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Aluminum 7040 · temper · default condition

Aluminum 7040-T7451

Properties of the T7451 condition, compared with the other 7040 tempers.

The standard supply condition for 7040 aerospace thick plate: near-T6 strength with good through-thickness toughness, SCC resistance and low residual stress for deep machining.

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What is 7040-T7451?

7040-T7451 is 7040 in the T7451 temper — the standard supply condition for 7040 aerospace thick plate: near-T6 strength with good through-thickness toughness, SCC resistance and low residual stress for deep machining. 7040-T7451 has a yield strength of 450 MPa (65.3 ksi) and a tensile strength of 505 MPa (73.2 ksi) — stronger than 91% of aluminum grades. Elongation at break is 10% and the elastic modulus is 71 GPa (10.3 Msi). 7040-T7451 has a density of 2.82 g/cm³ (0.102 lb/in³), heavier than 89% of aluminum grades. It melts at 480°C (896 °F).

Advantages

  • Tough — resists crack growth — 38 MPa·√m (34.6 ksi·√in), better than 96% of aluminum grades
  • High strength — 450 MPa (65.3 ksi), better than 91% of aluminum grades
  • High electrical conductivity — 40.5 % IACS, better than 77% of aluminum grades

Limitations

  • Difficult to weld — 20/100, worse than 89% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades

7040-T7451 properties

Typical room-temperature values for 7040-T7451 — 16 properties are specific to this condition; the rest are grade-level values shared by every 7040 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

7040-T7451 has a density of 2.82 g/cm³ (0.102 lb/in³), heavier than 89% of aluminum grades. It melts at 480°C (896 °F).

Density2.82 g/cm³0.1 lb/in³
Melting Point (Solidus)480°C896 °F
Liquidus Temperature635°C1,175 °F

Mechanical12

7040-T7451 has a yield strength of 450 MPa (65.3 ksi) and a tensile strength of 505 MPa (73.2 ksi) — stronger than 91% of aluminum grades. Elongation at break is 10% and the elastic modulus is 71 GPa (10.3 Msi).

Elastic (Young's) Modulus71 GPa10.3 Msi
Shear Modulus26.9 GPa3.9 Msi
Bulk Modulus75 GPa10.9 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)505 MPa73.2 ksi
Yield Strength (0.2% offset)450 MPa65.3 ksi
Elongation at Break10%
Compressive Strength465 MPa67.4 ksi
Shear Strength300 MPa43.5 ksi
Fatigue Strength (Endurance Limit)160 MPa23.2 ksi
Fracture Toughness (K_IC)38 MPa·√m34.6 ksi·√in
Hardness, Brinell145 HB

Thermal6

7040-T7451 is rated for continuous service to 120°C (248 °F). It conducts heat at 154 W/m·K (89 BTU/hr·ft·°F), better than 68% of aluminum grades. Thermal expansion is 23.4 µm/m·K (13 µin/in·°F).

Thermal Conductivity154 W/m·K89 BTU/hr·ft·°F
Specific Heat Capacity860 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)23.4 µm/m·K13 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)120°C248 °F
Min Service Temperature-196°C-321 °F

Electrical3

7040-T7451 conducts electricity at 40.5 % IACS, better than 77% of aluminum grades.

Electrical Conductivity40.5 % IACS
Electrical Resistivity4.26×10⁻⁸ Ω·m1.68 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (45/100), worse than 62% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.84 V
Corrosion ResistanceFair45/100
Chemical Resistance SummaryGood in neutral atmospheres and fresh water when anodized or painted; attacked by strong alkalis and mineral acids, susceptible to pitting in chlorides and to galvanic attack when coupled to steel or carbon fibre.

Sustainability4

Producing a kilogram of 7040-T7451 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% 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 Water1,200 L/kg144 gal/lb
Typical Recycled Content10%

Manufacturability7

7040-T7451's machinability is very good (70/100, better than 72% of aluminum grades); weldability poor (20/100); formability poor (25/100).

