6105 Aluminum vs. EN 1.0214 Steel
6105 aluminum belongs to the aluminum alloys classification, while EN 1.0214 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 6105 aluminum and the bottom bar is EN 1.0214 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 68 | |
190 |
Elongation at Break, % | 9.0 to 16 | |
12 to 31 |
Fatigue Strength, MPa | 95 to 130 | |
160 to 250 |
Poisson's Ratio | 0.33 | |
0.29 |
Shear Modulus, GPa | 26 | |
73 |
Shear Strength, MPa | 120 to 170 | |
250 to 290 |
Tensile Strength: Ultimate (UTS), MPa | 190 to 280 | |
330 to 460 |
Tensile Strength: Yield (Proof), MPa | 120 to 270 | |
210 to 360 |
Thermal Properties
Latent Heat of Fusion, J/g | 410 | |
250 |
Maximum Temperature: Mechanical, °C | 160 | |
400 |
Melting Completion (Liquidus), °C | 650 | |
1470 |
Melting Onset (Solidus), °C | 600 | |
1420 |
Specific Heat Capacity, J/kg-K | 900 | |
470 |
Thermal Conductivity, W/m-K | 180 to 190 | |
53 |
Thermal Expansion, µm/m-K | 23 | |
12 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 46 to 50 | |
6.9 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 150 to 170 | |
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 | 8.3 | |
1.4 |
Embodied Energy, MJ/kg | 150 | |
18 |
Embodied Water, L/kg | 1180 | |
46 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 25 to 27 | |
34 to 130 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 100 to 550 | |
120 to 340 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 51 | |
24 |
Strength to Weight: Axial, points | 20 to 29 | |
12 to 16 |
Strength to Weight: Bending, points | 28 to 35 | |
14 to 17 |
Thermal Diffusivity, mm2/s | 72 to 79 | |
14 |
Thermal Shock Resistance, points | 8.6 to 12 | |
11 to 14 |
Alloy Composition
Aluminum (Al), % | 97.2 to 99 | |
0.020 to 0.060 |
Carbon (C), % | 0 | |
0.080 to 0.12 |
Chromium (Cr), % | 0 to 0.1 | |
0 |
Copper (Cu), % | 0 to 0.1 | |
0 |
Iron (Fe), % | 0 to 0.35 | |
99.17 to 99.6 |
Magnesium (Mg), % | 0.45 to 0.8 | |
0 |
Manganese (Mn), % | 0 to 0.1 | |
0.3 to 0.5 |
Phosphorus (P), % | 0 | |
0 to 0.025 |
Silicon (Si), % | 0.6 to 1.0 | |
0 to 0.1 |
Sulfur (S), % | 0 | |
0 to 0.025 |
Titanium (Ti), % | 0 to 0.1 | |
0 |
Zinc (Zn), % | 0 to 0.1 | |
0 |
Residuals, % | 0 to 0.15 | |
0 |