Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/6617
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dc.contributorDepartment of Mechanical Engineering-
dc.creatorLu, ZB-
dc.creatorHalim, D-
dc.creatorCheng, L-
dc.date.accessioned2014-12-11T08:26:51Z-
dc.date.available2014-12-11T08:26:51Z-
dc.identifier.issn0001-4966-
dc.identifier.urihttp://hdl.handle.net/10397/6617-
dc.language.isoenen_US
dc.publisherAcoustical Society of Americaen_US
dc.rightsCopyright 2013 Acoustical Society of America. This article may be downloaded for personal use only. Any other use requires prior permission of the author and the Acoustical Society of America.en_US
dc.rightsThe following article appeared in Lu, Z. B., Halim, D., & Cheng, L. (2013). Closed-loop control of flow-induced sound in a flow duct with downstream resonant cavities. Journal of the Acoustical Society of America, 133(3), 1468-1479 and may be found at http://scitation.aip.org/content/asa/journal/jasa/133/3/10.1121/1.4789898.en_US
dc.subjectAcoustic fieldsen_US
dc.subjectActuatorsen_US
dc.subjectFlow of fluidsen_US
dc.subjectOptimal control systemsen_US
dc.subjectVortex sheddingen_US
dc.titleClosed-loop control of flow-induced sound in a flow duct with downstream resonant cavitiesen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage1468-
dc.identifier.epage1479-
dc.identifier.volume133-
dc.identifier.issue3-
dc.identifier.doi10.1121/1.4789898-
dcterms.abstractA closed-loop-controlled surface perturbation technique was developed for controlling the flow-induced sound in a flow duct and acoustic resonance inside downstream cavities. The surface perturbation was created by piezo-ceramic THUNDER (THin layer composite UNimorph Driver and sEnsoR) actuators embedded underneath the surface of a test model with a semi-circular leading edge. A modified closed-loop control scheme based on the down-sampling theory was proposed and implemented due to the practical vibration characteristic limitation of THUNDER actuators. The optimally tuned control achieved a sound pressure reduction of 17.5 dB in the duct and 22.6 dB inside the cavity at the vortex shedding frequency, respectively. Changes brought up by the control in both flow and acoustic fields were analyzed in terms of the spectrum phase shift of the flow field over the upper surface of the test model, and a shift in the vortex shedding frequency. The physical mechanism behind the control was investigated in the view of developing an optimal control strategy.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationJournal of the Acoustical Society of America, Mar. 2013, v. 133, no. 3, 1468-1479-
dcterms.isPartOfJournal of the Acoustical Society of America-
dcterms.issued2013-03-
dc.identifier.isiWOS:000316300900039-
dc.identifier.scopus2-s2.0-84874862214-
dc.identifier.eissn1520-8524-
dc.identifier.rosgroupidr62520-
dc.description.ros2012-2013 > Academic research: refereed > Publication in refereed journal-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_IR/PIRAen_US
dc.description.pubStatusPublisheden_US
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