Ti-6Al-6V-2Sn is a near-alpha titanium alloy containing 6% aluminum, 6% vanadium, and 2% tin, designed for elevated-temperature aerospace applications requiring moderate strength and creep resistance up to approximately 600°C. The alloy offers good fatigue performance and weldability with moderate density, making it suitable for jet engine components, airframes, and other high-temperature structural applications.
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9 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 | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | 113.1 | GPa | 22°C · Sheet/Strip/Plate | ||
Poisson's Ratio(ν) | 0.3100 | - | 22°C | ||
Shear Modulus(G)2 entries | 41.37 | GPa | 22°C · Bar/Extrusion | ||
| ↳ | 42.75 | GPa | 22°C · Sheet/Strip/Plate | ||
S–N Curve (Wöhler)(S–N) | — | Pa | 9 entriesClick to expand | ||
Young's Modulus(E) | 110.3 | 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 (17 pts) | 1/K | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (17 pts) | J/(kg·K) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (17 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 4.540 | kg/m³ | 22°C |