2090 is an Al-Cu-Li alloy designed for aerospace applications requiring high specific strength and low density. The T83 temper (solution heat-treated, stress-relieved, and artificially aged) provides intermediate strength with improved fracture toughness compared to higher-strength tempers, making it suitable for damage-tolerant structural applications in aircraft fuselage and wing components.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | 11,800 | ksi | 22°C · Sheet | ||
Poisson's Ratio(ν) | 0.3400 | - | 22°C | ||
Shear Modulus(G) | 4,300 | ksi | 22°C · Sheet | ||
Young's Modulus(E) | 11,500 | ksi | 22°C · Sheet |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.09400 | lb/in³ | 22°C |