教师个人信息
姓名：李东风
出生年月：1988.06
职称职务：讲师，硕士生导师。
电子邮件：lidongfeng@tyust.edu.cn
研究方向：计算流体力学，降阶模型，深度学习，流固耦合和气动弹性技术，涡轮机械，高端装备流体力学设计与控制等。
科研与教改项目：
[1] 2021.06-2021.12，横向课题，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，主持；
[2] 2011.12-2012.12，横向课题，XXX旋翼机式飞行汽车气动性能总体设计，主要完成人；
[3] 2021.04-至今，横向课题，大型水工弧门的结构有限元静力分析评价导则研究项目，主要完成人；
[4] 2022.01-2024.12，陕西省自然科学基金，半刚接网壳结构的失效机理及体系可靠度研究，主要完成人；
[5] 2017.01-2020.12，国家自然科学基金，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，主要完成人；
[6] 2014.10-2015.04，横向课题，快速泄压阀高温力学行为分析，主要完成人；
[7] 2016.04-2017.04，横向课题，XXX航天器贮液箱结构内液体晃动和振动的流固耦合分析，主要完成人。
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. (JCR=Q1, IF= 3.482)
[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. (JCR=Q1, IF= 5.457, Top期刊)
[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. (JCR=Q1, IF= 3.482)
[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. (JCR=Q1, IF= 5.457, Top期刊)
[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. (JCR=Q3, IF=1.478)
[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. (JCR=Q3, IF= 1.222)
[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. (JCR=Q1, IF= 3.482)
[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. (EI)
[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.
荣誉奖励：
[1] 2024年，机械工业科学技术奖，三等奖
[2] 指导学生获得获得省级大学生创新创业训练计划项目
