当前位置： 中文主页 > 科学研究 > 学术论文

陈刚

Personal profile

个人简介

暂未填写

学术论文

一、期刊论文

  1. 刘洋,孟凡一, 陈刚*.基于强化学习的变形飞行器抗扰补偿控制方法,系统工程与电子技术,2025, online.

  2. TieLin MA, Pu XUE, LuLu JIANG, Xin PAN , Gang CHEN*.An Efficient and High-Precision Aerodynamic Modeling Method for Hypersonic Vehicle Optimization Design,Aerospace Science and Technology,2025,accept.

  3. Ziyang Liu, Xiaotian Niu, Lulu Jiang, Xin Li, Gang Chen*.An intelligent experience learning framework for aerodynamic shape optimization with direct embedding of flow field features,Aerospace Science and Technology,2025,accept.

  4. Xin Li, Xiaotian Niu, Ziyang Liu, Lulu Jiang, Xing Ji, and Gang Chen*.A hybrid graph neural network-based framework for aerothermal prediction on hypersonic vehicles,Physics of Fluids, 2025,accept.

  5. Xin Li  Zhiwen Deng  Rui Feng, Ziyang Liu a, Renkun Han , Hongsheng Liu，Gang Chen*.Deep learning-based reduced order model for three-dimensional unsteady flow using mesh transformation and stitching.Computers & Fluids​​​​​​​,2024, 285:106441

  6. Jiang Lulu, Xue Xiaopeng,Chen Gang*.Surrogate-based Shape Optimization Design for the Stable Descent of Mars Parachutes ​​​​​​​.Aerospace Science and Technology, 2024,150:109208.

  7. Fanyi Meng, Taojun Wang, Gang Chen*.Prescribed performance-based active anti-disturbance backstepping control for morphing aircraft, Aerospace Science and Technology,online 14 July 2024, 109386​​​​​​​

  8. Xin PAN, Linlin WANG, Li LI, Lulu JIANG, Gang CHEN*​​​​​​​.Aerodynamic/control integrated optimization Method for unpowered high-speed Vehicle Configuration Design.Chinese Journal of Aeronautics,2024, 37(7): 153–167.

  9. GUO Wenzhi,Shui Yongtao, Nie Lu, Chen Gang. Fluid-structure interaction simulation for multibody flexible morphing structures[J]. Chinese Journal of Aeronautics, 2024. 37(2): 137-147.

  10. Zhe HUI, Yinan KONG, Weigang YAO, Gang CHEN.Aircraft parameter estimation using a stacked long short-term memory network and Levenberg-Marquardt method.Chinese Journal of Aeronautics,2024. 37(2):123-136.​​​​​​​

  11. Jiang Lulu,Dong Cao, Pan Xin,Chen Gang*.Aerodynamic/Control Coupling Optimization of Reentry Vehicle under Wide Speed Range.Acta Mechanica Sinica,2024,40, 324259.

  12. ​​​​​​​Shaoyang Ma,Yao Yang,Gang Chen*.AODiMP-TIR: Anti-occlusion thermal infrared targets tracker based on SuperDiMP.IET Image Processing,Volume18,Issue7,2024,Pages 1780-179.​​​​​​​​​​​​​​

  13. Jiaoxi Du, Xin Li, Siwei Dong, Ziyang Liu, Gang Chen*.A novel attention enhanced deep neural network for hypersonic spatiotemporal turbulence prediction. Physics of Fluids, 2024, 36(5): 055145.​​​​​​​

  14. Liu Z, Zhang M, Sun D, Li L.,Chen G*. A deep reinforcement learning optimization framework for supercritical airfoil aerodynamic shape design. Structural and Multidisciplinary Optimization, 2024, 67(3): 34​​​​​​​

  15. 孟俊苗,韩佳坤,陈刚*.翼型下表面柔性襟翼流动控制机理研究.西安交通大学学报，2023,9：22-30.

  16. Meng Xueguang,Chen Zengshuang,Wang Dingsheng,Jiang Shujie,Chen Gang*.Aerodynamic interference of three flapping wings in tandem configuration.Physics of Fluids,2023,35(3):031911

  17. Meng Xueguang,Liu Xinyu,Chen Zengshuang,Wu Jianghao,Chen Gang*​​​​​​​.Wing kinematics measurement and aerodynamics of hovering droneflies with wing damage.Bioinspiration & Biomimetics,2023,18(2):026013

  18. Hui Zhe,Chen Gang*.Aerodynamic Parameter Estimation for a Morphing Unmanned Aerial Vehicle from Flight Tests.Journal of Aerospace Information Systems​​​​​​​,2023,20（9）:588-595.

  19. Zhang Xitong,Chen Gui,Chen Gang*.A New Type Bionic Foldable Wing Design for High Maneuverable Unmanned Aerial Vehicle.Appl. Sci.,2023, 13(14), 8345.​​​​​​​

  20. 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).

  21. 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​​​​​​​
  22. 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
  23. 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)​​​​​​
  24. Xu Dan, Chen Gang*.Autonomous and cooperative control of UAV cluster with multi-agent reinforcement learning.The Aeronautical Journal,2022, 126：932-951.

  25. ​​​​​​​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​​​​​​​.

  26. 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)
  27. 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
  28. 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.
  29. 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. 

  30. 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

  31. 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

  32. 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)

  33. 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.

  34. 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.

  35. 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.

  36. 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）.

  37. 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)

  38. 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.

  39. 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.

  40. 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.

  41. 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.

  42. 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.

  43. 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)

  44. 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

  45. 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. 

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

  47. 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)

  48. 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.

  49. 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.

  50. 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

  51. 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.

  52.  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.

  53.  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

  54. 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. 

  55. 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

  56. 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.

  57. 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.

  58. 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.

  59. 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.

  60. 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.

  61. 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..

  62. 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.

  63. 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.

  64. 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.

  65. 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.

  66. 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. 

  67. 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.

  68. 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.

  69. 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.

  70. 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).

  71.  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.  

  72. 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.

  73. 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.

  74. 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. 

  75. 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.

  76. 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.

  77. 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.

  78.  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.  

  79. 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.

  80. 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.

  81.  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. 

  82. 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.

  83. 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. 

  84. 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.

  85. 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.

  86. 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.

  87. 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. 

  88.  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.

  89. 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.

  90. 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.

  91. 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.

  92. 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.

  93. 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.

  94. 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.

  95. 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.

  96. 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.

  97. 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.

  98. 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.

  99. 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.

  100. 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.

  101. 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.

  102. 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.

  103. 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.

  104. 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.

  105. 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.

  106. 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.

  107. 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.

  108. 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.

  109. 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.

  110. 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.

 

访问量：    最后更新时间：--

版权所有：西安交通大学 陕ICP备05001571号