Summary
Biography: Spencer Sherwin is Head of Department and Professor of Computational Fluid Mechanics in the Department of Aeronautics at Imperial College London. He received his MSE and PhD from the Department of Mechanical and Aerospace Engineering Department at Princeton University. Prior to this he received his BEng from the Department of Aeronautics at Imperial College London.
Group web page: www.sherwinlab.info
Research: Professor Sherwin leads an active research group specializing in the development and application of parallel high order spectral/hp element methods (Nektar ) for flow around complex geometries with a particular emphasis on vortical and bluff body flows and biomedical modelling of the cardiovascular system. More recently, he has been closely involved in industrial application of these methods through partnerships with McLaren Racing, Airbus and Rolls Royce. Previously he also held a RAEng/McLaren Racing Fellowship during which spectral/hp element methods were applied to problems of interest of Formula One aerodynamics that promoted the development of wall resolving large eddy simulation capabilities for highly unsteady and separated flows
Other Activities: Currently Professor Sherwin is Principal Investigator on the EPSRC funded Platform for Research In Simulation Methods.
Publications
Journals
Lindblad D, Isler J, Moragues Ginard M, et al. , 2024, Nektar++: development of the compressible flow solver for jet aeroacoustics, Computer Physics Communications, Vol:300, ISSN:0010-4655
Moura RC, Fernandes LD, da Silva AFC, et al. , 2024, Joint-mode diffusion analysis of discontinuous Galerkin methods: Towards superior dissipation estimates for nonlinear problems and implicit LES, Journal of Computational Physics, Vol:505, ISSN:0021-9991
Green MD, Kirilov KS, Turner M, et al. , 2024, NekMesh: An open-source high-order mesh generation framework, Computer Physics Communications, Vol:298, ISSN:0010-4655
Gao AK, Cantwell CD, Son O, et al. , 2023, Three-dimensional transition and force characteristics of low-Reynolds-number flows past a plunging airfoil, Journal of Fluid Mechanics, Vol:973, ISSN:0022-1120