Lijiabin  Assistant Research Fellow

Email：lijiabin@tsinghua.edu.cn

Address：Tsinghua University, Haidian District, Beijing, China

Education

Sep. 2014 – Jun. 2020: Ph.D. in Aerospace Propulsion Theory and Engineering, Beijing Institute of Technology

Sep. 2010 – Jun. 2014: B.Eng. in Aircraft Design and Engineering, Beijing Institute of Technology

Professional Experience

Mar. 2023 – Present: Assistant Research Fellow, Tsinghua University

Nov. 2020 – Mar. 2023: Postdoctoral Researcher, Tsinghua University

Research Interests

Internal and external flow aerodynamics, computational fluid dynamics, gas turbines and jet propulsion, air-breathing hypersonic flight propulsion, and advanced turbomachinery design technologies, high-loaded fan/compressor design.

Research Overview

Engaged in research on the flow mechanisms, flow control, and aerodynamic design of aero-engine fans/compressors, He had proposed the endwall vortex generator technology, a three-dimensional blade corner stall prediction factor, and the endwall flow field optimal chosen control technology. He had also explored the aerodynamic and thermodynamic layouts of highly loaded fans, small-sized vaneless counter-rotating fans/compressors, and axial supersonic through-flow fans. Additionally, He had developed the internal flow CFD calculation program TurboSim. He had published more than 30 academic papers and have been granted 9 invention patents.

Academic Achievements

[1] Li J, Ji L*. Efficient Design Method for Applying Vortex Generators in Turbomachinery. Journal of Turbomachinery. 2019; 141:081005.

[2] Li J, Ji L*, Yi W. An Improved Prediction Model for Corner Stall in Axial Compressors with Dihedral Effect. Chinese Journal of Aeronautics. 2020; 33(5):1433-1443.

[3] Li J, Li X, Ji L*, Yi W. Use of Blended Blade and End Wall method in compressor cascades: Definition and mechanism comparisons. Aerospace Science Technology. 2019; 92:738-749.

[4] Li J, Ji L, Zhou L*. Optimization Design of Blended Blade and Endwall in Compressor Cascade. Journal of Engineering for Gas Turbines and Power. 2020; 142:021003.

[5] Li J, Li W*, Ji L. Efficient Optimization Design of Vortex Generators in a Highly Loaded Compressor Stator. Journal of Engineering for Gas Turbines and Power. 2022; 144:061002.

[6] Jianci Ma, Jia Yu, Guanghao Shi, Lucheng Ji, Jiabin Li*. Flow control treatment for shock wave/boundary layer interaction of transonic shrouded rotors. Physics of Fluids, 2024, 36 (12): 126114.

[7] Jianhui Wu, Jiabin Li*, Teng Fei, Lucheng Ji. An evaluation strategy of control method for corner separation/stall in compressor cascades. Aerospace Science and Technology 2024, 155(3): 109743.

[8] Mengfei Hu, Jianhui Wu, Guanghao Shi, Lucheng Ji, Jiabin Li*. Effects of water ingestion on the aerodynamic performance of an axial compressor. Physics of Fluids, 2025, 37 (1): 013381.