Alclad 2524-T3 is a clad aluminum-copper-magnesium alloy in solution heat-treated and cold-worked condition, providing high strength with improved fatigue resistance and corrosion protection via the pure aluminum cladding layer. Primary applications include aircraft fuselage skin and pressurized structures requiring damage tolerance and sustained stress capability at moderate temperatures.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | 72.39 | GPa | 22°C · Sheet/Plate | ||
Poisson's Ratio(ν) | 0.3500 | - | 22°C | ||
Young's Modulus(E) | 71.02 | GPa | 22°C · Sheet/Plate |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 2.768 | kg/m³ | 22°C |
Reference data from cited sources. Not verified or certified by MatWorld Inc. Verify against the source before use in design. Terms: engineering data