2014 Aluminum T652
Verifiedmetal2014 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.
aerospacestructural
Compliance & Regulations
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| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru) | — | Pa | 17 entriesClick to expand | ||
Bearing Yield Strength(Fbry) | — | Pa | 24 entriesClick to expand | ||
Compressive Modulus(Ec) | — | Pa | 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) | — | Pa | 35 entriesClick to expand | ||
Elongation at Break(εf) | — | - | 30 entriesClick to expand | ||
Poisson's Ratio(ν) | — | - | 22°C | — | |
Shear Modulus(G) | — | Pa | 22°C · Bar/Extrusion/Rod | — | |
Ultimate Shear Strength(Fsu) | — | Pa | 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) | — | Pa | 32 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | — | Pa | 33 entriesClick to expand | ||
Young's Modulus(E) | — | Pa | 22°C · Bar/Extrusion/Rod | — | |
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| 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) | — | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | kg/m³ | 22°C | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
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Quality & Standards
RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.