Ti-8Al-1Mo-1V is a near-alpha titanium alloy with moderate strength and superior creep resistance, designed for elevated-temperature aerospace applications requiring service to approximately 1200°F. The alloy combines aluminum for strength and low density with molybdenum and vanadium for creep and heat-resistance properties, with Duplex Annealed condition providing optimized toughness and Solution Treated condition delivering maximum strength.
Compliance & Regulations
18 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)2 entries | 124.1 | GPa | 22°C · Bar | ||
| ↳ | Curve (10 pts) | Pa | L | ||
Compressive Tangent Modulus vs Stress(Etn(σ))4 entries | Curve (11 pts) | Pa | 21°C · L | ||
| ↳ | Curve (11 pts) | Pa | 21°C · LT | ||
| ↳ | Curve (11 pts) | Pa | 288°C · L | ||
| ↳ | Curve (11 pts) | Pa | 288°C · LT | ||
Poisson's Ratio(ν) | 0.3200 | - | 22°C | ||
Shear Modulus(G) | 46.19 | GPa | 22°C · Bar | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain)) | — | Pa | 10 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | Curve (14 pts) | Pa | L | ||
Yield Strength (0.2% offset)(σy) | Curve (17 pts) | Pa | L | ||
Young's Modulus(E)2 entries | 120.7 | GPa | 22°C · Bar | ||
| ↳ | Curve (10 pts) | Pa | 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 (5 pts) | 1/K | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (5 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 4.373 | kg/m³ | 22°C |