文广为博士后 - 分布与智能航天系统实验室

Wen Guangwei 文广为

Post-doc Researcher

通讯地址：北京市海淀区清华大学航天航空学院

邮箱：gwen@tsinghua.edu.cn

办公电话：

中南大学机电工程学院学士、美国新墨西哥州立大学博士，现为清华大学航天航空学院博士后，助理研究员。主要研究方向为计算流体力学，研究内容包括稀薄气体动力学、跨声速流体流动机理、层流稳定性分析等。AIAA会员，发表论文11篇，获北京市自然科学基金青年基金项目一项。

2011-2015 Bachelor, Central South University, China, Department of Mechanical Engineering, Mechanical Engineering

2015-2020 Doctor of Philosophy, New Mexico State University, United States of America, Department of Mechanical and Aerospace Engineering, Computational Fluid Mechanics

2011年-2015年，学士，中南大学，机电工程学院，机械设计制造及自动化

2015年-2020年，博士，新墨西哥州立大学，机械与航空航天学院，计算流体力学

2021-current Post-doc Researcher, Tsinghua University, School of Aerospace Engineering

2021年至今，博士后，清华大学，航天航空学院

Fluid Mechanics, Aircraft Design and Optimization, Computational Fluid Mechanics, Rarefied-gas Flow, Hydro-stability Analysis.

流体力学，飞行器设计与优化，计算流体力学，稀薄气体动力学，流体稳定性分析

北京市自然科学基金，资助编号1224039，基于清华大学重力与大气科学卫星轨道数据与稀薄气体数值模拟的航天器气动力学模型，2022.01至今，项目主持人；

中央军委装备发展部, 载人航天工程重大专项, 资助编号20194600024, 基于球形卫星的地球大气与长波重力场联合探测, 2019-01 至 2022-12, 项目参与人。

[1] Wen, G., Gross, A., " Numerical Investigation of Deep Dynamic Stall for a Helicopter Blade Section", AIAA Journal, Vol. 57, No. 4, 2019, pp. 1434–1451. doi: 10.2514/1.J057686

[2] Wang, Z, Han, D., Li, B., He, Y., Zhang Q., Wen, G., Zhang, Y., “Q-SAT for Atmosphere and Gravity Field Detection: Design, Mission and Preliminary Results,” Acta Astronautica, Vol. 198, 2022, pp. 521-520. doi:10.1016/j.actaastro.2022.06.035

[3] Huang, P., Li, H., Wen, G., Wang, Z., “Application of Adaptive Weighted Strong Tracking Unscented Kalman Filter in Non-Cooperative Maneuvering Target Tracking”, Aerospace, Vol. 9, No. 8, pp. 468-477. doi:10.3390/aerospace9080468

[4] Wen, G., Wang, Z., “Aerodynamic Design and Analysis of Multirotor Robot Under Microgravity Condition Inside China Space Station”, 73th International Astronautical Congress, 73rd International Astronautical Congress, IAC-22-A2,2,12,x70382, 2022, Paris, France

[5] Wang, Z., Han, D., He, Y., Wen, G., Zhang, Y., “Q-Sat for Atmosphere and Gravity Field Detection: Design, Mission and Preliminary Results”, 72nd International Astronautical Congress, IAC-21- B4, IP, 7, x64084, 2021, Dubai, United Arab Emirates

[6] Wen, G., Gross, A., “Bi-global Linear Stability Analysis of Laminar Separation Bubble for Helicopter Blade Section Undergoing Dynamic Stall”, AIAA Scitech 2021 Forum, AIAA-2021-0498. doi:10.2514/6.2021-0498

[7] Wen, G., Gross, A., "Local Stability Analysis of Laminar Separation Bubble for Helicopter Blade Section Undergoing Dynamic Stall", AIAA Scitech 2020 Forum, AIAA-2020-2241. doi: 10.2514/6.2020-2241

[8] Wen, G., Gross, A., "Modal Decomposition of Dynamic Stall for Helicopter Blade Section", AIAA Scitech 2019 Forum, AIAA-2019-1657. doi: 10.2514/6.2019-1657

[9] Wen, G., Gross, A., "Numerical Investigation of Dynamic Stall for a Helicopter Blade Section", 2018 AIAA Aerospace Sciences Meeting, AIAA-2018-1557. doi: 10.2514/6.2018-1557

[10] Wen, G., Gross, A., "Numerical Investigation of Helicopter Blade Section Undergoing Time-Periodic Motions", 55th AIAA Aerospace Sciences Meeting, AIAA-2017-0078. doi: 10.2514/6.2017-0078

[11] Gross, A., Wen, G., "Numerical Investigation of Helicopter Blade Section Undergoing Time-Periodic Motions", 8th AIAA Flow Control Conference, AIAA-2016-4244. doi: 10.2514/6.2016-424