The Influence of the Slot Aspect Ratio on the Flow Field of Synthetic Jets

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dc.contributor.advisor Sharma, R en
dc.contributor.advisor Mallinson, G en
dc.contributor.author Fischer, Christoph en
dc.date.accessioned 2013-08-30T02:30:39Z en
dc.date.issued 2012 en
dc.identifier.uri http://hdl.handle.net/2292/20715 en
dc.description.abstract In the last decade, there has been a surge of research interest in developing flow-controlling devices, which can provide appreciable aerodynamic performance gain, do not require a large energy input from the operating device, and are cheap and lightweight at the same time. The synthetic jet actuator is one such device that has advantages of low cost but also simple structure and easy installation amongst other things, for which it has attracted much research interest. The jet is synthesised from the ambient air, which is indeed a major benefit over a continuous jet that needs a constant, external fluid supply to maintain the jet. The synthetic jet has established itself as a useful fluidic device with increasing potential for a range of other practical applications, such as in heat and mass transfer enhancement and active flow control. The present study investigates the influence of initial conditions primarily that of the orifice aspect ratio, on the flow field of synthetic jets. The flow fields are also examined for dependence on cavity shape and height. The characteristics of synthetic jet flow fields actuated via circular and rectangular orifices (aspect ratios ranging from 1 to 64) are studied experimentally by hot-wire anemometry and flow visualisation methods using smoke and high-speed camera techniques. In addition, unsteady Reynolds-Averaged Navier-Stokes computations, using the hybrid turbulence ‘Scale-Adaptive Simulation’ model, are carried out to complement the data from the physical experiments, and to utilise the power of visualisation, to gain significant insights into the problem. Centreline flow statistics axially downstream and transverse profiles at different axial locations have been evaluated. Furthermore, turbulence intensities have been measured and computed respectively in order to fully investigate the flow fields. The outcomes of this fundamental study contribute to the understanding of synthetic jets from rectangular slots of various aspect ratios. A linear relationship between the slot aspect ratio and the location of axis-switching has been proposed. In addition, the widely accepted vortex formation criterion in SJ research has been extended by a saturation criterion for secondary vortices. Furthermore, several design specifications have been established to assist actuator optimisation. Finally, the usage of the hybrid turbulence model approach has been evaluated and its potential compared to Large-Eddy Simulations or Direct Numerical Simulations has been shown. en
dc.publisher ResearchSpace@Auckland en
dc.relation.ispartof PhD Thesis - University of Auckland en
dc.relation.isreferencedby UoA99248166214002091 en
dc.rights Items in ResearchSpace are protected by copyright, with all rights reserved, unless otherwise indicated. Previously published items are made available in accordance with the copyright policy of the publisher. en
dc.rights Whole document is available to authenticated members of The University of Auckland until Aug. 2015. Items in ResearchSpace are protected by copyright, with all rights reserved, unless otherwise indicated. en
dc.rights.uri https://researchspace.auckland.ac.nz/docs/uoa-docs/rights.htm en
dc.rights.uri http://creativecommons.org/licenses/by-nc-sa/3.0/nz/ en
dc.title The Influence of the Slot Aspect Ratio on the Flow Field of Synthetic Jets en
dc.type Thesis en
thesis.degree.discipline Mechanical Engineering en
thesis.degree.grantor The University of Auckland en
thesis.degree.level Doctoral en
thesis.degree.name PhD en
dc.rights.holder Copyright: The Author en
dc.rights.accessrights http://purl.org/eprint/accessRights/OpenAccess en
pubs.elements-id 405914 en
pubs.record-created-at-source-date 2013-08-30 en
dc.identifier.wikidata Q112889653


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