Deputy Director of Aero Engine Research Center (Engineering & Research), Senior Engineer.
Zhifeng Xie was born in Yili, Xijiang Province, China in 1982. He received the Ph.D. degree in theoretical physics from Chinese Academy of Sciences in 2010 and M.S. degree from the Zhejiang University in 2005. Since 2010, he has worked for Aero Engine Research Center, School of Aerospace Engineering, Tsinghua Univ., Beijing, China. His research interests mainly include the design of aeroengine, structural dynamics, fluid mechanism.
Tel/Fax：010-62794843; E-mail：xzhf@tsinghua.edu.cn;
Education background
2001-2005 Zhejiang Univ. Chu Kochen Honors College, Bachelor
2005-2010 Chinese Academy of Sciences, Institute of Theoretical Physic, Doctor
Experience
2010-2012 Tsinghua Univ. School of Aerospace Engineering, Postdoctor
2012-2021 Tsinghua Univ. School of Aerospace Engineering, Assistant Professor
Areas of Research Interests/Research Projects
Aero engine rotor dynamics
Design of helicopter rotor system
Fluid-structure interaction analysis of aircraft
Research Status
The research focuses on the overall design of aero-engine and fluid-structure interaction analysis of aircraft. More than 10 scientific research projects have been completed, some of which have been put into the market.
Academic Achievement
Published 30 SCI papers since 2016.
1 Xie Zhifeng, Xu Quanyong, Guan Nanxiang*&,Zhou Ming, A new closed-form method for the inertia force and moment calculation in reciprocating piston engine design, Science China Technological Sciences, 2018:1-7
2 Liang Feng&, Zhifeng Xie*, Xia Aiguo, Zhou Ming, Aeroelastic simulation of the first 1.5-stage aeroengine fan at rotating stall. Chinese Journal of Aeronautics,Chinese Journal of Aeronautics, 2019, 33(2): 529-549.
3 Guan Nanxiang, Gu Yongpeng, Xie Zhifeng*,Zhou Ming A novel coaxial balance mechanism for reciprocating piston engines, Applied Sciences, Accepted
4 Lv Kaixiong&, Xie Zhifeng*, Zhou Ming, Bu Jianguo, A Comparative Study of Three Starting Strategies for an Aero Flywheel Motor Using the Modified DTC Method. IEEE Access 7: 59548-59558 (2019)
5 Feng Guangshuo&*, Xie Zhifeng, Zhou Ming, Geometric design and analysis of face-gear drive with involute helical pinion. Mechanism and Machine Theory, 2019, 134: 169-196.
6 Kang Qinmiao&, Li Yong, Xie Zhifeng*, Yongquan Liu, Zhou Ming, An Innovative Rail Pressure Sensor Signal Processing Algorithm to Determine the Start of Injection and End of Injection of Diesel Engines with Common Rail Injection Systems. IEEE Access 6: 64674-64687 (2018)
7 Zhang Ke&, Huang Xudong, Xie Zhifeng*, Zhou Ming, Design and optimization of a novel electrically controlled high pressure fuel injection system for heavy fuel aircraft piston engine. Chinese Journal of Aeronautics, 2018, 31(9): 1920-1928.
8 Xie Jiayi&, Guan Nanxiang&, Zhou Ming, Xie Zhifeng*, Study on the mechanism of variable-speed rotor affecting rotor aerodynamic performance, Appl. Sci. 2018, 8(7):1030
