研究兴趣

1、智能飞行器总体技术：智能飞行器仿生流动机理与气动总体设计、智能飞行器多功能变形结构设计技术

2、飞行器流固耦合力学与控制技术：流固耦合系统人工智能建模与仿真技术、新型飞行器气动伺服弹性技术；
3、飞行器人工智能控制技术：智能仿生飞行器控制技术、无人集群人工智能控制方法；
4 、流动噪声与控制技术：高端装备（汽车、高铁、飞行器、船舶、动力装置等）流体噪声机理、数值模拟方法、实验技术及噪声抑制；

5、 高端装备热管理与先进冷却技术：装备结构（飞行器、发动机）热力耦合环境模拟、热管理与先进冷却技术

科研项目

没有找到条目。
项目编号 项目名称 项目来源 起讫时间 承担角色 项目类别
2022JC-03 智能飞行器柔性多体变形翼非线性流固耦合机理研究 陕西省杰出青年科学基金 2022-01~2024-12 负责人 纵向项目
202006 含间隙结构非线性气动伺服弹性分析方法 其他 2020-6~ 负责人 横向项目
2020061 刚柔结合多体动力学建模方法研究 其他 2020-6~ 负责人 横向项目
6142004190307 基于人工智能的飞行器非定常气动力建模方法研究 GF科技重点实验室基金 2020-1~ 负责人 纵向项目
2019 新型柔性仿生羽翼流动与降噪机理研究 气动噪声与控制重点实验室开放基金 2019-8~ 负责人 纵向项目
11872293 柔性仿生非线性流固耦合系统深度学习降阶模型研究 国家自然科学基金项目 2019-1~ 负责人 纵向项目
2019 新型仿生翼面流动控制技术 GF科技重点实验室基金 2019-1~ 负责人 纵向项目
2017JM006 XX控制器设计 校企合作 2017-9~2018-12 负责人 横向项目
2017 XX飞行器技术 国务院各部委项目 2017-7~2018-8 负责人 纵向项目
2017JM 超微器件动态特性测试技术 校企合作 2017-7~2018-10 负责人 横向项目
11672225 高雷诺数不可压湍流中柔性结构非线性流固耦合振动机理研究 国家自然科学基金项目 2017-1~ 负责人 纵向项目
2016JJ 考虑气动弹性影响的机翼气动设计 十二五预研究项目 2016-9~2019-6 负责人 纵向项目
20160652 变形翼多场耦合仿真复核 校企合作 2016-6~2017-6 负责人 横向项目
2016 XX飞行器静气动弹性模拟与修正方法 校企合作 2016-5~2018-2 负责人 横向项目
2016 轻质机翼优化设计及其3D打印验证 校企合作 2016-3~2017-12 骨干成员 纵向项目
2016JM1007 不可压湍流中非线性流固体耦合振动机理研究 陕西省自然科学基金项目 2016-1~2017-12 负责人 纵向项目
11511130053 基于GPU加速的湍流-结构耦合数值模拟方法研究 国家自然科学基金项目 2015-3~2017-12 负责人 纵向项目
X200501 快速泄压阀高温力学行为分析 中核苏阀科技 2015-1~2016-9 骨干成员 横向项目
2014XJ 基于GPU加速的柔性结构流固耦合机理高精度数值模拟方法 中央高校基本科研业务费 2014-3~2016-10 负责人 纵向项目
2014 大展弦比柔性机翼流固耦合机理与优化设计研究 国家重点实验室青年人才项目 2014-1~2015-12 负责人 纵向项目
20条目 每页

显示26结果中的1-20。

学术论文

一、期刊论文

  1. Han Jiakun, Shui Yongtao, Nie Lu, Chen Gang*.Unsteady flow control mechanisms of a bio-inspired flexible flap with the fluid–structure interaction.Physics of Fluids ,35, 057124 (2023).

  2. Deng Ziwen,Liu Hongshen, Wang Zhidong, Yu Fan,Liu Zhiyang,Chen Gang*.Temporal predictions of periodic flows using a mesh transformation and deep learning-based strategyAerospace Science and Technology 134C (2023) 108081​​​​​​​
  3. Liu Zhiyang,Han Renkun,Zhang Miao,Zhang Yang,Zhou Hao,Wang Gang,Chen Gang*.An enhanced hybrid deep neural network reduced-order model for transonic buffet flow prediction.Aerospace Science and Technology,Volume 126, July 2022, 107636​​​​​​​,10.1016/j.ast.2022.107636
  4. Meng XG,Chen ZS,Zhang Y,Chen G*.Aerodynamic performance and flow mechanism of multi-flapping wings with different spatial arrangements.Physics of fluids,34, 021907 (2022)(Featured & AIP Highlights)​​​​​​
  5. Xu Dan, Chen Gang*.Autonomous and cooperative control of UAV cluster with multi-agent reinforcement learning.The Aeronautical Journal,2022, 126：932-951.

