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Monel 400 vs. 5083 Aluminum

Monel 400 belongs to the nickel alloys classification, while 5083 aluminum belongs to the aluminum 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 Monel 400 and the bottom bar is 5083 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 160
68
Elongation at Break, % 20 to 40
1.1 to 17
Fatigue Strength, MPa 230 to 290
93 to 190
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 62
26
Shear Strength, MPa 370 to 490
170 to 220
Tensile Strength: Ultimate (UTS), MPa 540 to 780
290 to 390
Tensile Strength: Yield (Proof), MPa 210 to 590
110 to 340

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 1000
190
Melting Completion (Liquidus), °C 1350
640
Melting Onset (Solidus), °C 1300
580
Specific Heat Capacity, J/kg-K 430
900
Thermal Conductivity, W/m-K 23
120
Thermal Expansion, µm/m-K 14
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.3
29
Electrical Conductivity: Equal Weight (Specific), % IACS 3.4
96

Otherwise Unclassified Properties

Base Metal Price, % relative 50
9.5
Calomel Potential, mV -80
-780
Density, g/cm3 8.9
2.7
Embodied Carbon, kg CO2/kg material 7.9
8.9
Embodied Energy, MJ/kg 110
150
Embodied Water, L/kg 250
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 180
4.2 to 42
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 1080
95 to 860
Stiffness to Weight: Axial, points 10
14
Stiffness to Weight: Bending, points 21
50
Strength to Weight: Axial, points 17 to 25
29 to 40
Strength to Weight: Bending, points 17 to 21
36 to 44
Thermal Diffusivity, mm2/s 6.1
48
Thermal Shock Resistance, points 17 to 25
12 to 17

Alloy Composition

Aluminum (Al), % 0
92.4 to 95.6
Carbon (C), % 0 to 0.3
0
Chromium (Cr), % 0
0.050 to 0.25
Copper (Cu), % 28 to 34
0 to 0.1
Iron (Fe), % 0 to 2.5
0 to 0.4
Magnesium (Mg), % 0
4.0 to 4.9
Manganese (Mn), % 0 to 2.0
0.4 to 1.0
Nickel (Ni), % 63 to 72
0
Silicon (Si), % 0 to 0.5
0 to 0.4
Sulfur (S), % 0 to 0.024
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants