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A206.0 Aluminum vs. Monel 400

A206.0 aluminum belongs to the aluminum alloys classification, while Monel 400 belongs to the nickel alloys. There are 30 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 A206.0 aluminum and the bottom bar is Monel 400.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
160
Elongation at Break, % 4.2 to 10
20 to 40
Fatigue Strength, MPa 90 to 180
230 to 290
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
62
Shear Strength, MPa 260
370 to 490
Tensile Strength: Ultimate (UTS), MPa 390 to 440
540 to 780
Tensile Strength: Yield (Proof), MPa 250 to 380
210 to 590

Thermal Properties

Latent Heat of Fusion, J/g 390
270
Maximum Temperature: Mechanical, °C 170
1000
Melting Completion (Liquidus), °C 670
1350
Melting Onset (Solidus), °C 550
1300
Specific Heat Capacity, J/kg-K 880
430
Thermal Conductivity, W/m-K 130
23
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
3.3
Electrical Conductivity: Equal Weight (Specific), % IACS 90
3.4

Otherwise Unclassified Properties

Base Metal Price, % relative 11
50
Density, g/cm3 3.0
8.9
Embodied Carbon, kg CO2/kg material 8.0
7.9
Embodied Energy, MJ/kg 150
110
Embodied Water, L/kg 1150
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 37
140 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 440 to 1000
140 to 1080
Stiffness to Weight: Axial, points 13
10
Stiffness to Weight: Bending, points 46
21
Strength to Weight: Axial, points 36 to 41
17 to 25
Strength to Weight: Bending, points 39 to 43
17 to 21
Thermal Diffusivity, mm2/s 48
6.1
Thermal Shock Resistance, points 17 to 19
17 to 25

Alloy Composition

Aluminum (Al), % 93.9 to 95.7
0
Carbon (C), % 0
0 to 0.3
Copper (Cu), % 4.2 to 5.0
28 to 34
Iron (Fe), % 0 to 0.1
0 to 2.5
Magnesium (Mg), % 0 to 0.15
0
Manganese (Mn), % 0 to 0.2
0 to 2.0
Nickel (Ni), % 0 to 0.050
63 to 72
Silicon (Si), % 0 to 0.050
0 to 0.5
Sulfur (S), % 0
0 to 0.024
Tin (Sn), % 0 to 0.050
0
Titanium (Ti), % 0.15 to 0.3
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0