  6. ​​​​​​​Han RK,Wang YX,Qian WQ,Wang WZ,Zhang M,Chen G*.Deep neural network based reduced-order model for fluid–structure interaction system.​​​​​​​Physics of fluids,2022,34, 073610​​​​​​​.

  7. R Han,Z Zhang,Y Wang,Z Liu,Y Zhang,G Chen*.Hybrid deep neural network based prediction method for unsteady flows with moving boundaries.Acta Mechanica Sinica,pages 1557–1566 (2021)
  8. Han Jiakun,Chen Gang*.Transient effects during transitions of bio-inspired flapping foils between two different schooling configurations.Part C:JMES,December 6,2021.doi.org/10.1177/09544062211047356
  9. 王怡星, 韩仁坤, 刘子扬, 张扬, 陈刚.流体力学深度学习建模技术研究进展.航空学报,2021, 42(4): 524779-524779.
  10. Liu Yongqi,Dong Rui,Nie Liangchen,Chen Gang*.BP neural Network-Kalman filter fusion method for unmanned aerial vehicle target tracking.Part C:JMES,2021,203-210:1989-1996. 

  11. Hui Zhe,Zhang Yang,Chen Gang*.Experimental investigation on tip-vortex flow characteristics of novel bionic multi-tip winglet configurations,Physics of Fluids,2021,33(1):011902

  12. 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 Aeronautical Journal,2021,125(1286):720-741

  13. Jiakun HAN, Zhe HUI, Fangbao TIAN, Gang CHEN*.Review on bio-inspired flight systems and bionic aerodynamics.Chinese Journal of Aeronautics,2021,34(7):170-186.(Cover Paper)

  14. 杨鹏飞,陈刚*,薛杰,王珺.航天器弹性充液贮箱双向流固耦合响应特性数值分析. 振动与冲击,2021,40(12);283-288.

  15. 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.

  16. 刘永琦,徐丹,程归,陈刚*.基于改进A_算法的无人机快速轨迹规划方法研究.飞行力学,2020(2):40-46.

  17. 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,  31(12) , December 2019（Editor's Pick）.

  18. 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,2019,31(4):041903 (Editor's Pick&AIP Hilights)

  19. 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.

  20. Jian Sun,Pengbin Guo,Teng Wu,Gang Chen*.Pulsar/Star Tracker/INS Integrated Navigation Method Based on Asynchronous Observation Model. Journal of Aerospace Engineering,2019,32(5):04019075.

  21. 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., 2019,95.https://doi.org/10.1016/j.ast.2019.105419.

  22. 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.

  23. 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.

  24. 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)·Chao Liang,Yang Pengfei, Wang Yixing,Chen Gang*.Wind tunnel experimental study on fluid structure coupling vibration and noise of flexible thin plate wing.Science in China:Technical Science,2019,49(7):815-824.(In Chinese)

  25. 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

  26. 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. 

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

  28. Li Dongfeng,Wang Yixing, Chen Gang*,Li Yueming.An automatic flutter assessment method in time domain for transonic aeroelastic tailoring.,Science in China: physics mechanics astronomy, 2018,48(11):doi/10.1360/SSPMA2018-00072.(In Chinese)

  29. Zhou Qiang, Li Dongfeng,Chen Gang, Li Yueming.A general aeroelastic analysis method based on CFD and CSD coupling.Journal of power and propulsion,2018,33(2):355-363.

  30. 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.

  31. 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

  32. 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.

  33.  Chen Gang*，Zhou Qiang, A. Da Ronch,,Li Yue-ming.Computational Fluid Dynamics-based Aero-servo-elastic Analysis for Gust Load Alleviation. Journal of Aircraft,2018,55(4),1619-1628,doi:10.2514/1.C034621.

  34.  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

  35. 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. 

  36. 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

  37. 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.

  38. 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.

  39. 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.

  40. 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.

  41. 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.

  42. 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..

