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Research group
Aerodynamics and Flight Mechanics Group
Our group undertakes top-class research on fundamental fluid dynamics, applied aerodynamics, flow control, flight dynamics and aeroacoustics.
Part of
About
We undertake world-class research in aerodynamics and mechanics of flight whereby technological advancements achieved in our group can benefit academia, industry and society.
Our interactive and collegial community includes experts in:
- theoretical, computational and experimental fluid mechanics
- data-driven modelling and control
Using world-class experimental facilities and in-house computer simulation and modelling codes, we explore the underlying physics of fluid flow and control mechanisms. Our aim is to improve the aerodynamics and flight mechanics of the next generation of aerospace applications.
We proud to host the Airbus Noise Technology Centre. We also work with 2 Rolls-Royce University technology centres which carry out research into:
Research areas
Our main research areas include:
- flow instability, transition and turbulence
- compressible or high-speed flow
- biomimetic or urban or industrial aerodynamics
- aeroacoustics and aeroelasticity
- complex or multiphase fluid flow
- combustion and propulsion
- high-resolution optical flow diagnostics
- high-order DNS or LES and supercomputing technology
- data-driven modelling and control theory
People, projects and publications
People
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Research projects
Research project
The shadow of turbulence: algorithms and applications
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Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight
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Research project
Turb.Bound.Layers - Christina Vanderwel- MSCA IF
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UK Fluids Network
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UK Turbulence Consortium
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Understanding and exploiting non-equilibrium effects in turbulent boundary layers: towards realisable drag reduction strategies
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Vanderwel Christina - Simulating urban air pollution in the lab
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Z Hu - High-fidelity simulations and modelling of wall pressure on blade surfaces
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Z Xie - Large-Eddy Simulation Code for City Scale Environments
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Z Xie - Mathematical modelling of the mass transfer mechanisms at the top of an urban canopy: an LES and DNS study
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Publications
Felipe Alves Portela, Angela Busse & Neil Sandham,
2021, Physical Review Fluids, 6(8)
Type: article
Duo Zhang, Xueqiang Yuan, Shijie Liu, Xiaodong Cai, Haoyang Peng, Ralf Deiterding & Hoi Dick Ng,
2021, AIP Advances, 11(8)
DOI: 10.1063/5.0057586
Type: article
Daniel Kharlamov, Andrea Da Ronch, Jernej Drofelnik & Scott Walker,
2021, AIAA Journal, 59(8), 2916-2934
DOI: 10.2514/1.J059408
Type: article
Design and testing of a small-scale laboratory rotating detonation engine running on ethylene-oxygen
Hamilton Law, Tom Baxter, Charles Ryan & Ralf Deiterding,
2021
DOI: 10.2514/6.2021-3658
Type: conference
Peter Harmon, Ashish Vashishtha, Dean Callaghan, Cathal Nolan & Ralf Deiterding,
2021
DOI: 10.2514/6.2021-3529
Type: conference
I.K.A.P. Utama, Bagus Nugroho, M Yusuf, F A Prasetyo, M.L. Hakim, I K Suastika, Bharathram Ganapathisubramani, N. Hutchins & Jason P. Monty,
2021, Biofouling, 37(4), 372-386
Type: article
Eduardo Rodriguez-Lopez, Douglas Carter & Bharathram Ganapathisubramani,
2021, Journal of Fluids and Structures, 104
Type: article
David Lusher, Satya P Jammy & Neil Sandham,
2021, Computer Physics Communications, 267
Type: article
Olav Rømcke, Ivo R Peters & Jason R. Hearst,
2021, Physical Review Fluids, 6(6)
Type: article
2021, Journal of Computational Physics, 434
Type: article
Pagination
Wind tunnel: 2.1m by 1.5m by 4.4m
This is one of our larger wind tunnels. We use it for student research projects, wind engineering studies and marine industry work.
Wind tunnel: 3.5m by 2.4m by 10.5m
The R J Mitchell Wind Tunnel is the largest of our wind tunnels. It's ideal for vehicle aerodynamic work and performance sport testing. It can also be used for consultancy.
Soton UAV (Uncrewed Aerial Vehicle) laboratory
We design, manufacture and fly uncrewed aerial vehicles (UAVs) for research purposes.