李念，男，副教授，硕士生导师，1988年3月生，江苏扬州人。2016年12月获南京航空航天大学工学博士学位，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基金项目，承担多项科研院所与企业横向课题，并作为主要技术骨干参与国家重点研发项目。已在Composites Science and Technology、Thin–Walled Structures、Composites Part B、Composite Structures等国际Top或高水平期刊上发表SCI论文20余篇，并担任多个国际期刊审稿人。 长期致力于轻质结构完整性与可靠性研究，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mg4355线路检测官网E-301 学术主页：https://www.researchgate.net/profile/Nian-Li-5 近5年代表性论文： 1.Nian Li, Zhaoyang Li, Cheng Ju, Pengfei Yang, Puhui Chen, Jinling Zhao. Mechanical response and failure mechanism of composite laminates subjected to low velocity impact on free edge. Composite Structures, 2023, 306: 116617. 2.Kun Song,Nian Li, Xiang Ling, Peter Schiavone. Theoretical study on residual thermal stresses caused by the brazing process in annular and bilayer structures. Z. Angew. Math. Phys., 2023, 74: 36. 3.Nian Li, Cheng Ju, Pengfei Yang, Fujian Zhuang. Stress invariant-based failure criteria for predicting matrix failure of transversely isotropic composites: Theoretical assessment and rationalized improvement. Thin-Walled Structures, 2022, 181: 110110. 5.N. Li, Y.D. Zhou. Failure mechanism analysis of fiber-reinforced polymer composites based on multi-scale fracture plane angles. Thin-Walled Structures, 2021, 158: 107195. 6.N. Li, P.H. Chen, X. Ling. A microscopic elasto-plastic damage model for characterizing transverse responses of unidirectional fiber-reinforced polymer composites. Thin-Walled Structures, 2020, 154: 106828. 7.N. Li, C. Ju. Mode-independent and mode-interactive failure criteria for unidirectional composites based on strain energy density. Polymers, 2020, 12, 2813. 8.N. Li. Nonlinear micromechanical modelling of transverse tensile damage behavior in fiber-reinforced polymer composites. Structural Durability & Health Monitoring, 2019, 13: 331-346. 9.Y.J. Duan,N. Li, X. Ling. Numerical investigation into using coarse meshes to predict damage behaviors of laminated composites subjected to low-velocity impact. Materials Research Express, 2019, 6: 075307. 10.N. Li, J.F. Gu, P.H. Chen. Fracture plane based failure criteria for fibre-reinforced composites under three-dimensional stress state. Composite Structures, 2018, 204: 466-474. 11.N. Li, P.H. Chen. Prediction of Compression-After-Edge-Impact (CAEI) behaviour in composite panel stiffened with I-shaped stiffeners. Composites Part B, 2017, 110: 402-419. 12.N. Li, P.H. Chen. A damage mechanics model for low-velocity impact damage analysis of composite laminates. Aeronautical Journal, 2017, 128: 515-532. 13.N. Li, P.H. Chen. Failure prediction of T-stiffened composite panels subjected to compression after edge impact. Composite Structures, 2017, 162: 210-226. |
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