• Professor of Fluid-structure interaction

• 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

• Member of techincal committee of fluid-structure interaction in Chinese Mechanics Association

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  

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

2015-2020       Assistant Dean of the School of Aerospace Engineering, XJTU

(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 

1.  Yongqi Liu, Liangcheng Nie, Rui Dong, Gang Chen*.BP Neural Network-Kalman Filter Fusion Method for UAV Target Tracking.Part C:JMES,2020,accept

2. Zhong Zhang, Dan Xu, Bo Gao, Jianmin Wang, Gang Chen*, Weigang Yao. A generalized force equivalence based modeling method for Dry wind tunnel flutter test system.The Aeronuatical Journal,2020,accept.​​​​​​​

3. Jiakun HAN, Zhe HU, Fangbao TIAN, Gang CHEN*.Review on bio-inspired flight systems and bionic aerodynamics.Chinese Journal of Aeronautics,2020,

   doi: 10.1016/j.cja.2020.03.036.

4. 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.
5. 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）.
6. 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).
7. 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.
8. 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.
9. 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.
10. 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.
11. 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.
12. 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
13. 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. 
14. Han Jiakun,Yuan Zongjin,Chen Gang*.Effects of kinematic parameters on three-dimensional flapping wing at low Reynolds number.Physics of Fluids, 081901(2018).
15. 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.
16. 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
17. 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.
18.  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.
19.  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.
20. 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 Mechanics, 2018,34(2):193-207,DOI: 10.1017/jmech.2017.5
21. 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.
22. 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 Technology, 2017 , 63 :203-213.
23. 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.
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. 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.
26. 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.
27. 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).
28. 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.
29. Zuo Ying-tao, Chen Gang*, Li Yue-ming, Gao Zheng-hong. Efficient Aeroelastic Design Optimization Based on Discrete Adjoint Method. Trans. of Japan Soc. Aero. Space Sci., 2014,57(6): 343-351.
30. 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.
31. 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.
32.  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.  
33. 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.

34.  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. 

35. 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.
36. 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. 
37. 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.