Modeling and testing strain rate-dependent compressive strength of carbon/epoxy composites

被引:68
作者
Bing, QD [1 ]
Sun, CT [1 ]
机构
[1] Purdue Univ, Sch Aeronaut & Astronaut, W Lafayette, IN 47907 USA
关键词
carbon fiber; composite; titanium coating; strain rate; compressive strength; microbuckling; split Hopkinson pressure bar;
D O I
10.1016/j.compscitech.2005.06.012
中图分类号
TB33 [复合材料];
学科分类号
摘要
A technique for testing high modulus fiber-reinforced composites in compression at different strain rates is investigated. The rate-dependent compressive behavior of unidirectional AS4/3501-6 carbon/epoxy composite is characterized by using off-axis specimens. lt is found that, in the compression test, a titanium coating applied at the contact ends of the off-axis specimen can greatly reduce contact frictions, allowing a fully developed extension-shear coupling so that a state of uniform stress in the specimen can be achieved. A rate-dependent nonlinear constitutive model and a dynamic compressive strength model (fiber microbuckling model) for the unidirectional AS4/3501-6 composite are established based on the low strain rate off-axis test data. Model predictions and experimental data including high strain rate data are in very good agreement indicating that the constitutive model and compressive strength model obtained with low strain rate data are valid for high strain rates as well. A technique is also developed to extract the longitudinal compressive strength of the composite from those of the off-axis specimens. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2481 / 2491
页数:11
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