Professor Ning Qin
School of Mechanical, Aerospace and Civil Engineering
Professor of Aerodynamics
n.qin@sheffield.ac.uk
+44 114 222 7718
+44 114 222 7718
Sir Frederick Mappin Building
Full contact details
Professor Ning Qin
School of Mechanical, Aerospace and Civil Engineering
Sir Frederick Mappin Building
Mappin Street
Sheffield
S1 3JD
School of Mechanical, Aerospace and Civil Engineering
Sir Frederick Mappin Building
Mappin Street
Sheffield
S1 3JD
- Profile
-
Ning Qin has been a Professor of Aerodynamics in our Department of Mechanical Engineering since 2003. Before moving to Sheffield he was Professor of Computational Aerodynamics between 1999-2003 at Cranfield University. He obtained his PhD degree in Aerospace Engineering in 1987 from the University of Glasgow on the subject of computational aerodynamic prediction of hypersonic heating on space planes.
Professor Qin teaches in the Mechanical and Aerospace BEng/MEng and MSc programmes including Wind Turbine Aerodynamics(MEC316) and Compressible Flows(MEC449). He has conducted research in the development of computational fluid dynamics and its application to aircraft, gas turbines and wind turbines with over 300 publications. He has successfully supervised and graduated over 40 PhD students. He is a Fellow of the Royal Aeronautical Society and an Associate Fellow of the American Institute of Aeronautics and Astronautics. He serves as an Associate Editor for RAeS Aeronautical Journal and IMechE Journal of Aerospace Engineering.
You can find Professor Qin's Research Impact at https://impact.ref.ac.uk/casestudies/CaseStudy.aspx?Id=8246
- Publications
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Books
- Advances in Effective Flow Separation Control for Aircraft Drag Reduction Modeling, Simulations and Experimentations. Springer.
- The little book of thermofluids. Sheffield: University of Sheffield Dept.of Mechanical & Process Engineering. View this article in WRRO
Journal articles
- Sensor placement for data assimilation of turbulence models using eigenspace perturbations. Physics of Fluids, 36(1).
- Aerodynamic load reduction on a supercritical airfoil using tilted microjets. International Journal of Aerospace Engineering, 2023.
- Adjoint based aero-structural design optimisation of a transonic fan blade. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy.
- Gust load alleviation control based on jets for natural laminar airfoil. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 43(11).
- Numerical study on impact of shock control bump on transonic buffet. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 43(11).
- Fast prediction of transonic flow field using deep learning method. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 43(11).
- Cooperation of trailing-edge flap and shock control bump for robust buffet control and drag reduction. Aerospace, 9(11).
- A review of flow control for gust load alleviation. Applied Sciences, 12(20).
- A combined experimental and numerical study on aerodynamic load reduction for a swept wing by using jets. Aerospace Science and Technology, 107935-107935.
- Drag reduction in wall-bounded turbulence by synthetic jet sheets. Journal of Fluid Mechanics, 941.
- Gust load alleviation on an aircraft wing by trailing edge Circulation Control. Journal of Fluids and Structures, 107, 103407.
- Gust load alleviation by normal microjet. Aerospace Science and Technology, 117.
- Vortex-generating shock control bumps for robust drag reduction at transonic speeds. AIAA Journal.
- Balancing laminar extension and wave drag for transonic swept wings. AIAA Journal.
- Laminar separation bubble dynamics and its effects on thin airfoil performance during pitching-up motion. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.
- Anisotropic Adjoint Sensitivity-Based Mesh Movement for Industrial Applications. Computers & Fluids, 104929-104929.
- Uncertainty analysis and robust shape optimisation for laminar flow aerofoils. The Aeronautical Journal, 125(1284), 365-388.
- Using shock control bumps to improve engine intake performance and operability. The Aeronautical Journal, 124(1282), 1913-1944.
- Sequential feature‐based mesh movement and adjoint error‐based mesh refinement. International Journal for Numerical Methods in Fluids.
- Unsteady shock front waviness in shock-buffet of transonic aircraft. Advances in Aerodynamics, 2(1). View this article in WRRO
- Influence of Spanwise Load Distribution on Blended-Wing–Body Performance at Transonic Speed. Journal of Aircraft, 57(3), 408-417.
- Airfoil gust load alleviation by circulation control. Aerospace Science and Technology. View this article in WRRO
- Quantification of airfoil aerodynamic uncertainty due to pressure-sensitive paint thickness. AIAA Journal. View this article in WRRO
- Forebody shock control devices for drag and aero-heating reduction: A comprehensive survey with a practical perspective. Progress in Aerospace Sciences. View this article in WRRO
- Using shock control bumps to improve transonic fan/compressor blade performance. Journal of Turbomachinery, 141(8). View this article in WRRO
- Shock control of a low-sweep transonic laminar flow wing. AIAA Journal, 57(6), 2408-2420. View this article in WRRO
- Using the Reynolds Stress Model to Predict Shock-Induced Separation on Transport Aircraft. Journal of Aircraft. View this article in WRRO
- Delaunay graph-based moving mesh method with damping functions. Chinese Journal of Aeronautics, 31(11), 2093-2103. View this article in WRRO
- Bryan Richards: Contributions to aerospace engineering. Progress in Aerospace Sciences, 101, 1-12.
- Quantitative comparison of 2D and 3D shock control bumps for drag reduction on transonic wings. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 233(7), 2344-2359. View this article in WRRO
- The impact of realistic casing geometries and clearances on fan blade tip aerodynamics. Journal of Turbomachinery, 140(6). View this article in WRRO
- Drag reduction investigation for hypersonic lifting-body vehicles with aerospike and long penetration mode counterflowing jet. Aerospace Science and Technology, 76, 361-373. View this article in WRRO
- Nonconsistent mesh movement and sensitivity calculation on adjoint aerodynamic optimization. AIAA Journal, 56(4), 1541-1553. View this article in WRRO
- Development of a smoothed particle hydrodynamics method and its application to aircraft ditching simulations. Aerospace Science and Technology, 66, 28-43.
- Delaunay Graph Based Inverse Distance Weighting for Fast Dynamic Meshing. Communications in Computational Physics, 21(5), 1282-1309.
- Trailing-edge flow control devices for wind turbine performance and load control. Renewable Energy, 105, 419-435. View this article in WRRO
- Spike Effects on Drag Reduction for Hypersonic Lifting Body. Journal of Spacecraft and Rockets, 54(6), 1185-1195. View this article in WRRO
- Efficient Method to Eliminate Mesh Sensitivity in Adjoint-Based Optimization. AIAA Journal, 55(4), 1140-1151.
- Novel Compressor Blade Shaping Through a Free-Form Method. Journal of Turbomachinery, 139(8).
- Using Surface Sensitivity from Mesh Adjoint for Transonic Wing Drag Reduction. AIAA Journal, 55(3), 818-831.
- Deformable Overset Grid for Multibody Unsteady Flow Simulation. AIAA Journal, 54(8), 2392-2406. View this article in WRRO
- Comparison of turbulent flow through hexagram and hexagon orifices in circular pipes using large-eddy simulation. Fluid Dynamics Research, 48(2).
- Novel Method to Calculate Vibrational Thermal Conduction in Hypersonic Nonequilibrium Flow. Journal of Thermophysics and Heat Transfer, 30(1), 12-24.
