Chen Zhanjun Research Associate
Email：chenzhanjun@mail.tsinghua.edu.cn
Address：Tsinghua University, Haidian District, Beijing, P. R. China
Education
Doctor of Philosophy in Fluid Mechanics, China Academy of Aerospace Aerodynamics
Master of Science in Fluid Mechanics, Beihang University
Bachelor of Engineering in Aircraft Design and Engineering, Nanjing University of Aeronautics and Astronautics
Professional Experience
Nov 2025 - Present: Research Associate, Institute for Aero Engine, Tsinghua University
Apr 2021 - Nov 2025: Postdoctoral Fellow, School of Aerospace Engineering, Tsinghua University
Jan 2012 - Mar 2021: Engineer, China Academy of Aerospace Aerodynamics
Research Interests
Rotating Detonation Propulsion-based Aircraft-Engine Integration
New Concept Aircraft Design
Research Overview
Engaged in the overall design and aircraft-engine integration research of new propulsion aircraft, with a focus on rotating detonation propulsion aircraft design, key technology research and development, and engineering application research. Participated as a core member in more than 20 projects including basic scientific research, special projects and JKW Foundation programs. Completed over 10 high and low-speed flight tests. Published more than 10 journal papers and international academic reports, and obtained 10 authorized patents.
Academic Achievements
1. X. Jin, S. Xu, B. Wang, Z. Chen. Numerical investigation on the effects of InSb geometry on the InGaSb crystal growth under microgravity, Microgravity Science and Technology, 35, 2023
2. Z. Chen, Z. Liu. Nonlinear Flight Dynamics of Very Flexible Aircraft, The 24th International Conference on Structural, Computational & Experimental Research, Tokyo, Japan, 2019
3. Z. Chen, Z. Liu. Dynamic Analysis of Very Flexible Aircraft, The 2nd International Conference on Aerospace Engineering, Seoul, South Korea, 2018
4. Z. Chen, et al. Invention Patent: A Built-in Fixing Device for Solid Rocket Motors, CN 112610359 B
5. Z. Chen, et al. Invention Patent: A Design Method for Thermal Load Release of Bolted Connections, CN 111017250 B
