Conclusions
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1.
Deformation by rolling of naturally aged alloy 1163 with ε ≥7% leads to a reduction in fracture toughness.
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2.
After deformation with a degree of 11–15%, compared with deformation ε=7% adopted previously for manufacturing alloy D16 sheets, a greater increase in strength properties is achieved with the same levels of ductility, fracture toughness, homogeneous distribution of dislocations, and also low-cycle fatigue indices not lower than in the original naturally aged condition.
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Aviation Materials Institute, Moscow. Translated from Metallovedenie i Termicheskaya Obrabotka Metallov, No. 2, pp. 61–62, February, 1985.
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Leshchiner, L.N., Kishkina, S.I. & Gerchikova, N.S. Effect of degree of deformation on the structure and properties of naturally aged alloy 1163. Met Sci Heat Treat 27, 163–164 (1985). https://doi.org/10.1007/BF00736594
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DOI: https://doi.org/10.1007/BF00736594