李东风，男，1988.06，政治面貌：群众，学历：博士，职称：讲师。
教育经历：
2011.09-2014.06 中北大学 硕士 航空宇航制造工程
2014.09 -2019.09 西安交通大学 博士 航空宇航科学与技术
工作经历：
2019.10-至今 西北农林科技大学水利与建筑工程学院
研究方向：
CFD，流固耦合，气动弹性，闸门流激振动，多相流
主讲课程：
发表论文：SCI：
1. Li Dongfeng, Zhou Qiang, Chen Gang, et al. Structural dynamic reanalysis method for transonic aeroelastic analysis with global structural modifications[J]. Journal of Fluids and Structures, 2017, 74: 306-320.
2. Li Dongfeng, Gong Chunlin, Ronch Andrea Da, Chen Gang, Li Yueming. An efficient implementation of aeroelastic tailoring based on efficient computational fluid dynamics-based reduced order model[J]. Journal of Fluids and Structures, 2019, 84: 182-198.
3. Li Dongfeng, Ronch Andrea Da, Chen Gang, Li Yueming. Aeroelastic global structural optimization using an efficient CFD-based reduced order model[J].Aerospace Science and Technology, 2019, 94: 105354.
4. Chen Gang, Li Dongfeng, Zhou Qiang, et al. Efficient aeroelastic reduced order model with global structural modifications[J]. Aerospace Science and Technology, 2018, 76: 1-13.
5. Qiang Zhou, Dongfeng Li, Andrea Da Ronch, Gang Chen, Yueming Li. Computational fluid dynamics-based transonic flutter suppression with control delay[J]. Journal of Fluids & Structures, 2016. 66: 183-206.
其他：
1. Dongfeng Li, Gong C, Wang Y, et al. An Efficient Implementation of Transonic Aeroelastic Tailoring based on a Reduced-Order Model using Structural Dynamic Reanalysis Method[100]//2018 AIAA Modeling and Simulation Technologies Conference. 2018: 1928.
2. Wang Y, Yuan Z, Li Dongfeng, et al. Aero-structural optimization of the HIRENASD Model configuration[100]//2018 Aviation Technology, Integration, and Operations Conference. 2018: 4004.
3. Dongfeng Li, Qiang Zhou, Gang Chen, Yueming Li. Structural Dynamic Reanalysis Method Application for Wing Structural Design[J]. International Journal of Aerospace and Lightweight Structures, 2015, 5(4).
4. Dongfeng Li, Qiang Zhou, Gang Chen, Yueming Li. Structural Dynamic Reanalysis method for Aeroelastic Analysis of Cracked Wing. SBM000091. APISAT-2016, 24-27 Oct., Toyama, Japan.
5. Li Dongfeng, Zhou Qiang, Chen Gang, Li Yueming. Consideration of POD Interpolation for Aeroelastic Design use Structural Dynamic Reanalysis.WCCM-2016, 24-29 July,Seoul,South Korea.
6. 李东风, 李立州, 肖丰乐,等. 基于 CFD 的直升机主旋翼桨毂阻力分析[J]. 飞行力学, 2014, 32(2):129-131.
7. 周强, 李东风, 陈刚,等. 基于 CFD 和 CSM 耦合的通用静气弹分析方法[J]. 航空动力学报, 2018, 33(2):355-363.
8. 李东风, 王怡星, 陈刚, 李跃明. 面向跨音速气动弹性剪裁的颤振时域自动化预估方法[J]. 中国科学:物理学 力学 天文学, 2018, 48(11):43-55.


通讯地址：陕西杨凌渭惠路23号 西北农林科技大学水利与建筑工程学院
邮编：712100
邮箱: lidongfeng@nwafu.edu.cn