8011A Aluminum vs. 515.0 Aluminum
Both 8011A aluminum and 515.0 aluminum are aluminum alloys. They have a very high 97% 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 8011A aluminum and the bottom bar is 515.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 69 | |
70 |
Elongation at Break, % | 1.7 to 28 | |
10 |
Fatigue Strength, MPa | 33 to 76 | |
130 |
Poisson's Ratio | 0.33 | |
0.33 |
Shear Modulus, GPa | 26 | |
26 |
Tensile Strength: Ultimate (UTS), MPa | 100 to 180 | |
280 |
Thermal Properties
Latent Heat of Fusion, J/g | 400 | |
470 |
Maximum Temperature: Mechanical, °C | 170 | |
170 |
Melting Completion (Liquidus), °C | 650 | |
620 |
Melting Onset (Solidus), °C | 630 | |
620 |
Specific Heat Capacity, J/kg-K | 900 | |
900 |
Thermal Expansion, µm/m-K | 23 | |
23 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.0 | |
9.5 |
Density, g/cm3 | 2.7 | |
2.6 |
Embodied Carbon, kg CO2/kg material | 8.2 | |
8.4 |
Embodied Energy, MJ/kg | 150 | |
150 |
Embodied Water, L/kg | 1180 | |
1120 |
Common Calculations
Stiffness to Weight: Axial, points | 14 | |
15 |
Stiffness to Weight: Bending, points | 50 | |
52 |
Strength to Weight: Axial, points | 11 to 18 | |
30 |
Strength to Weight: Bending, points | 18 to 26 | |
36 |
Thermal Shock Resistance, points | 4.6 to 8.1 | |
13 |
Alloy Composition
Aluminum (Al), % | 97.5 to 99.1 | |
93.6 to 96.6 |
Chromium (Cr), % | 0 to 0.1 | |
0 |
Copper (Cu), % | 0 to 0.1 | |
0 to 0.2 |
Iron (Fe), % | 0.5 to 1.0 | |
0 to 1.3 |
Magnesium (Mg), % | 0 to 0.1 | |
2.5 to 4.0 |
Manganese (Mn), % | 0 to 0.1 | |
0.4 to 0.6 |
Silicon (Si), % | 0.4 to 0.8 | |
0.5 to 10 |
Titanium (Ti), % | 0 to 0.050 | |
0 |
Zinc (Zn), % | 0 to 0.1 | |
0 to 0.1 |
Residuals, % | 0 | |
0 to 0.15 |