Professor Ning Qin
BSc, MEng, PhD, AFAIAA, FRAeS

Professor of Aerodynamics
Head of Thermofluids Group
MEng Course Tutor (Year 3 & 4)
Department of Mechanical Engineering
Sir Frederick Mappin Building
Mappin Street
Sheffield
S1 3JD
UK
Telephone: +44(0)114 222 7718
Fax: +44(0)114 222 7890
email : n.qin@sheffield.ac.uk
Profile
With a PhD degree in Aerospace Engineering from the University of Glasgow, Ning Qin started his Aerodynamics/CFD research career working as a Research Fellow/Senior Research Fellow at Glasgow. He conducted research in the areas of predicting hypersonic heating (in the HOTOL spaceplane programme), investigating Navier-Stokes methods for high speed flows, developing Newton-like implicit methods for CFD and parallel computing on the Daresbury´s i860 Hypercube, an early national parallel computing system.
He moved to Cranfield University College of Aeronautics in 1994 and was appointed to the Chair of Computational Aerodynamics in 1999. At Cranfield, he established the Center for Computational Aerodynamics, with a wide range of funded research activities.
In 2003, he was appointed to a Chair of Aerodynamics and Fluid Mechanics at the University of Sheffield, heading the Aerodynamics and Thermo-Fluids Group.
Professor Qin is a Fellow of the Royal Aeronautical Society and an Associate Fellow of the American Institute of Aeronautics and Astronautics. He was awarded the RAeS Hafner Prize on VTOL Technology in 2000. He is an Associate Editor or on the Editorial Boards of a number of professional journals.
He is involved in a wide range of research and consultancy activities for Aerodynamic/CFD research and applications. He has published over 160 journal and conference papers in the area of Computational Fluid Dynamics and Aerodynamics. His recent research interest includes: flow control, aerodynamic and multi-disciplinary optimization, micro-fluidic simulations, helicopter unsteady aerodynamics; supersonic and hypersonic vortical flows and interactions; transonic flutter boundary prediction, and algorithm development for turbulence simulation. He obtained research funding from Research Councils and industries including EPSRC, Leverhulme Trust, EU, DERA(QinetiQ), BAE Systems, Westland Helicopters Ltd, Airbus, Rolls Royce and Aircraft Research Associates.
Areas of Research
The Aerodynamics Research Group's interest is in the development and application of computational aerodynamic tools to a wide range of industrial problems in aerospace, automotive, and environmental industries. These advanced tools provide in-depth analyses and design optimisation for engineering products, such as aircraft wing drag reduction, racing car down force enhancement, and wind turbine blade efficiency improvement.
The aerodynamic analysis and design tools vary from very fast panel methods to popular commercial CFD packages, from the most advanced adjoint method for optimisation (adj-MERLIN) to the detached eddy simulation software (DGDES) for massively separated turbulent flows, developed within the group.
Current projects include: wake vortex aircraft interactions for aviation safety, shock control for drag reduction, control bump optimisation for transonic wing performance, dynamic grid DES for synthetic jets flow control, and adaptive meshing techniques.
The Aerodynamics Research Group is equipped with a number of CFD pre- and post-processing packages for grid generation and flow visualisation, two Linux parallel computing clusters, and two low speed wind tunnels for experimental aerodynamic research and CFD validation.
Teaching
• MEC316 Solar and Wind Energ
• MEC380 Aircraft Design
• MEC404 Computational Fluid Dynamics
• MEC424 Aerodynamic Design
Recent Publications
- New dynamic grid algrithm and its application,
Liu, X., Li, Q., Chai, J., and Qin, N. (2008),
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 29(4), pp. 817-822. (journal subscription required)
- Three-dimensional contour bumps for transonic wing drag reduction,
Qin, N., Wong, W. S., and Le Moigne, A. (2008),
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 222(5), pp. 619-629.
Online (journal subscription required)
- Detached eddy simulation of a synthetic jet for flow control,
Qin, N. and Xia, H. (2008),
Proceedings of the Institution of Mechanical Engineers. Part I: Journal of Systems and Control Engineering, 222(5), pp. 373-380.
Online (journal subscription required)
- A combined experimental and numerical study of flow structures over three-dimensional shock control bumps,
Wong, W. S., Qin, N., Sellars, N., Holden, H., and Babinsky, H. (2008),
Aerospace Science and Technology, 12(6), pp. 436-447.
Online (journal subscription required)
- Development of a local MQ-DQ-based stencil adaptive method and its application to solve incompressible Navier-Stokes equations,
Shu, C., Shan, Y. Y., and Qin, N. (2007),
International Journal for Numerical Methods in Fluids, 55(4), pp. 367-386.
Online (journal subscription required)
- Study of the effects of wing sweep on the aerodynamic performance of a blended wing body aircraft,
Siouris, S. and Qin, N. (2007),
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 221(1), pp. 47-55.
Online (journal subscription required)
- Wake vortex model for real-time flight simulation based on large eddy simulation,
Spence, G. T., Le Moigne, A., Allerton, D. J., and Qin, N. (2007),
Journal of Aircraft, 44(2), pp. 467-475.
Online (journal subscription required)
- Iterative response surface based optimization scheme for transonic airfoil design,
Vavalle, A. and Qin, N. (2007),
Journal of Aircraft, 44(2), pp. 365-376.
Online (journal subscription required)
- Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps,
Wong, W. S., Le Molgne, A., and Qin, N. (2007),
Aeronautical Journal, 111(1117), pp. 165-174. (journal subscription required)
- BILU implicit multiblock Euler/Navier-Stokes simulation for rotor tip vortex and wake convection,
Zhong, B., Shaw, S., and Qin, N. (2007),
International Journal for Numerical Methods in Fluids, 55(6), pp. 509-536.
Online (journal subscription required)
- Fast dynamic grid deformation based on Delaunay graph mapping,
Liu, X., Qin, N., and Xia, H. (2006),
Journal of Computational Physics, 211(2), pp. 405-423.
Online (journal subscription required)
- Flow feature aligned grid adaptation,
Qin, N. and Liu, X. (2006),
International Journal for Numerical Methods in Engineering, 67(6), pp. 787-814.
Online (journal subscription required)
- Spanwise lift distribution for blended wing body aircraft,
Qin, N., Vavalle, A., and Moigne, A. L. (2005),
Journal of Aircraft, 42(2), pp. 356-365.
Online (journal subscription required)
- Elimination AD applied to Jacobian assembly for an implicit compressible CFD solver,
Tadjouddine, M., Forth, S. A., and Qin, N. (2005),
International Journal for Numerical Methods in Fluids, 47(10-11), pp. 1315-1321.
Online (journal subscription required)
- Variable-fidelity aerodynamic optimization for turbulent flows using a discrete adjoint formulation,
Moigne, A. L. and Qin, N. (2004),
AIAA Journal, 42(7), pp. 1281-1292.
Online (journal subscription required)
- Numerical study of active shock control for transonic aerodynamics,
Qin, N., Zhu, Y., and Shaw, S. T. (2004),
International Journal of Numerical Methods for Heat and Fluid Flow, 14(4), pp. 444-466.
Online (journal subscription required)
