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dc.contributor.advisorJacob, Jamey D.
dc.contributor.authorBolitho, Michael
dc.date.accessioned2014-04-17T19:52:05Z
dc.date.available2014-04-17T19:52:05Z
dc.date.issued2008-05-01
dc.identifier.urihttps://hdl.handle.net/11244/9904
dc.description.abstractThe current study examines the use of plasma actuators as flow control devices, including synthetic jet actuators, jet vectoring, and vortex generation. The study of the plasma actuators applied to flat plates is conducted in quiescent conditions, as well as in the wind tunnel. There are two arrangements of plasma actuators investigated, one of which consists of an inner circular electrode embedded under a dielectric material and an outer annular electrode exposed to the atmosphere, and is used to create flow structures similar to that of a conventional synthetic jet actuator. The other arrangement is made up of a single linear electrode embedded within a dielectric material with a linear electrode on either side exposed to the atmosphere, and is used to create vectored jets and generate streamwise vortices.
dc.formatapplication/pdf
dc.languageen_US
dc.publisherOklahoma State University
dc.rightsCopyright is held by the author who has granted the Oklahoma State University Library the non-exclusive right to share this material in its institutional repository. Contact Digital Library Services at lib-dls@okstate.edu or 405-744-9161 for the permission policy on the use, reproduction or distribution of this material.
dc.titleJet Vectoring and Vorticity Generation Using Plasma Actuators
dc.typetext
dc.contributor.committeeMemberChambers, Frank
dc.contributor.committeeMemberArena, Andrew S.
osu.filenameBolitho_okstate_0664M_2739.pdf
osu.collegeEngineering, Architecture, and Technology
osu.accesstypeOpen Access
dc.description.departmentMechanical & Aerospace Engineering
dc.type.genreThesis


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