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Aluminum 2214-T451

Temper

AA 2214 · EN AW-2214, AW 2214

T451 = t4, stress relieved by stretching

Plate/bar version of T4 with low residual stress — for parts that will be machined then artificially aged.

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Values for the T451 condition

Other 2214 tempers and conditions

2214 is listed in 7 conditions; see the grade overview at 2214.

Compare all 7 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest condition for deep forming, heavy bending or straightening before solution treatment.951851845 HB50 % IACS
Solution heat treated and naturally aged
Choose when moderate strength with better ductility and forming/riveting capability is needed before final aging.29042518105 HB34 % IACS
T451This page
T4, stress relieved by stretching
Plate/bar version of T4 with low residual stress — for parts that will be machined then artificially aged.29042516105 HB34 % IACS
T6, stress relieved by compression
Hand/die forging condition where stretching is impractical; low residual stress for heavily machined forgings.4004608130 HB40 % IACS
Solution heat treated and artificially aged
Peak-strength condition for forgings, extrusions and machined fittings where residual stress is not critical.41448313135 HB40 % IACS
T6, stress relieved by stretching
Standard aerospace plate/bar condition — full T6 strength with minimal residual stress so machined parts stay flat.4154709135 HB40 % IACS
T6, stress relieved by stretching, minor straightening
Extruded bar, rod and profile equivalent of T651 for long machined structural members.4154708135 HB40 % IACS

What is 2214-T451?

2214-T451 is 2214 in the T451 temper — plate/bar version of T4 with low residual stress — for parts that will be machined then artificially aged. 2214-T451 has a yield strength of 290 MPa (42.1 ksi) and a tensile strength of 425 MPa (61.6 ksi) — stronger than 74% of aluminum grades. Elongation at break is 16% and the elastic modulus is 72.5 GPa (10.5 Msi). 2214-T451 has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 507°C (945 °F).

Advantages

  • Tough — resists crack growth — 34 MPa·√m (30.9 ksi·√in), better than 90% of aluminum grades
  • Ductile — tolerates forming and impact — 16%, better than 84% of aluminum grades

Limitations

  • Needs corrosion protection — 28/100, worse than 99% of aluminum grades
  • Limited service temperature — 100°C (212 °F), worse than 91% of aluminum grades
  • Difficult to weld — 25/100, worse than 76% of aluminum grades

2214-T451 properties

Typical room-temperature values for 2214-T451; 22 are specific to this condition. Other listed values are 2214 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

2214-T451 has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 507°C (945 °F).

Density2.8 g/cm³0.1 lb/in³
Melting Point (Solidus)507°C945 °F
Liquidus Temperature638°C1,180 °F

Mechanical15

2214-T451 has a yield strength of 290 MPa (42.1 ksi) and a tensile strength of 425 MPa (61.6 ksi) — stronger than 74% of aluminum grades. Elongation at break is 16% and the elastic modulus is 72.5 GPa (10.5 Msi).

Elastic (Young's) Modulus72.5 GPa10.5 Msi
Shear Modulus27.5 GPa4 Msi
Bulk Modulus75 GPa10.9 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)425 MPa61.6 ksi
Yield Strength (0.2% offset)290 MPa42.1 ksi
Elongation at Break16%
Reduction in Area30%
Compressive Strength295 MPa42.8 ksi
Shear Strength260 MPa37.7 ksi
Fatigue Strength (Endurance Limit)140 MPa20.3 ksi
Fracture Toughness (K_IC)34 MPa·√m30.9 ksi·√in
Hardness, Brinell105 HB
Hardness, Rockwell B62 HRB
Hardness, Vickers112 HV

Thermal6

2214-T451 is rated for continuous service to 100°C (212 °F). It conducts heat at 134 W/m·K (77.4 BTU/hr·ft·°F), worse than 60% of aluminum grades. Thermal expansion is 22.5 µm/m·K (12.5 µin/in·°F).

Thermal Conductivity134 W/m·K77.4 BTU/hr·ft·°F
Specific Heat Capacity864 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)22.5 µm/m·K12.5 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)100°C212 °F
Min Service Temperature-196°C-321 °F

Electrical3

2214-T451 conducts electricity at 34 % IACS, worse than 52% of aluminum grades.

Electrical Conductivity34 % IACS
Electrical Resistivity5.07×10⁻⁸ Ω·m2 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is poor (28/100), worse than 99% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.78 V
Corrosion ResistancePoor28/100
Chemical Resistance SummaryGood in dry air and neutral organics; poor in chloride-bearing water, seawater and acids/alkalis — Cu-rich phases drive pitting and intergranular attack; requires alclad, anodize or primer, and isolation from steel/CFRP.

