High aerodynamic lift from the tail reduces drag in gliding raptors

Author:

Usherwood James R.1ORCID,Cheney Jorn A.1,Song Jialei12,Windsor Shane P.3,Stevenson Jonathan P. J.3,Dierksheide Uwe4,Nila Alex5,Bomphrey Richard J.1ORCID

Affiliation:

1. Structure and Motion Laboratory, The Royal Veterinary College, North Mymms, Hatfield, Herts AL9 7TA, UK

2. School of Mechanical Engineering, Dongguan University of Technology, Dongguan, Guangdong, China

3. Department of Aerospace Engineering, University of Bristol, Queens Building, University Walk, Bristol BS8 1TR, UK

4. LaVision GmbH, Anna-Vandenhoeck-Ring 19, 37081 Göttingen, Germany

5. LaVision UK Ltd, 2 Minton Place, Victoria Road, Bicester, Oxon OX26 6QB, UK

Abstract

ABSTRACT Many functions have been postulated for the aerodynamic role of the avian tail during steady-state flight. By analogy with conventional aircraft, the tail might provide passive pitch stability if it produced very low or negative lift. Alternatively, aeronautical principles might suggest strategies that allow the tail to reduce inviscid, induced drag: if the wings and tail act in different horizontal planes, they might benefit from biplane-like aerodynamics; if they act in the same plane, lift from the tail might compensate for lift lost over the fuselage (body), reducing induced drag with a more even downwash profile. However, textbook aeronautical principles should be applied with caution because birds have highly capable sensing and active control, presumably reducing the demand for passive aerodynamic stability, and, because of their small size and low flight speeds, operate at Reynolds numbers two orders of magnitude below those of light aircraft. Here, by tracking up to 20,000, 0.3 mm neutrally buoyant soap bubbles behind a gliding barn owl, tawny owl and goshawk, we found that downwash velocity due to the body/tail consistently exceeds that due to the wings. The downwash measured behind the centreline is quantitatively consistent with an alternative hypothesis: that of constant lift production per planform area, a requirement for minimizing viscous, profile drag. Gliding raptors use lift distributions that compromise both inviscid induced drag minimization and static pitch stability, instead adopting a strategy that reduces the viscous drag, which is of proportionately greater importance to lower Reynolds number fliers.

Funder

Air Force Office of Scientific Research

Wellcome Trust

Horizon 2020 research and innovation programme

Publisher

The Company of Biologists

Subject

Insect Science,Molecular Biology,Animal Science and Zoology,Aquatic Science,Physiology,Ecology, Evolution, Behavior and Systematics

Reference35 articles.

1. Wake patterns of the wings and tail of hovering hummingbirds;Altshuler;Exp. Fluids,2009

2. Caridi, G. C. A. (2018). Development and application of helium-filled soap bubbles: For large-scale PIV experiments in aerodynamics. PhD thesis, Delft University of Technology.

3. Durston, N. E. (2019). Quantifying the flight stability of free-gliding birds of prey. PhD Thesis, University of Bristol. https://research-information.bris.ac.uk/files/198573023/thesis_c.pdf.

4. Avian surface reconstruction in free flight with application to flight stability analysis of a barn owl and peregrine falcon;Durston;J. Exp. Biol.,2019

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