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Analytical and experimental studies on mechanical behavior of composites under high strain rate compressive loading

机译:高应变率压缩载荷下复合材料力学行为的分析和实验研究

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摘要

An analytical method is presented for the prediction of compressive strength at high strain rate loading for composites. The method is based on variable rate power law. Using this analytical method, high strain rate compressive stress-strain behavior is presented up to strain rate of 5000 s~(-1) starting with the experimentally determined compressive strength values at relatively lower strain rates. Experimental results were generated in the strain rate range of 472-1957 s~(-1) for a typical woven fabric E-glass/epoxy laminated composite along all the three principal directions. The laminated composite was made using resin film infusion technique. The experimental studies were carried out using compressive split Hopkinson pressure bar apparatus. It was generally observed that the compressive strength is enhanced at high strain rate loading compared with that at quasi-static loading. Also, compressive strength increased with increasing strain rate in the range of parameters considered. Analytically predicted results are compared with the experimental results up to strain rate of 1957 s~(-1).
机译:提出了一种分析方法,用于预测复合材料在高应变速率载荷下的抗压强度。该方法基于可变速率幂律。使用这种分析方法,以相对较低的应变速率通过实验确定的抗压强度值开始,以高达5,000 s〜(-1)的应变速率呈现出高应变速率的压缩应力-应变行为。对于典型的机织电子玻璃/环氧层压复合材料,在所有三个主要方向上的应变速率范围为472-1957 s〜(-1),产生了实验结果。层压复合材料使用树脂膜灌注技术制成。实验研究是使用压缩分流霍普金森压力棒设备进行的。通常观察到,与准静态载荷相比,高应变率载荷下的抗压强度有所提高。同样,在考虑的参数范围内,抗压强度随应变率的增加而增加。将解析预测结果与高达1957 s〜(-1)的应变率的实验结果进行比较。

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  • 来源
    《Materials & design》 |2013年第2期|246-255|共10页
  • 作者单位

    Aerospace Engineering Department, Indian Institute of Technology Bombay, Powai, Mumbai 400 076, India;

    Aerospace Engineering Department, Indian Institute of Technology Bombay, Powai, Mumbai 400 076, India;

    R&DE(E), Pune 411 015, India;

    R&DE(E), Pune 411 015, India;

    Aerospace Engineering Department, Indian Institute of Technology Bombay, Powai, Mumbai 400 076, India,R&DE(E), Pune 411 015, India;

    Aerospace Engineering Department, Indian Institute of Technology Bombay, Powai, Mumbai 400 076, India;

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