WEI Zuojun

Research

Research Assistant Professor Department of Mechanics and Aerospace Engineering

Dr. ZuoJun Wei, graduated from Northwestern Polytechnical University (China), is now a Research Associate in Southern University of Science and Technology in Shenzhen. His is majored in Aeronautical and Astronautical Science and Technology.

Personal Profile

Research

His main research interests are aerothermodynamics of aero-engine and aerodynamics of turbomachinery. He focuses on the study of theoretical foundations and engineering techniques. His research fields include: endwall flow mechanism and control of turbmachinery, micro-turbine engine design, high-load turbine aerodynamic design, Turbine cooling design and analysis, aircraft/engine integration analysis, etc.

Publications Read More

[1] Wei, Z. J., Qiao, W. Y., Liu, J. Duan, W. H.,Reduction of Endwall Secondary Flow Losses with Leading-Edge Fillet in a Highly-Loaded Low Pressure Turbine [J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 2016, 230(2): 184-195.

[2] Wei, Z. J., Qiao, W. Y., Shi, P. J., Chen, P. P., Zhao, L., Tip-leakage flow loss reduction in a two-stage turbine using axisymmetric-casing contouring. Chinese Journal of Aeronautics. 2014, 27(5): 1111-1121.

[3] Wei, Z. J., Qiao, W. Y., Chen, P. P., Liu, J., Formation and Transport of Secondary Flows Caused by Vortex-Blade Interaction in a High Pressure Turbine [C]. ASME Paper. GT2015-42426.

[4] Wei Z, Duan W, Qiao W, Liu J, Han P. Analysis and control of tip-leakage vortex core stability of turbine rotor. Journal of Aerospace Power. 2018; 33: 2139-49.

[5] Wei Z, Qiao W, Duan W, Liu J. Influence of scrapping effect on formation of casing passage vortex in turbine rotor. Journal of Aerospace Power. 2018; 33: 1695-704.

[6] Wei, Z., Qiao, W., Shi, P., Zhao, L. Effect of contoured casing design on tip-leakage loss in a turbine[J]. Journal of Aerospace Power, 2015, 30(3): 714-725.

[7] Wei, Z., Qiao, W., Zhao, L., Shi, P. Numerical investigation of endwall losses control in turbine by leading edge fillet based on teardrop curves[J]. Journal of Aerospace Power, 2015, 30(2): 473-482.

News More

SUSTech wins Shenzhen “Talent Bole Award” for 4th consecutive year
2019-11-14
SUSTech Annual Research Symposium 2019 comes to a successful close
2019-11-14
Global Scientist Interdisciplinary Forum2020
2019-10-24

Lab members Read More

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Founded in December 2015, the Department of Mechanics and Aerospace Engineering (MAE) is one of departments in the College of Engineering. It aims to establish a world-leading department in mechanics and aerospace engineering, covering various research areas such as fluid mechanics, aerodynamics, thermodynamics, aeroacoustics, mechanics, combustion, material, and system control. The Department will learn from the best practice of peer departments over the world in order to develop into an international research institution that attends to the national strategic needs in mechanics and aerospace, cultivates outstanding innovative talents, and conducts frontier fundamental research and applied research with social impact.

The goal of the Department is to become a top-tier international leader through introducing an innovative education system which emphasizes IUR (Industry-University-Research) in close association with the Chinese aerospace industry. The specific objectives are: 1) to nurture innovative talents (learning); 2) to research and develop key technologies (research); and 3) to provide technical services (production) for the national aerospace industry.