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physics.flu-dyn2020

Flow turning effect and laminar control by the 3D curvature of leading edge serrations from owl wing

Muthukumar Muthuramalingam, Edward Talboys, Hermann Wagner +1

This work describes a novel mechanism of laminar flow control of a backward swept wing with a comb-like leading edge device. It is inspired by the leading-edge comb on owl feathers…

physics.flu-dyn2020

The Peregrine Falcon's Dive: On the Pull-Out Maneuver and Flight Control Through Wing-Morphing

Omar Selim, Erwin R. Gowree, Christian Lagemann +3

During the pull-out maneuver, Peregrine falcons were observed to adopt specific flight configurations which are thought to offer an aerodynamic advantage over aerial prey. Analysis…

physics.flu-dyn2020

Effect of different geometries of self-oscillating trailing-edge flaplets on aerofoil self-noise

E. Talboys, T. F. Geyer, F. Pruefer +1

This paper presents an acoustic study of a standard NACA 0012 aerofoil with additional self-oscillating passive flaplets attached to the trailing edge. The tests with varying geome…

physics.flu-dyn2018

An aeroacoustic investigation into the effect of self-oscillating trailing edge flaplets

E. Talboys, T. F. Geyer, C. Bruecker

The aeroacoustics of a NACA 0012 aerofoil with an array of self-oscillating flexible flaplets attached on the trailing edge has been investigated at low to moderate chord based Rey…

physics.flu-dyn2018

Upstream Shear Layer Stabilisation via Self-Oscillating Trailing Edge Flaplets

Edward Talboys, Christoph Bruecker

The flow around a symmetric aerofoil (NACA 0012) with an array of flexible flaplets attached to the trailing edge has been investigated at Reynolds numbers of 100,000 - 150,000 by…