关注
Dr Alistair John
Dr Alistair John
Research Associate, University of Sheffield
在 sheffield.ac.uk 的电子邮件经过验证
标题
引用次数
引用次数
年份
Novel compressor blade shaping through a free-form method
A John, S Shahpar, N Qin
Journal of Turbomachinery 139 (8), 081002, 2017
462017
Using shock control bumps to improve transonic fan/compressor blade performance
A John, N Qin, S Shahpar
Journal of Turbomachinery 141 (8), 081003, 2019
232019
Alleviation of shock-wave effects on a highly loaded axial compressor through novel blade shaping
A John, S Shahpar, N Qin
Turbo Expo: Power for Land, Sea, and Air 49699, V02AT37A040, 2016
182016
Structurally constrained aerodynamic adjoint optimisation of highly loaded compressor blades
C Cuciumita, A John, N Qin, S Shahpar
Turbo Expo: Power for Land, Sea, and Air 84935, V02DT36A016, 2021
92021
The impact of realistic casing geometries and clearances on fan blade tip aerodynamics
A John, N Qin, S Shahpar
Journal of Turbomachinery 140 (6), 061002, 2018
82018
The influence of parameterisation setup on the constrained adjoint optimisation of transonic fan blades
A John, N Qin, S Shahpar
Turbo Expo: Power for Land, Sea, and Air 84096, V02DT38A020, 2020
72020
Exploring topology optimization for high pressure turbine blade tips
L Vincekovic, A John, N Qin, S Shahpar
Journal of Turbomachinery 144 (7), 071013, 2022
52022
Using Feature-Based Mesh Adaptation to Improve the Adjoint Optimisation of Transonic Compressor Blades
A John, G Vivarelli, N Qin, S Shahpar
Turbo Expo: Power for Land, Sea, and Air 84089, V02CT35A036, 2020
22020
Using shock control bumps to improve transonic fan/compressor blade performance
A John, N Qin, S Shahpar
Turbo Expo: Power for Land, Sea, and Air 50992, V02AT39A042, 2018
22018
Improving jet engine aerodynamic design via novel component shaping and analysis
A John
University of Sheffield, 2018
22018
Understanding fan blade tip aerodynamics
A John, S Shahpar, N Qin
12 th European Conference on Turbomachinery Fluid dynamics & Thermodynamics, 2017
22017
Using shock control bumps to improve engine intake performance and operability
A John, J Bower, N Qin, S Shahpar, A Smith
The Aeronautical Journal 124 (1282), 1913-1944, 2020
12020
Nacelle intake
N Qin, S Shahpar, AR Smith
US Patent App. 16/575,544, 2020
12020
Fan Blade Tip Aerodynamics With Realistic Operational Casing Geometries and Clearances
A John, N Qin, S Shahpar
Turbo Expo: Power for Land, Sea, and Air 50787, V02AT39A033, 2017
12017
DRAFT: THE INFLUENCE OF PARAMETERISATION SETUP ON THE CONSTRAINED ADJOINT OPTIMISATION OF TRANSONIC FAN BLADES
A John, N Qin, S Shahpar
DRAFT: USING FEATURE-BASED MESH ADAPTATION TO IMPROVE THE ADJOINT OPTIMISATION OF TRANSONIC COMPRESSOR BLADES
A John, G Vivarelli, N Qin, S Shahpar
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