- Delaunay graph and radial basis function for fast quality mesh deformation. Journal of Computational Physics, 294, 149-172. View this article in WRRO
- Numerical Computation of Compressible and Viscous FlowR. W. MacCormack American Institute of Aeronautics and Astronautics, 1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344, USA. 2014. Distributed by Transatlantic Publishers Group, 97 Greenham Road, London, N10 1LN, UK (Tel: 020-8815 5994; e-mail: mark.chaloner@tpgltd.co.uk). 521pp.Illustrated. £84 (20% discount available to RAeS members on request). ISBN 978-1-62410-264-6.. The Aeronautical Journal, 119(1214), 560-560.
- Modelling roughness effects for transitional low Reynolds number aerofoil flows. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 229(2), 280-289. View this article in WRRO
- A passive scalar-based method for numerical combustion. International Journal of Hydrogen Energy, 40(33), 10658-10661.
- Geometric Representation of Flow Features Using the Medial Axis for Mesh Generation. AIAA Journal, 53(1), 246-259. View this article in WRRO
- Using the medial axis to represent flow features for feature-aligned unstructured quad-dominant mesh generation. Computers & Fluids, 102, 1-14.
- Simulations of combustion with normal and angled hydrogen injection in a cavity-based supersonic combustor. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 228(4), 530-541.
- Intuitive Class/Shape Function Parameterization for Airfoils. AIAA Journal, 52(1), 17-25.
- Hybrid RANS/LES for active flow control. Aircraft Engineering and Aerospace Technology, 86(3), 179-187.
- Zipper layer method for linking two dissimilar structured meshes. Journal of Computational Physics, 255(0), 130-148.
- The influence of transition onset location on the performance of shock control bumps. AERONAUTICAL JOURNAL, 117(1196), 1037-1051.
- Shock control bump optimization for a low sweep supercritical wing. Science China Technological Sciences, 56(10), 2385-2390.
- Shock control bump optimization for drag reduction using parallel efficient global optimization algorithm. Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 45(4), 485-490.
- Aerodynamic optimization of transonic wing using discrete adjoint operator. Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 45(3), 347-352.
- Design of tip airfoil of wind turbine based on hybrid parameterization modification theory. Taiyangneng Xuebao/Acta Energiae Solaris Sinica, 34(4), 555-561.
- Aerodynamic performance, benefits of utilising camber morphing wings for unmanned air vehicles. Aeronautical Journal, 117(1189), 329-340.
- Aerodynamic performance benefits of utilising camber morphing wings for unmanned air vehicles. AERONAUTICAL JOURNAL, 117(1189), 315-327.
- Design optimization of casing grooves using zipper layer meshing. Journal of Turbomachinery, 136(3).
- Planform Effects for Low-Reynolds-Number Thin Wings with Positive and Reflex Cambers. JOURNAL OF AIRCRAFT, 50(3), 952-964. View this article in WRRO
- Three-dimensional laminar-separation bubble on a cambered thin wing at low reynolds numbers. Journal of Aircraft, 50(1), 152-163.
- Hybrid Reynolds-averaged Navier-Stokes/large-eddy simulation of jet mixing in a supersonic crossflow. Science China Technological Sciences, 1-14.
- Adjoint based on high precise aerodynamic shape optimization for transonic civil aircraft. Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 30(6).
- A numerical study of blade thickness and camber effects on vertical axis wind turbines. Proceedings of the Institution of Mechanical Engineers, Part A, Journal of Power and Energy. View this article in WRRO
- A NEW EFFICIENT CONTROL METHOD FOR BLENDED WING BODY. International Journal of Modern Physics: Conference Series, 19, 396-405.
- Balancing destruction and production in S-A Model-based hybrid RANS-LES for flow around an aerofoil with mild separation. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 117, 379-388.
- Training algorithms for EGO method and applications. Jisuan Wuli/Chinese Journal of Computational Physics, 29(3), 326-332.
- Comparison of hybrid RANS-LES methods for massively separated flows. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 117, 257-266.
- Surrogate-based multi-objective aerothermodynamic design optimization of hypersonic spiked bodies. AIAA Journal, 50(4), 797-810.
- Unsteady flow simulation and dynamic stall behaviour of vertical axis wind turbine blades. Wind Engineering, 35(4), 511-527.
- Numerical investigation of aeroheating characteristics of spiked blunt bodies at Mach six flight conditions. AERONAUT J, 115(1168), 377-386.
- Active Transonic Aerofoil Design Optimization Using Robust Multiobjective Evolutionary Algorithms. JOURNAL OF AIRCRAFT, 48(3), 1084-1094.
- Shock control bump design optimization on natural laminar aerofoil. Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010, 253-259.
- Recent advances in the aerothermodynamics of spiked hypersonic vehicles. Progress in Aerospace Sciences, 47(6), 425-449.
- A solution adaptive simulation of compressible multi-fluid flows with general equation of state. International Journal for Numerical Methods in Fluids, 67(5), 616-637.
- Recent advances in the aerothermodynamics of spiked hypersonic vehicles. Progress in Aerospace Sciences.
- Behavior of detached-eddy simulations for mild airfoil trailing-edge separation. Journal of Aircraft, 48(1), 193-202.
- Quadrilateral cell-based anisotropic adaptive solution for the euler equations. Communications in Computational Physics, 9(1), 68-88.
- Effects of pitching rotation on aerodynamics of tandem flapping wing sections of a hovering dragonfly. AERONAUT J, 114(1161), 699-710.
- Vortex Capturing Using PNS-WENO Schemes in Uniform and Non Uniform Mesh Formulations. ADV APPL MATH MECH, 2(4), 399-429.
- Metamodels for aerothermodynamic design optimization of hypersonic spiked blunt bodies. AEROSP SCI TECHNOL, 14(5), 364-376.
- Wind tunnel and numerical study of a small vertical axis wind turbine. RENEW ENERG, 35(2), 412-422. View this article in WRRO
- Drag Reduction Using Aerodisks for Hypersonic Hemispherical Bodies. J SPACECRAFT ROCKETS, 47(1), 62-80.
- A General Profile Parameterization of Hydrodynamic Journal Bearings for Efficient Shape Optimization. TRIBOL T, 53(1), 117-126.
- Multiquadric Finite Difference (MQ-FD) Method and its Application. ADV APPL MATH MECH, 1(5), 615-638.
- A combined experimental and numerical study of flow structures over three-dimensional shock control bumps. AEROSP SCI TECHNOL, 12(6), 436-447.
- Detached eddy simulation of a synthetic jet for flow control. P I MECH ENG I-J SYS, 222(I5), 373-380.
- Three-dimensional contour bumps for transonic wing drag reduction. P I MECH ENG G-J AER, 222(G5), 619-629.
- Biologically Inspired Shape Changing Aerodynamic Profiles and their Effect on Flight Performance of Future Aircraft. Advances in Science and Technology, 56, 534-544.
- New dynamic grid algrithm and its application. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 29(4), 817-822.
- BILU implicit multiblock Euler/Navier-Stokes simulation for rotor tip vortex and wake convection. INT J NUMER METH FL, 55(6), 509-536.
- Development of a local MQ-DQ-based stencil adaptive method and its application to solve incompressible Navier-Stokes equations. INT J NUMER METH FL, 55(4), 367-386.
