EN 1.0213 Steel vs. 4032 Aluminum
EN 1.0213 steel belongs to the iron alloys classification, while 4032 aluminum belongs to the aluminum 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 EN 1.0213 steel and the bottom bar is 4032 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 92 to 120 | |
| 120 |
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 73 |
| Elongation at Break, % | 12 to 25 | |
| 6.7 |
| Fatigue Strength, MPa | 160 to 240 | |
| 110 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 73 | |
| 28 |
| Shear Strength, MPa | 230 to 270 | |
| 260 |
| Tensile Strength: Ultimate (UTS), MPa | 320 to 430 | |
| 390 |
| Tensile Strength: Yield (Proof), MPa | 220 to 330 | |
| 320 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 570 |
| Maximum Temperature: Mechanical, °C | 400 | |
| 180 |
| Melting Completion (Liquidus), °C | 1470 | |
| 570 |
| Melting Onset (Solidus), °C | 1430 | |
| 530 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 900 |
| Thermal Conductivity, W/m-K | 53 | |
| 140 |
| Thermal Expansion, µm/m-K | 12 | |
| 19 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 6.9 | |
| 34 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 7.9 | |
| 120 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 1.8 | |
| 10 |
| Density, g/cm3 | 7.9 | |
| 2.6 |
| Embodied Carbon, kg CO2/kg material | 1.4 | |
| 7.8 |
| Embodied Energy, MJ/kg | 18 | |
| 140 |
| Embodied Water, L/kg | 46 | |
| 1030 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 33 to 98 | |
| 25 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 120 to 300 | |
| 700 |
| Stiffness to Weight: Axial, points | 13 | |
| 15 |
| Stiffness to Weight: Bending, points | 24 | |
| 53 |
| Strength to Weight: Axial, points | 11 to 15 | |
| 41 |
| Strength to Weight: Bending, points | 13 to 16 | |
| 45 |
| Thermal Diffusivity, mm2/s | 14 | |
| 59 |
| Thermal Shock Resistance, points | 10 to 14 | |
| 20 |
Alloy Composition
| Aluminum (Al), % | 0.020 to 0.060 | |
| 81.1 to 87.2 |
| Carbon (C), % | 0.060 to 0.1 | |
| 0 |
| Chromium (Cr), % | 0 | |
| 0 to 0.1 |
| Copper (Cu), % | 0 | |
| 0.5 to 1.3 |
| Iron (Fe), % | 99.245 to 99.67 | |
| 0 to 1.0 |
| Magnesium (Mg), % | 0 | |
| 0.8 to 1.3 |
| Manganese (Mn), % | 0.25 to 0.45 | |
| 0 |
| Nickel (Ni), % | 0 | |
| 0.5 to 1.3 |
| Phosphorus (P), % | 0 to 0.020 | |
| 0 |
| Silicon (Si), % | 0 to 0.1 | |
| 11 to 13.5 |
| Sulfur (S), % | 0 to 0.025 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 0.25 |
| Residuals, % | 0 | |
| 0 to 0.15 |