Inconel 706 is a nickel-iron-based superalloy strengthened by gamma-double-prime precipitation, designed for high-temperature structural applications requiring moderate strength retention to approximately 1300°F (704°C). Primary applications include aircraft engine casings, fasteners, and gas turbine components in aerospace and power generation industries, with excellent creep resistance and thermal fatigue resistance in the intermediate temperature range.
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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)2 entries | Curve (15 pts) | ksi | — | ||
| ↳ | 30,400 | ksi | 22°C · Sheet/Strip/Plate | ||
Poisson's Ratio(ν) | 0.3800 | - | 22°C | ||
Shear Modulus(G) | 11,000 | ksi | 22°C · Sheet/Strip/Plate | ||
Young's Modulus(E) | 30,400 | ksi | 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) | µin/in·°F | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (24 pts) | BTU/(lb·°F) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (25 pts) | BTU/(hr·ft·°F) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.2920 | lb/in³ | 22°C |