HAYNES®230 is a nickel-chromium-tungsten superalloy designed for high-temperature structural applications requiring oxidation resistance and creep strength to approximately 2250°F (1230°C). The 2250 Anneal condition provides stress-relieved properties suitable for aerospace applications including turbine shrouds, combustor liners, and other elevated-temperature engine components where moderate strength and excellent corrosion/oxidation resistance are required.
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2 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 | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 35.00 – 46.00 | - | 14 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | 737.7 – 813.6 | MPa | 15 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | 310.3 – 365.4 | MPa | 15 entriesClick to expand | ||
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 (10 pts) | 1/K | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (10 pts) | J/(kg·K) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (10 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 8.968 | kg/m³ | 22°C |