355.0 Aluminum vs. EN 1.6771 Steel
355.0 aluminum belongs to the aluminum alloys classification, while EN 1.6771 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 355.0 aluminum and the bottom bar is EN 1.6771 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 72 to 83 | |
280 to 350 |
Elastic (Young's, Tensile) Modulus, GPa | 71 | |
190 |
Elongation at Break, % | 1.5 to 2.6 | |
8.0 to 8.7 |
Fatigue Strength, MPa | 55 to 70 | |
440 to 680 |
Poisson's Ratio | 0.33 | |
0.29 |
Shear Modulus, GPa | 27 | |
73 |
Tensile Strength: Ultimate (UTS), MPa | 200 to 260 | |
930 to 1180 |
Tensile Strength: Yield (Proof), MPa | 150 to 190 | |
740 to 1140 |
Thermal Properties
Latent Heat of Fusion, J/g | 470 | |
250 |
Maximum Temperature: Mechanical, °C | 180 | |
440 |
Melting Completion (Liquidus), °C | 620 | |
1460 |
Melting Onset (Solidus), °C | 560 | |
1420 |
Specific Heat Capacity, J/kg-K | 890 | |
470 |
Thermal Conductivity, W/m-K | 150 to 170 | |
46 |
Thermal Expansion, µm/m-K | 22 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 38 to 43 | |
8.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 120 to 140 | |
9.2 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
5.0 |
Density, g/cm3 | 2.7 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 8.0 | |
1.9 |
Embodied Energy, MJ/kg | 150 | |
25 |
Embodied Water, L/kg | 1120 | |
58 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 2.7 to 5.9 | |
75 to 93 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 150 to 250 | |
1460 to 3450 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 51 | |
24 |
Strength to Weight: Axial, points | 20 to 27 | |
33 to 41 |
Strength to Weight: Bending, points | 28 to 33 | |
27 to 31 |
Thermal Diffusivity, mm2/s | 60 to 69 | |
13 |
Thermal Shock Resistance, points | 9.1 to 12 | |
27 to 35 |
Alloy Composition
Aluminum (Al), % | 90.3 to 94.1 | |
0 |
Carbon (C), % | 0 | |
0.27 to 0.33 |
Chromium (Cr), % | 0 to 0.25 | |
0.8 to 1.2 |
Copper (Cu), % | 1.0 to 1.5 | |
0 |
Iron (Fe), % | 0 to 0.6 | |
92.2 to 95 |
Magnesium (Mg), % | 0.4 to 0.6 | |
0 |
Manganese (Mn), % | 0 to 0.5 | |
0.6 to 1.0 |
Molybdenum (Mo), % | 0 | |
0.3 to 0.6 |
Nickel (Ni), % | 0 | |
3.0 to 4.0 |
Phosphorus (P), % | 0 | |
0 to 0.030 |
Silicon (Si), % | 4.5 to 5.5 | |
0 to 0.6 |
Sulfur (S), % | 0 | |
0 to 0.020 |
Titanium (Ti), % | 0 to 0.25 | |
0 |
Zinc (Zn), % | 0 to 0.35 | |
0 |
Residuals, % | 0 to 0.15 | |
0 |