Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/103350
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dc.contributor.authorRen, H.en
dc.contributor.authorWu, Y.en
dc.contributor.authorHuang, P. G.en
dc.date.accessioned2013-10-25T07:47:51Zen
dc.date.accessioned2019-12-06T21:10:36Z-
dc.date.available2013-10-25T07:47:51Zen
dc.date.available2019-12-06T21:10:36Z-
dc.date.copyright2013en
dc.date.issued2013en
dc.identifier.citationRen, H., Wu, Y., & Huang, P. G. (2013). Visualization and characterization of near-wake flow fields of a flapping-wing micro air vehicle using PIV. Journal of visualization, 16(1), 75-83.en
dc.identifier.issn1343-8875en
dc.identifier.urihttps://hdl.handle.net/10356/103350-
dc.description.abstractTwo-dimensional velocity fields are measured using particle image velocimetry (PIV) at four planes in the near-wake region of a pair of the side wings of a flapping-wing micro air vehicle (MAV) designed at Wright State University. A high-speed camera is used to identify the phases of the flapping motion of the wings. The results emphasize the importance of the coupling between the flexible wings and the flow in future CFD efforts. The results also show that a large-scale vortex ring is shed into the near-wake region during the fling motion of the side wings of the current MAV. The three-dimensional features of this vortex ring are visualized and characterized from the velocity and vorticity fields measured in the four particle image velocimetry planes.en
dc.language.isoenen
dc.relation.ispartofseriesJournal of visualizationen
dc.subjectDRNTU::Engineering::Mechanical engineering::Mechanics and dynamicsen
dc.titleVisualization and characterization of near-wake flow fields of a flapping-wing micro air vehicle using PIVen
dc.typeJournal Articleen
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen
dc.identifier.doi10.1007/s12650-012-0152-zen
item.fulltextNo Fulltext-
item.grantfulltextnone-
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