of freedom vibration, the corresponding results had been found that under the wake of the free steady flow, as the reduced velocity increases, the phase portraits displacements of the single degree of freedom vibrating cylinder will begin to rotate counterclockwise from the first and third quadrants to the second and fourth quadrants in a Cartesian coordinate system. Under the wake of the oscillating airfoil, the single bending curve and the single closed orbit (double “8-shape” like) of the displacements are newly found in the drag and thrust producing cases respectively. Except this, the two triplets of vortices have also been newly found in the pair and single plus pair wakes at each cycle. The vorticity dynamics behind the vibrating cylinder together with the corresponding force variations have also been obtained computationally and analyzed in details.en_US
dc.format.extent39 p.en_US
dc.language.isoenen_US
dc.relation.ispartofseriesActa Astronauticaen_US
dc.rights© 2017 International Academy of Astronautics. This is the author created version of a work that has been peer reviewed and accepted for publication in Acta Astronautica, published by Elsevier on behalf of International Academy of Astronautics. It incorporates referee’s comments but changes resulting from the publishing process, such as copyediting, structural formatting, may not be reflected in this document.  The published version is available at: [http://dx.doi.org/10.1016/j.actaastro.2017.01.019].en_US
dc.subjectVortex sheddingen_US
dc.subjectVortex-induced-vibrationen_US
dc.titleVortex-induced vibration for an isolated circular cylinder under the wake interference of an oscillating airfoil: Part II. Single degree of freedomen_US
dc.typeJournal Article
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.identifier.doihttp://dx.doi.org/10.1016/j.actaastro.2017.01.019
dc.description.versionAccepted versionen_US


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