- Promoting scientific and technical communication in aerospace engineering with China. P I MECH ENG G-J AER, 221(G2), I-I.
- Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps. AERONAUT J, 111(1117), 165-174.
- Wake vortex model for real-time flight simulation based on large eddy simulation. J AIRCRAFT, 44(2), 467-475.
- Iterative response surface based optimization scheme for transonic airfoil design. J AIRCRAFT, 44(2), 365-376.
- Editorial. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 221(2), i-i.
- Study of the effects of wing sweep on the aerodynamic performance of a blended wing body aircraft. P I MECH ENG G-J AER, 221(G1), 47-55.
- Aerofoil profile and sweep optimisation for a blended wing-body aircraft using a discrete adjoint method. AERONAUT J, 110(1111), 589-604.
- Flow feature aligned grid adaptation (vol 67, pg 787, 2006). INT J NUMER METH ENG, 67(6), 894-894.
- Flow feature aligned grid adaptation. INT J NUMER METH ENG, 67(6), 787-814.
- Fast dynamic grid deformation based on Delaunay graph mapping. J COMPUT PHYS, 211(2), 405-423.
- An efficient moving grid algorithm for large deformation. MODERN PHYSICS LETTERS B, 19(28-29), 1499-1502.
- Detached-Eddy Simulation for synthetic jets with moving boundaries. MODERN PHYSICS LETTERS B, 19(28-29), 1429-1434.
- ASYMMETRY OF FLOW AT HIGH ANGLE OF ATTACK(Compressible Flow). The Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF), 2005(0), 661-666.
- Elimination AD applied to Jacobian assembly for an implicit compressible CFD solver. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 47(10-11), 1315-1321.
- Spanwise lift distribution for blended wing body aircraft. J AIRCRAFT, 42(2), 356-365.
- Aerodynamic considerations of blended wing body aircraft. PROG AEROSP SCI, 40(6), 321-343.
- Variable-fidelity aerodynamic optimization for turbulent flows using a discrete adjoint formulation. AIAA J, 42(7), 1281-1292.
- Numerical study of active shock control for transonic aerodynamics. INT J NUMER METHOD H, 14(4), 444-466.
- Mechanism of windward vortex shocks about supersonic slender bodies. AERONAUT J, 106(1063), 507-519.
- Monotone integrated large eddy simulations for supersonic boundary layer flows. Computational Fluid Dynamics Journal, 10(4), 548-552. View this article in WRRO
- Non-inertial multiblock Navier-Stokes calculation for hovering rotor flowfields using relative velocity approach. AERONAUT J, 105(1049), 379-389.
- An eddy-viscosity limited algebraic stress model for shook-boundary-layer interaction. AERONAUT J, 105(1045), 105-118.
- Study of the aerodynamics of in-plane motion. P I MECH ENG G-J AER, 215(G2), 89-104.
- Calculation of compressible indicial response. AERONAUT J, 104(1042), 665-673.
- A matrix-free preconditioned Newton/GMRES method for unsteady Navier-Stokes solutions. INT J NUMER METH FL, 33(2), 223-248.
- Hypersonic performance of a lifting elliptic cone with and without strakes. JOURNAL OF SPACECRAFT AND ROCKETS, 37(1), 21-27.
- Grid adaption for shock/turbulent boundary-layer interaction. AIAA JOURNAL, 37(9), 1129-1131.
- Massively separated flows due to transverse sonic jet in laminar hypersonic stream. SHOCK WAVES, 9(2), 87-93.
- Unsteady flow around helicopter rotor blade sections in forward flight. AERONAUT J, 103(1019), 35-44.
- Computational prediction of pitch damping for supersonic blunt cones. JOURNAL OF SPACECRAFT AND ROCKETS, 35(6), 849-851.
- Surface suction on aerofoil aerodynamic characteristics at transonic speeds. P I MECH ENG G-J AER, 212(G5), 339-351.
- Calculation of pitch damping for a flared projectile. JOURNAL OF SPACECRAFT AND ROCKETS, 34(4), 566-568.
- Incipient separation boundary: Confirmation of an empirical criterion by Navier-Stokes solutions. AERONAUT J, 100(999), 381-384.
- Computational study of supersonic lateral jet flow interactions. J SPACECRAFT ROCKETS, 33(5), 651-656.
- ALPHA-GMRES - A NEW PARALLELIZABLE ITERATIVE SOLVER FOR LARGE SPARSE NONSYMMETRICAL LINEAR-SYSTEMS ARISING FROM CFD. INT J NUMER METH FL, 15(5), 613-623.
- Newton-like methods for Navier-Stokes solution.
- Newton-like methods for fast high resolution simulation of hypersonic viscous flows. Computing Systems in Engineering, 3(1-4), 429-435.
- Newton-like methods for Navier-Stokes solution.
- SHOCK-SHOCK, SHOCK-VORTEX INTERACTION AND AERODYNAMIC HEATING IN HYPERSONIC CORNER FLOW. AERONAUT J, 95(945), 152-160.
- Sparse Quasi- Newton Method for Navier- Stokes Solution, 474-483.
- Sparse quasi-Newton method for high resolution schemes. Notes on Numerical Fluid Mechanics, 20, 310-317.
- An Inverse method for boundary separated flows. Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 4(4), 12-21. View this article in WRRO
- On-the-Fly Unsteady Adjoint Aerodynamic and Aeroacoustic Optimization Method. AIAA Journal, 1-19.
- Optimization of transonic low-Reynolds number airfoil based on genetic algorithm. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.
- Cross-Field Structured Adaptive Mesh Using Medial Axis Flow Feature Extraction. AIAA Journal, 1-16.
- Closed-Loop Control of Transonic Buffet Using Active Shock Control Bump. Aerospace, 10(6), 537-537.
- Hybrid Mesh Deformation for Aerodynamic-Structural Coupled Adjoint Optimization. AIAA Journal, 1-14.
- EXPLORING TOPOLOGY OPTIMISATION FOR HIGH PRESSURE TURBINE BLADE TIPS. Journal of Turbomachinery, 1-14.
- Parameterizing Airfoil Shape Using Aerodynamic Performance Parameters. AIAA Journal, 1-14.
- Quantification of airfoil aerodynamics due to geometric uncertainties based on adjoint method. Journal of the Chinese Institute of Engineers, 1-9.
- An exploitation-enhanced multi-objective efficient global optimization algorithm for expensive aerodynamic shape optimizations. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 095441002110324-095441002110324.
- PNS solution using sparse Quasi-Newton method for fast convergence, 453-454.
- Simulation of hypersonic viscous flows around a cone-delta-wing combination by an implicit method with multigrid acceleration, 528-532.
- Benefit Assessment of Low-Sweep Transonic Natural Laminar Flow Wing for Commercial Aircraft. Journal of Aircraft, 1-8.
