6016 Aluminum vs. SAE-AISI 1008 Steel
6016 aluminum belongs to the aluminum alloys classification, while SAE-AISI 1008 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is 6016 aluminum and the bottom bar is SAE-AISI 1008 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 55 to 80 | |
| 93 to 100 |
| Elastic (Young's, Tensile) Modulus, GPa | 69 | |
| 190 |
| Elongation at Break, % | 11 to 27 | |
| 22 to 33 |
| Fatigue Strength, MPa | 68 to 89 | |
| 150 to 220 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 73 |
| Shear Strength, MPa | 130 to 170 | |
| 220 to 230 |
| Tensile Strength: Ultimate (UTS), MPa | 200 to 280 | |
| 330 to 370 |
| Tensile Strength: Yield (Proof), MPa | 110 to 210 | |
| 190 to 310 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 160 | |
| 400 |
| Melting Completion (Liquidus), °C | 660 | |
| 1470 |
| Melting Onset (Solidus), °C | 610 | |
| 1430 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 470 |
| Thermal Conductivity, W/m-K | 190 to 210 | |
| 62 |
| Thermal Expansion, µm/m-K | 23 | |
| 12 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 48 to 54 | |
| 6.9 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 160 to 180 | |
| 7.9 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 1.8 |
| Density, g/cm3 | 2.7 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 1.4 |
| Embodied Energy, MJ/kg | 150 | |
| 18 |
| Embodied Water, L/kg | 1180 | |
| 45 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 29 to 47 | |
| 78 to 91 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 82 to 340 | |
| 92 to 260 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 51 | |
| 24 |
| Strength to Weight: Axial, points | 21 to 29 | |
| 12 to 13 |
| Strength to Weight: Bending, points | 29 to 35 | |
| 13 to 15 |
| Thermal Diffusivity, mm2/s | 77 to 86 | |
| 17 |
| Thermal Shock Resistance, points | 9.1 to 12 | |
| 10 to 12 |
Alloy Composition
| Aluminum (Al), % | 96.4 to 98.8 | |
| 0 |
| Carbon (C), % | 0 | |
| 0 to 0.1 |
| Chromium (Cr), % | 0 to 0.1 | |
| 0 |
| Copper (Cu), % | 0 to 0.2 | |
| 0 |
| Iron (Fe), % | 0 to 0.5 | |
| 99.31 to 99.7 |
| Magnesium (Mg), % | 0.25 to 0.6 | |
| 0 |
| Manganese (Mn), % | 0 to 0.2 | |
| 0.3 to 0.5 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 1.0 to 1.5 | |
| 0 |
| Sulfur (S), % | 0 | |
| 0 to 0.050 |
| Titanium (Ti), % | 0 to 0.15 | |
| 0 |
| Zinc (Zn), % | 0 to 0.2 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |