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dc.contributor.authorArık, Mehmet
dc.contributor.authorUtturkar, Y. V.
dc.date.accessioned2015-10-28T09:54:14Z
dc.date.available2015-10-28T09:54:14Z
dc.date.issued2015-06-01
dc.identifier.issn1043-7398
dc.identifier.urihttp://hdl.handle.net/10679/994
dc.identifier.urihttp://electronicpackaging.asmedigitalcollection.asme.org/article.aspx?articleid=1935525
dc.descriptionDue to copyright restrictions, the access to the full text of this article is only available via subscription.en_US
dc.description.abstractSeamless advancements in electronics industry resulted in high performance computing. These innovations lead to smaller electronics systems with higher heat fluxes than ever. However, shrinking nature of real estate for thermal management has created a need for more effective and compact cooling solutions. Novel cooling techniques have been of interest to solve the demand. One such technology that functions with the principle of creating vortex rings is called synthetic jets. These jets are mesoscale devices operating as zero-net-mass-flux principle by ingesting and ejection of high velocity working fluid from a single opening. These devices produce periodic jet streams, which may have peak velocities over 20 times greater than conventional, comparable size fan velocities. These jets enhance heat transfer in both natural and forced convection significantly over bare and extended surfaces. Recognizing the heat transfer physics over surfaces require a fundamental understanding of the flow physics caused by microfluid motion. A comprehensive computational and experimental study has been performed to understand the flow physics of a synthetic jet. Computational study has been performed via FLUENT commercial software, while the experimental study has been performed by using laser Doppler anemometry (LDA). Since synthetic jets are typical sine-wave excited between 20 and 60 V range, they have an orifice peak velocity of over 60 m/s, resulting in a Reynolds number of over 2000. Computational fluid dynamics (CFD) predictions on the vortex dipole location fall within 10% of the experimental measurement uncertainty band.en_US
dc.description.sponsorshipU.S. Department of Energy
dc.language.isoengen_US
dc.publisherThe American Society of Mechanical Engineersen_US
dc.relation.ispartofJournal of Electronic Packaging
dc.rightsrestrictedAccess
dc.titleA computational and experimental investigation of synthetic jets for cooling of electronicsen_US
dc.typeArticleen_US
dc.peerreviewedyesen_US
dc.publicationstatuspublisheden_US
dc.contributor.departmentÖzyeğin University
dc.contributor.authorID(ORCID 0000-0002-9505-281X & YÖK ID 124782) Arık, Mehmet
dc.contributor.ozuauthorArık, Mehmet
dc.identifier.volume137
dc.identifier.issue2
dc.identifier.wosWOS:000353963000005
dc.identifier.doi10.1115/1.4029067
dc.subject.keywordsHeat-transferen_US
dc.identifier.scopusSCOPUS:2-s2.0-84993992084
dc.contributor.authorMale1
dc.relation.publicationcategoryArticle - International Refereed Journal - Institutional Academic Staff


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