Characterization and modeling of polymeric matrix under multi-axial static and dynamic loading

被引:34
|
作者
Werner, B. T. [1 ]
Daniel, I. M. [2 ]
机构
[1] Sandia Natl Labs, Livermore, CA 94550 USA
[2] Northwestern Univ, Robert McCormick Sch Engn & Appl Sci, Evanston, IL 60208 USA
关键词
Polymers; Nonlinear behavior; Modeling; Dynamic mechanical thermal analysis (DMTA); Casting; FIBER-REINFORCED COMPOSITES; RATE-DEPENDENT BEHAVIOR; SPLIT HOPKINSON BAR; STRAIN-RATE; CONSTITUTIVE MODEL; EPOXY-RESIN; THERMOSETTING RESINS; YIELDING BEHAVIOR; GLASSY-POLYMERS; IMPACT RATES;
D O I
10.1016/j.compscitech.2014.07.025
中图分类号
TB33 [复合材料];
学科分类号
摘要
A polymeric matrix (3501-6) used in composite materials was characterized under multi-axial loading at strain rates varying from quasi-static to dynamic. Tests were conducted under uniaxial compression, tension, pure shear and combinations of normal and shear stresses. Quasi-static and intermediate strain rate tests were conducted in a servo-hydraulic testing machine. High strain rate tests were conducted using a split Hopkinson pressure bar (Kolsky bar) system made of glass/epoxy composite bars having an impedance compatible to that of the test polymer. The typical stress-strain behavior of the polymeric matrix exhibits a linear elastic region up to a yield point, a nonlinear elastic-plastic region up to an initial peak or "critical stress," followed by strain softening up to a local minimum, plateau or saddle point stress, and finally, a strain hardening region up to ultimate failure. A general three-dimensional elastic-viscoplastic model, formulated in strain space, was developed. The model expresses the multi-axial state of stress in terms of an effective stress, incorporates strain rate effects and includes the large deformation region. Stress-strain curves obtained under multi-axial loading at different strain rates were used to develop and validate the new elastic-viscoplastic constitutive model. Excellent agreement was shown between model predictions and experimental results. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:113 / 119
页数:7
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