首页> 外文会议>Sixth Symposium on Composites: Fatigue and Fracture 16-18 May 1995 in Denver, Colorado >A Strength-Based Wearout Model for Predicting the Life of Composite Structures
【24h】

A Strength-Based Wearout Model for Predicting the Life of Composite Structures

机译:基于强度的磨损模型,用于预测复合结构的寿命

获取原文
获取原文并翻译 | 示例

摘要

A model to predict the residual strength and life of polymric composite structures subjected to spectrum fatigue loadings is described. The model is based on the fundamental assumptions that the structure undergoes proportional loading, that the residual strength is a monotonically decreasing function of the number of fatigue cycles, and that both the life distribution due to continuous constant amplitude cycling and theresidual strength distribution after an arbitrary load history may be represented by two parameter Weibull functions. The model also incorporates a "cycle mix factor" to account for the drastic reduction of fatigue life that may be caused by a large number of charges in the stress amplitude of the loading. The model's predictions are compared to experiemntally determined fatigue life dsitributions for uniaxial loadings of a number of laminates comprised of different materials and layups. Constant-amplitude, two-stress level, and spectrum fatigue loadings, including the FALSTAFF (Fighter Aircraft Loading STAndard For Fatigue) spectrum, are considered. The theoretical fatigue life distributions are shown to correlate well with the experimental results. Moreover, excllent correlation of theory and experiment is obtained for an "average fatigue life" that is based on the 63.2
机译:描述了一种模型,该模型可预测承受光谱疲劳载荷的多晶复合材料结构的剩余强度和寿命。该模型基于以下基本假设:结构承受比例载荷,残余强度是疲劳循环数的单调递减函数,并且连续不断的振幅循环引起的寿命分布和任意强度后的剩余强度分布负载历史记录可由两个参数Weibull函数表示。该模型还包含一个“循环混合因子”,以说明疲劳寿命的急剧下降,这可能是由于载荷应力幅值中的大量电荷导致的。将模型的预测与由不同材料和叠层组成的许多层压板的单轴载荷的经验确定的疲劳寿命分布进行比较。考虑了恒定振幅,两应力水平和频谱疲劳载荷,包括FALSTAFF(用于疲劳的战机载荷标准)频谱。结果表明,理论疲劳寿命分布与实验结果具有很好的相关性。此外,基于63.2的“平均疲劳寿命”获得了理论和实验的出色关联。

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