Chapters
- A Hybrid RANS-LES Dataset for Data-Driven Turbulent Mean Flow Reconstruction, Proceedings of the Cambridge Unsteady Flow Symposium 2024 (pp. 121-133). Springer Nature Switzerland
- Load Control on the Future Greener Aircraft by Circulation Control, Advances in Computational Methods and Technologies in Aeronautics and Industry (pp. 105-116). Springer International Publishing
- Plasma Models in Hybrid RANS-LES Simulation for Backward Facing Step Flow Control, Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 93-112). Springer International Publishing
- Active Flow Control Strategies and Tools for Turbulent Flows, Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 1-26). Springer International Publishing
- Novel Spanwise Vortex Generator for Separation Control on BFS: Experiment and Simulation, Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 255-264). Springer International Publishing
- Hybrid RANS-LES Simulations of Incipient Airfoil Trailing Edge Separation, Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 327-341). Springer International Publishing
- Effects of DBD Plasma Frequency, Voltage, and Modulation on BFS Flow Reattachment, Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 131-143). Springer International Publishing
- Description of the Test Cases, Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 27-53). Springer International Publishing
- Application of the Polymer Based Pressure Sensitive Paint for Qualitative and Quantitative Flow Visualisation in a Transonic Flow, 29th International Symposium on Shock Waves 1 (pp. 441-446). Springer International Publishing
- Oscillation-Free Adaptive Simulation of Compressible Two-Fluid Flows with Different Types of Equation of State, ERCOFTAC Series (pp. 103-117). Springer Netherlands
- Detached Eddy Simulation for Turbulent Flows in a Pipe with a Snowflake Fractal Orifice In Nicolleau FCGA, Cambon C, Redondo J-M, Vassilicos JC, Reeks M & Nowakowski AF (Ed.), New approaches in modelling multiphase flows and dispersion in turbulence, fractal methods and synthetic turbulence (pp. 9-21). Springer Netherlands
- Approaching morphing wing concepts on the basis of micro aerial vehicles - art. no. 65270K In Davis LP, Henderson BK & McMickell MB (Ed.), SPIE Smart Structures and Materials & Nondestructive Evaluation and Health Monitoring, 18 - 22 March 2007, San Diego, California USA (pp. K5270-K5270).
- From flying wings to blended wing body aircraft,, McGraw-Hill Yearbook of Science and Technology 2006 McGraw-Hill Professional; Revised edition edition (1 Jan. 2006)
- Godunov Methods Springer US
Conference proceedings papers
- Aerodynamic Shape Optimisation Using a Machine Learning-Augmented Turbulence Model. AIAA SCITECH 2024 Forum
- A Priori Sensor Placement Strategy for Turbulent Mean Flow Reconstruction Using Parametric Model Perturbations. AIAA SCITECH 2024 Forum
- Experimental and Numerical Investigation on Aerodynamic Performance of a Mars Rotor System. ICAS Proceedings
- Acoustic and Aerodynamic Performance of Serrated Leading Edges on the Bypass Outlet Guide Vanes. Volume 13D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery, 26 June 2023 - 30 June 2023.
- Multidisciplinary Optimisation of High Pressure Turbine Blade Tip With Turbine Inlet Capacity and Stage Reaction Constraints. AIAA AVIATION 2021 FORUM
- Structurally Constrained Aerodynamic Adjoint Optimisation of Highly Loaded Compressor Blades. Volume 2D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery, 7 June 2021 - 11 June 2021.
- Structural Integrity of Serrated Leading Edge Guide Vane Blades for Noise Reduction. Volume 9B: Structures and Dynamics — Fatigue, Fracture, and Life Prediction; Probabilistic Methods; Rotordynamics; Structural Mechanics and Vibration, 7 June 2021 - 11 June 2021.
- Using Feature-Based Mesh Adaptation to Improve the Adjoint Optimisation of Transonic Compressor Blades. Volume 2C: Turbomachinery, 21 September 2020 - 25 September 2020.
- The Influence of Parameterisation Setup on the Constrained Adjoint Optimisation of Transonic Fan Blades. Volume 2D: Turbomachinery, 21 September 2020 - 25 September 2020.
- Exploring Topology Optimisation of High Pressure Turbine Blade Tips. Volume 2B: Turbomachinery, 21 September 2020 - 25 September 2020.
- Using Shock Control Bumps to Improve Transonic Fan/Compressor Blade Performance. Volume 2A: Turbomachinery, 11 June 2018 - 15 June 2018. View this article in WRRO
- Efficient Adjoint-Based Mesh Adaptation Applied to Turbo-Machinery Flows. Volume 2C: Turbomachinery, 11 June 2018 - 15 June 2018.
- Prediction of Unsteady Transonic Buffeting using the SU2 Open-Source Code. Proceedings of the 7th European Conference on Computational Fluid Dynamics (ECFD 7). Glasgow, 11 June 2018 - 15 June 2018. View this article in WRRO
- Efficient adjoint-based mesh adaptation applied to turbo-machinery flows. Proceedings of the ASME Turbo Expo, Vol. 2C-2018
- Quantification and Multi-point Optimization of Natural Laminar Flow Airfoil Robustness to Transition Amplification Factor. 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
- An efficient multiobjective global optimization algorithm for expensive aerodynamic shape optimizations. 10th International Conference on Computational Fluid Dynamics, ICCFD 2018 - Proceedings
- Fan Blade Tip Aerodynamics With Realistic Operational Casing Geometries and Clearances. Volume 2A: Turbomachinery, 26 June 2017 - 30 June 2017.
- Robustness of Natural Laminar Flow Airfoil Drag Optimization to Transition Amplification Factor. 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
- Understanding fan blade tip aerodynamics. 12th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2017 View this article in WRRO
- Fan blade tip aerodynamics with realistic operational casing geometries and clearances. Proceedings of the ASME Turbo Expo, Vol. 2A-2017
- Effect of Non-Consistent Mesh Movements and Sensitivities on a Discrete Adjoint Based Aerodynamic Optimization. 55th AIAA Aerospace Sciences Meeting
- Understanding fan blade tip aerodynamics. 12th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2017
- Combined Hessian and Adjoint Error-Based Anisotropic Mesh Adaptation for Turbomachinery Flows. 55th AIAA Aerospace Sciences Meeting
- Local class shape transformation parameterization (l-CST) for airfoils. 55th AIAA Aerospace Sciences Meeting
- Understanding the aerodynamics of the fan blade tip. 12th European Conference on Turbomachinery Fluid Dynamics and hermodynamics, 3 April 2017 - 7 April 2017.
- Understanding fan blade tip aerodynamics. European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC
- Vortex Generators for Increased Maximum Lift and Enhanced High-α Stability of a Zimmerman-Wing MAV at Low Reynolds Number. 2016 Applied Aerodynamics Conference View this article in WRRO
- Robust Delaunay Graph Based Mesh Movement for Adjoint Mesh Sensitivity. 2016 Applied Aerodynamics Conference View this article in WRRO
- Alleviation of Shock-Wave Effects on a Highly Loaded Axial Compressor Through Novel Blade Shaping. Volume 2A: Turbomachinery, 13 June 2016 - 17 June 2016.
- Using A Fast and Explicit Mesh Movement Method To Efficiently Compute Mesh Sensitivity. 54th AIAA Aerospace Sciences Meeting View this article in WRRO
- Deformable Overset Grid for Unsteady Aerodynamic Simulation. 54th AIAA Aerospace Sciences Meeting, 4 January 2016 - 8 January 2016. View this article in WRRO
- Using surface sensitivity from mesh adjoint solution for transonic wing drag reduction. 54th AIAA Aerospace Sciences Meeting View this article in WRRO
- The effect of leading edge rounding on a caret waverider configuration at Mach 8.2. 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016
- FAST DYNAMIC MESHING METHOD BASED ON DELAUNAY GRAPH AND INVERSE DISTANCE WEIGHTING INTERPOLATION. International Journal of Modern Physics: Conference Series, Vol. 42 (pp 1660166-1660166)
- Investigation of pitching angle on pressure load for ditching of helicopter using SPH method. 46th AIAA Fluid Dynamics Conference
- Fluid Structure Interaction on a Flexible Micro Air Vehicle. 53rd AIAA Aerospace Sciences Meeting View this article in WRRO
- Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings. 53rd AIAA Aerospace Sciences Meeting View this article in WRRO
- Kriging-algorithm-based Aerodynamic Model for Flush Airdata System. Procedia Engineering, Vol. 99 (pp 507-514)
- Effects of Gurney Flap and Shock Bump on Supercritical and NLF Transonic Aerofoil. Royal Aeronautical Society Applied Aerodynamics Conference 2014. London, UK, 22 July 2014 - 24 July 2014.
- Further Development of CST Geometric Parameterisation Method forAdjoint Aerodynamic Optimisation. ADVANCED AERO CONCEPTS, DESIGN AND OPERATIONS, APPLIED AERODYNAMICS CONFERENCE 2014. London, 22 July 2014 - 24 July 2014.
- Robust Design of 3D Shock Control Bumps on a Transonic Wing. ADVANCED AERO CONCEPTS, DESIGN AND OPERATIONS, APPLIED AERODYNAMICS CONFERENCE 2014. London, 22 July 2014 - 24 July 2014.
- Using the Medial Axis to Represent Complex Flow Structures for Flow Feature-Aligned Mesh Generation. AIAA Paper 2013-0150. Grapevine, Texas, USA, 7 January 2013 - 13 January 2013.
- Multi-Objective Aerothermodynamic Design of Hypersonic Spikes and Forebodies. Proceedings of International Symposium on Hypersonic Aerothermodynamics – Recent Advances. Bangalore, India, 9 December 2012 - 13 December 2012.
- Simulation of aerodynamic flow control. The 2nd International Conference on Scientific Computing in Aerodynamics. Beijing, China, 18 October 2012 - 20 October 2012.
- Hybrid RANS/LES Simulation of Flow Control. Proceedings of the 9th Asian Computational Fluid Dynamics Conference. Nanjing, China, 11 October 2012 - 13 October 2012.
- Shock Control Bump Optimization For a Low Sweep Supercritical Wing And Its Impact On Fuel Reduction. Proceedings of the 9th Asian Computational Fluid Dynamics Conference. Nanjing, China, 11 October 2012 - 13 October 2012.
- A New Method For Linking Two Dissimilar Structured Meshe. Proceedings of the 9th Asian Computational Fluid Dynamics Conference. Nanjing, China, 11 October 2012 - 13 October 2012.
- Development of CST Geometric Parameterisation Method for an Entire Transport Aircraft. RAeS Applied Aerodynamic Conference: Modelling and Simulation in the Aerodynamic Design Process, 17 July 2012 - 19 July 2012.
- Propeller Effects on Low Reynolds Number Aerodynamics. RAeS Applied Aerodynamic Conference: Modelling and Simulation in the Aerodynamic Design Process, 17 July 2012 - 19 July 2012.
- Investigation of the flow asymmetry around axi-symmetric spiked blunt bodies at hypersonic speeds. RAeS Applied Aerodynamic Conference: Modelling and Simulation in the Aerodynamic Design Process, 17 July 2012 - 19 July 2012.
- Drag Reduction for Transonic Wings Combining Reduced Wing Sweep with Shock Control (pp 45-53)
- Prediction of Transition Location and Its Effects on Shock Bump Control on a Natural Laminar Flow Aerofoil (pp 251-256)
- Surrogate-Based Multi-objective Aerothermodynamic Design Optimization of Hypersonic Spiked Bodies (pp 727-733)
- Numerical Simulation of Thermal-Chemical Non-equilibrium and Radiating Hypersonic Flow (pp 165-171)
- Zipper layer method. Proceedings of the 20th International Meshing Roundtable, IMR 2011 (pp 587-599)
- Design optimisation of casing grooves using the zipper layer meshing method. Proceedings of the ASME Turbo Expo, Vol. 7(GT2011-45483) (pp 1163-1174). Vancouver, Canada, 6 June 2011 - 10 June 2011.
- Boundary Layer Effects on Shock Bump Performance. RAeS Aerodynamics Conference 2010, Applied Aerodynamics: Capabilities and Future Requirements. Bristol, UK, 27 July 2011 - 28 July 2011.
- Adaptive Wing/Aerofoil Design Optimisation Using MOEA Coupled to Uncertainty Design Method. 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition View this article in WRRO
- Comparison of RANS, DES and DDES Results for ONERA M-6 Wing at Transonic Flow Speed Using an In-House Parallel Code. 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition View this article in WRRO
- 2-D Numerical Analysis of a VAWT Wind Farm for Different Configurations. 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
- Delaunay Graph Mapping-Based Mesh Deformation for Simulation of a Spanwise Rigid and flexible Flapping NACA0012 Wing Using DES with Parallel Implementation. 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition View this article in WRRO
- Study of CFD simulation of a 3-D wind turbine. ICMREE2011 - Proceedings 2011 International Conference on Materials for Renewable Energy and Environment, Vol. 1 (pp 596-600)
- A MUSCL and WENO - PNS approach for vortex dominated flowfields. AIAA Paper 2010-503. Orlando, Florida, USA, 4 January 2010 - 7 January 2010.
- Drag Reduction Using Aerodisks for Hypersonic Hemispherical Bodies. CEAS 2009 Air and Space Conference. Manchester, UK, 26 October 2009 - 29 October 2009.
- Alleviating UAV Pitch Divergence at High Lift Condition. RAeS Aerodynamics Conference 2010, Applied Aerodynamics: Capabilities and Future Requirements. London, 27 July 2010 - 28 July 2010.
- Numerical Simulations of Plunging NACA0012 Wing for MAV Propulsion Systems. International Micro Air Vehicle Conference and Flight Competition, IMAV 2010. Braunschweig, Germany, 6 July 2010 - 9 July 2010.
- Detached-Eddy Simulation of Weapon Bay at Transonic Speed. IBCAST 2010 : The 7th International Bhurban Conference on Applied Sciences & Technology. Islamabad, Pakistan, 11 January 2010 - 14 January 2010.
- Metamodels for aerothermodynamic design optimization of hypersonic spiked blunt bodies. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition(AIAA-2010-1318). Orlando, Florida, USA, 4 January 2010 - 7 January 2010.
- Three dimensional adaptive method for compressible multi-fluids flows. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition(AIAA-2010-812). Orlando, Florida, USA, 4 January 2010 - 8 January 2010. View this article in WRRO
- Flow separation on cambered plate wing MAVs with various aspect ratios. RAeS Conference on Applied Aerodynamics: Capabilities and Future Requirements
- Assessment of des on the flow after a snow-flake orifice. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 111 (pp 157-165)
- Flapping Wing Simulation and Kinematics Analysis Based on Dragonfly Wing Section in Hover. CEAS 2009 Air and Space Conference. Manchester, UK, 26 October 2009 - 29 October 2009.
