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. Jiakun HAN, Zhe HUI, Fangbao TIAN, Gang CHEN*.Review on bio-inspired flight systems and bionic aerodynamics.Chinese Journal of Aeronautics,2020,accept.
  2. Zhe Hui, Yang Zhang, Gang Chen*.Tip-vortex flow characteristics investigation of a novel bird-like morphing discrete wing structure.Physics of Fluids,2020,doi.org/10.1063/1.5144432.
  3. Renkun Han, Yixing wang, Yang Zhang, and Gang Chen*.A novel spatial-temporal prediction method for unsteady wake flows based on hybrid deep neural network.Physics of Fluids,Accept(Editor's Pick).
  4. Yang Zhang, Jiakun Han, and Gang Chen*.Effects of the flapping frequency on the thrust performance for three-dimensional bionic multi-wings in a schooling.Physics of Fluids,Accept.(Editor's Pick&AIP Hilights).
  5. Zhe Fang,Chunlin Gong,Alistair Revell,Gang Chen, Andrian Harwood and  Joseph O'Connor.Passive Separation Control of a NACA0012 Airfoil via a Flexible Flap.Physics of Fluids 31, 101904 (2019); https://doi.org/10.1063/1.5118933.
  6. Hui zhe,Zhang Yang,Chen Gang*.Aerodynamic performance investigation on a morphing unmanned aerial vehicle with bio-inspired discrete wing structures.Aerospace Science and Technology., accept.
  7. 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.
  8. 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.
  9. 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.
  10. 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
  11. 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. 
  12. Han Jiakun,Yuan Zongjin,Chen Gang*.Effects of kinematic parameters on three-dimensional flapping wing at low Reynolds number.Physics of Fluids, 081901(2018).
  13. 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.
  14. 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
  15. 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.
  16.  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.
  17.  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 370432.
  18. 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
  19. 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.
  20. 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.
  21. 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.
  22. 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.
  23. 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.
  24. 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.
  25. 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).
  26. 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.
  27. 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.
  28. 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.
  29. 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 Sciences, 2014, 57(2): 368-378.
  30.  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.  
  31. 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.
  32.  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. 

  33. 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.
  34. 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. 
  35. 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.