Visualization and characterization of near-wake flow fields of a flapping-wing micro air vehicle using PIV

Two-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 mo...

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Bibliographic Details
Main Authors: Ren, H., Wu, Y., Huang, P. G.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Journal Article
Language:English
Published: 2013
Subjects:
Online Access:https://hdl.handle.net/10356/103350
http://hdl.handle.net/10220/16928
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author Ren, H.
Wu, Y.
Huang, P. G.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Ren, H.
Wu, Y.
Huang, P. G.
author_sort Ren, H.
collection NTU
description Two-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.
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spelling ntu-10356/1033502020-03-07T13:22:21Z Visualization and characterization of near-wake flow fields of a flapping-wing micro air vehicle using PIV Ren, H. Wu, Y. Huang, P. G. School of Mechanical and Aerospace Engineering DRNTU::Engineering::Mechanical engineering::Mechanics and dynamics Two-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. 2013-10-25T07:47:51Z 2019-12-06T21:10:36Z 2013-10-25T07:47:51Z 2019-12-06T21:10:36Z 2013 2013 Journal Article Ren, 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. 1343-8875 https://hdl.handle.net/10356/103350 http://hdl.handle.net/10220/16928 10.1007/s12650-012-0152-z en Journal of visualization
spellingShingle DRNTU::Engineering::Mechanical engineering::Mechanics and dynamics
Ren, H.
Wu, Y.
Huang, P. G.
Visualization and characterization of near-wake flow fields of a flapping-wing micro air vehicle using PIV
title Visualization and characterization of near-wake flow fields of a flapping-wing micro air vehicle using PIV
title_full Visualization and characterization of near-wake flow fields of a flapping-wing micro air vehicle using PIV
title_fullStr Visualization and characterization of near-wake flow fields of a flapping-wing micro air vehicle using PIV
title_full_unstemmed Visualization and characterization of near-wake flow fields of a flapping-wing micro air vehicle using PIV
title_short Visualization and characterization of near-wake flow fields of a flapping-wing micro air vehicle using PIV
title_sort visualization and characterization of near wake flow fields of a flapping wing micro air vehicle using piv
topic DRNTU::Engineering::Mechanical engineering::Mechanics and dynamics
url https://hdl.handle.net/10356/103350
http://hdl.handle.net/10220/16928
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