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首页> 外文期刊>Journal of Composite Materials >The Influence of G(I) and G(II) on the compression after impact strength of carbon fiber/epoxy laminates
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The Influence of G(I) and G(II) on the compression after impact strength of carbon fiber/epoxy laminates

机译:G(I)和G(II)对碳纤维/环氧层压材料冲击强度的影响

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摘要

This study measured the compression after impact strength of IM7 carbon fiber laminates made from epoxy resins with various mode I and mode II toughness values to observe the effects of these toughness values on the resistance to damage formation and subsequent residual compression strength-carrying capabilities. A total of seven different epoxy resin systems were used ranging in approximate GI values of 245-665 J/m(2) and approximate GII values of 840-2275 J/m(2). The results for resistance to impact damage formation showed that there was a direct correlation between GII and the planar size of damage as measured by thermography. Subsequent residual compression strength testing suggested that GI had no influence on the measured values and most of the difference in compression strength was directly related to the size of damage. Thus, delamination growth assumed as an opening type of failure mechanism does not appear to be responsible for the loss of compression strength.
机译:该研究测量了由各种模式I和模式II韧性值的环氧树脂制成的IM7碳纤维层压板冲击强度的压缩,以观察这些韧性值对抗损伤形成的抗性和随后的残留压缩强度承载能力的影响。 总共七种不同的环氧树脂系统在245-665J / m(2)的近似GI值中,近似GII值为840-2275 J / m(2)。 抗冲击损伤形成的结果表明,GII与热成像测量的损伤之间存在直接相关性。 随后的残留压缩强度试验表明GI对测量值没有影响,并且大多数压缩强度差异直接相关的损坏的尺寸。 因此,假定作为开放式故障机制的分层生长似乎对压缩强度的损失负责。

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