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Scaling trends of bird's alular feathers (1 Viewer)

Fred Ruhe

Well-known member
Netherlands
Thomas Linehan & Kamran Mohseni, 2020

Scaling trends of bird's alular feathers in connection to leading-edge vortex flow over hand-wing.

Scientific Reports 10, Article number: 7905
doi: https://doi.org/10.1038/s41598-020-63181-7
https://www.nature.com/articles/s41598-020-63181-7

Free pdf:
https://www.nature.com/articles/s41598-020-63181-7.pdf

Abstract:

An aerodynamic structure ubiquitous in Aves is the alula; a small collection of feathers muscularized near the wrist joint. New research into the aerodynamics of this structure suggests that its primary function is to induce leading-edge vortex (LEV) flow over bird's outer hand-wing to enhance wing lift when manuevering at slow speeds. Here, we explore scaling trends of the alulaâs spanwise position and its connection to this function. Specifically, we test the hypothesis that the relative distance of the alula from the wing tip is that which maximizes LEV-lift when the wing is spread and operated in a deep-stall flight condition. To test this, we perform experiments on model wings in a wind tunnel to approximate this distance and compare our results to positional measurements of the alula on spread-wing specimens. We found the position of the alula on non-aquatic birds selected for alula optimization to be located at or near the lift-maximizing position predicted by wind tunnel experiments. These findings shed new light on avian wing anatomy and the role of unconventional aerodynamics in shaping it.

Enjoy,

Fred
 
Figure. Model alula induces and stabilizes leading-edge vortex (LEV) over outer portion of unswept wing in deep-stall flight condition. (a) Three-dimensional streamlines of time-averaged flow measured around a model wing with and without the alula. Streamlines originating at the wing’s leading-edge are colored black. Streamlines originating at the wing’s tip are colored magenta. Isosurfaces of spanwise flow are included in isometric views. = 1.5 wing at an angle of attack of 28 deg. Alula’s root is centered on the wing. (b) Corresponding contour slices of measured flow quantities. (I) Non-dimensional spanwise vorticity ωy and velocity v in streamwise-oriented planes at spanwise stations outboard of the alula. (II) Non-dimensional streamwise vorticity ωx in spanwise-oriented planes along the chord of the wing. c is the wing chord length, b is the wing span, U is the free-stream velocity, and α is the angle of attack.

Fred
 

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