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

被引:3
|
作者
Eleonsky, S., I [1 ]
Pisarev, V. S. [1 ]
Zajtsev, M. D. [1 ]
Zichenkov, M. Ch [1 ]
Abdullin, M. R. [2 ]
机构
[1] Cent Aerohydrodynam Inst, 1 Zhukovsky St, Zhukovskii 140180, Russia
[2] Publ Joint Stock Co Tupolev, 1 Dementiev St, Kazan 420127, Russia
关键词
High-cycle fatigue; Cold hole expansion; Residual stress intensity factor; Residual stress evolution;
D O I
10.3221/IGF-ESIS.56.14
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Experimental method for a characterization of high-cycle fatigue evolution of residual stress near cold-expanded hole is developed and implemented. The technique is based on simultaneous measurements of deformation response to narrow notch, inserted in residual stress field, on opposite specimen's faces by electronic speckle-pattern interferometry (ESPI). Two-side measurements of through notch opening displacements are performed when a single notch, emanating from cold-expanded hole edge, is inserted. The transition from in-plane displacement component to residual stress intensity factor (SIF) values follows from the relationships of modified version of the crack compliance method. The approach provides a difference in residual stress values referred to mandrel entrance and exit surface. Notches are inserted at different stages of high-cycle fatigue without applying external load. The results obtained describe fine nuances of residual stress evolution, which cannot be considered as monotonic relaxation.
引用
收藏
页码:171 / 186
页数:16
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