一、个人基本信息
姓名：李顶河
出生年月：1983.10
籍 贯：湖北
性 别：男
民 族：汉
职 称：副教授
最高学历：博士
工作单位：中国民航大学 航空工程学院
通信地址：中国民航大学北教三-110
邮政编码：300300
办公电话：
电子邮箱：lidinghe@163.com
二、学习和工作经历
2003-2009 毕业于中国民航大学，获学士和硕士学位
2009-2012 中国民航大学助教
2012-2015 毕业于清华大学，获博士学位
2015-今 中国民航大学副教授
2017-2018 哥伦比亚大学（纽约）客座副研究员
三、主要研究方向
1.先进复合材料结构损伤分析理论与数值方法
研究内容包括：复合材料材料结构分析理论、复合材料断裂与损伤分析、有限元方法和扩展有限元方法、复合材料多尺度多物理场建模。
2.航空复合材料结构修理技术与工程应用
研究内容包括：航空复合材料结构修理技术建模分析、方案优化设计以及相关软件开发与应用。
3.航空复合材料结构健康监测技术与工程应用
研究内容包括：复合材料结构健康监测技术的全系统耦合建模分析以及健康监测技术在修理结构中的应用。
近年来主持和参与的项目：
 民用航空发动机热障涂层结构跨尺度多物理场耦合断裂机理及计算框架研究，民航联合研究基金，项目起止年月：2020年1月至 2022年12月；
 复合材料板壳结构低速冲击损伤问题的扩展逐层理论研究及其应用，国家自然基金青年科学基金项目，项目起止年月：2016年01月至 2018年 12月；
 复合材料层合板壳结构损伤疲劳扩展问题的逐层理论研究，天津市自然科学基金青年基金项目，项目起止年月：2017年04月至 2020年 03月；
 飞机复合材料结构智能补片的关键技术研究，中央高校基本科研业务费（B类），项目起止年月：2017年01月至 2019年12月；
 功能梯度材料多场耦合断裂行为预测理论及数值方法研究，中国民航大学省部级科研机构开放基金，项目起止年月：2016年10月至 2019年9月；
 三维纺织复合材料高速冲击问题的质点型细观结构建模与模拟，国家自然基金面上项目，项目起止年月：2015年01月至 2018年 12月，
四、学术兼职
中国民航大学蓝天青年****、高水平人才支持计划
天津市131创新人才培养工程第二层次人选
《航空科学技术》青年编委
《计算力学学报》特邀审稿人
世界计算力学学会会员
中国力学学会会员
五、著作和论文目录
[1] D Li*. (2020) Layerwise Theories of Laminated Composite Structures and Their Applications: A Review. Archives of Computational Methods in Engineering, DOI: 10.1007/s11831-019-09392-2.
[2] 李顶河，徐建新. 飞机复合材料结构修理：理论、设计及应用. 北京：科学出版社, 2019
[3] D Li*, W Shan. (2019) Numerical fracture analysis for chemo-mechanical coupling problems in multilayered porous media. International Journal of Mechanical Sciences, 105412.
[4] JX Xu, ZG Xiao, YG Wu, DH Li*. (2019) Extended layerwise method for laminated piezoelectric and composite plates with delaminations, cracks or debonding of a piezoelectric patch. Composite Structures, 111692.
[5] D Li*, Z Wang, C Zhang. (2019) A multi-level and multi-site mesh refinement method for the 2D problems with microstructures. Mechanics of Advanced Materials and Structures, 1-18.
[6] D Li*, W Shan, F Zhang. (2019) Steady-state thermomechanical analysis of composite laminated plate with damage based on extended layerwise method. Archive of Applied Mechanics, 1-21.
[7] Wu Y, Xiao Z, Li D, Xu J, Shen X. (2019) Numerical and experimental study on crack identification based on the piezoelectric ceramic lead zirconate titanate impedance technology. Journal of Intelligent Material Systems and Structures, 30: 1706-1716.
[8] Li D*, Fish J, Yuan Z. (2018) Two-scale and three-scale computational continua models of composite curved beams. International Journal for Multiscale Computational Engineering, 6: 527-554.
[9] Li D*, Yang X, Qian R L, et al. (2018) Static and dynamic response analysis of functionally graded material plates with damage. Mechanics of Advanced Materials & Structures 1:1-14.
[10] Lu X, Yang J Y, Xu D, Li D*. (2018) Extended Layerwise/Solid-Element method of composite sandwich plates with damage. Mechanics of Advanced Materials & Structures, 26 (16), 1376-1389.
[11] Li D*, Fish J. (2018) Thermomechanical Extended Layerwise Method for laminated composite plates with multiple delaminations and transverse cracks. Composite Structures. 185: 665-683.
[12] Xu J X, Zhang F, Li D*. (2017) Accuracy improvement of XFEM using Wilson's incompatible element technique[J]. Mechanics of Advanced Materials & Structures, 26 (5), 443-450.
