Abstract

The alula is a small structure located at the joint between the hand-wing and arm-wing of birds and is known to be used in slow flight with high angles of attack such as landing. It is assumed to function similarly to a leading-edge slat that increases lift and delays stall. However, in spite of its universal presence in flying birds and the wide acceptance of stall delay as its main function, how the alula delays the stall and aids the flight of birds remains unclear. Here, we investigated the function of alula on the aerodynamic performance of avian wings based on data from flight tasks and wind-tunnel experiments. With the alula, the birds performed steeper descending flights with greater changes in body orientation. Force measurements revealed that the alula increases the lift and often delays the stall. Digital particle image velocimetry showed that these effects are caused by the streamwise vortex, formed at the tip of the alula, that induces strong downwash and suppresses the flow separation over the wing surface. This is the first experimental evidence that the alula functions as a vortex generator that increases the lift force and enhances manoeuvrability in flights at high angles of attack.

Highlights

  • The alula is a small structure located at the joint between the hand-wing and arm-wing of birds and is known to be used in slow flight with high angles of attack such as landing

  • Two possible three-dimensional effects of the alula were hypothesized[5,6]: (i) the induction of leading edge vortex over the hand-wing and (ii) the prevention of the spanwise thickening of the boundary layer by inhibiting the spanwise flow with small-scale vortices created by the alula

  • We measured the lift and drag forces at free-stream velocities of U0 5 3 2 15 ms[21] for three fixed wings (UJ07, UJ13, and KS20), and at U0 5 3 ms[21] for one fixed wing (UJ30) of adult male magpies

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Summary

The Function of the Alula in Avian Flight

Sang-im Lee[1,2], Jooha Kim[3], Hyungmin Park[1,3], Piotr G. Digital particle image velocimetry showed that these effects are caused by the streamwise vortex, formed at the tip of the alula, that induces strong downwash and suppresses the flow separation over the wing surface This is the first experimental evidence that the alula functions as a vortex generator that increases the lift force and enhances manoeuvrability in flights at high angles of attack. We measured the velocity field using DPIV to examine the modification of the flow structures around the bird wing (UJ30) at the attack angle of 24u by the presence of the alula (see Fig. S6 for detailed setup), at which the lift force was increased by the amount of 6.68% with the alula. The alula-tip vortex is the key mechanism for lift enhancement and stall delay at high angles of attack which endows birds with greater flight manoeuvrability. We suggest that the alula may be used in any flight that involves high angles of attack (such as turning flights7), and that more detailed studies on the contexts of alula usage are warranted

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