2014 aluminum is a copper-alloyed high-strength aluminum used primarily in aircraft structural forgings and landing gear components, offering tensile strengths in the 60–70 ksi range with good fatigue resistance. The T652 temper (solution heat-treated, stress-relieved, and artificially aged) provides dimensional stability and controlled strength suitable for precision forged parts requiring consistent mechanical properties and minimal distortion.
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11 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) | 572.3 – 875.6 | MPa | 17 entriesClick to expand | ||
Bearing Yield Strength(Fbry) | 489.5 – 648.1 | MPa | 24 entriesClick to expand | ||
Compressive Modulus(Ec) | 75.84 | GPa | 22°C · Bar/Extrusion/Rod | ||
Compressive Tangent Modulus vs Stress(Etn(σ))3 entries | Curve (7 pts) | Pa | 21°C · L | ||
| ↳ | Curve (7 pts) | Pa | 21°C · LT | ||
| ↳ | Curve (8 pts) | Pa | 21°C · ST | ||
Compressive Yield Strength(Fcy) | 268.9 – 427.5 | MPa | 35 entriesClick to expand | ||
Elongation at Break(εf) | 1.000 – 8.000 | - | 30 entriesClick to expand | ||
Poisson's Ratio(ν) | 0.3300 | - | 22°C | ||
Shear Modulus(G) | 28.27 | GPa | 22°C · Bar/Extrusion/Rod | ||
Ultimate Shear Strength(Fsu) | 248.2 – 648.1 | MPa | 12 entriesClick to expand | ||
Stress–Strain Curve(σ–ε)2 entries | Curve (11 pts) | Pa | 21°C · L | ||
| ↳ | Curve (10 pts) | Pa | 21°C · LT | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain)) | — | Pa | 6 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | 393.0 – 461.9 | MPa | 32 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | 330.9 – 406.8 | MPa | 33 entriesClick to expand | ||
Young's Modulus(E) | 74.46 | GPa | 22°C · Bar/Extrusion/Rod | ||
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) | 1/K | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (12 pts) | J/(kg·K) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (15 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 2.796 | kg/m³ | 22°C |