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Aerodynamic characterization of 'DelFly Micro' in forward flight configuration by force measurements and flow field visualization
Date
2015-01-01
Author
Deng, Shuanghou
Perçin, Mustafa
van Oudheusden, Bas
Metadata
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This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
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This study explores the flow structures and unsteady force generation mechanisms of a flapping-wing micro air vehicle 'DelFly Micro' in forward flight configuration. Stereoscopic Particle Image Velocimetry (Stereo-PIV) measurements were performed to acquire three dimensional flow fields in the wake. Six components of forces and moments were captured simultaneously by use of a miniature force sensor.
Subject Keywords
Flapping-wing MAV
,
DelFly Micro
,
Aerodynamic force
,
Wake flow topolygy
URI
https://hdl.handle.net/11511/44408
DOI
https://doi.org/10.1016/j.proeng.2014.12.623
Collections
Department of Aerospace Engineering, Conference / Seminar