EN AC-71100 Aluminum vs. EN 1.7362 Steel
EN AC-71100 aluminum belongs to the aluminum alloys classification, while EN 1.7362 steel belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (5, 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 EN AC-71100 aluminum and the bottom bar is EN 1.7362 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 110 | |
| 150 to 180 |
| Elastic (Young's, Tensile) Modulus, GPa | 72 | |
| 190 |
| Elongation at Break, % | 1.1 | |
| 21 to 22 |
| Fatigue Strength, MPa | 150 | |
| 140 to 250 |
| Poisson's Ratio | 0.32 | |
| 0.29 |
| Shear Modulus, GPa | 27 | |
| 74 |
| Tensile Strength: Ultimate (UTS), MPa | 260 | |
| 510 to 600 |
| Tensile Strength: Yield (Proof), MPa | 230 | |
| 200 to 360 |
Thermal Properties
| Latent Heat of Fusion, J/g | 490 | |
| 260 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 510 |
| Melting Completion (Liquidus), °C | 580 | |
| 1460 |
| Melting Onset (Solidus), °C | 520 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 860 | |
| 470 |
| Thermal Expansion, µm/m-K | 22 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 32 | |
| 8.1 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 97 | |
| 9.4 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 4.5 |
| Density, g/cm3 | 2.9 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 7.4 | |
| 1.8 |
| Embodied Energy, MJ/kg | 140 | |
| 23 |
| Embodied Water, L/kg | 1010 | |
| 69 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 2.8 | |
| 90 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 360 | |
| 100 to 340 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 47 | |
| 25 |
| Strength to Weight: Axial, points | 25 | |
| 18 to 21 |
| Strength to Weight: Bending, points | 31 | |
| 18 to 20 |
| Thermal Shock Resistance, points | 12 | |
| 14 to 17 |
Alloy Composition
| Aluminum (Al), % | 78.7 to 83.3 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.1 to 0.15 |
| Chromium (Cr), % | 0 | |
| 4.0 to 6.0 |
| Copper (Cu), % | 0 to 0.1 | |
| 0 to 0.3 |
| Iron (Fe), % | 0 to 0.3 | |
| 91.5 to 95.2 |
| Magnesium (Mg), % | 0.2 to 0.5 | |
| 0 |
| Manganese (Mn), % | 0 to 0.15 | |
| 0.3 to 0.6 |
| Molybdenum (Mo), % | 0 | |
| 0.45 to 0.65 |
| Nickel (Ni), % | 0 | |
| 0 to 0.3 |
| Nitrogen (N), % | 0 | |
| 0 to 0.012 |
| Phosphorus (P), % | 0 | |
| 0 to 0.020 |
| Silicon (Si), % | 7.5 to 9.5 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 | |
| 0 to 0.0050 |
| Titanium (Ti), % | 0 to 0.15 | |
| 0 |
| Zinc (Zn), % | 9.0 to 10.5 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |