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A Journal of Russian Academy of Sciences
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IssuesArchive of Issues2024-2pp.734-745

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A.S. Dzuba, S.I. Eleonsky, M.D. Zajtsev, and V.S. Pisarev, "Evolution of Damage Indicators under Cyclic Loading of a Composite Plate with a Hole," Mech. Solids. 59 (2), 734-745 (2024)
Year 2024 Volume 59 Number 2 Pages 734-745
DOI 10.1134/S0025654423601866
Title Evolution of Damage Indicators under Cyclic Loading of a Composite Plate with a Hole
Author(s) A.S. Dzuba (Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Zhukovsky, 140100 Russia, dzuba@tsagi.ru)
S.I. Eleonsky (Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Zhukovsky, 140100 Russia, juzzepka@mail.ru)
M.D. Zajtsev (Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Zhukovsky, 140100 Russia, zaytcev@list.ru)
V.S. Pisarev (Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Zhukovsky, 140100 Russia, VSP5335@mail.ru)
Abstract A new experimental method has been developed that provides a quantitative description of the evolution of damage indicators under cyclic loading of composite samples with stress concentrators. Damage parameters are defined as the deformation response to the application of an artificial cut of a given length, which extends from the contour of the central through hole in a flat rectangular sample under constant external load. Based on the test results of eight samples, the current values of damage indicators at various stages of fatigue loading were obtained. These data reveal the dependence of the required parameters on the number of loading cycles. On this basis, a damage accumulation function was constructed for the considered range of cycles. It has been established that this function refers to the first stage of the process under study. The results obtained are a necessary basis for planning further experiments.
Keywords composite materials, cyclic loading, damage accumulation, artificial notch, speckle interferometry
Received 13 July 2024Revised 07 September 2024Accepted 21 September 2024
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