An experimental investigation was performed in an anechoic wind tunnel involving acoustic
measurements, hot-wire anemometry and surface flow visualisation techniques to …

A review on passive acoustic control of airfoil self-noise by means of porous trailing edge is
presented. Porous surfaces are defined using various terms such as porosity, permeability …

Slat/fuselage juncture noise or slat horn noise has been identified as a major airframe noise
component and is commonly assumed to be similar to the flap side-edge noise. However …

This paper deals with the development of a three-dimensional (3D) array for imaging
aeraocoustic sources in the open section of an anechoic wind-tunnel, together with the …

One known method to reduce vortex shedding from the tip of a blade is the use of end plates
or winglets. Although the aerodynamic impact of such end plates has been investigated in …

The reduction of wingtip vortices is a critical and challenging task for aircraft wing-design.
Inspired by the wingtip morphology of soaring birds, Whitcomb created winglets to reduce …

As a result of vortex instability, wingtip vortex exhibits a behavior of wandering. In the paper,
a canonical wingtip vortex generated by a NACA0015 rectangular wing was experimentally …

The last 10 years have seen the establishment of the hybrid anechoic wind tunnel as a
significant tool for experimental aeroacoustics research. The hybrid anechoic wind tunnel …

The noise generated by finite, wall-mounted airfoils strongly affects the total noise from
aerodynamic applications such as small unmanned aerial vehicles, micro wind turbines and …

The application of the turbulent boundary layer trailing edge (TBL-TE) noise component of
the semi-empirical Brooks-Pope-Marcolini (BPM) model in an axial flow fan case study is …