[13] Li D*, Guo Q, Xu D, Yang X. (2017) Three-dimensional micromechanical analysis models of fiber reinforced composite plates with damage. Computers & Structures 191, 100-114.
[14] Li D*, Zhang F. (2017) Full extended layerwise method for the simulation of laminated composite plates and shells. Computers & Structures 187, 101-113.
[15] Lu X, Yang JY, Wu YG, Zhang F, Li D*. (2017) An extended layerwise/solid-element method of stiffened composite plates with delaminations and transverse crack. International Journal of Mechanics and Materials in Design, 1-14.
[16] Li D*. (2017) Three-dimensional analysis of transverse crack fiber bridging in laminated composite plates. Composite Structures. 164(15): 277-290.
[17] Li D*. (2016) Extended Layerwise method of laminated composite shells. Composite Structures, 136: 313-344.
[18] Li D*. (2016) Delamination and transverse crack growth prediction for laminated composite plates and shells. Computers & Structures, 177:39-55.
[19] Li D., Zhang X.*, Sze K., Liu Y.. (2016) Extended Layerwise method for laminated composite plates with multiple delaminations and matrix cracks. Computational Mechanics. 58(4): 657–679.
[20] Li D.*, Zhang F., Xu J.. (2016) Incompatible extended layerwise method for laminated composite shells. International Journal of Mechanical Sciences, 119: 243-252.
[21] Li D.*, Wang R., Qian R., Liu Y., Qing G.. (2016) Static response and free vibration analysis of the composite sandwich structures with multi-layer cores. International Journal of Mechanical Sciences, 111-112: 101-115.
[22] Li D., Liu Y., Zhang X.* (2015). An extended Layerwise method for composite laminated beams with multiple delaminations and matrix cracks. International Journal Numerical Methods Engineering, 101(6): 407-434.
[23] Li D., Liu Y., Zhang X.* (2013). A layerwise/solid-element method of the linear static and free vibration analysis for the composite sandwich plates. Composites: Part B Engineering, 252: 187-198.
[24] Li D., Liu Y., Zhang X.* (2013). Linear statics and free vibration sensitivity analysis of the composite sandwich plates based on a layerwise/solid-element method. Composite Structures, 106: 175-200.
[25] Li D., Liu Y., Zhang X.* (2014). Low-velocity impact responses of the stiffened composite laminated plates based on the progressive failure model and the layerwise/solid-elements method. Composite Structures, 110: 249-275.
[26] Li D.*, Qing G. (2014). Free vibration analysis of composite laminates with delamination based on state space theory. Mechanics of Advanced Materials and Structures, 21: 402-411.
[27] Li D.*, Qing G., Liu Y. (2013). A layerwise/solid-element method for the composite stiffened laminated cylindrical shell structures. Composite Structures, 98: 215-227.
[28] Li D.*, and Qing G. (2013). Sensitivity analysis of composite laminated plates using the meshless in the state space framework. International Journal Computational Methods, 10(5): **-1-26.
[29] Li D.*, Liu Y. (2012). Three-dimensional semi-analytical model for the static response and sensitivity analysis of the composite stiffened laminated plate with interfacial imperfections. Composite Structures, 94(6): 1943-1958.
[30] Li D.*, Xu J., Qing G. (2011). Free vibration analysis and eigenvalues sensitivity analysis for the composite laminates with interfacial imperfection. Composite, Part: B Engineering, 42: 1588-1595.
[31] Li D.*, Qing G., Liu Y. (2011). A three-dimensional semi-analytical model for the composite laminated plates with a stepped lap repair. Composite Structures, 93: 1673-1682.
[32] Li D.*, Xu J., Qing G. (2010). Sensitivity analysis of composite laminated plates with bonding imperfection in Hamilton system. Appl. Math. Mech. -Engl. Ed. 31(12): 1549-1560.
[33] G. Qing, Y. Liu, D. Li. (2011) A semi-analytical model for the energy release rate analyses of composite laminates with a delamination. Finite Elements in Analysis and Design, 47(9): 1017-1024.
[34] Y. Liu, Y. Shi, D. Li. (2011) B-Spline Wavelet on the Interval Element for the Solution of Hamilton Canonical Equation. Mechanics of Advanced Materials and Structures, 18(6): 446-453.
[35] Li D.* (2012). Delamination buckling for composite laminated cylindrical shells in Hamilton system. The IES Journal Part A: Civil & Structural Engineering, 5(4): 222-230.
[36] Li D.*, Xu J., Qing G. (2012). Meshless method of composite laminated plates with bonding interfacial imperfections in Hamilton system (in Chinese). Engineering Mechanics, 29(2): 9-15.
[37] Li D.*, Zhao L., Xu J., Qing G. (2012). Parametric investigation of orthotropic stiffened composite laminated cylindrical shells with a stepped-lap repair (in Chinese). Engineering Mechanics, 29(9): 308-317.
[38] Li D.*, Qing G., Xu J. (2011). Meshless method of radial point interpolation functions for elasticity Hamilton canonical equation (in Chinese). Engineering Mechanics, 28(10): 46-51.

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