COMPUTATIONAL AND EXPERIMENTAL STUDY OF SPANWISE SYNTHETIC JET FLOW CONTROL

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dc.contributor.authorHo, Howard
dc.contributor.authorMachado, Adnan
dc.contributor.authorSullivan, Pierre
dc.date.accessioned2025-05-08T14:26:19Z
dc.date.available2025-05-08T14:26:19Z
dc.date.issued2024-06-28
dc.description.abstractThis study investigates the reattachment of flow on a stalled NACA 0025 airfoil with an array of circular synthetic jet actuators. Experimental flow visualizations are used to assess the spanwise control authority of the array and the three-dimensionality of the flow. Numerical simulations provide insights into the flow structures created by the actuation, and how they evolve with different parameters.
dc.identifier.doihttps://doi.org/10.48550/arXiv.2412.07726
dc.identifier.urihttps://hdl.handle.net/1807/142812
dc.language.isoen
dc.rightsAttribution-ShareAlike 4.0 Internationalen
dc.rights.urihttp://creativecommons.org/licenses/by-sa/4.0/
dc.subjectAirfoil
dc.subjectCFD
dc.subjectSJA
dc.titleCOMPUTATIONAL AND EXPERIMENTAL STUDY OF SPANWISE SYNTHETIC JET FLOW CONTROL
dc.typeConference Paper

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