姓名：李东风
出生年月：1988.06
职称职务：讲师
· 电子邮件：lidongfeng@tyust.edu.cn
· 研究方向
主要研究方向：计算空气动力学，高端装备流固耦合力学分析与控制，降阶模型，深度学习，空压机
· 科研与教改项目
1. 2021.06-2021.12 国网甘肃刘家峡水电厂泄水道工作闸门局部开启运行可行性研究。主要负责：水工闸门不同开度下，研究闸门结构在实际约束状态下的静、动力特性，主持；
2. 2020.05-2020.12 汽车制动系统刹车振动分析及减震设计。主要负责：汽车刹车片振动、稳定性、散热分析，提出降低刹车片振动措施，参与；
3. 2021.04-至今 大型水工弧门的结构有限元静力分析评价导则研究项目。主要负责：通过有限元计算结果分析闸门结构强度、刚度、稳定性的安全评价方法，参与；
4. 2022.01-至今 半刚接网壳结构的失效机理及体系可靠度研究，构建可并行高精度数值模拟方法，研究半刚接网壳结构的失效机理，参与；
5. 2017.01-2020.12 高雷诺数不可压湍流中柔性结构非线性流固耦合振动机理研究，构建高精度柔性结构非线性流固耦合降阶模型数值模拟方法，参与。
· 代表性论文专著：
· [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] 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.
· [3] Dongfeng Li, Chunlin Gong, Andrea Da Ronch, Gang Chena, Yueming Li. 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.
· [4] Li Dongfeng, Andrea Da Ronch, Chen Gang, et al. Aeroelastic global structural optimization using an efficient CFD-based reduced order model[J]. Aerospace Science and Technology, 2019, 94: 105354.
· [5] Li Dongfeng, Wang Zhengzhong, Da Ronch A, et al. An efficient evaluation method for wing fuel mass variations effect on transonic aeroelasticity[J]. Aircraft Engineering and Aerospace Technology, 2022, 94: 881-894.
· [6] Li Dongfeng, Wang Zhengzhong, Da Ronch A, et al. An efficient reduced-order framework for active/passive hybrid flutter suppression[J]. The Aeronautical Journal, 2022: 1-17.
· [7] 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).
· [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评估方法[J].中国科学:物理学 力学 天文学, 2018, 48(11).
· [9] 李东风，李立州，肖丰乐. 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.
· [10] 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 and Structures, 2016. 66: 183-206. [11] 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[C]// 2018 AIAA Modeling and Simulation Technologies Conference. 8-12 January, 2018, Kissimmee, Florida, USA: 1928.
· [12] Dongfeng Li, Qiang Zhou, Gang Chen, Yueming Li. Structural Dynamic Reanalysis method for Aeroelastic Analysis of Cracked Wing[C]. SBM000091. APISAT-2016, 24-27 Oct, Toyama, Japan.
· [13] Li Dongfeng, Zhou Qiang, Chen Gang, Li Yueming. Consideration of POD Interpolation for Aeroelastic Design use Structural Dynamic Reanalysis[C]. WCCM-2016, 24-29 July, Seoul, South Korea.
· [14] 李东风，陈刚，李跃明. 一种自动化气动弹性剪裁技术[C]. 第十五届届全国气弹学术交流会，大连, 2017. 08.
· [15] Dongfeng Li, Yixing Wang, Andrea Da Ronch, Gang Chen, Yueming Li. An Efficient Computational Fluid Dynamics-based Aeroelastic Reduced Order Model for Aeroelastic Global Optimization[C]. WCCM-2018, 22-27 July, New York, USA.
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· 授权发明专利
无
· 荣誉奖励
1. 机械工业科学技术奖，2024，科技进步奖，三等奖
