...
首页> 外文期刊>Journal of biomechanical engineering. >Evaluation of Global Load Sharing and Shear-Lag Models to Describe Mechanical Behavior in Partially Lacerated Tendons
【24h】

Evaluation of Global Load Sharing and Shear-Lag Models to Describe Mechanical Behavior in Partially Lacerated Tendons

机译:评估全局载荷分担和剪力滞后模型以描述部分裂筋的力学行为

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

The mechanical effect of a partial thickness tear or laceration of a tendon is analytically modeled under various assumptions and results are compared with previous experimental data from porcine flexor tendons. Among several fibril-level models considered, a shear-lag model that incorporates fibril-matrix interaction and a fibril-fibril interaction defined by the contact area of the interposed matrix best matched published data for tendons with shallow cuts (less than 50% of the cross-sectional area). Application of this model to the case of many disrupted fibrils is based on linear superposition and is most successful when more fibrils are incorporated into the model. An equally distributed load sharing model for the fraction of remaining intact fibrils was inadequate in that it overestimates the strength for a cut less than half of the tendon's cross-sectional area. In a broader sense, results imply that shear-lag contributes significantly to the general mechanical behavior of tendons when axial loads are nonuniformly distributed over a cross section, although the predominant hierarchical level and microstructural mediators for this behavior require further inquiry.
机译:在各种假设下对肌腱部分厚度撕裂或撕裂的机械作用进行了分析建模,并将结果与​​以前的猪屈肌腱实验数据进行了比较。在考虑的几种原纤维水平模型中,剪切滞后模型结合了原纤维与基体的相互作用以及由插入基质的接触面积所定义的原纤维与原纤维的相互作用,最适合已公布的浅切口肌腱的数据(少于50%横截面面积)。该模型在许多破裂的原纤维情况下的应用基于线性叠加,当将更多的原纤维结合到模型中时最成功。对于剩余的完整原纤维比例,采用均等分布的负荷分担模型是不够的,因为它高估了小于肌腱截面积一半的切口的强度。从广义上讲,结果表明,当轴向载荷在横截面上不均匀分布时,剪力滞后对钢筋的一般机械性能有显着影响,尽管这种行为的主要层次结构和微结构介质需要进一步研究。

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