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

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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

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Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

S. Deng, M. Perçin, and B. van Oudheusden, “Aerodynamic characterization of ‘DelFly Micro’ in forward flight configuration by force measurements and flow field visualization,” 2015, vol. 99, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/44408.