FabDigit

Aluminum 2618 · temper

Aluminum 2618-T651

Properties of the T651 condition, compared with the other 2618 tempers.

Pick for plate and rolled bar that will be heavily machined — low residual stress means minimal distortion.

CNC machiningSheet metalPremium cost $$$

What is 2618-T651?

2618-T651 is 2618 in the T651 temper — pick for plate and rolled bar that will be heavily machined — low residual stress means minimal distortion. 2618-T651 has a yield strength of 375 MPa (54.4 ksi) and a tensile strength of 440 MPa (63.8 ksi) — stronger than 85% of aluminum grades. Elongation at break is 9% and the elastic modulus is 74.5 GPa (10.8 Msi). 2618-T651 has a density of 2.76 g/cm³ (0.0997 lb/in³), heavier than 69% of aluminum grades. It melts at 549°C (1,020 °F).

Advantages

  • High service temperature — 200°C (392 °F), better than 90% of aluminum grades
  • High strength — 375 MPa (54.4 ksi), better than 85% of aluminum grades

Limitations

  • Needs corrosion protection — 32/100, worse than 94% of aluminum grades
  • Difficult to weld — 22/100, worse than 83% of aluminum grades

2618-T651 properties

Typical room-temperature values for 2618-T651 — 9 properties are specific to this condition; the rest are grade-level values shared by every 2618 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

2618-T651 has a density of 2.76 g/cm³ (0.0997 lb/in³), heavier than 69% of aluminum grades. It melts at 549°C (1,020 °F).

Density2.76 g/cm³0.1 lb/in³
Melting Point (Solidus)549°C1,020 °F
Liquidus Temperature638°C1,180 °F

Mechanical15

2618-T651 has a yield strength of 375 MPa (54.4 ksi) and a tensile strength of 440 MPa (63.8 ksi) — stronger than 85% of aluminum grades. Elongation at break is 9% and the elastic modulus is 74.5 GPa (10.8 Msi).

Elastic (Young's) Modulus74.5 GPa10.8 Msi
Shear Modulus28 GPa4.1 Msi
Bulk Modulus76 GPa11 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)440 MPa63.8 ksi
Yield Strength (0.2% offset)375 MPa54.4 ksi
Elongation at Break9%
Reduction in Area20%
Compressive Strength380 MPa55.1 ksi
Shear Strength262 MPa38 ksi
Fatigue Strength (Endurance Limit)125 MPa18.1 ksi
Fracture Toughness (K_IC)28 MPa·√m25.5 ksi·√in
Hardness, Brinell118 HB
Hardness, Rockwell B70 HRB
Hardness, Vickers125 HV

Thermal6

2618-T651 is rated for continuous service to 200°C (392 °F). It conducts heat at 146 W/m·K (84.4 BTU/hr·ft·°F), better than 55% of aluminum grades. Thermal expansion is 22.3 µm/m·K (12.4 µin/in·°F).

Thermal Conductivity146 W/m·K84.4 BTU/hr·ft·°F
Specific Heat Capacity875 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)22.3 µm/m·K12.4 µin/in·°F
Latent Heat of Fusion389 J/g167 BTU/lb
Max Service Temperature (continuous)200°C392 °F
Min Service Temperature-196°C-321 °F

Electrical3

2618-T651 conducts electricity at 37 % IACS, better than 58% of aluminum grades.

Electrical Conductivity37 % IACS
Electrical Resistivity4.66×10⁻⁸ Ω·m1.83 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is poor (32/100), worse than 94% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.7 V
Corrosion ResistancePoor32/100
Chemical Resistance SummaryGood in dry air and neutral organics/oils; poor in chlorides, seawater and acids/alkalis due to Cu and Fe-Ni intermetallics driving galvanic pitting — protect by anodizing, cladding or paint; avoid direct contact with steel or carbon composites.

Sustainability4

Producing a kilogram of 2618-T651 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 5%.

