Modelling and control of coherent turbulent structures in aerodynamics and aeroacoustics
Time: Wed 2025-11-05 10.00 - 11.00
Location: Faxén, Teknikringen 8
Video link: https://kth-se.zoom.us/j/3366544548
Participating: André Cavalieri (ITA, Brazil)
Abstract: Despite the intrinsic complexity of turbulent flows, large-scale coherent structures are present in turbulence, and are related to aerodynamic drag and sound radiation, for example. This presentation shows methods to model such coherent structures, and approaches to control flows in order to reduce drag and noise radiation. Linear models will be considered first, with coherent structures modelled as dominant responses from the linearised Navier-Stokes system. Such dominant modes compare favourably with coherent structures educed from experimental or numerical data, and allow the proposition of changes to the system aiming at drag or noise reduction; moreover, such linearised models allow the formulation of estimation and control problems, with successful experimental applications. Non-linear reduced-order models (ROMs) are then obtained by the Galerkin projection of the full governing equations onto a basis of modes obtained from the linearised system. Quantitative agreement with reference statistics is obtained for a number of canonical flow configurations. Finally, a ROM for turbulent Couette flow is used to devise a control method aiming at turbulence suppression. The obtained strategy is seen to relaminarise turbulence in direct numerical simulations, showing that ROMs so obtained have promising applications in optimisation and control.
Bio: André Cavalieri is an Associate Professor at ITA. He has a degree in Aeronautical Engineering from ITA, and a PhD in Fluid Mechanics from the University of Poitiers under the supervision of Peter Jordan and Yves Gervais. Prof. Cavalieri has research on aeroacoustics, turbulence and flow control, with a close collaboration with KTH for the last ten years. Since 2024, André Cavalieri is the Dean of Graduate Studies of ITA.