356.0 Aluminum vs. 5083 Aluminum
Both 356.0 aluminum and 5083 aluminum are aluminum alloys. They have a moderately high 93% of their average alloy composition in common. There are 32 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is 356.0 aluminum and the bottom bar is 5083 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 55 to 75 | |
| 75 to 110 |
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 68 |
| Elongation at Break, % | 2.0 to 3.8 | |
| 1.1 to 17 |
| Fatigue Strength, MPa | 55 to 75 | |
| 93 to 190 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 27 | |
| 26 |
| Shear Strength, MPa | 140 to 190 | |
| 170 to 220 |
| Tensile Strength: Ultimate (UTS), MPa | 160 to 240 | |
| 290 to 390 |
| Tensile Strength: Yield (Proof), MPa | 100 to 190 | |
| 110 to 340 |
Thermal Properties
| Latent Heat of Fusion, J/g | 500 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 190 |
| Melting Completion (Liquidus), °C | 620 | |
| 640 |
| Melting Onset (Solidus), °C | 570 | |
| 580 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 900 |
| Thermal Conductivity, W/m-K | 150 to 170 | |
| 120 |
| Thermal Expansion, µm/m-K | 21 | |
| 24 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 40 to 43 | |
| 29 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 140 to 150 | |
| 96 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 9.5 |
| Calomel Potential, mV | -730 | |
| -780 |
| Density, g/cm3 | 2.6 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 8.0 | |
| 8.9 |
| Embodied Energy, MJ/kg | 150 | |
| 150 |
| Embodied Water, L/kg | 1110 | |
| 1170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 3.2 to 8.2 | |
| 4.2 to 42 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 70 to 250 | |
| 95 to 860 |
| Stiffness to Weight: Axial, points | 15 | |
| 14 |
| Stiffness to Weight: Bending, points | 53 | |
| 50 |
| Strength to Weight: Axial, points | 17 to 26 | |
| 29 to 40 |
| Strength to Weight: Bending, points | 25 to 33 | |
| 36 to 44 |
| Thermal Diffusivity, mm2/s | 64 to 71 | |
| 48 |
| Thermal Shock Resistance, points | 7.6 to 11 | |
| 12 to 17 |
Alloy Composition
| Aluminum (Al), % | 90.1 to 93.3 | |
| 92.4 to 95.6 |
| Chromium (Cr), % | 0 | |
| 0.050 to 0.25 |
| Copper (Cu), % | 0 to 0.25 | |
| 0 to 0.1 |
| Iron (Fe), % | 0 to 0.6 | |
| 0 to 0.4 |
| Magnesium (Mg), % | 0.2 to 0.45 | |
| 4.0 to 4.9 |
| Manganese (Mn), % | 0 to 0.35 | |
| 0.4 to 1.0 |
| Silicon (Si), % | 6.5 to 7.5 | |
| 0 to 0.4 |
| Titanium (Ti), % | 0 to 0.25 | |
| 0 to 0.15 |
| Zinc (Zn), % | 0 to 0.35 | |
| 0 to 0.25 |
| Residuals, % | 0 | |
| 0 to 0.15 |