Vortex Formation and Force Generation Mechanisms of the DelFly II in Hovering Flight

Date

2014-08-12

Author

Tenaglia, A
Perçin, Mustafa
Van Oudheusden, Bas W.
Deng, Shuanghou
Remes, Bart

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This paper addresses the unsteady aerodynamic mechanisms in the hovering flight of the DelFly II flapping-wing Micro Aerial Vehicle (MAV). Stereoscopic Particle Image Velocimetry (Stereo-PIV) were carried out around the wings at a high framing rate. Thrust-force was measured to investigate the relation between the vortex dynamics and the aerodynamic force generation. The results reveal that the Leading-Edge-Vortex (LEV), as well as the high flexibility of the wings, have a major effect on thrust generation. Comparison of three wing pairs with different aspect ratio (AR) is also reported, yielding significant differences in both vortical structures and thrust generation.

Subject Keywords

IMAV2014 , MAV , Micro Air Vehicle , Vortex Formation, Force Generation Mechanism, Delfly II, Hovering Flight

URI

https://hdl.handle.net/11511/84603

DOI

https://doi.org/10.4233/uuid:d503baae-c4d9-4b3d-ac87-2f25ad793d5a

Conference Name

International Micro Air Vehicle Conference and Flight Competition (IMAV2014) (12 - 15 Ağustos 2014)

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

A. Tenaglia, M. Perçin, B. W. Van Oudheusden, S. Deng, and B. Remes, “Vortex Formation and Force Generation Mechanisms of the DelFly II in Hovering Flight,” Delft, Hollanda, 2014, p. 1, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/84603.