Sustainability4

Producing a kilogram of 2214-T451 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 76% of aluminum grades. Typical recycled content is 10%.

Embodied Energy (primary production)205 MJ/kg88,134 BTU/lb
Embodied Carbon (primary production)12.5 kg CO₂/kg
Embodied Water1,150 L/kg138 gal/lb
Typical Recycled Content10%

Manufacturability8

2214-T451's machinability is good (68/100, better than 67% of aluminum grades); weldability poor (25/100); formability good (55/100).

MachinabilityGood68/100
Machinability Rating (AISI 1212 = 100 %)130%
WeldabilityPoor25/100
Formability (cold)Good55/100
CastabilityPoor30/100
Brazeability / SolderabilityPoor15/100
PolishabilityGood55/100
Anodizing Responsefair — high Cu gives dark, patchy and less protective sulfuric films; hard-coat is possible but thinner and more brittle; chromic acid anodize or alclad preferred for aerospace parts.

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with 2214-T451

Is 2214 easy to machine?

Excellent chip control in T6/T651 — use polished-flute carbide, high speeds with flood or MQL; avoid re-introducing residual stress in thin machined webs.

Can 2214 be welded?

Not recommended for fusion welding (hot cracking with Cu-rich melt); join by rivets, bolts, adhesive or friction-stir; if arc welded, use 4145/4043 filler and re-heat-treat.

Can 2214 be formed, bent or molded?

Form in O or fresh T4 (within a few hours of quench, or hold sub-zero); T6/T651 has limited bend ductility and springback is high.

What surface finishes work on 2214?

Chromic-acid anodize, chemical conversion coat or alclad plus epoxy primer for corrosion protection; sulfuric anodize gives dark, non-uniform color due to CuAl2 phases.

2214 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Si0.5 – 1.20.8
FeLower Fe than 2014 — the defining difference of 2214≤ 0.30.15
Cu3.9 – 54.4
Mn0.4 – 1.20.8
Mg0.2 – 0.80.5
Cr≤ 0.1—
Zn≤ 0.25—
Ti≤ 0.15—
Zr+Ticombined limit where applicable≤ 0.2—
Others (each)≤ 0.05—
Others (total)≤ 0.15—
Albalance—

2214-T451 — frequently asked

What is 2214-T451 used for?

2214-T451 is typically used for aerospace structural forgings, wheel hubs, machined airframe fittings, thick-plate machined components, high-stress tooling and dies and extruded structural sections. In short: high-strength forging; 2014 variant.

What is the yield strength of 2214-T451?

2214-T451 has a typical yield strength of 290 MPa (42.1 ksi) and a tensile strength of 425 MPa (61.6 ksi) — stronger than 74% of aluminum grades. Strength varies by condition: see the 7 listed tempers.

Is 2214-T451 easy to machine?

Reasonably — machinability is rated good (68/100, better than 67% of aluminum grades). Excellent chip control in T6/T651 — use polished-flute carbide, high speeds with flood or MQL; avoid re-introducing residual stress in thin machined webs.

Can 2214-T451 be welded?

Not readily — weldability is rated poor (25/100). Not recommended for fusion welding (hot cracking with Cu-rich melt); join by rivets, bolts, adhesive or friction-stir; if arc welded, use 4145/4043 filler and re-heat-treat.

What surface finishes work on 2214-T451?

Chromic-acid anodize, chemical conversion coat or alclad plus epoxy primer for corrosion protection; sulfuric anodize gives dark, non-uniform color due to CuAl2 phases.

Can 2214-T451 be formed, bent or molded?

Form in O or fresh T4 (within a few hours of quench, or hold sub-zero); T6/T651 has limited bend ductility and springback is high.

What is the maximum service temperature of 2214-T451?

2214-T451 is rated for continuous use to about 100°C (212 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Can FabDigit make parts in 2214-T451?

Yes — 2214-T451 is available for CNC machining and sheet metal; every part is priced by an engineer rather than instantly. Upload a STEP file to get a price and a DFM check.

Sources

  1. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum (Teal Sheets) — The Aluminum Association (2018)
  2. EN 573-3 Aluminium and aluminium alloys — Chemical composition — CEN (2019)
  3. ASTM B209 / B211 / B247 (aluminum plate, bar, forgings) — ASTM International (2021)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  5. MMPDS-17 Metallic Materials Properties Development and Standardization — Battelle/FAA (2022)
  6. ASM Handbook Vol. 13B — Corrosion: Materials — ASM International (2005)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.