Teng Fei Assistant Research Professor
Email：feiteng@tsinghua.edu.cn
Address：Tsinghua University, Haidian District, Beijing
Education
2011.09~2015.06, School of Aerospace Engineering, Beijing Institute of Technology. Bachelor
2015.09~2021.03, School of Aerospace Engineering, Beijing Institute of Technology. Doctoral degree
Research Interests
Internal and external flow aerodynamics, turbomachinery aero-thermodynamic layout design, high-loaded fan/compressor design.
Research Overview
Fei Teng has been engaged in the research of turbomachinery aerodynamic design, with a focus on the development and refinement of aerodynamic design systems. He has developed a through-flow design and optimization platform tailored for the compression system of variable cycle engines. His research covers aerodynamic and thermodynamic layout design and optimization of turbomachinery, aerodynamic performance modeling of high-loaded compressors, and unsteady flow analysis.
Academic Achievements
[1] Zhang S, Ji L, Fei T*. Flow Mechanism and Performance Modeling for Variable Camber Stator in Variable Cycle Engine. Aerospace Science and Technology, 2025.
[2] Shen Y, Ji L, Fei T*. Inter-Row Traveling Shock in a Transonic Turbine. Chinese Journal of Aeronautics, 2025.
[3] Fei T, Ji L, Zhou L. Application of Neural Network Model in Compressor Through-Flow Analysis. Journal of Aerospace and Power, 2022.
[4] Fei T, Ji L. Application of New Empirical Models Based on Mathematical Statistics in the Through-Flow Analysis. Journal of Thermal Science, 2021.
[5] Fei T, Ji L, Yi W. Performance Characteristic Modeling for 2D Compressor Cascades. International Journal of Turbo & Jet-Engines, 2019.
[6] Fei T, Ji L. Yi W. Investigation of the Dihedral Angle Effect on the Boundary Layer Development Using Special-Shaped Expansion Pipes. Proceedings of the ASME Turbo Expo, 2018.
[7] Fei T, Li J. Ji L. Yi W. Investigation of the Boundary Layer Development at the Corner of the Special-Shaped Expansion Pipe. International Society for Air Breathing Engines, 2017.
