7108A Aluminum vs. 5059 Aluminum
Both 7108A aluminum and 5059 aluminum are aluminum alloys. They have a moderately high 94% of their average alloy composition in common. There are 30 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is 7108A aluminum and the bottom bar is 5059 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 69 | |
69 |
Elongation at Break, % | 11 to 13 | |
11 to 25 |
Fatigue Strength, MPa | 120 to 130 | |
170 to 240 |
Poisson's Ratio | 0.33 | |
0.33 |
Shear Modulus, GPa | 26 | |
26 |
Shear Strength, MPa | 210 | |
220 to 250 |
Tensile Strength: Ultimate (UTS), MPa | 350 | |
350 to 410 |
Tensile Strength: Yield (Proof), MPa | 290 to 300 | |
170 to 300 |
Thermal Properties
Latent Heat of Fusion, J/g | 380 | |
390 |
Maximum Temperature: Mechanical, °C | 210 | |
210 |
Melting Completion (Liquidus), °C | 630 | |
650 |
Melting Onset (Solidus), °C | 520 | |
510 |
Specific Heat Capacity, J/kg-K | 870 | |
900 |
Thermal Conductivity, W/m-K | 150 | |
110 |
Thermal Expansion, µm/m-K | 24 | |
24 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 36 | |
29 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 110 | |
95 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 10 | |
9.5 |
Density, g/cm3 | 2.9 | |
2.7 |
Embodied Carbon, kg CO2/kg material | 8.3 | |
9.1 |
Embodied Energy, MJ/kg | 150 | |
160 |
Embodied Water, L/kg | 1150 | |
1160 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 38 to 44 | |
42 to 75 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 610 to 640 | |
220 to 650 |
Stiffness to Weight: Axial, points | 13 | |
14 |
Stiffness to Weight: Bending, points | 47 | |
50 |
Strength to Weight: Axial, points | 33 to 34 | |
36 to 42 |
Strength to Weight: Bending, points | 38 | |
41 to 45 |
Thermal Diffusivity, mm2/s | 59 | |
44 |
Thermal Shock Resistance, points | 15 to 16 | |
16 to 18 |
Alloy Composition
Aluminum (Al), % | 91.6 to 94.4 | |
89.9 to 94 |
Chromium (Cr), % | 0 to 0.040 | |
0 to 0.25 |
Copper (Cu), % | 0 to 0.050 | |
0 to 0.25 |
Gallium (Ga), % | 0 to 0.030 | |
0 |
Iron (Fe), % | 0 to 0.3 | |
0 to 0.5 |
Magnesium (Mg), % | 0.7 to 1.5 | |
5.0 to 6.0 |
Manganese (Mn), % | 0 to 0.050 | |
0.6 to 1.2 |
Silicon (Si), % | 0 to 0.2 | |
0 to 0.45 |
Titanium (Ti), % | 0 to 0.030 | |
0 to 0.2 |
Zinc (Zn), % | 4.8 to 5.8 | |
0.4 to 0.9 |
Zirconium (Zr), % | 0.15 to 0.25 | |
0.050 to 0.25 |
Residuals, % | 0 | |
0 to 0.15 |