5040 Aluminum vs. 201.0 Aluminum
Both 5040 aluminum and 201.0 aluminum are aluminum alloys. They have a moderately high 95% of their average alloy composition in common. There are 30 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is 5040 aluminum and the bottom bar is 201.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 66 to 74 | |
95 to 140 |
Elastic (Young's, Tensile) Modulus, GPa | 70 | |
71 |
Elongation at Break, % | 5.7 to 6.8 | |
4.4 to 20 |
Fatigue Strength, MPa | 100 to 130 | |
120 to 150 |
Poisson's Ratio | 0.33 | |
0.33 |
Shear Modulus, GPa | 26 | |
27 |
Shear Strength, MPa | 140 to 150 | |
290 |
Tensile Strength: Ultimate (UTS), MPa | 240 to 260 | |
370 to 470 |
Tensile Strength: Yield (Proof), MPa | 190 to 230 | |
220 to 400 |
Thermal Properties
Latent Heat of Fusion, J/g | 400 | |
390 |
Maximum Temperature: Mechanical, °C | 190 | |
170 |
Melting Completion (Liquidus), °C | 650 | |
650 |
Melting Onset (Solidus), °C | 600 | |
570 |
Specific Heat Capacity, J/kg-K | 900 | |
870 |
Thermal Conductivity, W/m-K | 160 | |
120 |
Thermal Expansion, µm/m-K | 23 | |
19 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 41 | |
30 to 33 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 130 | |
87 to 97 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
38 |
Density, g/cm3 | 2.8 | |
3.1 |
Embodied Carbon, kg CO2/kg material | 8.3 | |
8.7 |
Embodied Energy, MJ/kg | 150 | |
160 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 14 to 15 | |
19 to 63 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 260 to 380 | |
330 to 1160 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 50 | |
45 |
Strength to Weight: Axial, points | 24 to 26 | |
33 to 42 |
Strength to Weight: Bending, points | 31 to 32 | |
37 to 44 |
Thermal Diffusivity, mm2/s | 64 | |
45 |
Thermal Shock Resistance, points | 10 to 11 | |
19 to 25 |
Alloy Composition
Aluminum (Al), % | 95.2 to 98 | |
92.1 to 95.1 |
Chromium (Cr), % | 0.1 to 0.3 | |
0 |
Copper (Cu), % | 0 to 0.25 | |
4.0 to 5.2 |
Iron (Fe), % | 0 to 0.7 | |
0 to 0.15 |
Magnesium (Mg), % | 1.0 to 1.5 | |
0.15 to 0.55 |
Manganese (Mn), % | 0.9 to 1.4 | |
0.2 to 0.5 |
Silicon (Si), % | 0 to 0.3 | |
0 to 0.1 |
Silver (Ag), % | 0 | |
0.4 to 1.0 |
Titanium (Ti), % | 0 | |
0.15 to 0.35 |
Zinc (Zn), % | 0 to 0.25 | |
0 |
Residuals, % | 0 | |
0 to 0.1 |