李念，男，工学博士，南京工业大学机械与动力工程学院化工机械研究所助理教授/硕导，现任中国航空学会、江苏省力学学会会员。目前主持国家自然科学青年基金项目，参与国家重点研发项目，承担多项科研院所与企业横向课题。近5年内在Composites Science and Technology、Thin–Walled Structures、Composites Part B、Composite Structures等国际高水平杂志上发表SCI论文十余篇。
长期致力于化工及航空航天领域工程结构的轻量化与可靠性研究，主要研究包括多尺度复合材料损伤理论与数值分析、复合材料结构冲击损伤与损伤容限分析、典型结构损伤修理等。
Email: linian@njtech.edu.cn
地址：南京工业大学江浦校区机械与动力工程学院E-301
近5年代表性论文：
1.Li N, Zhou YD. Failure mechanism analysis of fiber-reinforced polymer composites based on multi-scale fracture plane angles. Thin–Walled Structures, 2021, 158: 107195.
2. Li N, Chen PH, Ling X. A microscopic elasto-plastic damage model for characterizing transverse responses of unidirectional fiber-reinforced polymer composites. Thin–Walled Structures, 2020, 154: 106828.
3. Li N. Nonlinear Micromechanical Modelling of Transverse Tensile Damage Behavior in Fiber-Reinforced Polymer Composites. Structural Durability & Health Monitoring, 2019, 13(4): 331-346.
4. Duan YJ, Li N(*), Ling X. Numerical investigation into using coarse meshes to predict damage behaviors of laminated composites subjected to low-velocity impact. Materials Research Express, 2019, 6: 075307.
5. Li N(*), Gu JF, Chen PH. Fracture plane based failure criteria for fibre-reinforced composites under three-dimensional stress state. Composite Structures, 2018, 204: 466-474.
6. Li N, Chen PH. Prediction of Compression-After-Edge-Impact (CAEI) behaviour in composite panel stiffened with I-shaped stiffeners. Composites Part B, 2017, 110: 402-419.
7. Li N, Chen PH. Failure prediction of T-stiffened composite panels subjected to compression after edge impact. Composite Structures, 2017, 162: 210-226.
8. Li N, Chen PH, Ye Q. A damage mechanics model for low-velocity impact damage analysis of composite laminates. Aeronautical Journal, 2017, 128: 515-532.
9. Li N, Chen PH. Experimental investigation on edge impact damage and Compression-After-Impact (CAI) behavior of stiffened composite panels .Composite Structures, 2016, 138: 134-150.
10. Li N, Chen PH. Micro-macro FE modeling of damage evolution in laminated composite plates subjected to low velocity impact. Composite Structures, 2016, 147: 111-121.
11. Li N, Chen PH, Liu XY, et al. A micro-macro finite element model for failure prediction of Comeld^TMjoints. Composites Science and Technology, 2015, 117: 334-341.