Zhang Bocheng, Research Fellow, his research interests include aeroelasticity, structural dynamics and aircraft design, including aeroelastic mechanism analysis and design of intelligent aircraft structures, flutter analysis and design, static aeroelastic analysis and design, structural dynamics analysis and design, wind tunnel model design and manufacturing technology, scaled flight test technology, etc. He used to be the deputy chief engineer of aeroelasticity of COMAC Beijing Research Center, and served as the technical leader and project leader in the key technology research projects of the early demonstration of  long-range wide-body aircraft, the key technology project of C929 model development, the future model pre-research project and the civil aircraft special pre-research project. As a reviewer for journals such as Journal of Aircraft and Engineering Applications of Computational Fluid Mechanics.

Mechanics, mechanics, aerospace, structure, structure dynamics and other related majors are welcome to apply for the research group graduate students. The research group has  aeroelastic laboratories in the Hangzhou campus to satisfy the experimental needs of students, postdocs and researchers.

E-mail: zbchz@buaa.edu.cn.

Representative papers:

（1）Transonic Flutter Analysis of the AGARD 445.6 Wing in Frequency Domain Using the Euler Method, Engineering Applications of Computational Fluid Mechanics，Zhang Bocheng*, Ding Weilong, Ji Shengcheng, Zhang Jiazhen. 2016: 244-255；

（2）Damping anti-vibration design and opti miｚation method of co mposite skin with hard coating, Journal of Beihang, Bocheng Zhang *, Jian Zhang, et.al. 2020、46(8): 1469-1475；

（3）Aeroelastic two-level optimization for preliminary design of wing structures considering robust constraints  Chinese Journal of aeronautics、Wan Zhiqiang, Zhang Bocheng，duziliang，Yang Chao*、2014、27(2)：259-265；

（4）A Method for Static Aeroelastic Analysis Based on the High-order Panel Method and Modal Method, SCIENCE CHINA: Technological Sciences Yang Chao, Zhang Bocheng*, Wan Zhiqiang, Wang Yaokun、2011、54(3)：741-748；

（5）Static Aeroelastic Analysis of a High-aspect-ratio Wing Based on Wind-tunnel Experimental Aerodynamic Forces.  SCIENCE CHINA: Technological Sciences、Wan Zhiqiang, Zhang Bocheng*, Yang Chao, Xu Yan、2011、54(10)：2716-2722；

（6）Load calibration experiment analysis for scaled model of large aspect ratio wing (ID: AE1007),the 2022 International Conference on Mechanical, Aerospace and Automotive Engineering( CMAAE 2022), Qiaozhen Sun, Bocheng Zhang, Haoqian Yuan.

（7）Zhang Bocheng.  Low Speed Flutter Wind Tunnel Experiment Technology Based on Binocular Vision System.  IEEE ICICSP 2024 conference.

Recent research projects:

(1) Research on Dynamic Mechanism of flying wing, National Key Laboratory Fund Project, 2025-2026, Project leader;

(2) Calculation of hinge Torque and Aeroelastic response of a rotor, Company Project, 2024, Project leader;

(3) *** Verification of Flutter and Dynamic Characteristics of Civil Aircraft in Flight Test, 2017-2022, Project leader;

(4) *** Flutter Prediction Technology Research Sub-topic, 2020-2024, Project leader;

(5) Design, Manufacture and Verification of Wing Low-speed flutter wind tunnel model based on Additive Manufacturing, Key Technology Research, 2018-2022, Project leader.

Patents:

(1) A method for manufacturing a low-speed flutter wind tunnel model of a wing, 1/4;

(2) A wing wind tunnel model manufacturing method and wing wind tunnel model, 1/6;

(3) A wing wind tunnel model, 1/6;

(4) Flutter wind tunnel model of aircraft winglets, 2/6;

(5) An aircraft engine model, 2/6;

(6) A parametric modeling and analysis system for wing flutter V1.0, 2/3;

(7) A dmping anti-vibration design and opti miｚation method of co mposite skin with hard coating, 1/5.