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First published online July 31, 2009
Journal of Experimental Biology 212, 2705-2719 (2009)
Published by The Company of Biologists 2009
doi: 10.1242/jeb.022269
Rotational accelerations stabilize leading edge vortices on revolving fly wings
1 Experimental Zoology Group, Wageningen University, 6709 PG Wageningen, The
Netherlands
2 Bioengineering and Biology, California Institute of Technology, Pasadena, CA
91125, USA
* Author for correspondence (e-mail: david.lentink{at}wur.nl)
Accepted 19 April 2009
The aerodynamic performance of hovering insects is largely explained by the presence of a stably attached leading edge vortex (LEV) on top of their wings. Although LEVs have been visualized on real, physically modeled, and simulated insects, the physical mechanisms responsible for their stability are poorly understood. To gain fundamental insight into LEV stability on flapping fly wings we expressed the Navier–Stokes equations in a rotating frame of reference attached to the wing's surface. Using these equations we show that LEV dynamics on flapping wings are governed by three terms: angular, centripetal and Coriolis acceleration. Our analysis for hovering conditions shows that angular acceleration is proportional to the inverse of dimensionless stroke amplitude, whereas Coriolis and centripetal acceleration are proportional to the inverse of the Rossby number. Using a dynamically scaled robot model of a flapping fruit fly wing to systematically vary these dimensionless numbers, we determined which of the three accelerations mediate LEV stability. Our force measurements and flow visualizations indicate that the LEV is stabilized by the `quasi-steady' centripetal and Coriolis accelerations that are present at low Rossby number and result from the propeller-like sweep of the wing. In contrast, the unsteady angular acceleration that results from the back and forth motion of a flapping wing does not appear to play a role in the stable attachment of the LEV. Angular acceleration is, however, critical for LEV integrity as we found it can mediate LEV spiral bursting, a high Reynolds number effect. Our analysis and experiments further suggest that the mechanism responsible for LEV stability is not dependent on Reynolds number, at least over the range most relevant for insect flight (100<Re<14,000). LEVs are stable and continue to augment force even when they burst. These and similar findings for propellers and wind turbines at much higher Reynolds numbers suggest that even large flying animals could potentially exploit LEV-based force augmentation during slow hovering flight, take-offs or landing. We calculated the Rossby number from single-wing aspect ratios of over 300 insects, birds, bats, autorotating seeds, and pectoral fins of fish. We found that, on average, wings and fins have a Rossby number close to that of flies (Ro=3). Theoretically, many of these animals should therefore be able to generate a stable LEV, a prediction that is supported by recent findings for several insects, one bat, one bird and one fish. This suggests that force augmentation through stably attached (leading edge) vortices could represent a convergent solution for the generation of high fluid forces over a quite large range in size.
Key words: leading edge vortex, stability, Coriolis, centripetal, acceleration, insect, flight, wing
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  K. Knight CORIOLIS KEEPS LEADING EDGE VORTEX IN PLACE J. Exp. Biol., August 15, 2009; 212(16): i - ii. [Full Text] [PDF]
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D. Lentink and M. H. Dickinson Biofluiddynamic scaling of flapping, spinning and translating fins and wings J. Exp. Biol., August 15, 2009; 212(16): 2691 - 2704. [Abstract] [Full Text] [PDF]
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