EN AC-42100 Aluminum vs. 5086 Aluminum
Both EN AC-42100 aluminum and 5086 aluminum are aluminum alloys. They have a moderately high 93% of their average alloy composition in common. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is EN AC-42100 aluminum and the bottom bar is 5086 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 91 | |
65 to 100 |
Elastic (Young's, Tensile) Modulus, GPa | 70 | |
68 |
Elongation at Break, % | 3.4 to 9.0 | |
1.7 to 20 |
Fatigue Strength, MPa | 76 to 82 | |
88 to 180 |
Poisson's Ratio | 0.33 | |
0.33 |
Shear Modulus, GPa | 26 | |
26 |
Tensile Strength: Ultimate (UTS), MPa | 280 to 290 | |
270 to 390 |
Tensile Strength: Yield (Proof), MPa | 210 to 230 | |
110 to 320 |
Thermal Properties
Latent Heat of Fusion, J/g | 500 | |
400 |
Maximum Temperature: Mechanical, °C | 170 | |
190 |
Melting Completion (Liquidus), °C | 610 | |
640 |
Melting Onset (Solidus), °C | 600 | |
590 |
Specific Heat Capacity, J/kg-K | 910 | |
900 |
Thermal Conductivity, W/m-K | 150 | |
130 |
Thermal Expansion, µm/m-K | 22 | |
24 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 41 | |
31 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 140 | |
100 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
9.5 |
Density, g/cm3 | 2.6 | |
2.7 |
Embodied Carbon, kg CO2/kg material | 8.0 | |
8.8 |
Embodied Energy, MJ/kg | 150 | |
150 |
Embodied Water, L/kg | 1110 | |
1180 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 9.1 to 23 | |
5.8 to 42 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 300 to 370 | |
86 to 770 |
Stiffness to Weight: Axial, points | 15 | |
14 |
Stiffness to Weight: Bending, points | 53 | |
50 |
Strength to Weight: Axial, points | 30 to 31 | |
28 to 40 |
Strength to Weight: Bending, points | 37 to 38 | |
34 to 44 |
Thermal Diffusivity, mm2/s | 66 | |
52 |
Thermal Shock Resistance, points | 13 | |
12 to 17 |
Alloy Composition
Aluminum (Al), % | 91.3 to 93.3 | |
93 to 96.3 |
Chromium (Cr), % | 0 | |
0.050 to 0.25 |
Copper (Cu), % | 0 to 0.050 | |
0 to 0.1 |
Iron (Fe), % | 0 to 0.19 | |
0 to 0.5 |
Magnesium (Mg), % | 0.25 to 0.45 | |
3.5 to 4.5 |
Manganese (Mn), % | 0 to 0.1 | |
0.2 to 0.7 |
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 0.070 | |
0 to 0.25 |
Residuals, % | 0 | |
0 to 0.15 |