Experimental and Numerical Study on the Tensile Behaviour of UACS/Al Fibre Metal Laminate

被引:12
作者
Xue, Jia [1 ,3 ]
Wang, Wen-Xue [2 ]
Zhang, Jia-Zhen [1 ]
Wu, Su-Jun [3 ]
Li, Hang [4 ]
机构
[1] COMAC, Beijing Aeronaut Sci & Technol Res Inst, Beijing, Peoples R China
[2] Kyushu Univ, Appl Mech Res Inst, Kasuga, Fukuoka 8168580, Japan
[3] Beihang Univ, Mat Sci & Engn Sch, Beijing 100191, Peoples R China
[4] Hunan Univ, Coll Civil Engn, Changsha 410082, Hunan, Peoples R China
关键词
Fibre metal laminate; Discontinuous reinforcement; Tensile test; Finite element analysis; Cohesive zone modelling; ARRAYED CHOPPED STRANDS; PROGRESSIVE FAILURE; COHESIVE ELEMENTS; ANGLED SLITS; SIMULATION; GROWTH; STRENGTH; PREPREG; STRESS; MODEL;
D O I
10.1007/s10443-014-9419-y
中图分类号
TB33 [复合材料];
学科分类号
摘要
A new fibre metal laminate fabricated with aluminium sheets and unidirectionally arrayed chopped strand (UACS) plies is proposed. The UACS ply is made by cutting parallel slits into a unidirectional carbon fibre prepreg. The UACS/Al laminate may be viewed as aluminium laminate reinforced by highly aligned, discontinuous carbon fibres. The tensile behaviour of UACS/Al laminate, including thermal residual stress and failure progression, is investigated through experiments and numerical simulation. Finite element analysis was used to simulate the onset and propagation of intra-laminar fractures occurring within slits of the UACS plies and delamination along the interfaces. The finite element models feature intra-laminar cohesive elements inserted into the slits and inter-laminar cohesive elements inserted at the interfaces. Good agreement are obtained between experimental results and finite element analysis, and certain limitations of the finite element models are observed and discussed. The combined experimental and numerical studies provide a detailed understanding of the tensile behaviour of UACS/Al laminates.
引用
收藏
页码:489 / 505
页数:17
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