...
首页> 外文期刊>Composite Structures >Delamination and kink-band failure of pultruded GFRP laminates under elevated temperatures and compression
【24h】

Delamination and kink-band failure of pultruded GFRP laminates under elevated temperatures and compression

机译:高温和压缩状态下拉挤GFRP层压板的分层和扭折带破坏

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

Compression experiments were conducted on slender glass fiber-reinforced polymer (GFRP) laminates at different temperatures in the elevated range. Experimental buckling loads, lateral second-order deformations, and shear strength decreased with increasing temperature until stable values were reached at a much lower level in the leathery material state. The resin-dominated bending stiffness decreased at a higher rate than the fiber-dominated compressive stiffness. Global buckling followed by a delamination failure during the post-buckling process was observed for temperatures below 180 ℃, while pre-buckling kink-band failure occurred when the temperature increased to 220 ℃. Recently proposed thermome-chanical models were further validated and enabled the changing failure mode and associated Tresca and kink-band shear stress and strength conditions to be modeled.
机译:在细长的玻璃纤维增​​强聚合物(GFRP)层压板上,在升高的温度范围内的不同温度下进行了压缩实验。实验屈曲载荷,横向二阶变形和剪切强度随着温度的升高而降低,直到在皮革状材料状态下稳定值降至更低的水平为止。树脂主导的弯曲刚度以比纤维主导的压缩刚度更高的速率降低。在温度低于180℃时,观察到整体屈曲,然后在屈曲过程中发生分层破坏,而当温度升至220℃时,发生预屈曲带断裂。最近提出的热力学模型得到了进一步的验证,使不断变化的失效模式以及相关的Tresca和扭结带剪切应力以及强度条件得以建模。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号