5083 Aluminum vs. Monel 400
5083 aluminum belongs to the aluminum alloys classification, while Monel 400 belongs to the nickel alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is 5083 aluminum and the bottom bar is Monel 400.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 68 | |
160 |
Elongation at Break, % | 1.1 to 17 | |
20 to 40 |
Fatigue Strength, MPa | 93 to 190 | |
230 to 290 |
Poisson's Ratio | 0.33 | |
0.32 |
Shear Modulus, GPa | 26 | |
62 |
Shear Strength, MPa | 170 to 220 | |
370 to 490 |
Tensile Strength: Ultimate (UTS), MPa | 290 to 390 | |
540 to 780 |
Tensile Strength: Yield (Proof), MPa | 110 to 340 | |
210 to 590 |
Thermal Properties
Latent Heat of Fusion, J/g | 400 | |
270 |
Maximum Temperature: Mechanical, °C | 190 | |
1000 |
Melting Completion (Liquidus), °C | 640 | |
1350 |
Melting Onset (Solidus), °C | 580 | |
1300 |
Specific Heat Capacity, J/kg-K | 900 | |
430 |
Thermal Conductivity, W/m-K | 120 | |
23 |
Thermal Expansion, µm/m-K | 24 | |
14 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 29 | |
3.3 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 96 | |
3.4 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
50 |
Calomel Potential, mV | -780 | |
-80 |
Density, g/cm3 | 2.7 | |
8.9 |
Embodied Carbon, kg CO2/kg material | 8.9 | |
7.9 |
Embodied Energy, MJ/kg | 150 | |
110 |
Embodied Water, L/kg | 1170 | |
250 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 4.2 to 42 | |
140 to 180 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 95 to 860 | |
140 to 1080 |
Stiffness to Weight: Axial, points | 14 | |
10 |
Stiffness to Weight: Bending, points | 50 | |
21 |
Strength to Weight: Axial, points | 29 to 40 | |
17 to 25 |
Strength to Weight: Bending, points | 36 to 44 | |
17 to 21 |
Thermal Diffusivity, mm2/s | 48 | |
6.1 |
Thermal Shock Resistance, points | 12 to 17 | |
17 to 25 |
Alloy Composition
Aluminum (Al), % | 92.4 to 95.6 | |
0 |
Carbon (C), % | 0 | |
0 to 0.3 |
Chromium (Cr), % | 0.050 to 0.25 | |
0 |
Copper (Cu), % | 0 to 0.1 | |
28 to 34 |
Iron (Fe), % | 0 to 0.4 | |
0 to 2.5 |
Magnesium (Mg), % | 4.0 to 4.9 | |
0 |
Manganese (Mn), % | 0.4 to 1.0 | |
0 to 2.0 |
Nickel (Ni), % | 0 | |
63 to 72 |
Silicon (Si), % | 0 to 0.4 | |
0 to 0.5 |
Sulfur (S), % | 0 | |
0 to 0.024 |
Titanium (Ti), % | 0 to 0.15 | |
0 |
Zinc (Zn), % | 0 to 0.25 | |
0 |
Residuals, % | 0 to 0.15 | |
0 |