Abstract

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 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 low-cycle fatigue without applying external load. The results obtained describe fine nuances of residual stress evolution, which cannot be considered as monotonic relaxation.

Highlights

  • Cold hole expansion process is widely used to improve the fatigue life of aerospace structures [1]

  • The technique is based on two-side measurements of deformation response to narrow notch, which is simultaneously inserted on opposite specimen’s faces

  • Deformation response has a form of notch opening displacements, which are measured by electronic speckle-pattern interferometry (ESPI)

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Summary

Introduction

Cold hole expansion process is widely used to improve the fatigue life of aerospace structures [1]. Deriving additional information, which is related to residual stress redistribution near cold-expanded holes in plane rectangular specimens under high-cycle fatigue on a base of two-side measurements, is the main goal of this paper. Low interference level provides reason enough to obtain residual SIF values as a result of direct measurements of notch opening displacements.

Results
Conclusion

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