6014 Aluminum vs. EN 1.0234 Steel
6014 aluminum belongs to the aluminum alloys classification, while EN 1.0234 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 6014 aluminum and the bottom bar is EN 1.0234 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 69 | |
| 190 |
| Elongation at Break, % | 9.1 to 17 | |
| 12 to 29 |
| Fatigue Strength, MPa | 43 to 79 | |
| 170 to 270 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 73 |
| Shear Strength, MPa | 96 to 150 | |
| 260 to 300 |
| Tensile Strength: Ultimate (UTS), MPa | 160 to 260 | |
| 350 to 480 |
| Tensile Strength: Yield (Proof), MPa | 80 to 200 | |
| 220 to 410 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 180 | |
| 400 |
| Melting Completion (Liquidus), °C | 640 | |
| 1460 |
| Melting Onset (Solidus), °C | 620 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 470 |
| Thermal Conductivity, W/m-K | 200 | |
| 53 |
| Thermal Expansion, µm/m-K | 23 | |
| 12 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 53 | |
| 7.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 180 | |
| 8.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 1.8 |
| Density, g/cm3 | 2.7 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 8.6 | |
| 1.4 |
| Embodied Energy, MJ/kg | 160 | |
| 18 |
| Embodied Water, L/kg | 1190 | |
| 46 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 22 | |
| 36 to 130 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 46 to 300 | |
| 130 to 440 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 24 |
| Strength to Weight: Axial, points | 16 to 26 | |
| 12 to 17 |
| Strength to Weight: Bending, points | 24 to 33 | |
| 14 to 17 |
| Thermal Diffusivity, mm2/s | 83 | |
| 14 |
| Thermal Shock Resistance, points | 7.0 to 11 | |
| 11 to 15 |
Alloy Composition
| Aluminum (Al), % | 97.1 to 99.2 | |
| 0.020 to 0.060 |
| Carbon (C), % | 0 | |
| 0.13 to 0.17 |
| Chromium (Cr), % | 0 to 0.2 | |
| 0 |
| Copper (Cu), % | 0 to 0.25 | |
| 0 |
| Iron (Fe), % | 0 to 0.35 | |
| 99.02 to 99.5 |
| Magnesium (Mg), % | 0.4 to 0.8 | |
| 0 |
| Manganese (Mn), % | 0.050 to 0.2 | |
| 0.35 to 0.6 |
| Phosphorus (P), % | 0 | |
| 0 to 0.025 |
| Silicon (Si), % | 0.3 to 0.6 | |
| 0 to 0.1 |
| Sulfur (S), % | 0 | |
| 0 to 0.025 |
| Titanium (Ti), % | 0 to 0.1 | |
| 0 |
| Vanadium (V), % | 0.050 to 0.2 | |
| 0 |
| Zinc (Zn), % | 0 to 0.1 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |