个人简历
詹志新，博士，副教授。2016年1月于北京航空航天大学获固体力学专业博士学位。曾任北航飞机系卓百博士后研究员、新加坡南洋理工大学Research Fellow。2019年9月起任北京航空航天大学固体力学所副教授、硕士生导师。研究方向
疲劳与损伤力学
缺陷容限
3D打印材料与数据驱动寿命预测
社会兼职
担任以下学术期刊审稿人：
International Journal of Fatigue
International Journal of Mechanical Sciences
International Journal of Damage Mechanics
Aerospace Science and Technology
Mechanics of Materials
Engineering Failure Analysis
Advances in Mechanical Engineering
论文成果
当前位置: 中文主页 >> 论文成果[1]Zhan ZX, Li H, Lam K.Y. Development of a novel fatigue damage model with AM effects for life prediction of commonly-used alloys in aerospace. International Journal of Mechanical Sciences. 2019, 155: 110-124.
[2]Zhan ZX. Experiments and numerical simulations for the fatigue behavior of a novel TA2-TA15 titanium alloy fabricated by laser melting deposition. International Journal of Fatigue. 2019, 121: 20-29.
[3]Zhan ZX, Hu WP, Li BK, et al. Continuum damage mechanics combined with the extended finite element method for the total life prediction of a metallic component. International Journal of Mechanical Sciences. 2017, 124: 48-58.
[4]Zhan ZX, Meng QC, Hu WP, et al. Continuum damage mechanics based approach to study the effects of the scarf angle, surface friction and clamping force over the fatigue life of scarf bolted joints. International Journal of Fatigue. 2017, 102: 59-78.
[5]Zhan ZX, Hu WP, Shen F, et al. Fatigue life calculation for a specimen with an impact pit considering impact damage, residual stress relaxation and elastic-plastic fatigue damage. International Journal of Fatigue. 2017, 96: 208-223.
[6]Zhan ZX, Hu WP, Zhang M, et al. The fatigue life prediction for structure with surface scratch considering cutting residual stress, initial plasticity damage and fatigue damage. International Journal of Fatigue. 2015, 74: 173-182.
[7]Zhan ZX, Hu WP, Zhang M, et al. A revised damage evolution equation for high cycle fatigue life prediction of aluminum alloy LC4 under uniaxial loading. Applied Mathematics and Mechanics. 2015, 36(9): 1185-1196.
[8]Zhan ZX, Hu WP, Meng QC, et al. Continuum damage mechanics based approach to the fatigue life prediction for 7050-T7451 aluminum alloy with impact pit. International Journal of Damage Mechanics. 2016, 25(7): 943-966.
[9]Zhan ZX, Hu WP, Zhang M, et al. Experimental method for and theoretical research on defect tolerance of fixed plate based on damage mechanics. Chinese Journal of Aeronautics. 2013, 26(5): 1195-1201.
[10]Zhan ZX, Hu WP, Meng QC, et al. Fatigue life and defect tolerance calculation for specimens with foreign object impact and scratch damage. Archive of Applied Mechanics. 2018, 88(3): 373-390.
[11]Zhan ZX. Fatigue life calculation for TC4-TC11 titanium alloy specimens fabricated by laser melting deposition. Theoretical and Applied Fracture Mechanics. 2018, 96: 114-122.
[12]Zhan ZX, Hu WP, Zhang M, et al. A study on the effect of surface defect on the fatigue performance of metal component based on damage mechanics. Mechanika. 2015, 21(1): 5-10.
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研究领域
当前位置: 中文主页 >> 研究领域材料的疲劳
损伤力学
缺陷容限
3D打印航空航天金属材料的疲劳损伤特性分析
机器学习
科研项目
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开授课程
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荣誉及奖励
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