Inconel 706 is a nickel-iron-chromium precipitation-hardening superalloy with columbium and titanium additions, designed for high-strength applications in aerospace gas turbines and fasteners operating to approximately 1300°F (704°C). The heat-treated condition provides excellent tensile strength and bearing properties with good ductility, making it suitable for critical rotating and structural components requiring sustained elevated-temperature performance with reliable stress-rupture resistance.
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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 | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru) | 1.765 – 2.372 | GPa | 14 entriesClick to expand | ||
Bearing Yield Strength(Fbry) | 1.248 – 1.675 | GPa | 14 entriesClick to expand | ||
Compressive Modulus(Ec) | Curve (15 pts) | Pa | — | ||
Compressive Yield Strength(Fcy) | 0.9377 – 1.048 | GPa | 7 entriesClick to expand | ||
Elongation at Break(εf) | 12.00 | - | 7 entriesClick to expand | ||
Poisson's Ratio(ν) | 0.3800 | - | 22°C | ||
Reduction of Area(RA)4 entries | 15.00 | - | 22°C · Bar/Forging · Heat treated per indicated specification · AMS 5701 · L · t=<2.500 in | ||
| ↳ | 15.00 | - | 22°C · Bar/Forging · Heat treated per indicated specification · AMS 5701 · L · t=2.500-4.000 in | ||
| ↳ | 15.00 | - | 22°C · Bar/Forging · Heat treated per indicated specification · AMS 5702 OR AMS 5703 · L · t=<2.500 in | ||
| ↳ | 15.00 | - | 22°C · Bar/Forging · Heat treated per indicated specification · AMS 5702 OR AMS 5703 · L · t=2.500-4.000 in | ||
Shear Modulus(G) | 75.84 | GPa | 22°C · Sheet/Strip/Plate | ||
Ultimate Shear Strength(Fsu) | 710.2 – 751.5 | MPa | 7 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | 1.138 – 1.207 | GPa | 7 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | 896.3 – 999.7 | MPa | 7 entriesClick to expand | ||
Young's Modulus(E) | 209.6 | 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 (25 pts) | 1/K | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (24 pts) | J/(kg·K) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (25 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 8.083 | kg/m³ | 22°C |