陈普会
    博士生导师
  • 招生学科专业:
    航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 航空学院
    机械 -- 【招收博士、硕士研究生】 -- 航空学院
  • 学位:工学博士学位
  • 职称:教授
  • 所在单位:航空学院
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所在单位:航空学院
学历:南京航空航天大学

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标题:
Mesoscale modelling of damage in half-hole pin bearing composite laminate specimens
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所属单位:
航空学院
发表刊物:
Compos. Struct.
摘要:
This paper presents the development and validation of a mesoscale numerical model for predicting the bearing damage and failure of composite laminates reinforced by unidirectional fibers. Firstly, half-hole pin bearing tests were carried out on composite laminates with both quasi-isotropic and soft lay-ups, as well as in specimens with variations in ply thickness and stacking sequence, using multiple measurement and inspection tools for a comprehensive characterization of the damage mechanisms. Then, three dimensional (3D) finite element models with a fiber-aligned mesh for composite plies and considering various frictional contacts were built to simulate the bearing tests using a commercial explicit solver. The embedded material model incorporated 3D phenomenological invariant-based failure criteria using in situ ply strengths, together with mechanism-based continuum damage models (longitudinal bi-linear damage model and transverse 3D smeared crack model) for intralaminar damage, and the cohesive zone model for interlaminar damage. Finally, detailed analyses and comparisons of the experimental and numerical results were performed in both macroscopic mechanical behavior and mesoscale failure mechanisms, where a good correlation was observed. Sensitivity studies on the effect of the modelling parameters on the post-peak response prediction were also conducted, providing relevant guidelines to identify future research directions. © 2019 Elsevier Ltd
ISSN号:
0263-8223
是否译文:
发表时间:
2019-01-01
合写作者:
Zhuang, Fujian,Arteiro, Albertino,Camanho, Pedro P.
通讯作者:
陈普会
发表时间:
2019-01-01
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