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Effective thermoelastic constants of short-fiber composites 短纤维复合材料的有效热弹性常数
Fibre Science and Technology
Pub Date : 1984-01-01 DOI: 10.1016/0015-0568(84)90042-3
J. Aboudi
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引用次数: 20
GRP in structural engineering GRP在结构工程中的应用
Fibre Science and Technology
Pub Date : 1984-01-01 DOI: 10.1016/0015-0568(84)90020-4
S.A. Paipetis
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引用次数: 0
International symposium on composites: Materials and engineering, 国际复合材料研讨会:材料与工程，
Fibre Science and Technology
Pub Date : 1984-01-01 DOI: 10.1016/0015-0568(84)90029-0
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引用次数: 0
Composite materials: Mechanics, mechanical properties and fabrication 复合材料:力学、力学性能及制造
Fibre Science and Technology
Pub Date : 1983-04-01 DOI: 10.1016/0015-0568(83)90044-1
S.A. Paipetis
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引用次数: 0
Transient hygrothermal stresses in plates with and without cavities 有腔和无腔板的瞬态湿热应力
Fibre Science and Technology
Pub Date : 1983-04-01 DOI: 10.1016/0015-0568(83)90040-4
G. Sih
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引用次数: 11
Transverse cracking and delamination in composite materials 复合材料的横向开裂和分层
Fibre Science and Technology
Pub Date : 1983-04-01 DOI: 10.1016/0015-0568(83)90041-6
R. Kim, R. Aoki
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引用次数: 10
Damage development in CFRP laminates under monotonic and cyclic stressing CFRP复合材料在单调和循环应力作用下的损伤发展
Fibre Science and Technology
Pub Date : 1983-04-01 DOI: 10.1016/0015-0568(83)90039-8
R.P. Harrison, M.G. Bader

Simple [0°/90°/0°], [±45°] and quasi-isotropic carbon fibre reinforced epoxy laminates were tested in uniaxial tension. The first sign of damage was fibre/resin debonds in the transverse plies. The transverse (90°) ply cracking strain was found to increase with decreasing transverse ply thickness. A similar effect was found in the [±45°] laminates—thinner plies being able to support higher loads. The failure mode in quasi-isotropic laminates was found to depend on the ply stacking sequence. Again, the transverse ply cracking strain was greater for thinner transverse plies. In fatigue, the transverse ply cracking strain of [0°/90°/0°] specimens was found to be lower than that of similar specimens tested in uniaxial tension. A resin-rich area between the transverse and longitudinal plies delayed the propagation of transverse ply cracks under fatigue loading, thus delaying the appearance of delamination along the 0°/90° interface.

简单的[0°/90°/0°]、[±45°]和准各向同性碳纤维增强环氧树脂层压板在单轴拉伸下进行了测试。损伤的第一个迹象是横向帘布层中的纤维/树脂脱胶。发现横向（90°）帘布层开裂应变随着横向帘布层厚度的减小而增加。在[±45°]层压板中也发现了类似的效果——较薄的层压板能够支撑更高的载荷。发现准各向同性层压板的失效模式取决于层板的堆叠顺序。同样，对于较薄的横向帘布层，横向帘布层的开裂应变较大。疲劳试验中，[0°/90°/0°]试样的横向层裂应变低于单轴拉伸试验中的类似试样。横向和纵向帘布层之间的树脂富集区域延缓了疲劳载荷下横向帘布层裂纹的扩展，从而延缓了沿0°/90°界面分层的出现。
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引用次数: 48
Transverse cracking and delamination in composite materials 复合材料的横向开裂和分层
Fibre Science and Technology
Pub Date : 1983-04-01 DOI: 10.1016/0015-0568(83)90041-6
R.Y. Kim, R.M. Aoki

An experimental investigation has been conducted on damage behaviour related with matrix cracking under static and fatigue loading using two stacking sequences of the (0/90n/±45)s and (0/±45/90n)s laminates for n = 1, 3, and 6. The latter stacking sequence produces tensile interlaminar normal stress along free edges of a tensile coupon, whereas the other stacking sequence produces compression at the same edges. Emphasis in this study was on the interaction between transverse cracks and delamination, and effect of layer thickness on crack density and propagation. Transverse crack and delamination were periodically measured by interrupting testing until final failure. Experimental results indicate that the crack density and propagation are influenced by layer thickness, and delamination appears to be mainly governed by either, or a combination of, tensile interlaminar normal stress and size of transverse crack. The applied force at incipient delamination can be predicted by an existing theory with a certain limitation.

使用（0/90n/±45）s和（0/±45/90n）s层压板的两个堆叠顺序，对静载荷和疲劳载荷下与基体开裂相关的损伤行为进行了实验研究，其中n=1、3和6。后一种堆叠顺序沿着拉伸试片的自由边缘产生拉伸层间法向应力，而另一种堆叠序列在相同边缘产生压缩。本研究的重点是横向裂纹和分层之间的相互作用，以及层厚度对裂纹密度和扩展的影响。通过中断测试定期测量横向裂纹和分层，直到最终失效。实验结果表明，裂纹密度和扩展受层厚的影响，分层似乎主要受层间拉伸正应力和横向裂纹尺寸的控制，或两者的组合。在存在一定局限性的情况下，现有理论可以预测初始分层时施加的力。
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引用次数: 12
Sixth international conference on fracture 第六届国际骨折会议
Fibre Science and Technology
Pub Date : 1983-04-01 DOI: 10.1016/0015-0568(83)90045-3
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引用次数: 0
The effect of fibre-interface and processing variables on the mechanical properties of glass-fibre filled nylon 6 研究了纤维界面及工艺参数对玻璃纤维填充尼龙6力学性能的影响
Fibre Science and Technology
Pub Date : 1983-04-01 DOI: 10.1016/0015-0568(83)90042-8
M. G. Bader, J. Collins
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引用次数: 24
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