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 Content5%

Manufacturability8

2618-T651's machinability is good (68/100, better than 68% of aluminum grades); weldability poor (22/100); formability poor (25/100).

MachinabilityGood68/100
Machinability Rating (AISI 1212 = 100 %)150%
WeldabilityPoor22/100
Formability (cold)Poor25/100
CastabilityPoor20/100
Brazeability / SolderabilityPoor15/100
PolishabilityGood55/100
Anodizing Responsefair — Cu/Fe/Ni intermetallics give grey, mottled and less protective films; hard-anodize (Type III) is used on pistons but expect dark, non-decorative colour

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

Other 2618 tempers and conditions

2618 is also supplied in 5 other conditions. The full side-by-side table is on the 2618 overview.

Working with 2618-T651

Is 2618 easy to machine?

Machines cleanly in T6/T61 with sharp PCD or polished carbide, high speed and flood coolant; hard Fe-Ni intermetallics accelerate edge wear compared with 6061.

Can 2618 be welded?

Not recommended for fusion welding (hot cracking, loss of aged strength); join by mechanical fasteners, friction welding or FSW with post-weld ageing where qualified.

Can 2618 be formed, bent or molded?

Hot forge/extrude at 400–450 °C; cold forming only in O temper — T61 material is essentially non-formable and must be machined to shape.

What surface finishes work on 2618?

Hard anodize (Type III) for piston crowns and wear faces gives a dark grey, non-uniform film; chromate/TCP conversion coat plus primer for corrosion protection, and avoid bare seawater exposure.

2618 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
Si0.1 – 0.250.18
Feforms Al9FeNi dispersoids for creep strength0.9 – 1.31.1
Cu1.9 – 2.72.3
Mg1.3 – 1.81.5
Ni0.9 – 1.21.05
Ti0.04 – 0.10.07
Zn≤ 0.1
Others (each)≤ 0.05
Others (total)≤ 0.15
Albalance

2618-T651 — frequently asked

What is 2618-T651 used for?

2618-T651 is typically used for forged engine pistons, turbocharger compressor wheels, cylinder heads, aero-engine accessory components, high-temperature structural forgings and supersonic aircraft skin panels. In short: concorde alloy; high-temp aerospace.

What is the yield strength of 2618-T651?

2618-T651 has a typical yield strength of 375 MPa (54.4 ksi) and a tensile strength of 440 MPa (63.8 ksi) — stronger than 85% of aluminum grades. Strength varies by condition: see the 6 listed tempers.

Is 2618-T651 easy to machine?

Reasonably — machinability is rated good (68/100, better than 68% of aluminum grades). Machines cleanly in T6/T61 with sharp PCD or polished carbide, high speed and flood coolant; hard Fe-Ni intermetallics accelerate edge wear compared with 6061.

Can 2618-T651 be welded?

Not readily — weldability is rated poor (22/100). Not recommended for fusion welding (hot cracking, loss of aged strength); join by mechanical fasteners, friction welding or FSW with post-weld ageing where qualified.

What surface finishes work on 2618-T651?

Hard anodize (Type III) for piston crowns and wear faces gives a dark grey, non-uniform film; chromate/TCP conversion coat plus primer for corrosion protection, and avoid bare seawater exposure.

Can 2618-T651 be formed, bent or molded?

Hot forge/extrude at 400–450 °C; cold forming only in O temper — T61 material is essentially non-formable and must be machined to shape.

What is the maximum service temperature of 2618-T651?

2618-T651 is rated for continuous use to about 200°C (392 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Can FabDigit make parts in 2618-T651?

Yes — 2618-T651 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. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys and Special-Purpose MaterialsASM International (1990)
  3. MMPDS (Metallic Materials Properties Development and Standardization)FAA/Battelle (2023)
  4. AMS 4132 — Aluminum Alloy Forgings 2618, Solution and Precipitation Heat TreatedSAE International (2019)
  5. EN 573-3 / EN 586 — Aluminium and aluminium alloys, chemical composition and forgingsCEN (2019)

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.