2025 aluminum alloy is a copper-alloyed system providing high strength suitable for aerospace fuselage and structural components, with T6 temper (solution heat-treated and artificially aged) delivering peak strength and hardness; characterized by moderate corrosion resistance and operating capability to approximately 300°F (150°C).
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | 72.39 | GPa | 22°C · Die forging | ||
Poisson's Ratio(ν) | 0.3300 | - | 22°C | ||
Shear Modulus(G) | 26.89 | GPa | 22°C · Die forging | ||
Young's Modulus(E) | 71.02 | GPa | 22°C · Die forging |
1 interactive curve for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (17 pts) | 1/K | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 2.796 | kg/m³ | 22°C |