Inconel X-750 is a nickel-based superalloy strengthened by gamma-prime precipitation, designed for high-temperature aerospace applications requiring sustained strength to approximately 1300°F (704°C). The alloy exhibits excellent creep resistance, fatigue strength, and corrosion resistance in jet engine components, gas turbine blades, and fasteners, with the Equalized and Aged temper providing optimal strength development through controlled solution treatment and precipitation hardening.
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11 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 | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru) | Curve (9 pts) | ksi | — | ||
Bearing Yield Strength(Fbry) | Curve (11 pts) | ksi | — | ||
Compressive Modulus(Ec)2 entries | 30,600 | ksi | 22°C · Strip | ||
| ↳ | Curve (9 pts) | ksi | L | ||
Compressive Yield Strength(Fcy) | Curve (11 pts) | ksi | L | ||
Poisson's Ratio(ν) | 0.3000 | - | 22°C | ||
Shear Modulus(G)2 entries | 11,800 | ksi | 22°C · Strip | ||
| ↳ | Curve (8 pts) | ksi | — | ||
Ultimate Shear Strength(Fsu) | Curve (9 pts) | ksi | — | ||
Ultimate Tensile Strength(σUTS)2 entries | Curve (20 pts) | ksi | L | ||
| ↳ | Curve (16 pts) | ksi | L | ||
Yield Strength (0.2% offset)(σy)2 entries | Curve (14 pts) | ksi | L | ||
| ↳ | Curve (14 pts) | ksi | L | ||
Young's Modulus(E)2 entries | 30,600 | ksi | 22°C · Strip | ||
| ↳ | Curve (9 pts) | ksi | L |
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 | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (14 pts) | µin/in·°F | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (11 pts) | BTU/(lb·°F) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.2980 | lb/in³ | 22°C |