A-286 is an austenitic iron-nickel-cobalt superalloy strengthened by precipitation hardening, designed for jet engine components and high-temperature structural applications requiring sustained service to 1300°F (704°C). The alloy combines excellent creep resistance, fatigue strength, and corrosion resistance with moderate density, making it suitable for turbine discs, fasteners, and casings in aerospace propulsion systems.
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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) | 200.6 | GPa | 22°C · Sheet/Strip/Plate | ||
Poisson's Ratio(ν) | 0.3100 | - | 22°C | ||
Shear Modulus(G)2 entries | 76.53 | GPa | 22°C · Sheet/Strip/Plate | ||
| ↳ | Curve (17 pts) | Pa | — | ||
Young's Modulus(E) | 200.6 | GPa | 22°C · Sheet/Strip/Plate |
3 interactive curves 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 | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (17 pts) | J/(kg·K) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (21 pts) | W/(m·K) | — |
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 | |
|---|---|---|---|---|---|
Density(ρ)2 entries | 7.944 | kg/m³ | 22°C | ||
| ↳ | Curve (18 pts) | kg/m³ | — |