Stress–Strain Properties of Artificially Aged 6061 Al Alloy: Experiments and Modeling

Keyphrases

• Stress-strain 100%
• 6061 Al Alloy 100%
• Metal Matrix 66%
• Void Growth 66%
• Fracture Strength 66%
• Mechanical Behavior 33%
• Model Prediction 33%
• Tensile Test 33%
• Ultimate Strength 33%
• Corrosion Resistance 33%
• Strain Hardening Exponent 33%
• Formability 33%
• Yield Strength 33%
• Peak Strength 33%
• Aging Condition 33%
• Plastic Strain 33%
• Fracture Strain 33%
• Aerospace 33%
• Strain Hardening 33%
• Artificial Aging 33%
• Non-uniform Deformation 33%
• Tensile Deformation Behavior 33%
• Aircraft Industry 33%
• Al-Mg-Si Alloy 33%
• Natural Aging 33%
• Fracture Stress 33%
• Equivalent Strain 33%
• Strain Development 33%
• Tempering Conditions 33%
• Weldability 33%
• Eshelby 33%
• Strength Coefficient 33%
• Porous Domain 33%
• Mechanical Material Properties 33%
• Uniform Strain 33%
• Total Strain 33%
• Deformation Region 33%
• Hardness Strength 33%
• Equivalent Stress 33%
• Average Stress 33%
• Heat Treatment Process 33%

Engineering

• Al Alloy 100%
• Fracture Strength 66%
• Strain Hardening 66%
• Good Agreement 33%
• Model Prediction 33%
• Tensile Test 33%
• Ultimate Strength 33%
• Main Reason 33%
• Heat Treatment 33%
• Hardening Exponent 33%
• Deformation Behavior 33%
• Peak Strength 33%
• Plastic Strain 33%
• Fracture Strain 33%
• Equivalent Stress 33%
• Artificial Ageing 33%
• Equivalent Strain 33%
• Nonuniform Deformation 33%
• Tensile Deformation 33%
• Porosity 33%
• Mechanical Property 33%
• Corrosion Resistance 33%
• Yield Point 33%

Material Science

• Fracture Toughness 100%
• Work Hardening 100%
• Mechanical Property 50%
• Aircraft 50%
• Materials Property 50%
• Corrosion Resistance 50%
• Heat Treatment 50%
• Weldability 50%
• Silicon Alloys 50%