EN AC-43200 Aluminum vs. 515.0 Aluminum
Both EN AC-43200 aluminum and 515.0 aluminum are aluminum alloys. They have a moderately high 95% of their average alloy composition in common. There are 22 material properties with values for both materials. Properties with values for just one material (9, in this case) are not shown.
For each property being compared, the top bar is EN AC-43200 aluminum and the bottom bar is 515.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 72 | |
70 |
Elongation at Break, % | 1.1 | |
10 |
Fatigue Strength, MPa | 67 | |
130 |
Poisson's Ratio | 0.33 | |
0.33 |
Shear Modulus, GPa | 27 | |
26 |
Tensile Strength: Ultimate (UTS), MPa | 190 to 260 | |
280 |
Thermal Properties
Latent Heat of Fusion, J/g | 540 | |
470 |
Maximum Temperature: Mechanical, °C | 170 | |
170 |
Melting Completion (Liquidus), °C | 600 | |
620 |
Melting Onset (Solidus), °C | 590 | |
620 |
Specific Heat Capacity, J/kg-K | 900 | |
900 |
Thermal Expansion, µm/m-K | 22 | |
23 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
9.5 |
Density, g/cm3 | 2.6 | |
2.6 |
Embodied Carbon, kg CO2/kg material | 7.8 | |
8.4 |
Embodied Energy, MJ/kg | 150 | |
150 |
Embodied Water, L/kg | 1070 | |
1120 |
Common Calculations
Stiffness to Weight: Axial, points | 15 | |
15 |
Stiffness to Weight: Bending, points | 54 | |
52 |
Strength to Weight: Axial, points | 20 to 28 | |
30 |
Strength to Weight: Bending, points | 28 to 35 | |
36 |
Thermal Shock Resistance, points | 8.8 to 12 | |
13 |
Alloy Composition
Aluminum (Al), % | 86.1 to 90.8 | |
93.6 to 96.6 |
Copper (Cu), % | 0 to 0.35 | |
0 to 0.2 |
Iron (Fe), % | 0 to 0.65 | |
0 to 1.3 |
Lead (Pb), % | 0 to 0.1 | |
0 |
Magnesium (Mg), % | 0.2 to 0.45 | |
2.5 to 4.0 |
Manganese (Mn), % | 0 to 0.55 | |
0.4 to 0.6 |
Nickel (Ni), % | 0 to 0.15 | |
0 |
Silicon (Si), % | 9.0 to 11 | |
0.5 to 10 |
Titanium (Ti), % | 0 to 0.2 | |
0 |
Zinc (Zn), % | 0 to 0.35 | |
0 to 0.1 |
Residuals, % | 0 | |
0 to 0.15 |