中国航空研究院,工学硕士, 飞行器设计与气动弹性
北京航空航天大学,学士, 飞行器设计
工作经历
中国科学院力学研究所,流固耦合系统力学重点实验室,先后任助理研究员、副研究员、研究员和博导
美国University of Texas at Austin,高级访问学者
北京大学,力学与工程科学系,博士后-大型空间柔性结构的智能材料结构振动主动控制
成都飞机设计研究所,工程师-先进飞机气动弹性和结构强度分析[2]Dynamic characteristics and stability of flexible riser under consideration of non-uniform tension and internal flow. Ocean Engineering, 223(2021): 108631(1-10).
[3]LQR Control on Multimode Vortex-Induced Vibration of Flexible Riser Undergoing Shear Flow. Marine Structures, 79(2021), 103047(1-21).
[4]Moment-tensor inversion and decomposition for cracks in thin plates. Chinese Journal of Aeronautics. 2021, 34(4):352-359.
[5]Structural configuration and dynamic performances of flexible riser with distributed buoyancy modules based on FEM simulations. International Journal of Naval Architecture and Ocean Engineering. 2021, 13: 650-658
[6]Structural responses of large-sized floating wind turbine with consideration of mooring-lines dynamics based on coupled FEM simulations. Ships and Offshore Structures. 2021, 1918942(1-16).
[7]Study on Suppressing the vortex-induced vibration of flexible riser in frequency domain. Applied Ocean Researches, 116(2021), 102882(1-12).
[8]Distortion model design of flexible marine riser. J. Marine Science & Techno. 27(2022), 92-103.
[9]A moment tensor inversion approach based on the correlation between defined functions and waveforms. Physics of the Earth and Planetary Interiors, 312(2021), 106674
[10]Impacts of Mooring-lines Hysterisis on dynamic response of floating wind turbine to random wind loads. Energies, 2021,14,2109
[11]Analysis on Restoring Stiffness and Its Hysteresis Behavior of Slender Catenary Mooring-Line. Ocean Engineering. 209(2020): 107521(1-12)
[12]Accuracy of the moment-tensor inversion of far-field P waves, Geophysical Journal International, 2020, 220(1): 248-256
[13]Active control of flexible riser vibration by boundary control based on LQR controller. Proc. ASME OMAE2019 5A: Pipelines, Risers, and Subsea Systems, V05AT04A049.
[14]Analysis on multi-frequency vortex-induced vibration and mode competition of flexible ocean riser in sheared fluid field. Petroleum Science and Engineering, 2018,163: 378-386.
[15]Dynamic response analysis on flexible riser with different configurations in deep-water based on FEM simulations. Proc. ASME OMAE2010; Vol. 5: Pipelines, Risers, and Subsea Systems, V005T04A016
[16]Mechanical Deterioration of Rock Salt at Different Confinement Levels: a Grain-based Lattice Scheme Assessment. Comp. Geote. 2017(84): 210-224.
[17]Study on Multi-mode VIV of Deepwater Riser in Different Flow Fields by Finite Element Simulations. J. Offshore Mechanics and Arctic Engineering. 2016, 138(1):1-8.
[18]Non-linearly restoring performance of SFT’s catenary mooring-lines under consideration of its dynamic behaviors. Procedia Engineering 166(2016): 202-211.
[19]Impacts of top-end vessel sway on vortex-induced vibration of the submarine riser for a floating platform in deep water, Ocean Engineering, 2015, 99:1-8.
[20]Dynamic Characteristics and VIV of Deepwater Riser with Axially Varying Structural Properties, Ocean Engineering, 42(2012): 7-12.
[21] Dynamic analysis of coupling between floating top-end heave and riser’s vortex-induced vibration by using finite element simulations, Applied Ocean Research, 2014, 48(1-9).
[22]Elastic-Plastic Deformation Regimes, the One Parameter Regime and the Two Parameter Regime, of Spherical Contact by Finite Element Simulations, Vacuum, 2011, 85(9):898-903.
[23]Controlling parameter for wave types of long flexible riser undergoing vortex-induced vibration, Procedia Engineering. 2010, 4: 161-170.
[24]Indentation of Power Law Creep Solids by Self-Similar Indenters, Materials Science and Engineering: A, 2010, 527: 5613-5618.
[25]Hydroelastic dynamic characteristics of slender axis-symmetric body, Science in China Series G-Mechanical Sciences, 2010, 53(7): 1339-1347.
[26]Influence of Contact Geometry on Hardness Behavior in Nano-indentation, Vacuum, 2010, 84(2): 315-320.
[27]Factors Resulting in Micron Indentation Hardness Descending in Indentation Tests, Chinese Journal of Aeronautics, 2009, 22(1):43-48.
[28]A load simulation method of piezoelectric actuator in FEM for smart structures, Science in China Series E-Tech. Sci., 2009, 52:2576-2584.
[29]Study on the Variation of Added Mass and Its Application to the Calculation of Amplitude Response for a Circular Cylinder at Lock-in, China Ocean Engineering, 2007, 21(3):429-437.
[30]Influence of indenter tip roundness on hardness behavior in nano-indentation, Materials Science and Engineering A, 2007, 445-446: 323-327.
[31]Reduction Approaches for Vibration Control of Repetitive Structures, Applied Math. & Mech., 2006, 27(5): 637-644.
[32]Static shape control of repetitive structures integrated with piezoelectric actuators, Smart Materials and Structures, 2005, 14(6): 1410-1420.
[33]A Numerical Study of the Indentation Using Indenters of Different Geometry. J. of Materials Research, 2004, 19(1): 73-78.
[34]Distribution of measuring points and piezoelectric Actuators in flutter suppression, Chinese Journal of Aeronautics, 2002, 15(1): 33-37.
[35]Flutter Suppression Using Distributed Piezoelectric Actuators, Chinese Journal of Aeronautics, 2000, 13(4): 211-215.
[36]海洋柔性结构涡激振动的流固耦合机理和响应, 力学进展, 2017, 47(201702): 25-91.
[37]页岩气开采中的若干力学前沿问题, 力学进展,2019 (201903): 61-295.
[38]基于FEM 研究含孔隙介质中裂纹矩张量反演精度.北航学报, 2019, 45 (6 ): 1114-21.
[39]锚链动态效应对海上浮式风机整体系统动响应的影响. 中国科学, 2016, Vol.46(12): 124711.
[40]考虑塔架和叶片动力耦合的随机风载下风机结构动响应, 可再生能源, 2015, 33(5):649-655.
[41]内波波致剪切流作用下深海立管涡激振动,工程力学, 2011, 28(12): 250-56
[42]压电纤维复合材料铺层用于翼面设计驱动特性与刚度影响,航空学报. 2010, 31(2): 418-425.
[43]细长轴对称体的水弹性振动特性分析,中国科学G, 2010, 40(9): 1165-73.
[44]压电驱动的载荷比拟方法, 中国科学E, 2009, 39(11): 1810-1817.
[45]压电驱动器的气动弹性应用, 航空学报, 2009, 30(12): 1-10.
[46]重复结构振动控制降维方法, 应用数学和力学, 27(5): 637-644.
[47]固体火箭发动机柔性接头的结构分析, 推进技术, 2006, 27(5): 450-454.
[48]压痕投影接触面积标定方法的研究,力学学报. 2005, 37: 645-653.
[49]压电驱动器用于薄板型结构振动主动控制研究, 航空学报, 2001, 22(2): 109-112.