Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/64554
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dc.contributor.authorWen, Xinen
dc.date.accessioned2015-05-28T03:22:57Zen
dc.date.available2015-05-28T03:22:57Zen
dc.date.copyright2015en
dc.date.issued2015en
dc.identifier.citationWen, X. (2015). Study of synthetic jets in boundary layers. Doctoral thesis, Nanyang Technological University, Singapore.en
dc.identifier.urihttps://hdl.handle.net/10356/64554en
dc.description.abstractAs a zero-net-mass-flux actuator, a synthetic jet (SJ) actuator is a promising active flow separation control device. In order to make this technology more feasible in real-world applications, this research aims to uncover more underlying physics associated with SJ-based flow separation control. Both a CFD framework and a water-tunnel platform are developed, and decomposition methods are applied to extract coherent flow structures. It is found that the single-SJ-induced hairpin vortex in the turbulent boundary layer (TBL) is asymmetric, oscillates laterally, and dissipates fast, whereas it is symmetric and persistent in the laminar boundary layer (LBL). Using in line twin SJs in attached LBLs, three types of vortex structures are identified at various operational phase differences: one combined vortex at 90 degree, two completely separated vortices at 270 degree, and partially interacting vortex structures at 0 and 180 degree. Distinct flow control effect is found by applying these vortex structures on a separated LBL.en
dc.format.extent174 p.en
dc.language.isoenen
dc.subjectDRNTU::Engineering::Mechanical engineering::Fluid mechanicsen
dc.titleStudy of synthetic jets in boundary layersen
dc.typeThesisen
dc.contributor.supervisorTang Huien
dc.contributor.supervisorFei Duanen
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen
dc.description.degreeDOCTOR OF PHILOSOPHY (MAE)en
dc.identifier.doi10.32657/10356/64554en
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