Aluminum Alloys and Tempers
Nine common aluminum alloys with temper, strength, density, weldability and typical uses.
Aluminum is sold as alloys identified by a four-digit number and a temper. The first digit gives the main alloying element: 1xxx is nearly pure aluminum, 2xxx has copper, 3xxx manganese, 5xxx magnesium, 6xxx magnesium and silicon, and 7xxx zinc. The temper (H for work hardened, T for heat treated) says how the metal was strengthened.
This table compares nine alloys you will meet in everyday work: their strength in the usual temper, density, how well they weld, and what they are used for.
The table
| Alloy | Series | Main alloying elements | Typical temper | Yield strength (MPa) | Tensile strength (MPa) | Yield strength (ksi) | Tensile strength (ksi) | Density (kg/m3) | Fusion weldability | Typical use |
|---|---|---|---|---|---|---|---|---|---|---|
| 1100 | 1xxx | Pure aluminum (99.0 percent) | H14 | 105 | 110 | 15.2 | 16 | 2710 | Excellent | Chemical equipment, foil, heat exchanger fins |
| 3003 | 3xxx | Manganese | H14 | 145 | 150 | 21 | 21.8 | 2730 | Excellent | Cookware, tanks, general sheet work |
| 5052 | 5xxx | Magnesium 2.5 percent | H32 | 193 | 228 | 28 | 33.1 | 2680 | Excellent | Sheet metal, marine and fuel tanks |
| 5083 | 5xxx | Magnesium 4.5 percent, manganese | H116 | 228 | 317 | 33.1 | 46 | 2660 | Excellent | Ships, pressure vessels, welded structures |
| 6061 | 6xxx | Magnesium and silicon | T6 | 276 | 310 | 40 | 45 | 2700 | Good | Structural parts, machined parts, frames |
| 6063 | 6xxx | Magnesium and silicon | T6 | 214 | 241 | 31 | 35 | 2700 | Good | Extrusions: architectural and tubing |
| 6082 | 6xxx | Magnesium, silicon, manganese | T6 | 260 | 310 | 37.7 | 45 | 2710 | Good | Structural parts (the common European alloy) |
| 2024 | 2xxx | Copper and magnesium | T3 | 345 | 483 | 50 | 70.1 | 2780 | Poor (not fusion welded) | Aircraft structure, high-strength parts |
| 7075 | 7xxx | Zinc, magnesium, copper | T6 | 503 | 572 | 73 | 83 | 2810 | Poor (not fusion welded) | Highest-strength machined parts, aircraft, molds |
Source and notes: Typical room-temperature values for the named temper (ASM Handbook, Aluminum Association "Aluminum Standards and Data"; minimums in the standards are lower). Temper codes: H = work hardened, T6 = solution heat treated and artificially aged, T3 = solution treated and cold worked. Density in kg/m3; the ksi columns are converted from MPa.
How to use this table
- Choose the alloy by the job: strength, corrosion, welding and machining all pull in different directions.
- Read the yield and tensile strength for the temper you are buying (strength drops after welding on heat-treated alloys).
- Use the density for weight, and the specific strength (strength ÷ density) to compare with steel.
Worked example: strength for weight
- 6061-T6: yield 276 MPa ÷ density 2 700 kg/m³ = 102 kN·m/kg.
- 7075-T6: 503 ÷ 2 810 = 179 kN·m/kg, about 1.8 times better than 6061.
- Mild steel A36 (250 MPa, 7 850 kg/m³) is only 32 kN·m/kg, so 6061-T6 gives about 3.2 times the strength per kilogram.
Notes and cautions
- Welding a heat-treated alloy (6061-T6) lowers the strength next to the weld by 30 to 40 percent unless the part is heat treated again.
- 5052 and 5083 are the best for marine use and the cheapest to weld; 2024 and 7075 are strong but poor in corrosion resistance and not fusion welded.
- Typical values only: minimum values in the standards are lower, and thick plate, extrusions and castings differ.
Related tools and guides
- Aluminum, Copper, Titanium and Other Alloys (guide)
- Material Properties Table
- Steel Grade Cross Reference
- Steel Bar Weight per Meter
- All reference tables
FAQ
Which aluminum is the strongest?
7075-T6 is the strongest common alloy (about 570 MPa tensile). It is hard to weld and less corrosion resistant than 5xxx and 6xxx alloys.
Which aluminum alloy is best for welding?
5052 and 5083 weld very well and keep their strength; 6061 welds well but loses strength next to the weld unless re-heat-treated.
What does T6 mean?
Solution heat treated, then artificially aged. It is the common high-strength temper of 6xxx and 7xxx alloys.
Sources
- Aluminum Association, Aluminum Standards and Data; ASM Handbook, Volume 2; ASTM B209 (sheet and plate). Typical values for the named temper.
- Typical room-temperature values for the named temper (ASM Handbook, Aluminum Association "Aluminum Standards and Data"; minimums in the standards are lower). Temper codes: H = work hardened, T6 = solution heat treated and artificially aged, T3 = solution treated and cold worked. Density in kg/m3; the ksi columns are converted from MPa.
