Ti-6Al-2Sn-4Zr-2Mo is a near-alpha titanium alloy combining aluminum, tin, zirconium, and molybdenum additions for elevated temperature strength and creep resistance; used primarily in compressor and fastener applications in military and commercial jet engines operating up to ~600°C with good fatigue and stress-rupture performance.
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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 | 18,000 | ksi | 22°C · Sheet | ||
| ↳ | Curve (17 pts) | ksi | — | ||
Poisson's Ratio(ν) | 0.3200 | - | 22°C | ||
Shear Modulus(G) | 6,200 | ksi | 22°C · Sheet | ||
Young's Modulus(E) | 16,500 | ksi | 22°C · Sheet |
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 (15 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 |