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Abstract

Staying aloft when hovering and flying slowly is demanding. According to quasi–steady-state aerodynamic theory, slow-flying vertebrates should not be able to generate enough lift to remain aloft. Therefore, unsteady aerodynamic mechanisms to enhance lift production have been proposed. Using digital particle image velocimetry, we showed that a small nectar-feeding bat is able to increase lift by as much as 40% using attached leading-edge vortices (LEVs) during slow forward flight, resulting in a maximum lift coefficient of 4.8. The airflow passing over the LEV reattaches behind the LEV smoothly to the wing, despite the exceptionally large local angles of attack and wing camber. Our results show that the use of unsteady aerodynamic mechanisms in flapping flight is not limited to insects but is also used by larger and heavier animals.
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References and Notes

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We thank R. von Busse and Y. Winter for their support. This work was supported by grants from the Swedish Research Council, the Swedish Foundation for International Cooperation in Research and Higher Education, the Knut and Alice Wallenberg Foundation, the Crafoord Foundation, the Magnus Bergvall Foundation, and the Royal Physiographical Society.

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Published In

Science
Volume 319 | Issue 5867
29 February 2008

Submission history

Received: 15 November 2007
Accepted: 17 January 2008
Published in print: 29 February 2008

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Authors

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F. T. Muijres
Department of Theoretical Ecology, Lund University, SE-223 62 Lund, Sweden.
L. C. Johansson
Department of Theoretical Ecology, Lund University, SE-223 62 Lund, Sweden.
R. Barfield
Department of Theoretical Ecology, Lund University, SE-223 62 Lund, Sweden.
M. Wolf
Department of Theoretical Ecology, Lund University, SE-223 62 Lund, Sweden.
G. R. Spedding
Department of Aerospace and Mechanical Engineering, University of Southern California, Los Angeles, CA 90089–1191, USA.
A. Hedenström*
Department of Theoretical Ecology, Lund University, SE-223 62 Lund, Sweden.

Notes

* To whom correspondence should be addressed. E-mail: [email protected]

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