  43. 于志鹏,陈刚*,李跃明.反吸气式临近空间飞行器空基拦截弹制导律设计.飞行力学, 2017 , 35 (1) :66-69.

  44. 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.

  45. 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.

  46. 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.

  47. 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. 

  48. 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.

  49. 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.

  50. 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.

  51. 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).

  52.  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. 

  53. 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, 2015, 32(2): 47-52+188.

  54. 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.

  55. 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. 

  56. 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.

  57. 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.

  58. 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.

  59.  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.  

  60. 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.

  61. 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.

  62.  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. 

  63. 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.

  64. 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. 

  65. 李跃明, 陈刚, 许丁. 面向高端装备制造CAE技术的机遇和挑战. 计算机辅助工程, 2012, 21(1): 1-7.

  66. 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.

  67. 陈刚, 李跃明. 非定常流场降阶模型及应用研究进展与展望. 力学进展, 2011, 41 (6): 686-701.

  68. Chen Gang, Li Yue-ming, Yan Gui-rong. A Nonlinear POD Reduced Order Model for Limit Cycle Oscillation Prediction. Science in China G, 2010, 53(6): 1325-1332. 

  69.  陈刚*, 李跃明, 闫桂荣等. 基于降阶模型的气动弹性主动控制律设计. 航空学报, 2010, 31(1):12-18.

  70. 陈刚*, 李跃明, 闫桂荣等. 基于POD降阶模型的气动弹性快速预测方法研究. 宇航学报, 2009,Vol.30(5):1765-1769.

  71. 康兴无, 陈刚*,董龙雷,闫桂荣.轨道快速机动期间的姿态鲁棒稳定控制方法研究.宇航学报,2009,30(4):1510-1515.

  72. 康兴无, 陈刚*,董龙雷,闫桂荣.具备目标重定向能力的自适应再入制导律.弹道学报,2009,21(2):61-64.

  73. 陈刚*, 康兴无, 乔洋,陈士橹.航天器相对大角度姿态跟踪非线性控制器设计.宇航学报,2009,30(2):556-559.

  74. 康兴无, 陈刚*, 乔洋, 陈士橹. 天对地精确攻击武器末段制导律设计.固体火箭技术,2009,31(1):11-14.

  75. 陈刚,康兴无,闫桂荣,陈士橹.基于伪谱方法的自适应鲁棒实时再入制导律研究.系统仿真学报, 2008,20(20):5623-5626.

  76. 陈刚*,康兴无,闫桂荣,徐敏,陈士橹.基于多目标多学科设计优化方法的再入弹道设计研究.宇航学报,2008,29(4):1210-1215.

  77. 乔洋,陈刚*,陈士橹,徐敏.一种快速爬升和快速下降的奇异摄动最优中制导律设计.固体火箭技术,2008,31(3):205-207.

  78. 陈刚*,董龙雷,闫桂荣,徐敏,陈士橹.航天器再入制导方法研究现状与发展评述.飞行力学,2008,26(1):1-4.

  79. 陈刚*,乔洋,陈士橹,徐敏.实现快速轨道大机动的混合制导策略研究.固体火箭技术,2007,30(6):463-465.

  80. 陈刚*, 徐敏, 陈士橹. 机动再入飞行器神经网络闭路初制导研究. 弹道报,2007,19(2):1-4.

  81. 乔洋,刘勇,徐敏,陈刚.基于多块结构网格的多侧喷瞬态干扰流场研究.固体火箭技术,2007,30(2):98-101.

  82. 陈刚*,徐敏,万自明,陈士橹.基于多学科设计优化算法的再入轨迹优化设计. 宇航学报,2006,27(6):1147-1151.

  83. 陈刚*,徐敏,万自明,陈士橹.具有内点状态约束的机动再入弹道优化设计. 固体火箭技术,2006(2): 79-82.

  84. 陈刚*,万自明,徐敏,陈士橹.遗传算法在航天器轨道优化中的应用. 弹道学报,2006,18(1):1-5.

  85. 陈刚*,胡莹,徐敏,万自明,陈士橹.基于NSGA-Ⅱ算法的RLV 多目标再入轨迹优化设计.西北工业大学学报,2006(2): 133-137.

  86. 陈刚*,胡莹,徐敏,万自明,陈士橹. 基于遗传算法的RLV 再入轨迹优化设计. 固体火箭技术,2006(4): 235-238.

