8011A Aluminum vs. A360.0 Aluminum
Both 8011A aluminum and A360.0 aluminum are aluminum alloys. They have 90% of their average alloy composition in common. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is 8011A aluminum and the bottom bar is A360.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 25 to 50 | |
| 75 |
| Elastic (Young's, Tensile) Modulus, GPa | 69 | |
| 72 |
| Elongation at Break, % | 1.7 to 28 | |
| 1.6 to 5.0 |
| Fatigue Strength, MPa | 33 to 76 | |
| 82 to 150 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 26 | |
| 27 |
| Tensile Strength: Ultimate (UTS), MPa | 100 to 180 | |
| 180 to 320 |
| Tensile Strength: Yield (Proof), MPa | 34 to 170 | |
| 170 to 260 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 530 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 170 |
| Melting Completion (Liquidus), °C | 650 | |
| 680 |
| Melting Onset (Solidus), °C | 630 | |
| 590 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 900 |
| Thermal Conductivity, W/m-K | 210 | |
| 110 |
| Thermal Expansion, µm/m-K | 23 | |
| 21 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 56 | |
| 30 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 180 | |
| 100 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.0 | |
| 9.5 |
| Density, g/cm3 | 2.7 | |
| 2.6 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 7.8 |
| Embodied Energy, MJ/kg | 150 | |
| 150 |
| Embodied Water, L/kg | 1180 | |
| 1070 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 3.0 to 22 | |
| 4.6 to 13 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 8.2 to 200 | |
| 190 to 470 |
| Stiffness to Weight: Axial, points | 14 | |
| 15 |
| Stiffness to Weight: Bending, points | 50 | |
| 53 |
| Strength to Weight: Axial, points | 11 to 18 | |
| 19 to 34 |
| Strength to Weight: Bending, points | 18 to 26 | |
| 27 to 39 |
| Thermal Diffusivity, mm2/s | 86 | |
| 48 |
| Thermal Shock Resistance, points | 4.6 to 8.1 | |
| 8.5 to 15 |
Alloy Composition
| Aluminum (Al), % | 97.5 to 99.1 | |
| 85.8 to 90.6 |
| Chromium (Cr), % | 0 to 0.1 | |
| 0 |
| Copper (Cu), % | 0 to 0.1 | |
| 0 to 0.6 |
| Iron (Fe), % | 0.5 to 1.0 | |
| 0 to 1.3 |
| Magnesium (Mg), % | 0 to 0.1 | |
| 0.4 to 0.6 |
| Manganese (Mn), % | 0 to 0.1 | |
| 0 to 0.35 |
| Nickel (Ni), % | 0 | |
| 0 to 0.5 |
| Silicon (Si), % | 0.4 to 0.8 | |
| 9.0 to 10 |
| Tin (Sn), % | 0 | |
| 0 to 0.15 |
| Titanium (Ti), % | 0 to 0.050 | |
| 0 |
| Zinc (Zn), % | 0 to 0.1 | |
| 0 to 0.5 |
| Residuals, % | 0 | |
| 0 to 0.25 |