- Control of NACA0015 Aerofoil Stall using Synthetic Jet Actuators. CEAS 2009 Air and Space Conference. Manchester, UK, 26 October 2009 - 29 October 2009.
- Vortex Capturing Using PNS-WENO Schemes. CEAS 2009 Air and Space Conference. Manchester, UK, 26 October 2009 - 29 October 2009.
- Mesh movement, adaptation and feature alignment. Modern Trends in Computational Aerodynamics (Invited). Birmingham, UK, 16 September 2009 - 16 September 2009.
- Comparison of Response Surface and Kriging Surrogates in Aerodynamic Design Optimization of Hypersonic Spiked Blunt Bodies. Aerospace Science and Technology Conference. Egypt, 1 May 2009 - 5 May 2009.
- Buffer layer method for linking two non-matching multi-block structured grids. 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition(AIAA-2009-1361). Orlando, Florida, USA, 5 January 2009 - 8 January 2009.
- Detached Eddy Simulation of Turbulence Flows in a Pipe with Fractal Shape Orifices. ADVANCES IN TURBULENCE XII - PROCEEDINGS OF THE 12TH EUROMECH EUROPEAN TURBULENCE CONFERENCE, Vol. 132 (pp 947-948)
- Biologically Inspired Shape Changing Aerodynamic Profiles and their Effect on Flight Performance of Future Aircraft. EMBODING INTELLIGENCE IN STRUCTURES AND INTEGRATED SYSTEMS, Vol. 56 (pp 534-544)
- Fluid-structure interaction of HALE wing configuration with an efficient moving grid method. 46th AIAA Aerospace Sciences Meeting and Exhibit(AIAA 2008-309). Reno, Nevada, 7 January 2008 - 10 January 2008.
- Flapping dragonfly tandem wings and their practicalities to hovering micro aerial vehicles. The Aerodynamics of Novel configurations: capabilities and future requirements. Proceedings of the 2008 Royal Aeronautical Society Annual Applied Aerodynamics Research Conference. London, 27 October 2008 - 28 October 2008.
- Unsteady Flow Simulation and Dynamic Stall Around Vertical Axis Wind Turbine Blades. 46th AIAA Aerospace Sciences Meeting and Exhibit
- Wind Tunnel and Numerical Study of a Small Vertical Axis Wind Turbine. 27th ASME Wind Energy Symposium(AIAA-2008-1316). Reno, Nevada, 7 January 2008 - 10 January 2008.
- Dynamic Mesh and Unsteady Flow for Flapping Airfoil with a Flexible Tail. 46th AIAA Aerospace Sciences Meeting and Exhibit(AIAA 2008-654). Reno, Nevada, 7 January 2008 - 10 January 2008.
- Unsteady flow simulation and dynamic stall around vertical axis wind turbine blades. 46th AIAA Aerospace Sciences Meeting and Exhibit
- Wind tunnel and numerical study of a small vertical axis wind turbine. 46th AIAA Aerospace Sciences Meeting and Exhibit
- Numerical simulation of flexible flapping airfoil propulsion using dynamic mesh at low reynolds numbers. 46th AIAA Aerospace Sciences Meeting and Exhibit
- DES applied to an isolated synthetic jet flow. ADVANCES IN HYBRID RANS-LES MODELLING (pp 252-260)
- Enhancing MAV Stability in Gusty Wind by Wing Flexibility: Analyses and Flight Tests. Unmanned Air Vehicle Systems. Bristol, UK, 16 April 2007 - 18 April 2007.
- Adjoint-based optimisation of a blended wing body aircraft with shock control bumps. Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, Vol. 1(AIAA-2007-57) (pp 531-543). Reno, Nevada, 8 January 2007 - 11 January 2007.
- Comparison of unsteady laminar and des solutions of synthetic jet flow. Collection of Technical Papers - AIAA Applied Aerodynamics Conference, Vol. 2(AIAA-2006-3161) (pp 878-888). San Francisco, California, 5 June 2006 - 8 June 2006.
- LES with numerical dissipation for aircraft wake vortices. Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting, Vol. 20(AIAA-2006-1258) (pp 15245-15257)
- Real-time model of wake vortices based on large eddy simulation datasets. Collection of Technical Papers - AIAA Modeling and Simulation Technologies Conference 2005, Vol. 1(AIAA-2005-6205) (pp 623-636). San Francisco, California,, 15 August 2005 - 18 August 2005.
- A numerical study of transonic flow in a wind tunnel over 3D bumps. 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers(AIAA 2005-1057) (pp 161-169)
- BILU implicit multiblock euler/navier-stokes simulation for helicopter rotor vortical flow. 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers(AIAA 2005-0465) (pp 2209-2222)
- Dynamic grid and unsteady boundary conditions for synthetic jet flow. 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers(AIAA 2005-0106) (pp 4047-4055)
- Differentiating a Time-dependent CFD Solver. The ADCompEng Meeting. Shrivenham, UK, 23 June 2005 - 23 June 2005.
- Validation and optimisation od 3D bumps for transonic wing drag reduction. CEAS KATnet Conference on Key Aerodynamic Technologies. Bremen, Germany, 20 June 2005 - 22 June 2005.
- Large Eddy Simulation of Aircraft Wake Vortices on a Hybrid Grid. CEAS/KATnet Conference on Key Aerodynamic Technologies. Bremen, Germany, 20 June 2005 - 22 June 2005.
- Detached-Eddy Simulation for Synthetic Jets in Cross-flows Using Dynamic Grid. CEAS/KATnet Conference on Key Aerodynamic Technologies. Bremen, Germany, 20 June 2005 - 22 June 2005.
- Detached-eddy simulation for synthetic jets with moving boundaries,. 1st International Symposium on Physics of Fluids. Huangshan, China, 9 June 2005 - 12 June 2005.
- An efficient moving grid algorithm for large deformation. 1st International Symposium on Physics of Fluids. Huangshan, China, 9 June 2005 - 12 June 2005.
- Dynamic grid solution of synthetic jets with oscillating membrane. RTO-MP-AVT-123 Flow-Induced Unsteady Loads and the Impact on Military Applications. Budapest, Hungery, 25 April 2005 - 28 April 2005.
- Application of Engineering Transition Models to an Isolated Helicopter Rotor in Hovering Flight. 43rd AIAA Aerospace Sciences Meeting and Exhibit
- Development and application of engineering transition model for rotorcraft aerodynamics. 30th European Rotorcraft Forum, Vol. 2005 (pp 143-160)
- Investigation of transition modelling for aerofoil dynamic stall. ICAS 2004 CD-ROM PROCEEDINGS, 29 August 2004 - 3 September 2004.
- Variable-Fidelity Aerodynamic Optimization for Turbulent Flows Using a Discrete Adjoint Formulation. 42nd AIAA Aerospace Sciences Meeting and Exhibit
- CFD for Better Understanding of Wind Tunnel Tests. First Symposium on Integrating CFD and Experiments in Aerodynamics. Glasgow, Scotland, UK, 8 September 2003 - 9 September 2003. View this article in WRRO
- A study of spanwise lift distribution for blended wing body aircraft. CEAS Aerospace Aerodynamics Research Conference. Cambridge, UK, 3 June 2002 - 6 June 2002.