  87. 陈刚*,万自明,徐敏,陈士橹.飞行器轨迹优化应用遗传算法的参数化与约束处理方法研究.系统仿真学报,2005,11(4): 2737-2740.

  88. 徐敏,陈刚,陈志敏,陈士橹.侧向脉冲喷流瞬态干扰流场探讨.推进技术,2005,26(2):120-124.

  89. 徐敏,陈刚*,陈士橹,韦祥文.基于非定常气动力低阶模型的气动弹性主动控制律设计.西北工业大学学报2004 (6):748-752.

  90. 陈刚*,徐敏, 陈士橹.非定常气动力状态空间模型及其在气动伺服弹性建模中的应用. 空军工程大学学报（自然科学版）, 2004(5): 1-4.

  91. 陈刚*,徐敏,陈士橹.基于Volterra 级数的非线性非定常气动力降阶模型.宇航学报,2004(5):492-495+540.

二、会议论文

  1. Hui zhe,Zhang Yang,Chen Gang. Analysis of Wing-tip Vortex of a Bird-like Morphing Wing using Numerical and Experimental Approaches.FSSIC 2019, Crete,Greece,26-30th,Oct. 2019.

  2. 李东风,王怡星,陈刚,李跃明.高效气动弹性降阶模型在跨音速气动弹性结构全局优化中的应用.2018年全国固体力学学术会议，哈尔滨，2018.11.23-25.

  3. Wang Yixing,Yuan Zhelong, Bai Junqiang,Chen Gang.Aero-structural optimization of the HIRENASD Model configuration.ATIO.DE-02, Design Optimization and Model Based Design I ,AIAA AVIATION 2018, 25-29 June,2018,Atalanta,USA.

  4. Chen Gang, Lv Jinan, Han Jiakun, Zhang Yang, Gong. Chunlin.Numerical investigation on the Thrust performance of bionic motion wing in schools.IUTAM Symposium "Critical Flow Dynamics involving moving/deformable structures with design applications", 18-22 June 2018 in Santorini island, Greece.

  5. Wang Yixng,Chen Gang.Feature-Based Recombination Deep Neural Network for Reduced Order Modeling of Aeroelastic System[R].13th World Congress in Computational Mechanics, 2020801 in MS182,July 22-27, 2018,New York, USA.
  6.  Li Dongfeng,Gong Chunlin, A.D.Ronch, Chen Gang, Li Yueming.An Efficient Implementation of Aeroelastic Tailoring Based on a Reduced-Order Model Using Structural Dynamic Reanalysis Method.MST-15, Multidisciplinary Modeling and Simulation Across Domains II , AIAA SciTech Forum,8-12,January 11,2018, 10.2514/6.2018-1928,Kissimmee,Florida.
  7. 陈刚,陈志敏,李跃明.直流式低成本研究型航空声学风洞设计与校测.第二届全国气动声学会议，2016.11.4-6,北京航空航天大学，北京.
  8. Dongfeng Li, Qiang Zhou, Gang Chen, Yueming Li. Structural Dynamic Reanalysis method for Aeroelastic Analysis of Cracked Wing. SBM000091. APISAT-2016, 24-27 Oct., Toyama, Japan.
  9. 周强, 陈刚,李跃明.大展弦比轻质机翼非线性气动弹性分析.第十届海峡两岸航空航天研讨会, 2016.8.29-9.3，南京航空航天大学，南京.
  10. Li Dongfeng, Zhou Qiang, Chen Gang, Li Yueming. Consideration of POD Interpolation for Aeroelastic Design use Structural Dynamic Reanalysis.WCCM-2016, 24-29 July,Seoul,South Korea.
  11. Gong Chunlin, Fangzhe, Chen Gang, Alistair Revell.A Lattice Boltzmann–Immersed Boundary-finite Element Method to Simulate the Fluid Interaction with Moving and Elastic Objects. 25th International Conference on Discrete Simulation of Fluid Dynamics (DSFD 2016) , 4-6 July, 2016,Shenzhen, China.
  12. Z.Qiang,G.Chen,Y.LI,A.DoRonch.Transonic Aeroelastic Moving Gust Responses and Alleviation based on CFD.AIAA-2016-3387,AVIATION2016,13-17,June,2016,Washington D.C.,USA.
  13. 苑宗敬,姬兴,陈刚,李跃明.仿生波动翼IB-LBM非定常流动数值模拟.全国第三届非定常空气动力学会议, 2016.4.9-5.1, 厦门大学.
  14. 陈刚.面向多学科设计的高可信度流固耦合系统降阶模型技术.中国科协第300次青年科学家论坛:复杂装备数字化设计软件的前沿问题, 201528-20，北京理工大学.
  15. 周强, 李东风, 陈刚, 李跃明. 基于CFD降阶的运动阵风减缓设计和仿真. 第14届全国空气弹性力学会议, 西安, 2015年9月20-21日.
  16. 周强, 李东风, 陈刚, 李跃明. 基于POD降阶的气动弹性稳定性分析及运动阵风响应预测. CSTAM2015-A21-E2569, 中国力学大会-2015, 中国上海, 2015年8月16-18日.
  17. 姬兴, 苑宗敬, 陈刚, 李跃明. IB-LBM仿生运动翼型三维流场并行数值模拟. 中国力学大会2015, 上海, 2015.年8月16-18日.
  18. 上官燕琴, 王娴, 陈刚, 李跃明. 基于格子Boltzmann方法的平板射流高性能数值模拟. 第八届全国流体力学学术会议, CSTAM 2014-A26-S09063, 中国兰州, 2014年9月18-21日.  
  19. 周强, 陈刚, 李跃明, 王娴. 基于降阶模型预测阵风响应的方法研究. 第八届全国流体力学学术会议，中国兰州，2014.9.18. 
  20. Shangguan Yan-qin, Wang Xian, Chen Gang, Li Yue-ming. Large Eddy Simulation of High Reynolds Number Turbulent Flows Using Lattice Boltzmann Method and CUDA-GPU. The 24th Inter. Symposium on Transport Phenomena, Yamaguchi, Japan, Nov. 1-5, 2013.
  21. Chen Gang, Wang Xian, Li Yue-ming. A Reduced-Order-Model-Based Multiple-in Multiple-out Gust Alleviation Control Law Design for Transonic Aeroelastic Wings. Proceedings of the 5th Asia Pacific Congress on Computational Mechanics & 4th International Symposium on Computational Mechanics, Paper ID 1371, Singapore, Dec. 11-14, 2013.
  22. 周强, 陈刚, 李跃明. 复杂外形飞行器跨音速气动弹性CFD/CSD耦合数值模拟研究. 第十三届全国空气弹性学术交流会, 中国哈尔滨, 2013年8月.
  23. 路晶晶, 左英桃, 陈刚, 李跃明. 基于CFD/CSD耦合的机翼多学科优化设计方法研究. 第十三届全国空气弹性学术交流会, 中国哈尔滨, 2013年8月.
  24. 周强, 陈刚, 李跃明. 基于块Arnoldi降阶方法的气动弹性分析. CSTAM2013-A31-2135, 中国力学大会-2013, 中国西安, 2013年8月.
  25. 张顺, 周强, 陈刚, 李跃明. 基于热流固耦合的舵面热颤振数值模拟研究. CSTAM2013-A31-2041, 中国力学大会-2013, 中国西安, 2013年8月.
  26. 周强, 路晶晶, 陈刚, 李跃明. 基于RBF插值的通用多块静气弹求解器研究. 2013航空宇航科学与技术博士生论坛, 中国长沙, 2013年7月.
  27. Chen Gang, Li Yue-ming, P.Hu. Linear Parameter Varying Control for Active Flutter Suppression Based on Adaptive Reduced Order Model. Presentation Type: 52nd AIAA/ASME /ASCE/AHS/ASC Structures, Structural Dynamics and Materials: Technical Paper Session: SDM-13, Aeroservoelasticity, April, 2011.
  28. Chen Gang, Li Yue-ming. Active Control Law Design for LCO Suppression Based on Nonlinear Reduced Order Model Method. Presentation Type: 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials: Technical Paper Session: SDM-09, Limit Cycle Oscillations, April , 2011.
  29. Chen Gang, Sun Jian, Zuo Y., Li Yue-ming. Linear Parameter Varying Control for Active Flutter Suppression Based on Adaptive reduced Order Model. 52nd AIAA/ASME/ ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2011-1773, Denver, Colorado, April 4-7, 2011. (EI)
  30. Chen Gang, Zuo Ying-tao, Sun Jian, Li Yue-ming. Limit Cycle Oscillation Prediction via Support Vector Machine Based Reduced Order Model. 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2011-1774, 2011.4-7 April, Denver, Colorado.