MachinabilityVery good70/100
Machinability Rating (AISI 1212 = 100 %)90%
WeldabilityPoor20/100
Formability (cold)Poor25/100
Brazeability / SolderabilityNot recommended10/100
PolishabilityGood60/100
Anodizing Responsegood — clear sulfuric and hard (Type III) anodize used routinely on aerospace parts; coating slightly grey/yellow-tinted, chromic/TSA anodize plus primer typical for corrosion protection

Common Calculations5

Specific Strength (UTS / density)calculated179 kN·m/kg
Specific Stiffness (E / density)calculated25.2 MN·m/kg
Modulus of Resiliencecalculated1,426 kJ/m³
Thermal Diffusivitycalculated63.5 mm²/s
Thermal Shock Resistance Indexcalculated47

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Other 7040 tempers and conditions

7040 is also supplied in 6 other conditions. The full side-by-side table is on the 7040 overview.

Working with 7040-T7451

Is 7040 easy to machine?

Excellent chip formation in T74/T76 tempers — high-speed carbide, polished flutes, 3–8 % emulsion coolant; stretch-relieved plate keeps distortion low on deep pocket milling.

Can 7040 be welded?

Not suitable for fusion welding (hot cracking, SCC in HAZ); join by riveting, bolting or friction-stir welding with qualified procedures.

Can 7040 be formed, bent or molded?

Form in O or freshly quenched W condition only; aged plate has limited bend ductility and needs generous radii and stress-relief planning.

What surface finishes work on 7040?

Chromic/tartaric-sulfuric anodize plus primer or hard anodize for wear; alkaline etch and conversion coatings work well, avoid strong caustics and dissimilar-metal contact without insulation.

7040 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
Si≤ 0.10.05
Fe≤ 0.130.07
Cu1.5 – 2.31.9
Mn≤ 0.040.01
Mg1.7 – 2.42
Cr≤ 0.040.01
Zn5.7 – 6.76.2
Zrgrain-structure control (Al3Zr dispersoids)0.05 – 0.120.09
Ti≤ 0.060.02
Others (each)each≤ 0.05
Others (total)total≤ 0.15
Albalance

7040-T7451 — frequently asked

What is 7040-T7451 used for?

7040-T7451 is typically used for wing spars, bulkheads and heavy frames. In short: thick aerospace plate.

What is the yield strength of 7040-T7451?

7040-T7451 has a typical yield strength of 450 MPa (65.3 ksi) and a tensile strength of 505 MPa (73.2 ksi) — stronger than 91% of aluminum grades. Strength varies by condition: see the 7 listed tempers.

Is 7040-T7451 easy to machine?

Yes — machinability is rated very good (70/100, better than 72% of aluminum grades). Excellent chip formation in T74/T76 tempers — high-speed carbide, polished flutes, 3–8 % emulsion coolant; stretch-relieved plate keeps distortion low on deep pocket milling.

Can 7040-T7451 be welded?

Not readily — weldability is rated poor (20/100). Not suitable for fusion welding (hot cracking, SCC in HAZ); join by riveting, bolting or friction-stir welding with qualified procedures.

What surface finishes work on 7040-T7451?

Chromic/tartaric-sulfuric anodize plus primer or hard anodize for wear; alkaline etch and conversion coatings work well, avoid strong caustics and dissimilar-metal contact without insulation.

Can 7040-T7451 be formed, bent or molded?

Form in O or freshly quenched W condition only; aged plate has limited bend ductility and needs generous radii and stress-relief planning.

What is the maximum service temperature of 7040-T7451?

7040-T7451 is rated for continuous use to about 120°C (248 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 7040-T7451 and 7040-O?

T7451 is the default condition — the standard supply condition for 7040 aerospace thick plate: near-T6 strength with good through-thickness toughness, SCC resistance and low residual stress for deep machining. O: pick for maximum formability or before re-solution heat treating; strength is far below service level. Yield strength is 450 MPa in T7451 versus 115 MPa in O.

Can FabDigit make parts in 7040-T7451?

Yes — 7040-T7451 is available for CNC machining and sheet metal with instant online pricing. 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. Aerospace thick plate alloys 7040/7050 (T7451, T7651) plate dataConstellium (formerly Pechiney/Alcan) (2020)
  3. ASM Handbook Vol. 2: Properties and Selection — Nonferrous AlloysASM International (1990)
  4. MMPDS-17 Metallic Materials Properties Development and StandardizationBattelle/FAA (2022)
  5. EN 485-2 Aluminium and aluminium alloys — Sheet, strip and plate: mechanical propertiesCEN (2016)

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.