- A discrete adjoint method for aerodynamic sensitivities for Navier-Stokes flows. CEAS Aerodynamics Research Conference. Cambridge, UK
- Aerodynamic studies of blended wing body aircraft. AIAA Paper 2002-5448. Atlanta, Georgia, USA, 4 September 2002 - 6 September 2002.
- 3D bumps for transonic wing shock control and drag reduction. CD-ROM. London, 10 June 2002 - 13 June 2002. View this article in WRRO
- The application of a parabolized navier-stokes solver to some hypersonic flow problems. 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference(AIAA 2001-1753)
- A numerical investigation of the flows in and around plug nozzle configurations. 19th AIAA Applied Aerodynamics Conference(AIAA 2001-2417), 11 June 2001 - 14 June 2001.
- Experience with the Osher scheme for applied aerodynamics. GODUNOV METHODS: THEORY AND APPLICATIONS (pp 707-715)
- Active control of transonic aerodynamics using suction, blowing, bumps and synthetic jets (Invited). AIAA 18th Applied Aerodynamics Conference, Vol. Invited Paper on Active Flow Control(AIAA 2000-4329). Denver, USA, 14 August 2000 - 17 August 2000.
- Viscous effects on transonic aeroelastic stability. Proceedings of the 4th Asian Computational Fluid Dynamics Conference, 18 September 2000 - 22 September 2000.
- Monotone integrated large eddy simulation for supersonic boundary layers. Proceedings of the 4th Asian Computational Fluid Dynamics Conference. Mianyang, China, 18 September 2000 - 22 September 2000.
- Non-inertial multiblock Navier-Stokes calculation for hovering rotor flowfields using high order approximate Riemann solver. Proceedings of the 4th Asian Computational Fluid Dynamics Conference. Mianyang, China, 18 September 2000 - 22 September 2000.
- Matrix-free implicit methods for applied aerodynamics. Proceedings of the 4th Asian Computational Fluid Dynamics Conference(Invited paper). Mianyang, China, 18 September 2000 - 22 September 2000.
- Towards a robust, efficient and accurate numerical solver for super/hypersonic flows over arbitrary geometries. ICAS 2000 CD-ROM PROCEEDINGS, 27 August 2000 - 1 September 2000.
- Phantom vorticity in Euler solutions on highly stretched grids. ICAS 2000 CD-ROM PROCEEDINGS. Harrogate, UK, 27 August 2000 - 1 September 2000.
- CFD study of shock control at Cranfield. ICAS 2000 CD-ROM PROCEEDINGS. Harrogate, UK, 27 August 2000 - 1 September 2000.
- A numerical investigation of the flows in and around annular plug nozzle configurations. ICAS 2000 CD-ROM PROCEEDINGS. Harrogate, UK, 27 August 2000 - 1 September 2000.
- Direct calculation of compressible indicial response using CFD. Aerodynamics Conference 2000: RAeS Proceedings 399. London, 3 April 2000 - 3 April 2000.
- Vorticity curvature based algebraic turbulence model for unsteady synthetic jet flow around aerofoils. Aerodynamics Conference 2000: RAeS Proceedings 399. London
- Non-inertial multiblock Navier-Stokes calculation for hovering rotor flowfields using high order upwind scheme. Aerodynamics Conference 2000: RAeS Proceedings 399. London
- A parametric study of the aerodynamics of inplane motion. Proceedings of the 25th European Rotorcraft Forum. Rome, 14 September 1999 - 16 September 1999.
- Numerical investigation of the appearance of windward vortex shock about slender bodies. Proceedings of the 22nd International Symposium on Shock Waves. London, 18 July 1999 - 23 July 1999.
- A numerical study of the relationship between steady and unsteady flow development for self-excited periodic flows. Proceedings of the 22nd International Symposium on Shock Waves. London, 18 July 1999 - 23 July 1999.
- Inclined suction and blowing for shock control at transonic speeds. Proceedings of the 22nd International Symposium on Shock Waves. London, 18 July 1999 - 23 July 1999.
- Abnormalities of Osher and AUSM+ scheme for hypersonic flows around swept cylinders and a cure. Proceedings of the 22nd International Symposium on Shock Waves. London, 18 July 1999 - 23 July 1999.
- Lifting elliptic cones with and without strakes at hypersonic speeds. Proceedings of 10th Symposium on Shock Waves in JAPAN 1999, 19 March 1999 - 21 March 1999.
- Effects of compressibility and roughness for turbulence modelling of hypersonic ramp flow. 37th Aerospace Sciences Meeting and Exhibit
- Multigrid acceleration of a preconditioned GMRES implicit PNS solver. 37th Aerospace Sciences Meeting and Exhibit
- Multigrid acceleration of a preconditioned GMRES implicit PNS solver. 37th Aerospace Sciences Meeting and Exhibit
- Algebraic turbulence modelling for vortical flows around slender bodies. Proceedings of the AGARD 82nd Fluid Dynamics Panel Symposium on Missile Aerodynamics, Vol. AGARD CP-608(Paper 20). Sorrento
- A matrix-free preconditioned Krylov-subspace method for the PNS equations. 36th AIAA Aerospace Sciences Meeting and Exhibit
- Computational prediction of pitch damping for high Mach number blunt projectiles. 36th AIAA Aerospace Sciences Meeting and Exhibit
- Grid adaptation for shock/turbulent boundary layer interaction. 36th AIAA Aerospace Sciences Meeting and Exhibit
- Linear and non-linear turbulence models for shock-wave/turbulent boundary-layer interaction using a strongly coupled approach. 36th AIAA Aerospace Sciences Meeting and Exhibit
- A matrix-free preconditioned Krylov-subspace method for the PNS equations. 36th AIAA Aerospace Sciences Meeting and Exhibit
- Linear and non-linear turbulence models for shock-wave/ turbulent boundary-layer interaction using a strongly coupled approach. 36th AIAA Aerospace Sciences Meeting and Exhibit
- Numerical simulation of flows in and around clustered module plug nozzles. European Space Agency Advanced Nozzles Workshop. Rome, Italy, 13 October 1997 - 13 October 1997.
- Numerical prediction of the aerodynamic response of aerofoils subject to step increases in Mach number. Proceedings of the 23nd European Rotorcraft Forum, Vol. 1 (pp 31.1-31.9)
- Control of shock induced separation by surface suction. Proceedings of the 3rd Pacific International Conference on Aerospace Science and Technology (pp 204-210)
- Computational and experimental investigation of hypersonic performance of a lifting elliptic cone with and without strakes. 15th Applied Aerodynamics Conference
- Structured grid adaptation and turbulence modelling for shock/boundary layer interactions. Proceedings of the 7th International Symposium on Computational Fluid Dynamics (pp 464-473)
- Solution of Delery’s transonic channel flow using the SST model. ECCOFTAC Workshop on Turbulence Models for Shock/Boundary Layer Interactions, 3 March 1997 - 3 March 1997.
- Calculation of pitch damping coefficients for projectiles. 35th Aerospace Sciences Meeting and Exhibit
- Two equation turbulence modelling using a strongly coupled high resolution approach. RAeS 1997 Aerodynamics Research Forum. London, 6 January 1997 - 6 January 1997.
