导师姓名：黄锐
性别：男
人气指数：57

所属院校：南京航空航天大学
所属院系：航空宇航学院
职称：副研究员
导师类型：硕导
招生专业：飞行器设计


通讯方式 :
电子邮件：ruihwang@nuaa.edu.cn


个人简述 :
教育经历：
毕业于西北工业大学飞行器设计与工程专业（2006年）;2014年12月获南航飞行器设计专业博士学位。攻读博士学位期间，曾在匈牙利布达佩斯工业与经济大学应用力学系访学。2015年1月留校任教，2016年破格晋升副研究员
社会兼职：AIAA Journal, Journal of Sound and Vibration, Journal of Fluids and Structures, Journal of Aerospace Engineering, Aerospace Science and Technology, ASME Journal of Computational and Nonlinear Dynamics, Meccanica, Shock and Vibration, 力学学报，振动与冲击，西安交通大学学报等国内外知名期刊审稿人。

科研工作 :
发表学术论文,出版专著情况：
发表学术论文：
1. Rui Huang, Haojie, Liu, Zhijun Yang, Yonghui Zhao, Haiyan Hu. Nonlinear Reduced-Order Models for Transonic Aeroelastic and Aeroservoelastic Problems, AIAA Journal(revised), 2018.
2. Rui Huang, Yonghui Zhao and Haiyan Hu. “Wind-Tunnel Tests for Active Flutter Control and Closed-Loop Flutter Identification,” AIAA Journal, Vol.54, No.7, 2016, pp: 2089-2099.
3. Rui Huang, Hongkun Li, Haiyan Hu, and Yonghui Zhao. “Open-/Closed-Loop Aeroservoelastic Predictions via Nonlinear, Reduced-Order Aerodynamic Models,” AIAA Journal, Vol.53, No.7, 2015, pp: 1812-1824.
4. Rui Huang, Wenmin Qian, Haiyan Hu, and Yonghui Zhao. “Design of Active Flutter Suppression and Wind-Tunnel Tests of a Wing Model Involving a Control Delay,” Journal of Fluids and Structures, Vol.55, 2015, pp: 409-427.
5. Rui Huang, Haiyan Hu, and Yonghui Zhao. “Nonlinear Reduced-Order Modeling for Multiple-Input/Multiple-Output Aerodynamic Systems,” AIAA Journal, Vol.52, No.6, 2014, pp 1219-1231.
6. Rui Huang, Haiyan Hu, and Yonghui Zhao. “Nonlinear Aeroservoelastic Analysis of a Controlled Multiple-Actuated-Wing Model with Free-Play,” Journal of Fluids and Structures, Vol.42, 2013, pp 245-269.
7. Rui Huang, Haiyan Hu, and Yonghui Zhao. “Designing Active Flutter Suppression for High-Dimensional Aeroelastic Systems Involving a Control Delay,” Journal of Fluids and Structures, Vol.34, 2012, pp 33-50.
8. Rui Huang, Haiyan Hu, and Yonghui Zhao. “Single-Input/Single-Output Adaptive Flutter Suppression of a Three-Dimensional Aeroelastic System,” AIAA Journal of Guidance, Control and Dynamics, Vol.35, No.2, 2012, pp 659-665.
9. Rui Huang, Wenmin Qian, Yonghui Zhao, and Haiyan Hu. “Flutter Analysis: Using Piecewise Quadratic Interpolation with Tracking and Wind-Tunnel Tests,” AIAA Journal of Aircraft, Vol. 47, No.4, 2010, pp 1447-1451.
10. Zhijun Yang, Rui Huang, Yonghui Zhao, Haiyan Hu. Design of an Active Disturbance Rejection Control for Transonic Flutter Suppression, AIAA Journal of Guidance, Control and Dynamics, Vol.40, No.11, 2017, pp 2905-2916.
11. 杨执钧，黄锐，刘豪杰，赵永辉，胡海岩，王乐. 大长细比导弹的气动弹性降阶模型，力学学报，Vol.49, No.3, 2017.
12. Haojie Liu, Rui Huang, Yonghui Zhao and Haiyan Hu. Reduced-Order Modeling of Unsteady Aerodynamics for an Elastic Wing with Control Surfaces, Journal of Aerospace Engineering, Vol.30, No.3, 2017, pp:1-19.
13. 胡海岩，赵永辉，黄锐.飞机结构气动弹性分析与控制研究. 力学学报，2016, 48(1)：1-27.
14. Haojie Liu, Haiyan Hu, Yonghui Zhao and Rui Huang. “Efficient Reduced-Order Modeling of Unsteady Aerodynamics Robust to flight Parameter Variations” Journal of Fluids and Structures, Vol.49, 2014, pp 728-741.
15. Wenmin Qian, Rui Huang, Haiyan Hu and Yonghui, Zhao. “Active flutter suppression of a multiple-actuated-wing wind tunnel model” Chinese Journal of Aeronautics, Vol.27, No.6, 2014, pp:1451-1460.
16. Wenmin Qian, Rui Huang, Haiyan Hu and Yonghui, Zhao. “New Method of Modeling Uncertainty for Robust Flutter Suppression,” Journal of Aircraft, Vol.50, No.3, 2013, pp: 994-998.
17. 出版专著：赵永辉，黄锐，高等气动弹性力学与控制，北京，科学出版社，2015.

科研成果获奖及专利：
2017年荣获航空宇航科学与技术全国优秀博士论文奖；2015年，南京航空航天大学2015年度“青年学者”创新奖； 2014/11-至今，美国航空航天学会（AIAA）高级会员（Senior Member）； 2012/09，第二届“临近空间杯”博士生科技创新一等奖；
承担的科研项目情况：
主持国家自然科学青年基金、江苏省自然科学青年基金、航空科学基金和航天一院CALT基金；参与空装预研基金，总装备部重点基金，国防基础预研基金重点项目等。