Volume 42, Issue 9 pp. 2061-2078
SPECIAL ISSUE CONTRIBUTION

Residual stress/strain evolution due to low-cycle fatigue by removing local material volume and optical interferometric data

Yury Matvienko

Corresponding Author

Yury Matvienko

Mechanical Engineering Research Institute of the Russian Academy of Science, 4 Maly Kharitonievsky Pereulok, 101990 Moscow, Russia

Correspondence

Y. G. Matvienko. Mechanical Engineering Research Institute of the Russian Academy of Science, 4 Maly Kharitonievsky Pereulok, 101990 Moscow, Russia.

Email: [email protected]

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Vladimir Pisarev

Vladimir Pisarev

Central Aero-Hydrodynamics Institute named after Prof. N.E. Zhukovsky (TsAGI), 1 Zhukovsky Street, Zhukovsky, 140180 Moscow Region, Russia

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Svyatoslav Eleonsky

Svyatoslav Eleonsky

Central Aero-Hydrodynamics Institute named after Prof. N.E. Zhukovsky (TsAGI), 1 Zhukovsky Street, Zhukovsky, 140180 Moscow Region, Russia

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Andrey Chernov

Andrey Chernov

Central Aero-Hydrodynamics Institute named after Prof. N.E. Zhukovsky (TsAGI), 1 Zhukovsky Street, Zhukovsky, 140180 Moscow Region, Russia

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First published: 08 July 2019
Citations: 4

Abstract

Three experimental methods, based on optical interferometric measurements of deformation response to local material removing, have been implemented for residual stresses determination. Two first techniques are employed to characterize initial residual stress values and their evolution near welded joints of aluminium plates under low-cycle fatigue. The hole-drilling method gives high-accurate dependencies between residual stress components and number of cycles. The second approach comprises cracks modelling by narrow notches to describe residual stress distributions in more wide spatial range near the weld. The results demonstrate residual stress evolution is of complex character and cannot be uniquely qualified as a gradual relaxation. Besides, the secondary hole drilling method is developed and used as a fast and reliable tool to quantify the redistribution of residual strains near cold-expanded holes due to low-cycle fatigue. Dependencies of circumferential residual strains along the secondary hole edge versus number of cycles are constructed.

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