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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
N. Sandham - FP7- LAPCAT II
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Research project
NIOPLEX-EU FP7-Prof. B. Ganapathisubramani
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Research project
Numerical Investigation of The True Sources of Jet Noise
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Research project
Please Mind The Gap: An Equations-driven Approach To Characterise The Aerodynamics Of Complex Vehicles
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Research project
Powrie - Track Systems for High Speed Railways: Getting it Right
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Research project
Prediction Of Boil-off Gas For LNG And LH2 Ships
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Research project
R Sandberg - UK Turbulence Consortium
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Research project
R Sandberg - UK Turbulence Consortium
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Research project
Richardson Ed - Cool Combustion Feasibility Study
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Research project
Sandham - EP/G058318/1 - Engineering of surfaces for drag reduction in water
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Publications
Gholamhossein Bagheri, Eberhard Bodenschatz, John Lawson, Moláček Jan, Freja Nordsiek & Oliver Schlenczek,
2022
Type: bookChapter
Dongfeng Li, Zhengzhong Wang, Andrea Da Ronch & Gang Chen,
2022, Aircraft Engineering and Aerospace Technology, 94(6), 881-894
Type: article
Xinxin Wang, Ralf Deiterding, Jianhan Liang, Xiaodong Cai & Wandong Zhao,
2022, Computers & Fluids, 237(105314)
Type: article
Thankgod, Enatimi Boye & Zheng-Tong Xie,
2022, Journal of Wind Engineering and Industrial Aerodynamics, 223, 1-40
Type: article
Magnus K. Vinnes, Stefano Gambuzza, Bharathram Ganapathisubramani & R. Jason Hearst,
2022, Journal of Renewable and Sustainable Energy, 14(2)
DOI: 10.1063/5.0074218
Type: article
Kelsey C. Tang-Yuk, XiaoCheng Mi, John H.S. Lee, Hoi Dick Ng & Ralf Deiterding,
2022, Combustion and Flame, 236
Type: article
Han Peng, Chay, William Charles Atkins & Ralf Deiterding,
2022, Computers & Fluids, 232
Type: article
Chengyang Huang, Yuan Wang, Ralf Deiterding, Dehai Yu & Zheng Chen,
2022, Acta Mechanica Sinica, 38(2)
Type: article
John Lawson & Bharathram Ganapathisubramani,
2022, Experiments in Fluids, 63(1)
Type: article
Jose Miguel Garro Fernandez, David Angland & Zhiwei Hu,
2022
DOI: 10.2514/6.2022-4100
Type: conference
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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.