The influence of surface ply fibre angle on the compressive strength of composite laminates containing delamination
The influence of surface ply fibre angle on the compressive strength of composite laminates containing delamination
复制标题
表层纤维角度对含分层复合材料层合板抗压强度的影响
DOI:
10.1017/s000192400000765x
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发表时间:
2012
期刊:
影响因子:
--
通讯作者:
N. Baker
中科院分区:
文献类型:
--
作者:
A. Rhead;R. Butler;W. Liu;N. Baker
Abstract A combination of uniaxial compression tests and Strip Model and Finite Element analyses of laminates artificially delaminated to create circular (±θ) sublaminates is used to assess the influence of fibre angle on the compressive strength of composite laminates. Sublaminates with 0° < θ < 40° are found to fail by sublaminate-buckling-driven delamination propagation and provide poor tolerance of delamination. This is a consequence of their relatively high axial stiffnesses, low sublaminate buckling strains, Poisson’s ratio induced compressive transverse strains and extension-twist coupling which produces unexpected sublaminate buckling mode shapes. Sublaminates with 40° < θ < 60° are most tolerant to delamination; axial and transverse stiffnesses are minimal, formation of sublaminate buckles is resisted, high laminate buckling strains reduce interaction between laminate and sublaminate buckling mode shapes and extension-twist coupling is minimal. Sublaminates with 60° < θ < 90° are shown to produce varied tolerance of delamination. Sublaminate buckling is generally prevented owing to transverse tensile strains induced by mismatches between laminate and sublaminate Poisson’s ratios but may occur in laminates with low Poisson’s ratios.
影响因子:
1.2
作者:
Wadee M
通讯作者:
Wadee M