一、个人基本信息
姓名：李顶河
出生年月：1983.10
籍贯：湖北咸宁
性别：男
民族：汉
职称：教授
政治面貌：中共党员
最高学历：博士研究生
工作单位：5元可提现的电玩城5元可提现的电玩城
通讯地址：天津市东丽区津北公路2898号
邮政编码：300300
办公电话：022-24092870
电子邮箱：lidinghe@163.com
二、学习和工作经历
受教育经历：
2012年08月-2015年01月，清华大学，航空宇航科学与技术专业，博士
2007年09月-2009年06月，5元可提现的电玩城，人机与环境工程专业，硕士
2003年09月-2007年07月，5元可提现的电玩城，飞行器动力工程专业，学士
工作与研究经历：
2022年05月-今，5元可提现的电玩城，院长，教授；
2020年12月-2022年5月，航空工程学院，副院长，教授；
2015年12月-2020年12月，航空工程学院，飞机系系主任、副院长，副教授、教授
2017年07月-2018年07月，哥伦比亚大学（纽约），访问学者；
2009年09月-2012年06月，航空工程学院，助教；
三、主要研究方向
[1] 高精度板壳分析理论、先进数值方法；
[2] 异性材料断裂与损伤力学、多物理场求解理论、多尺度分析理论；
[3] 复合材料结构修理技术、民用飞机结构健康监测与管理技术。
四、学术兼职
商用航空发动运维技术开发联合实验室主任（5元可提现的电玩城与中国航发商用发动机有限公司共建）、民用飞机维修工程系列教材专家委员会副主任委员、全国专业标准化技术委员会浮空器分技术委员会委员（SAC/TC435/SC2）、《航空科学技术》青年编委、《应用力学学报》青年编委、《计算力学学报》特邀审稿人。
五、著作和论文目录
[1] D Li*, F You, Y Liu, Q Guo. On oxide growth fracture analysis of thermal barrier coatings based on a three-dimensional chemo-mechanical model. Materials Today Communications 31, 103793
[2] D Li. (2022) Analysis of Composite Laminates: Theories and Their Applications. Elsevier.
[3] D Li*, S Ma. (2022) Dynamic thermomechanical analysis on stiffened composite plates with damage. The Journal of Thermal Stresses
[4] Z Xiao, Y Wu, D Li*. (2022) Thermo-electro-mechanical dynamic fracture analysis on laminated piezoelectric plates. Composite Structures, 285: 115158
[5] D Li*, P Wu, A Wan. (2022) A two-scale computational continua multiscale analysis model for honeycomb sandwich plates. Mechanics of Advanced Materials and Structures
[6] D Li*, Z Yun, (2022) Thermo-mechanical progressive analysis on multiple delaminations in composite laminates. Continuum Mechanics and Thermodynamics, 34: 341-366
[7] Y Wu, X Shen，D Li. (2021) Modeling, identification and optimization of damage deterioration in the bolted repaired metallic plate. Ferroelectrics, 583(1): 278-294.
[8] Y Wu, Z Xiao, K Liu, D Li*. (2021) A three-dimensional numerical model for delaminations, transverse crack or debonding in composite sandwich plates with piezoelectric sensors. Journal of Intelligent Material Systems and Structures, 33(7): 883-900
[9] D Li*, S Ma. (2021) Dynamic thermomechanical analysis on composite sandwich plates with damage. Continuum Mechanics and Thermodynamics, 33: 2167–2201
[10] D Li, Z Wang, C Zhang*. (2021) Computational continua method and multilevel-multisite mesh refinement method for multiscale analysis of woven composites laminates. Composite Structures, 259: 113441
[11] W Shan, D Li*. (2021) Thermo-mechanic-chemical coupling fracture analysis for thermal barrier coating based on extended layerwise method. Surface and Coatings Technology, 405: 126520
[12] D Li*, A Wan. (2021) A layerwise multiscale analysis method for composite laminated plates. Composite Structures, 257: 113157
[13] Wu Y, Xiao Z, D Li*, et al. (2020) On numerical static analysis of stiffened laminated composite plates with delaminations, cracks, or debonding of a piezoelectric patch. Mechanics of Advanced Materials and Structures, 29(1): 89-103.
[14] D Li*. (2020) Layerwise Theories of Laminated Composite Structures and Their Applications: A Review. Archives of Computational Methods in Engineering, 28: 577–600
[15] 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
[16] D Li*, W Shan. (2020) Numerical fracture analysis for chemo-mechanical coupling problems in multilayered porous media. International Journal of Mechanical Sciences, 172: 105412.
[17] J Xu, Z Xiao, Y Wu, D Li*. (2020) Extended layerwise method for laminated piezoelectric and composite plates with delaminations, cracks or debonding of a piezoelectric patch. Composite Structures, 234: 111692.
[18] D Li*, Z Wang, C Zhang. (2021) A multi-level and multi-site mesh refinement method for the 2D problems with microstructures. Mechanics of Advanced Materials and Structures, 28(14).
[19] D Li*, W Shan, F Zhang. (2020) Steady-state thermomechanical analysis of composite laminated plate with damage based on extended layerwise method. Archive of Applied Mechanics, 90: 415–435.
[20] 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.
[21] 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.
[22] 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.
[23] 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.
[24] Li D*, Fish J. (2018) Thermomechanical Extended Layerwise Method for laminated composite plates with multiple delaminations and transverse cracks. Composite Structures. 185: 665-683.
[25] Xu J X, Zhang F, Li D*. (2017) Accuracy improvement of XFEM using Wilson's incompatible element technique. Mechanics of Advanced Materials & Structures, 26 (5), 443-450.
[26] 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.
[27] Li D*, Zhang F. (2017) Full extended layerwise method for the simulation of laminated composite plates and shells. Computers & Structures 187, 101-113.
[28] 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.
[29] Li D*. (2017) Three-dimensional analysis of transverse crack fiber bridging in laminated composite plates. Composite Structures. 164(15): 277-290.
[30] Li D*. (2016) Extended Layerwise method of laminated composite shells. Composite Structures, 136: 313-344.
[31] Li D*. (2016) Delamination and transverse crack growth prediction for laminated composite plates and shells. Computers & Structures, 177:39-55.
[32] 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.
[33] Li D.*, Zhang F., Xu J.. (2016) Incompatible extended layerwise method for laminated composite shells. International Journal of Mechanical Sciences, 119: 243-252.
[34] 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.
[35] 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.
[36] 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.
[37] 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.
[38] 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.
[39] 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.
[40] 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.
[41] 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): 1350023-1-26.
[42] 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.
[43] 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.
[44] 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.
[45] 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.
[46] 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.
[47] 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.
[48] 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.
