Publication:
An investigation into momentum and temperature fields of a meso-scale synthetic jet

dc.contributor.authorGhaffari, Omidreza
dc.contributor.authorDoğruöz, M. B.
dc.contributor.authorArık, Mehmet
dc.contributor.departmentMechanical Engineering
dc.contributor.ozuauthorARIK, Mehmet
dc.contributor.ozugradstudentGhaffari, Omidreza
dc.date.accessioned2016-02-17T06:33:23Z
dc.date.available2016-02-17T06:33:23Z
dc.date.issued2014
dc.descriptionDue to copyright restrictions, the access to the full text of this article is only available via subscription.
dc.description.abstractThermal management has become a critical part of advanced micro and nano electronics systems due to high heat transfer rates. More constraints such as compactness, small footprint area, lightweight, high reliability, easy-access and low cost are exposed to thermal engineers. Advanced electronic systems such as laptops, tablets, smart phones and slim TV systems carry those challenging thermal needs. For these devices, smaller thermal real estates with higher heat fluxes than ever have created issues that current thermal technologies cannot meet those needs easily. Therefore, innovative cooling techniques are necessary to fulfill these aggressive thermal demands. Synthetic jets have been studied as a promising technology to satisfy the thermal needs of such tight electronics devices. The effect of nozzle-to-surface distance for a synthetic jet on its cooling performance has neither been studied extensively nor been well-understood. In a few available experimental studies, it was reported that synthetic jet performance is very sensitive to this distance and when the jet gets closer to the hot surface its performance degrades. Therefore, a computational study has been performed to understand the flow physics of a small-scale synthetic jet for a jet-to-surface spacing of H/Dh=5. Spatial discretization is implemented via a second order upwind scheme and a second order implicit scheme is used for temporal discretization to ensure stability. It is found that pulsating flow at the nozzle exit generates vortices and these vortices seem to have minimal effect on the target surface profiles. Local surface pressure, velocity, turbulence profiles and heat transfer coefficient distributions are determined, then the effects of jet frequency as well as near-wall vortices are discussed.
dc.description.sponsorshipTÜBİTAK
dc.identifier.doi10.1109/ITHERM.2014.6892375
dc.identifier.endpage896
dc.identifier.issn1087-9870
dc.identifier.scopus2-s2.0-84907710906
dc.identifier.startpage889
dc.identifier.urihttp://hdl.handle.net/10679/2759
dc.identifier.urihttps://doi.org/10.1109/ITHERM.2014.6892375
dc.identifier.wos000366567000118
dc.language.isoengen_US
dc.peerreviewedyes
dc.publicationstatuspublished
dc.publisherIEEE
dc.relationinfo:eu-repo/grantAgreement/TUBITAK/1001 - Araştırma/112M154
dc.relation.ispartofThermal and Thermomechanical Phenomena in Electronic Systems (ITherm), 2014 IEEE Intersociety Conference on
dc.relation.publicationcategoryInternational
dc.rightsrestrictedAccess
dc.subject.keywordsSynthetic jet
dc.subject.keywordsPulsating
dc.subject.keywordsImpingement
dc.subject.keywordsVortex
dc.subject.keywordsCFD
dc.titleAn investigation into momentum and temperature fields of a meso-scale synthetic jeten_US
dc.typeconferenceObjecten_US
dspace.entity.typePublication
relation.isOrgUnitOfPublicationdaa77406-1417-4308-b110-2625bf3b3dd7
relation.isOrgUnitOfPublication.latestForDiscoverydaa77406-1417-4308-b110-2625bf3b3dd7

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