Postdoc: Resolvent-based Optimisation for Airframe Aeroacoustics

Building on recent advances in mean-field-based linearised modelling for aeroacoustics, and in particular for modelling sound generation by flow–structure interaction, the 2AT group is developing resolvent-based shape-optimisation tools. The successful candidate will collaborate with Airbus and 2AT researchers to develop an adjoint-based shape-optimisation framework for landing-gear aeroacoustics. The numerical methodology will rely on a resolvent formulation of the Boundary Element Method. Optimised geometries will be tested in the anechoïc windtunnels of Institut PPRIME using microphone-array based source localisation.