Michael Carley
Published 2022-02-28Version 1
A method of noise reduction proposed for the next generation of aircraft is to shield noise from the propulsion system, by positioning the noise source over a wing or another surface. In this paper, an approximate analysis is developed for the acoustic field far from a circular source placed near the edge of a semi-infinite plate, a model problem for shielding of noise by a wing and for scattering by a trailing edge. The approximation is developed for a source of small radius and is found to be accurate when compared to full numerical evaluation of the field.
Developed liquid film passing a trailing edge: small-scale analysis and the `teapot effect' at large Reynolds numbers
On the Mechanism of Large Amplitude Flapping of Inverted Foil in a Uniform Flow
On Secondary Tones Arising in Trailing-Edge Noise at Moderate Reynolds Numbers
![QR code for arXiv:2202.13936 [physics.flu-dyn]](http://oss.arxitics.com/images/favicon.svg)