Ti-15V-3Cr-3Sn-3Al is a metastable beta titanium alloy designed for high-strength aerospace applications requiring excellent damage tolerance and fatigue resistance. The alloy offers tensile strengths exceeding 150 ksi with good fracture toughness, making it suitable for aircraft fuselage structure, fasteners, and landing gear components.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | 105.5 | GPa | 22°C · Sheet | ||
Young's Modulus(E) | 104.8 | GPa | 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 (16 pts) | 1/K | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (16 pts) | J/(kg·K) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (16 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 4.761 | kg/m³ | 22°C |