...
首页> 外文期刊>Frattura e Integrita Strutturale >Residual stresses near cold-expanded hole at different stages of highcycle fatigue by crack compliance data
【24h】

Residual stresses near cold-expanded hole at different stages of highcycle fatigue by crack compliance data

机译:通过裂缝合规性数据在高循环疲劳的不同阶段附近的残余应力

获取原文
   

获取外文期刊封面封底 >>

       

摘要

Experimental method for a characterization of high-cycle fatigueevolution of residual stress near cold-expanded hole is developed andimplemented. The technique is based on simultaneous measurements ofdeformation response to narrow notch, inserted in residual stress field, onopposite specimen’s faces by electronic speckle-pattern interferometry(ESPI). Two-side measurements of through notch opening displacements areperformed when a single notch, emanating from cold-expanded hole edge, isinserted. The transition from in-plane displacement component to residualstress intensity factor (SIF) values follows from the relationships of modifiedversion of the crack compliance method. The approach provides a differencein residual stress values referred to mandrel entrance and exit surface. Notchesare inserted at different stages of high-cycle fatigue without applying externalload. The results obtained describe fine nuances of residual stress evolution,which cannot be considered as monotonic relaxation. .
机译:开发了冷膨胀孔附近的残余应力高周脂肪屈光度的表征实验方法。该技术基于对窄凹口的同时测量,插入残余应力场中,通过电子散斑图案干涉测定法(ESPI)。通过凹口开口位移的两侧测量值在单个凹口,从冷膨胀孔边缘发出时,通过缺口。从面内位移分量到残留的强度因子(SIF)值的过渡遵循裂缝顺应方法的修正率的关系。该方法提供了差异差应力值,称为心轴入口和出口表面。在不申请外部插入的情况下,在高循环疲劳的不同阶段插入缺口。得到的结果描述了残余应力进化的细微差别,不能被认为是单调弛豫。 。

著录项

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