1350 Aluminum vs. ZA-27
1350 aluminum belongs to the aluminum alloys classification, while ZA-27 belongs to the zinc alloys. They have a modest 27% of their average alloy composition in common, which, by itself, doesn't mean much. There are 31 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is 1350 aluminum and the bottom bar is ZA-27.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 20 to 45 | |
| 100 to 120 |
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 78 |
| Elongation at Break, % | 1.4 to 30 | |
| 2.0 to 4.5 |
| Fatigue Strength, MPa | 24 to 50 | |
| 110 to 170 |
| Poisson's Ratio | 0.33 | |
| 0.27 |
| Shear Modulus, GPa | 26 | |
| 31 |
| Shear Strength, MPa | 44 to 110 | |
| 230 to 330 |
| Tensile Strength: Ultimate (UTS), MPa | 68 to 190 | |
| 400 to 430 |
| Tensile Strength: Yield (Proof), MPa | 25 to 170 | |
| 260 to 370 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 130 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 120 |
| Melting Completion (Liquidus), °C | 660 | |
| 480 |
| Melting Onset (Solidus), °C | 650 | |
| 380 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 530 |
| Thermal Conductivity, W/m-K | 230 | |
| 130 |
| Thermal Expansion, µm/m-K | 24 | |
| 26 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 61 to 62 | |
| 30 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 200 to 210 | |
| 53 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 11 |
| Density, g/cm3 | 2.7 | |
| 5.0 |
| Embodied Carbon, kg CO2/kg material | 8.3 | |
| 4.2 |
| Embodied Energy, MJ/kg | 160 | |
| 80 |
| Embodied Water, L/kg | 1200 | |
| 570 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 0.77 to 54 | |
| 8.1 to 18 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 4.4 to 200 | |
| 420 to 890 |
| Stiffness to Weight: Axial, points | 14 | |
| 8.6 |
| Stiffness to Weight: Bending, points | 50 | |
| 28 |
| Strength to Weight: Axial, points | 7.0 to 19 | |
| 22 to 24 |
| Strength to Weight: Bending, points | 14 to 27 | |
| 24 to 25 |
| Thermal Diffusivity, mm2/s | 96 | |
| 47 |
| Thermal Shock Resistance, points | 3.0 to 8.2 | |
| 14 to 15 |
Alloy Composition
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| Aluminum (Al), % | 99.5 to 100 | |
| 25 to 28 |
| Boron (B), % | 0 to 0.050 | |
| 0 |
| Cadmium (Cd), % | 0 | |
| 0 to 0.0060 |
| Chromium (Cr), % | 0 to 0.010 | |
| 0 |
| Copper (Cu), % | 0 to 0.050 | |
| 2.0 to 2.5 |
| Gallium (Ga), % | 0 to 0.030 | |
| 0 |
| Iron (Fe), % | 0 to 0.4 | |
| 0 to 0.1 |
| Lead (Pb), % | 0 | |
| 0 to 0.0060 |
| Magnesium (Mg), % | 0 | |
| 0.010 to 0.020 |
| Manganese (Mn), % | 0 to 0.010 | |
| 0 |
| Nickel (Ni), % | 0 | |
| 0 to 0.020 |
| Silicon (Si), % | 0 to 0.1 | |
| 0 to 0.080 |
| Tin (Sn), % | 0 | |
| 0 to 0.0030 |
| Titanium (Ti), % | 0 to 0.020 | |
| 0 |
| Vanadium (V), % | 0 to 0.020 | |
| 0 |
| Zinc (Zn), % | 0 to 0.050 | |
| 69.3 to 73 |
| Residuals, % | 0 to 0.1 | |
| 0 |