Basic information

  • Professor of Fluid-structure interaction, Assistant Dean of the School of Aerospace Engineering

  • Deputy director of Shannxi Province Key Laboratory of flight enviroment and control for advance flight vechicles

  • Director of the XJTU-UoM jiont laboratory on Fluid structure interaction and bio-inspired technologies 

  • Member of techincal committee of aeroelasticiy in Chinese Aerodyanmics Association

Education

1997-2001 College of Astronautics, Northwestern Polytechnical University (NWPU)
2001-2004 College of Astronautics, NWPU, Msc in Aerospace Engineering

2003-2006 College of Astronautics, NWPU, Ph.D in Aerospace Engineering  

Working Experience

2004~2008      TA and Lecturer at College of Astronautics, NWPU, PRC

2006-2008       Postdoc, School of Aerospace Engieering, Xi’an Jiaotong University (XJTU)

2008-2014       Associate professor, School of Aerospace Engineering, XJTU, PRC

2011- 2013      Assistant Professor, Tokyo University of Science, Yamaguchi, Japan

2014-Current   Professor in the Department of Aerospace Engineering, XJTU

2015-Current   Assistant Dean of the School of Aerospace Engineering, XJTU

Research Interests

(1) Fluid-Structure Interaction and control of flexible aircraft
(2) Data Driven and machinle learning modeling for FSI  systems

(3) Bio-inspired flow control and morphing UAV technology

(4) Smart aircraft design and AI flight control

(5) Unsteady flow and aeroacoustics 

 

Journal Publications

  1. Li Dongfeng,A.D Ronch, Chen Gang*,Li Yueming.Aeroelastic Global Structural Optimization using an Efficient CFD-based Reduced Order Model.Aerospace Science and Technology.,https://doi.org/10.1016/j.ast.2019.105354,online.

  2. Xu Dan,Hui Zhe,Liu Yongqi,Chen Gang*..Morphing Control of a New Bionic Morphing UAV with Deep Reinforcement Learning..Aerospace Science and Technology,https:// 10.1016/j.ast.2019.05.058,online.

  3. Han jiakun,Zhang Yang,Chen Gang*.Effects of individual horizontal distance on the three-dimensional bionic flapping multi-wings in different schooling configurations.Physics of Fluids, 31, 041903 (2019); https://doi.org/10.1063/1.5087624.

  4. Li Dongfeng,Gong Chulin,A.D Ronch, Chen Gang*,Li Yueming.An Efficient Implementation of Aeroelastic Tailoring based on Efficient Computational Fluid Dynamics-based Reduced Order Model. Journal of Fluids and Structures, 2019, 84: 182-198,doi:10.1016/j.jfluidstructs.2018.10.011

  5. Gong Chunlin, Han Jiakun, Yuan Zongjing , Fang Zhe , Chen Gang*. Numerical investigation of the effects of different parameters on the thrust performance of three dimensional flapping wings.Aerospace Science and Technology,2019,84,431-445,doi.org/10.1016/j.ast.2018.10.021. 

  6. Han Jiakun,Yuan Zongjin,Chen Gang*.Effects of kinematic parameters on three-dimensional flapping wing at low Reynolds number.Physics of Fluids, 081901(2018),doi.org/10.1063/1.5041292

  7. 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评估方法.中国科学:物理学 力学 天文学,2018,48(11):doi/10.1360/SSPMA2018-00072

  8. 曹亮,杨鹏飞,王怡星,陈刚*.柔性薄板翼流固耦合振动噪声风洞实验研究.中国科学:技术科学,Online,10.1360/N092017-00433
  9. Gong Chunlin,Fangzhe,Chen Gang*.Numerical Investigation of Nonlinear Fluid-structure Interaction Dynamic Behaviors Under a General Immersed Boundary-lattice Boltzmann-Finite Element Method.International Journal of Mordern Physic C.,2018,29(4):1850038.
  10. Chen Gang*, Li Dongfeng,Zhou Qiang, A. Da Ronch,,Li Yue-ming.Efficient Aeroelastic Reduced Order Model with Global Structural Modifications..Aerospace Science and Technology, 2018,76:1-13,/doi.org/10.1016/j.ast.2018.01.023

