A-286 is an iron-nickel-cobalt superalloy strengthened by gamma-prime precipitation, used in gas turbine engines and high-temperature aerospace applications requiring strength retention to approximately 1,300°F. The F temper represents the as-fabricated condition (annealed after final fabrication without further heat treatment), providing moderate strength and good ductility suitable for demanding structural applications.
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13 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 | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | 200.6 | GPa | 22°C · Sheet/Strip/Plate | ||
Poisson's Ratio(ν) | 0.3100 | - | 22°C | ||
Shear Modulus(G) | 76.53 | GPa | 22°C · Sheet/Strip/Plate | ||
S–N Curve (Wöhler)(S–N) | — | Pa | 13 entriesClick to expand | ||
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) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 7.944 | kg/m³ | 22°C |