Delaying Separation Through Sweeping Jet Flow Control

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dc.contributor.authorSalinas, Maximiliano B.
dc.contributor.authorWojewodka, Jameson
dc.contributor.authorWerling, Brandon
dc.contributor.authorLewis, Marvin
dc.contributor.authorSchatzman, David M.
dc.contributor.authorWilson, Jacob
dc.contributor.authorNorberg, Seth A.
dc.contributor.authorAshcraft, Timothy A.
dc.date.accessioned2023-10-16T17:45:42Z
dc.date.available2023-10-16T17:45:42Z
dc.date.issued2018
dc.description.abstractThis study investigated a proof of concept, low profile, externally mounted, additive-manufactured fluidic actuator array that can be attached, tested, and removed from an aerodynamic surface...
dc.description.sponsorshipDepartment of Civil and Mechanical Engineering
dc.identifier.citationMaximiliano B. Salinas, Jameson Wojewodka, Brandon Werling, Marvin Lewis, David M. Schatzman, Jacob Wilson, Seth Norberg and Timothy A. Ashcraft. "Delaying Separation Through Sweeping Jet Flow Control," AIAA 2018-1797. 2018 AIAA Aerospace Sciences Meeting. January 2018.
dc.identifier.doihttps://doi/10.2514/6.2018-1797
dc.identifier.urihttps://hdl.handle.net/20.500.14216/879
dc.publisherAerospace Research Central
dc.relation.ispartof2018 AIAA Aerospace Sciences Meeting
dc.subjectFlow Conditions
dc.subjectSweeping Jet Actuators
dc.subjectBoundary Layers
dc.subjectLift Coefficient
dc.titleDelaying Separation Through Sweeping Jet Flow Control
dc.typeproceedings-article
local.peerReviewedYes

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