  11. CL. Gong,Z.Fang, G.Chen.A Lattice Boltzmann-Immersed Boundary-Finite Element Method For Nonlinear Fluid-Solid Interaction Simulation With Moving Objects.International Journal of Computational Method,2018,doi.org/10.1142/S0219876218500639.
  12.  Chen Gang*,Zhou Qiang, A. Da Ronch,,Li Yue-ming.Computational Fluid Dynamics-based Aero-servo-elastic Analysis for Gust Load Alleviation.AIAA Journal of Aircraft,2018,55(4),1619-1628,doi:10.2514/1.C034621.
  13.  FeiFei Liu,ShuJie Jiang,Gang Chen* and Yueming Li.Numerical Investigation on Vortex-Structure Interaction Generating Aerodynamic Noises for Rod-Airfoil Models.Mathematical Problems in Engineering,Article ID 3704324
  14. 蒋树杰;刘菲菲;陈刚*.流固耦合振动效应对机翼气动噪声辐射的影响研究.振动与冲击,2018, 37(19): 7-13. 
  15. CL. Gong, ZJ Fang, Q Zhou, G.Chen*, Z.Fang. Numerical Investigation Of Unsteady Flows Past Flapping Wings With Immersed  Boundary-Lattice Boltzmann Method.Journal of Mechanics2018,34(2):193-207,DOI: 10.1017/jmech.2017.5
  16. 周强,李东风, 陈刚*,李跃明.基于CFD和CSD耦合的通用静气弹分析方法研究.航空动力学报,2018,33(2):355-363.
  17. 苑宗敬,韩佳坤,陈刚*.低雷诺数下展弦比对仿生拍动翼推进性能的影响研究[J].空气动力学学报,2018,36(1):156-162.
  18. Li Dong-feng,Zhou Qiang,  Chen Gang*, Li Yue-ming.Structural Dynamic Reanalysis method for Transonic Aeroelastic Analysis with Global Structural Modifications. Journal of Fluids and Structures, 2017,74, 306-320, DOI: 10.1016/j.jfluidstructs.2017.06.004.
  19. Zhou Qiang, Li Dong-feng, A. Da Ronch, Chen Gang*,Li Yue-ming.Reduced Order Unsteady Aerodynamic Model of a Rigid Aerofoil in  Gust Encounters.Aerospace Science and Technology2017 , 63 :203-213.
  20. 陈刚,苑宗敬,张鸿志,韩佳坤,龚春林.几何参数对三维仿生运动翼推进性能的影响研究.西安交通大学学报,2017,51(9):131-137.

  21. 宛宗敬,姬兴,陈刚*.仿生运动翼IB-LBM非定常流动数值模拟.气体物理, 2017,2(1):30-47..
  22. Shuai Li,Zongjing Yuan,Gang Chen*.Numerical investigation of unsteady mixing mechanism in plate film cooling.Theoretical and Applied Mechanics Letters.2016,6:213-221.
  23. 张鸿志,周强,陈刚*,李跃明.气动弹性系统本征正交分解降阶模型精度的参数影响研究.西安交通大学学报,2016,50(11):104-109.

