6016 Aluminum vs. ASTM A372 Grade M Steel
6016 aluminum belongs to the aluminum alloys classification, while ASTM A372 grade M 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 ASTM A372 grade M steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 55 to 80 | |
| 240 to 280 |
| Elastic (Young's, Tensile) Modulus, GPa | 69 | |
| 190 |
| Elongation at Break, % | 11 to 27 | |
| 18 to 21 |
| Fatigue Strength, MPa | 68 to 89 | |
| 450 to 520 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 73 |
| Shear Strength, MPa | 130 to 170 | |
| 510 to 570 |
| Tensile Strength: Ultimate (UTS), MPa | 200 to 280 | |
| 810 to 910 |
| Tensile Strength: Yield (Proof), MPa | 110 to 210 | |
| 660 to 770 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 160 | |
| 450 |
| Melting Completion (Liquidus), °C | 660 | |
| 1460 |
| Melting Onset (Solidus), °C | 610 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 470 |
| Thermal Conductivity, W/m-K | 190 to 210 | |
| 46 |
| Thermal Expansion, µm/m-K | 23 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 48 to 54 | |
| 8.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 160 to 180 | |
| 9.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 5.0 |
| Density, g/cm3 | 2.7 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 2.0 |
| Embodied Energy, MJ/kg | 150 | |
| 27 |
| Embodied Water, L/kg | 1180 | |
| 61 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 29 to 47 | |
| 160 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 82 to 340 | |
| 1140 to 1580 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 51 | |
| 24 |
| Strength to Weight: Axial, points | 21 to 29 | |
| 29 to 32 |
| Strength to Weight: Bending, points | 29 to 35 | |
| 24 to 27 |
| Thermal Diffusivity, mm2/s | 77 to 86 | |
| 12 |
| Thermal Shock Resistance, points | 9.1 to 12 | |
| 24 to 27 |
Alloy Composition
| Aluminum (Al), % | 96.4 to 98.8 | |
| 0 |
| Carbon (C), % | 0 | |
| 0 to 0.23 |
| Chromium (Cr), % | 0 to 0.1 | |
| 1.5 to 2.0 |
| Copper (Cu), % | 0 to 0.2 | |
| 0 |
| Iron (Fe), % | 0 to 0.5 | |
| 92.5 to 95.1 |
| Magnesium (Mg), % | 0.25 to 0.6 | |
| 0 |
| Manganese (Mn), % | 0 to 0.2 | |
| 0.2 to 0.4 |
| Molybdenum (Mo), % | 0 | |
| 0.4 to 0.6 |
| Nickel (Ni), % | 0 | |
| 2.8 to 3.9 |
| Phosphorus (P), % | 0 | |
| 0 to 0.015 |
| Silicon (Si), % | 1.0 to 1.5 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 | |
| 0 to 0.010 |
| Titanium (Ti), % | 0 to 0.15 | |
| 0 |
| Vanadium (V), % | 0 | |
| 0 to 0.080 |
| Zinc (Zn), % | 0 to 0.2 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |