2618 aluminum is a copper-alloyed aerospace aluminum alloy designed for elevated-temperature service, offering high strength retention up to approximately 300°C in forged and cast applications. The T61 temper provides solution heat treatment and artificial aging, delivering optimal strength and creep resistance for gas turbine engines, compressor housings, and other high-temperature structural components.
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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 | |
|---|---|---|---|---|---|
Compressive Modulus(Ec)2 entries | 75.15 | GPa | 22°C · Die forging | ||
| ↳ | Curve (20 pts) | Pa | — | ||
Poisson's Ratio(ν) | 0.3300 | - | 22°C | ||
Shear Modulus(G) | 28.27 | GPa | 22°C · Die forging | ||
Young's Modulus(E) | 73.77 | 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 (16 pts) | 1/K | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 2.768 | kg/m³ | 22°C |