Chappell, S. and Angland, David (2012) Active control of a wing tip vortex with a dielectric barrier discharge plasma actuator. In 6th AIAA Flow Control Conference. American Institute of Aeronautics and Astronautics. 15 pp . (doi:10.2514/6.2012-2952).
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Published date: 2012
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6th AIAA Flow Control Conference, New Orleans, United States, 2012-06-25 - 2012-06-28
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Local EPrints ID: 419081
URI: http://eprints.soton.ac.uk/id/eprint/419081
PURE UUID: 2d181c99-ec86-481c-95a2-6cef3f972a37
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Date deposited: 29 Mar 2018 16:30
Last modified: 15 Mar 2024 19:04
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