355.0 Aluminum vs. 6016 Aluminum
Both 355.0 aluminum and 6016 aluminum are aluminum alloys. They have a moderately high 95% of their average alloy composition in common. There are 31 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is 355.0 aluminum and the bottom bar is 6016 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 72 to 83 | |
| 55 to 80 |
| Elastic (Young's, Tensile) Modulus, GPa | 71 | |
| 69 |
| Elongation at Break, % | 1.5 to 2.6 | |
| 11 to 27 |
| Fatigue Strength, MPa | 55 to 70 | |
| 68 to 89 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 27 | |
| 26 |
| Shear Strength, MPa | 150 to 240 | |
| 130 to 170 |
| Tensile Strength: Ultimate (UTS), MPa | 200 to 260 | |
| 200 to 280 |
| Tensile Strength: Yield (Proof), MPa | 150 to 190 | |
| 110 to 210 |
Thermal Properties
| Latent Heat of Fusion, J/g | 470 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 180 | |
| 160 |
| Melting Completion (Liquidus), °C | 620 | |
| 660 |
| Melting Onset (Solidus), °C | 560 | |
| 610 |
| Specific Heat Capacity, J/kg-K | 890 | |
| 900 |
| Thermal Conductivity, W/m-K | 150 to 170 | |
| 190 to 210 |
| Thermal Expansion, µm/m-K | 22 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 38 to 43 | |
| 48 to 54 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 120 to 140 | |
| 160 to 180 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 9.5 |
| Density, g/cm3 | 2.7 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 8.0 | |
| 8.2 |
| Embodied Energy, MJ/kg | 150 | |
| 150 |
| Embodied Water, L/kg | 1120 | |
| 1180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 2.7 to 5.9 | |
| 29 to 47 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 150 to 250 | |
| 82 to 340 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 51 | |
| 51 |
| Strength to Weight: Axial, points | 20 to 27 | |
| 21 to 29 |
| Strength to Weight: Bending, points | 28 to 33 | |
| 29 to 35 |
| Thermal Diffusivity, mm2/s | 60 to 69 | |
| 77 to 86 |
| Thermal Shock Resistance, points | 9.1 to 12 | |
| 9.1 to 12 |
Alloy Composition
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| Aluminum (Al), % | 90.3 to 94.1 | |
| 96.4 to 98.8 |
| Chromium (Cr), % | 0 to 0.25 | |
| 0 to 0.1 |
| Copper (Cu), % | 1.0 to 1.5 | |
| 0 to 0.2 |
| Iron (Fe), % | 0 to 0.6 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0.4 to 0.6 | |
| 0.25 to 0.6 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 to 0.2 |
| Silicon (Si), % | 4.5 to 5.5 | |
| 1.0 to 1.5 |
| Titanium (Ti), % | 0 to 0.25 | |
| 0 to 0.15 |
| Zinc (Zn), % | 0 to 0.35 | |
| 0 to 0.2 |
| Residuals, % | 0 to 0.15 | |
| 0 to 0.15 |