HAYNES 230 is a nickel-chromium-tungsten superalloy designed for high-temperature structural applications requiring excellent creep resistance and oxidation resistance up to 1150°C (2100°F). The 2200 Anneal condition provides stress relief and recrystallization, delivering optimal combination of tensile strength and ductility for gas turbine engines, aerospace fasteners, and chemical processing equipment operating in oxidizing environments at elevated temperatures.
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26 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)4 entries | 40.00 | - | 22°C · Plate · 2200 Anneal · AMS 5878 · LT · t=≤0.400 in | ||
| ↳ | 43.00 | - | 22°C · Plate · 2200 Anneal · AMS 5878 · LT · t=≤0.400 in | ||
| ↳ | 39.00 | - | 22°C · Plate · 2200 Anneal · AMS 5878 · LT · t=0.401 to 1.500 in | ||
| ↳ | 42.00 | - | 22°C · Plate · 2200 Anneal · AMS 5878 · LT · t=0.401 to 1.500 in | ||
Stress–Strain Curve(σ–ε) | — | ksi | 15 entriesClick to expand | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain)) | — | ksi | 9 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | 111 – 120 | ksi | 5 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | 48.00 – 55.00 | ksi | 5 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 (19 pts) | µin/in·°F | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (20 pts) | BTU/(lb·°F) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (19 pts) | BTU/(hr·ft·°F) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.3240 | lb/in³ | 22°C |