  24. Zhou Qiang, Li Dong-feng, A. Da Ronch, Chen Gang*, Li Yue-ming. Computational Fluid Dynamics-based Transonic Flutter Suppression with Control Delay. Journal of Fluids and Structures, 2016,66:183-206.
  25. 周强, 陈刚*, 李跃明. 基于CFD降阶的非线性气动弹性稳定性分析[J]. 振动与冲击,2016, 35(16): 17-23. 
  26. 乔洋,于志鹏,陈刚*.弹性飞行器气动伺服弹性稳定性分析与设计.应用力学学报,2016,33(2):287-291.
  27. Zuo Ying-tao, Gao Zheng-hong, Chen Gang*, Wang Xiao-peng,Li Yue-ming.  Efficient  aero-structural design optimization: Coupling based on reverse iteration of structural model.Science China Technological Sciences, 2015, 58(2): 307-315.
  28. Yingtao Zuo, Pingjian Chen, Lin Fu, Zhenghong Gao, and Gang Chen*.Advanced Aerostructural Optimization Techniques for Aircraft Design .Mathematical Problems in Engineering,Volume 2015, Article ID 753042, http://dx.doi.org/10.1155/2015/753042.
  29. Dongfeng Li, Qiang Zhou, Gang Chen*, Yueming Li and Andrea Da Ronch. Structural Dynamic Reanalysis Method Application for Wing Structural Design. International Journal of Aerospace and Lightweight Structures[J]. 2015, 5(4).
  30.  刘菲菲陈刚*李跃明用于飞机机翼涡固干扰噪声数值模拟的RAMS/NLAS方法. 西安交通大学学报2015, 49(9): 141-146. 
  31. 周强,陈刚*,李跃明. 考虑流固耦合效应的某飞行器力学性能分析. 应用力学学报201532(2): 47-52+188.
  32. 左英桃,王晓鹏,陈云,陈刚,高正红.一种高效的CFD/CSD耦合飞行器多学科优化设计方法. 航空动力学报,Vol.29(12):2898-2904,2014.
  33. Zhou Qiang, Chen Gang, Li Yue-ming. A reduced order model based on block arnoldi method for aeroelastic system. Int. J. Appl. Mechanics, 2014, 6(6): 1450069. DOI: 10.1142/S1758825114500690. 
  34. Zuo Ying-tao, Chen Gang*, Li Yue-mingGao Zheng-hong. Efficient Aeroelastic Design Optimization Based on Discrete Adjoint Method. Trans. of Japan Soc. Aero. Space Sci., 2014,57(6): 343-351.
  35. Chen Gang*, Wang Xian, Li Yue-ming. Reduced-Order-Model-Based Placement Optimization of Multiple Control Surfaces for Active Aeroelastic Control. International Journal of Computational Method, 2014, 11(06): 1350081.
  36. Chen Gang*, Wang Xian, Li Yue-ming. A reduced-order-model-based multiple-in multiple-out gust alleviation control law design method in transonic flow. SCIENCE CHINA, Technological Sciences2014, 57(2): 368-378.
  37.  Chen Gang*, Wang Xian, Li Yue-ming. Active Aeroelastic Control using Multiple Control Surfaces Based on a High-Fidelity Reduced Order Model. Trans. Japan Soc. Aero. Space Sci., 2013, 56(5): 261–268.  
  38. Chen Gang*, Sun Jian, Mao Wen-tao,  Li Yue-ming. Limit Cycle Oscillation Control for Transonic Aeroelastic Systems Based on Support Vector Machine Reduced Order Model.Trans. Japan Soc. Aero. Space Sci., 2013, Vol. 56(1): 8-14.
  39. 许丁, 陈刚, 王娴, 李跃明. 基于多GPU得格子Boltzmann法对槽道湍流的直接数值模拟. 应用数学和力学, 2013, 34(9): 956-964.
  40.  Chen Gang, Sun Jian, Li Yue-ming. Active Flutter Suppression Control Law Design Method Based on Balanced Proper Orthogonal Decomposition Reduced Order Model. Nonlinear Dynamics,2012, 70: 1-12. 
  41. Chen Gang*, Zuo Ying-tao, Sun Jian, Li Yue-ming. Support-Vector-Machine-Based Reduced-Order Model for Limit Cycle Oscillation Prediction of Nonlinear Aeroelastic System.Mathematical Problems in Engineering, 2012. DOI:10.1155/2012/152123.
  42. Chen Gang*, Sun Jian,  Li Yue-ming. Adaptive Reduced-Order-Model-Based Control-Law Design for Active Flutter Suppression. Journal of Aircraft, 2012, 49(4): 973-980. 
  43. Chen Gang*,  Li Yue-ming, Yan Gui-rong. Limit Cycle Oscillation Prediction and Control Design method for Aeroelastic System Based on New Nonlinear Reduced Order Model.International Journal of Computational Method, 2011, 8(1):77-90.