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

被引:0
作者
Jia Xue
Wen-Xue Wang
Jia-Zhen Zhang
Su-Jun Wu
Hang Li
机构
[1] Beijing Aeronautical Science & Technology Research Institute of COMAC,Research Institute for Applied Mechanics
[2] Future Sic-Tech Park,Material Science & Engineering School
[3] Kyushu University,College of Civil Engineering
[4] Beihang University,undefined
[5] Hunan University,undefined
来源
Applied Composite Materials | 2015年 / 22卷
关键词
Fibre metal laminate; Discontinuous reinforcement; Tensile test; Finite element analysis; Cohesive zone modelling;
D O I
暂无
中图分类号
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.
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页码:489 / 505
页数:16
相关论文
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[1]  
Taketa I(2011)Flowability of unidirectionally arrayed chopped strands in compression molding Compos. Part B 42 1764-1769
[2]  
Okabe T(2009)Notched behavior of prepreg-based discontinuous carbon fiof /epoxy systems Compos. Part A 40 289-299
[3]  
Matsutani H(2010)Defect and damage analysis of advanced discontinuous carbon/epoxy composite materials Compos. Part A 41 888-901
[4]  
Kitano A(2008)A new compression-molding approach using unidirectionally arrayed chopped strands Compos. Part A 39 1884-1890
[5]  
Feraboli P(2009)Strength improvement in unidirectional arrayed chopped strands with interlaminar toughening Compos. Part A 40 1174-1178
[6]  
Peitso E(2010)Enhancement of strength and uniformity in unidirectionally arrayed chopped strands with angled slits Compos. Part A 41 1639-1646
[7]  
Cleveland T(2009)Fracture behavior in CFRP cross-ply laminates with initially cut fibers Compos. Part A 40 938-947
[8]  
Stickler P(2013)New designs of unidiretionally arrayed chopped strands by introducing discontinuous angled slits into prepreg Compos. Part A 45 127-133
[9]  
Halpin JC(2014)Multiscale analysis of damage progression in newly designed UACS laminates Compos. Part A 57 108-117
[10]  
Feraboli P(1997)Fiber metal laminates: an advanced material for future aircraft J. Mater. Process. Technol. 63 384-394