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) | 16,400 | ksi | 22°C · Sheet/Strip/Plate | ||
Poisson's Ratio(ν) | 0.3100 | - | 22°C | ||
Shear Modulus(G)2 entries | 6,000 | ksi | 22°C · Bar/Extrusion | ||
| ↳ | 6,200 | ksi | 22°C · Sheet/Strip/Plate | ||
S–N Curve (Wöhler)(S–N) | — | ksi | 9 entriesClick to expand | ||
Young's Modulus(E) | 16,000 | 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 (17 pts) | µin/in·°F | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (17 pts) | BTU/(lb·°F) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (17 pts) | BTU/(hr·ft·°F) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.1640 | lb/in³ | 22°C |