- Calculation of pitch damping coefficients for projectiles. 35th Aerospace Sciences Meeting and Exhibit
- A unified high resolution approach for two equation turbulence modelling. Proceedings of the 3rd Pacific International Conference on Aerospace Science and Technology (pp 219-225)
- Massively separated flows due to transverse sonic jet in hypersonic laminar stream. Fluid Dynamics Conference
- Solution of the Navier-Stokes equations for the flow around an aerofoil in oscillating free stream. Proceeding of the 20th Congress of the International Council of the Aeronautical Sciences, Vol. 1 (pp 19-29)
- Solution of Navier-Stokes equations for aerofoils undergoing combined translation-pitch oscillations. Proceedings of the 22nd European Rotorcraft Forum, Vol. 1 (pp 55.1-55.14)
- A matrix-free Newton-GMRES method for steady and unsteady Navier-Stokes solutions. Proceedings of the 3rd ECCOMAS Computational Fluid Dynamics Conference (pp 784-790)
- Study of flow interactions due to a supersonic lateral jet using high resolution Navier-Stokes solutions. Fluid Dynamics Conference
- CFD modelling of a transverse control jet. TTCP WTP-2 Conference(Paper 23.2)
- Computation of supersonic viscous flows around a slender body at incidence. AIAA 12th Applied Aerodynamic Conferenc(AIAA paper 94-1938)
- High resolution numerical simulation of transonic turbulent flow around RAE2822 airfoil. 9th International Conference on System Engineering. Las Vegas, USA
- PARALLELIZING EXPLICIT AND FULLY IMPLICIT NAVIER-STOKES SOLUTIONS FOR COMPRESSIBLE FLOWS. PARALLEL COMPUTATIONAL FLUID DYNAMICS 92 (pp 407-418)
- SFDN ALPHA-GMRES AND SQN ALPHA-GMRES METHODS FOR FAST HIGH-RESOLUTION N-S SIMULATIONS. NUMERICAL METHODS FOR FLUID DYNAMICS 4 (pp 583-592)
- Fast, accurate, robust Navier-Stokes solvers for hypersonic flows over configurations. The 1st Hypersonic Aerodynamic Advisory Group(HAAG) Meeting. London
- Parallel alpha-GMRES solver and its application for Navier-Stokes equations. Proceedings of the Second Workshop on Parallel Numerical Analysis(EPCC-TR92-22). Edinburgh, UK
- Numerical modelling of the aerothermochemistry of spacecraft re-entry. Aerothermochemistry of spacecraft and associated hypersonic flows : proceedings of the IUTAM symposium (pp 228-235). Marseille, France, 1 September 1992 - 4 September 1992.
- Newton-like methods for Navier-Stokes solution
- A study of hypersonic laminar/turbulent flow over a slender cone by the LCNS code. Workshop on Hypersonic Flows for Re-entry Problems, Vol. Part II, Vol 2 (pp 1-13)
- Finite Volume 3DNS and PNS Solutions of Hypersonic Viscous Flow Around a Delta Wing using Osher’s Flux Difference Splitting (pp 947-959)
- Hypersonic viscous flows around waverider configurations. Proceedings of the 1st International Hypersonic Waverider Symposium. College Park, Maryland, U.S.A., 17 October 1990 - 19 October 1990.
- Numerical experiments using Navier-Stokes codes for generalised hypersonic shapes. Proceedings of the 17th Congress of the International Council of the Aeronautical Sciences, (pp 1927-1937)
- Shock-shock, shock-vortex interaction and aerodynamic heating in hypersonic corner flow. Proceedings of the International Conference on Hypersonic Aerodynamics (pp 26.1-26.15). Manchester, UK
- A parallelised Navier-Stokes code combining high resolution with fast convergence. Validation of Methods for Computational Fluid Mechanics and Progress in Methods for Navier-Stokes an. Surrey, UK
- Prediction of the hypersonic flow on the leeside of a cone-delta-wing combination. Euromech 225: the Aerodynamics of Spacecraft. Cranfield, UK
- Numerical experiments with hypersonic flow beneath a cone-delta-wing combination. Proceedings of AGARD Conference on Aerodynamics of Hypersonic Lifting Vehicles, Vol. AGARD-CP-428 (pp 20.1-20.14)
- Semi-inverse iterative solution for the supersonic separated flows over a compression corner. Proceedings of the Third National Conference on Computational Fluid Dynamics
- A new numerical method for solving supersonic separated flows over a compression corner by introducing an interactive boundary condition. Proceedings of the Third National Conference on Computational Fluid Dynamics
- Turbulent Mean Flow Reconstruction Based on Sparse
Multi-sensor Data and Adjoint-based Field Inversion. AIAA AVIATION 2022 Forum
- An open-source adjoint-based field inversion
tool for data-driven RANS modelling. AIAA AVIATION 2022 Forum
- Adjoint Based Aerodynamic Optimisation of a UCAV. AIAA Paper 2013-0146. Grapevine, Taxas, USA, 7 January 2013 - 13 January 2013. View this article in WRRO
- Home Page
Patents
- A Turbomachine Comprising an Annular Casing and a Bladed Rotor. GB Patent number 1101811.6 Appl. 01 May 2011.
- A Method of Connecting Meshes. GB Patent number 1101810.8 Appl. 01 May 2011.
- Shock Control Vortex Generating Bumps. International Patent No WO 2011/098807 A1 Appl. 09 Feb 2010.
- Shock Control Vortex Generating Bumps. GB Patent No. GB1002281.2 Appl. 09 Feb 2010.
- nacelle intake. US20200102067A1 Appl. 01 Jan 1970.
Theses / Dissertations
- Towards numerical simulation of hypersonic flow around space-plane shapes. University of Glasgow.
- Towards statistical inference to improve turbulence RANS closures for multi-element aerofoils.
Datasets
- Advances in Effective Flow Separation Control for Aircraft Drag Reduction Modeling, Simulations and Experimentations. Springer.
- Grants
-
ROLLS-ROYCE PLC (UK) 2021-2023, FANTASIA - MDO for Noise Reduction and Performance of Engine Components £282,922
EUROPEAN COMMISSION - HORIZON 2018-2021, MADELEINE, £371,308
ROLLS-ROYCE PLC (UK) 2019-2020, Design Guidelines for Low Noise Outlet Guide Vanes, £150,702
AIRBUS UK LIMITED 2019-2021, Aerodynamic optimisation for industrial implications, £7,886
ROLLS-ROYCE PLC (UK), 2019, Adjoint driven mesh sensitivity study for mesh adaption and quality control - extension, £30,000
EUROPEAN COMMISSION - HORIZON 2017-2019, DRAGY, £134,058
ROLLS-ROYCE PLC (UK) 2019, Composite Fan Tip Rubbing Investigation, £10,000
FIRST 4 WIND TURBINES LIMITED 2018, First 4 Wind Turbines, £25,371
ROLLS-ROYCE PLC (UK) 2017-2019, Adjoint driven mesh sensitivity study for mesh adaption and quality control, £100,698EUROPEAN COMMISSION - FP6/FP7, GReener Aeronautics International Networking-2 (GRAIN-2), £14,659
EUROPEAN COMMISSION - FP6/FP7, MARS, £197,366
- Teaching activities
-
MEC316 Renewable Energy: wind turbine aerodynamics
MEC449 Advanced Fluid Dynamics: compressible flows