[HTML][HTML] Design and characterisation of an open-jet pressure gradient test rig for an aeroacoustic wind tunnel
This paper summarises an approach to generating controllable pressure gradients within an
open-jet configuration for aeroacoustics research. A novel open-jet pressure gradient test rig …
open-jet configuration for aeroacoustics research. A novel open-jet pressure gradient test rig …
[PDF][PDF] On the implementation of simultaneous unsteady surface pressure, far-field noise and PIV flow measurements in an anechoic wind tunnel
Aeroacoustic noise arises from the unsteady surface pressures caused by the interaction
between an object and the surrounding fluid flow. Identifying flow structures contributing to …
between an object and the surrounding fluid flow. Identifying flow structures contributing to …