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Aluminum 7178 · temper

Aluminum 7178-T651

Properties of the T651 condition, compared with the other 7178 tempers.

Standard plate temper — same peak strength as T6 but low residual stress for stable machining of thick parts.

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What is 7178-T651?

7178-T651 is 7178 in the T651 temper — standard plate temper — same peak strength as T6 but low residual stress for stable machining of thick parts. 7178-T651 has a yield strength of 530 MPa (76.9 ksi) and a tensile strength of 600 MPa (87 ksi) — stronger than 97% of aluminum grades. Elongation at break is 9% and the elastic modulus is 71.7 GPa (10.4 Msi). 7178-T651 has a density of 2.83 g/cm³ (0.102 lb/in³), heavier than 91% of aluminum grades. It melts at 477°C (891 °F).

Advantages

  • High strength — 530 MPa (76.9 ksi), better than 97% of aluminum grades
  • Easy to machine — 75/100, better than 86% of aluminum grades

Limitations

  • Difficult to weld — 12/100, worse than 98% of aluminum grades
  • Needs corrosion protection — 32/100, worse than 94% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades

7178-T651 properties

Typical room-temperature values for 7178-T651 — 11 properties are specific to this condition; the rest are grade-level values shared by every 7178 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

7178-T651 has a density of 2.83 g/cm³ (0.102 lb/in³), heavier than 91% of aluminum grades. It melts at 477°C (891 °F).

Density2.83 g/cm³0.1 lb/in³
Melting Point (Solidus)477°C891 °F
Liquidus Temperature629°C1,164 °F

Mechanical13

7178-T651 has a yield strength of 530 MPa (76.9 ksi) and a tensile strength of 600 MPa (87 ksi) — stronger than 97% of aluminum grades. Elongation at break is 9% and the elastic modulus is 71.7 GPa (10.4 Msi).

Elastic (Young's) Modulus71.7 GPa10.4 Msi
Shear Modulus26.9 GPa3.9 Msi
Bulk Modulus70 GPa10.2 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)600 MPa87 ksi
Yield Strength (0.2% offset)530 MPa76.9 ksi
Elongation at Break9%
Compressive Strength550 MPa79.8 ksi
Shear Strength330 MPa47.9 ksi
Fatigue Strength (Endurance Limit)150 MPa21.8 ksi
Fracture Toughness (K_IC)22 MPa·√m20 ksi·√in
Hardness, Brinell160 HB
Hardness, Vickers175 HV

Thermal6

7178-T651 is rated for continuous service to 120°C (248 °F). It conducts heat at 125 W/m·K (72.2 BTU/hr·ft·°F), worse than 72% of aluminum grades. Thermal expansion is 23.4 µm/m·K (13 µin/in·°F).

Thermal Conductivity125 W/m·K72.2 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

7178-T651 conducts electricity at 31 % IACS, worse than 68% of aluminum grades.

Electrical Conductivity31 % IACS
Electrical Resistivity5.56×10⁻⁸ Ω·m2.19 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

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

Galvanic Potential (seawater, vs SCE)-0.83 V
Corrosion ResistancePoor32/100
Chemical Resistance SummaryGood in neutral atmospheres and dry environments; poor in chloride-bearing or marine service — sustained short-transverse tensile stress in T6 risks stress-corrosion cracking; attacked by strong acids and alkalis; clad or anodize plus prime for aerospace use.

Sustainability4

Producing a kilogram of 7178-T651 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 15%.

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 Content15%

Manufacturability7

7178-T651's machinability is very good (75/100, better than 86% of aluminum grades); weldability not recommended (12/100); formability poor (20/100).

MachinabilityVery good75/100
Machinability Rating (AISI 1212 = 100 %)70%
WeldabilityNot recommended12/100
Formability (cold)Poor20/100
Brazeability / SolderabilityNot recommended10/100
PolishabilityGood60/100
Anodizing Responsegood — clear/sulfuric and hard-coat anodizing work well; high Zn/Cu gives a slightly grey-bronze tint and lower clarity than 6061; chromic/sulfuric anodize widely used on aerospace parts

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

Other 7178 tempers and conditions

7178 is also supplied in 7 other conditions. The full side-by-side table is on the 7178 overview.

Working with 7178-T651

Is 7178 easy to machine?

Machines well in T6/T76 with sharp carbide, high speed and flood coolant; relieve stresses (T651/T7651) before heavy pocket milling to control distortion.

Can 7178 be welded?

Not fusion weldable — hot cracking and severe HAZ SCC; join by riveting, bolting or adhesive bonding (friction-stir only with qualified procedures).

Can 7178 be formed, bent or molded?

Form in O or freshly quenched W temper and age afterwards; T6 sheet tolerates only large-radius bends and is prone to cracking.

What surface finishes work on 7178?

Clad or anodize (chromic/sulfuric) plus chromate conversion and primer for corrosion protection; avoid sustained short-transverse tensile stress and use T76 tempers in exfoliation-prone areas.

7178 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≤ 0.4
Fe≤ 0.5
Cu1.6 – 2.42
Mn≤ 0.3
Mg2.4 – 3.12.7
Cr0.18 – 0.280.23
Zn6.3 – 7.36.8
Ti≤ 0.2
Others (each)each≤ 0.05
Others (total)total≤ 0.15
Albalance

7178-T651 — frequently asked

What is 7178-T651 used for?

7178-T651 is typically used for aircraft upper wing skins, wing stringers, compression-loaded airframe panels, extruded stiffeners and spar caps, alclad aerospace sheet components and legacy airframe replacement parts. In short: compression aerospace alloy.

What is the yield strength of 7178-T651?

7178-T651 has a typical yield strength of 530 MPa (76.9 ksi) and a tensile strength of 600 MPa (87 ksi) — stronger than 97% of aluminum grades. Strength varies by condition: see the 8 listed tempers.

Is 7178-T651 easy to machine?

Yes — machinability is rated very good (75/100, better than 86% of aluminum grades). Machines well in T6/T76 with sharp carbide, high speed and flood coolant; relieve stresses (T651/T7651) before heavy pocket milling to control distortion.

Can 7178-T651 be welded?

Not readily — weldability is rated not recommended (12/100). Not fusion weldable — hot cracking and severe HAZ SCC; join by riveting, bolting or adhesive bonding (friction-stir only with qualified procedures).

What surface finishes work on 7178-T651?

Clad or anodize (chromic/sulfuric) plus chromate conversion and primer for corrosion protection; avoid sustained short-transverse tensile stress and use T76 tempers in exfoliation-prone areas.

Can 7178-T651 be formed, bent or molded?

Form in O or freshly quenched W temper and age afterwards; T6 sheet tolerates only large-radius bends and is prone to cracking.

What is the maximum service temperature of 7178-T651?

7178-T651 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.

Can FabDigit make parts in 7178-T651?

Yes — 7178-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 AlloysASM International (1990)
  3. MMPDS-17 Metallic Materials Properties Development and StandardizationBattelle/FAA (2022)
  4. ASTM B209 / B221 — Aluminum Sheet, Plate and Extruded ProductsASTM International (2021)
  5. ASM Handbook Vol. 13B — Corrosion: MaterialsASM 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.