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AZ91D Magnesium vs. Monel 400

AZ91D magnesium belongs to the magnesium 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 (6, 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 AZ91D magnesium and the bottom bar is Monel 400.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
160
Elongation at Break, % 2.3 to 4.5
20 to 40
Fatigue Strength, MPa 74 to 85
230 to 290
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 18
62
Shear Strength, MPa 120 to 140
370 to 490
Tensile Strength: Ultimate (UTS), MPa 160 to 220
540 to 780
Tensile Strength: Yield (Proof), MPa 80 to 130
210 to 590

Thermal Properties

Latent Heat of Fusion, J/g 350
270
Maximum Temperature: Mechanical, °C 130
1000
Melting Completion (Liquidus), °C 600
1350
Melting Onset (Solidus), °C 490
1300
Specific Heat Capacity, J/kg-K 990
430
Thermal Conductivity, W/m-K 78
23
Thermal Expansion, µm/m-K 27
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
3.3
Electrical Conductivity: Equal Weight (Specific), % IACS 58
3.4

Otherwise Unclassified Properties

Base Metal Price, % relative 12
50
Density, g/cm3 1.7
8.9
Embodied Carbon, kg CO2/kg material 22
7.9
Embodied Energy, MJ/kg 160
110
Embodied Water, L/kg 990
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.2 to 7.7
140 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 69 to 170
140 to 1080
Stiffness to Weight: Axial, points 15
10
Stiffness to Weight: Bending, points 69
21
Strength to Weight: Axial, points 26 to 34
17 to 25
Strength to Weight: Bending, points 38 to 46
17 to 21
Thermal Diffusivity, mm2/s 45
6.1
Thermal Shock Resistance, points 9.5 to 13
17 to 25

Alloy Composition

Aluminum (Al), % 8.3 to 9.7
0
Carbon (C), % 0
0 to 0.3
Copper (Cu), % 0 to 0.030
28 to 34
Iron (Fe), % 0 to 0.0050
0 to 2.5
Magnesium (Mg), % 88.7 to 91.2
0
Manganese (Mn), % 0.15 to 0.5
0 to 2.0
Nickel (Ni), % 0 to 0.0020
63 to 72
Silicon (Si), % 0 to 0.1
0 to 0.5
Sulfur (S), % 0
0 to 0.024
Zinc (Zn), % 0.35 to 1.0
0