TENSILE DEFORMATION BEHAVIOR AND CONSTITUTIVE MODELING OF SOLID-SOLUTION-TREATED 6061 ALUMINUM ALLOY
Abstract
To systematically investigate the tensile deformation behavior of solid-solution-treated 6061 aluminum alloy under varying temperatures and strain rates and to establish an applicable constitutive model, uniaxial tensile tests were conducted using a 68TM-50 universal tensile testing machine and a Gleeble-3800 thermomechanical simulator. The experiments covered a temperature range of 25–300 °C and strain rates of 0.001–0.1 s–1 to obtain true stress-strain data. The results indicate that, at a constant strain rate, the peak stress decreases significantly with increasing temperature, whereas at a constant temperature, the peak stress increases with the strain rate. Temperature exhibits a more pronounced influence on peak stress than strain rate. For room-temperature conditions (25 °C), the Swift model accurately predicts the deformation behavior, achieving an overall correlation coefficient (R) of 0.99846 and an average absolute relative error (AARE) of 1.41 %. For elevated temperatures (150 °C and 300 °C), a modified Johnson-Cook (J-C) model was developed by incorporating a quadratic polynomial strain-hardening term and a temperature-strain rate coupling factor, effectively integrating the effects of strain hardening, strain rate sensitivity, and thermal softening. The modified J-C model demonstrates robust predictive capability in the warm temperature regime, with an overall R of 0.99739 and an overall AARE of 5.29 %.
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