Ti-6Al-2Sn-4Zr-2Mo is a near-alpha titanium alloy strengthened by aluminum and molybdenum additions, designed for elevated-temperature applications requiring moderate strength and creep resistance up to approximately 600°C in aerospace gas turbine engines and compressor casings. Duplex annealed condition provides optimal combination of strength and fracture toughness through controlled recrystallization and alpha-phase stabilization, with yield strengths typically 800–1000 MPa and good ductility (8–15% elongation) across bar, forging, and sheet product forms.
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14 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) | 1.344 – 2.034 | GPa | 16 entriesClick to expand | ||
Bearing Yield Strength(Fbry) | 1.179 – 1.496 | GPa | 16 entriesClick to expand | ||
Compressive Modulus(Ec) | Curve (6 pts) | Pa | L | ||
Compressive Yield Strength(Fcy) | 910.1 – 979.1 | MPa | 17 entriesClick to expand | ||
Elongation at Break(εf) | 8.000 – 10.00 | - | 12 entriesClick to expand | ||
Poisson's Ratio(ν) | 0.3200 | - | 22°C | ||
Reduction of Area(RA) | 25.00 | - | 6 entriesClick to expand | ||
Shear Modulus(G) | 42.75 | GPa | 22°C · Sheet | ||
Stress–Strain Curve(σ–ε)3 entries | Curve (15 pts) | Pa | 21°C · L | ||
| ↳ | Curve (16 pts) | Pa | 316°C · L | ||
| ↳ | Curve (19 pts) | Pa | 482°C · L | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain)) | — | Pa | 6 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | 896.3 – 992.8 | MPa | 24 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | 827.4 – 937.7 | MPa | 24 entriesClick to expand | ||
Young's Modulus(E) | Curve (6 pts) | Pa | L | ||
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 (6 pts) | 1/K | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (5 pts) | J/(kg·K) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (5 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 4.540 | kg/m³ | 22°C |