When the pressure fluctuations caused by turbulence vorticity in the boundary layer are
scattered by a sharp trailing edge, acoustic energy is generated and propagated to the far …

The ability of some species of owl to fly in effective silence is unique among birds and
provides a distinct hunting advantage, but it remains a mystery as to exactly what aspects of …

Trailing edge serrations designed to reduce airfoil self-noise are retrofitted on a NACA 0018
airfoil. An investigation of the boundary layer flow statistical properties is performed using …

This paper presents an analytic solution for aerodynamic noise generated by an unsteady
wall pressure gust interacting with a spanwise-variable trailing edge in a background steady …

This paper investigates the effects of finite flat porous extensions to semi-infinite
impermeable flat plates in an attempt to control trailing-edge noise through bio-inspired …

This paper considers the effects of smoothly varying chordwise porosity of a finite perforated
plate on turbulence–aerofoil interaction noise. The aeroacoustic model is made possible …

Numerical simulations, using a lattice-Boltzmann technique, have been carried out to study
the effect of aerodynamic loading and Reynolds number on the aeroacoustics of a porous …

Lattice Boltzmann simulations were carried out to investigate the noise mitigation
mechanisms of a 3-D printed porous trailing-edge insert, elucidating the link between noise …

A large-eddy simulation of turbulent, compressible flow around a NACA 0012 airfoil at zero
angle of attack and Mach number 0.115 is used to study mechanisms of trailing-edge noise …

In this paper, an approach for the reduction of trailing edge noise due to flow scattering from
a semi-infinite splitter plate is proposed. It utilizes the fluid–structure interactions of well …