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5110A Aluminum vs. 60Cr-40Ni Alloy

5110A aluminum belongs to the aluminum alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. There are 19 material properties with values for both materials. Properties with values for just one material (11, 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 5110A aluminum and the bottom bar is 60Cr-40Ni alloy.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
220
Poisson's Ratio 0.33
0.25
Shear Modulus, GPa 26
87
Tensile Strength: Ultimate (UTS), MPa 100 to 190
870
Tensile Strength: Yield (Proof), MPa 32 to 170
660

Thermal Properties

Latent Heat of Fusion, J/g 400
370
Specific Heat Capacity, J/kg-K 900
490
Thermal Expansion, µm/m-K 23
16

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
49
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
7.4
Embodied Energy, MJ/kg 150
110
Embodied Water, L/kg 1190
380

Common Calculations

Resilience: Unit (Modulus of Resilience), kJ/m3 7.6 to 200
1000
Stiffness to Weight: Axial, points 14
16
Stiffness to Weight: Bending, points 50
26
Strength to Weight: Axial, points 10 to 19
31
Strength to Weight: Bending, points 18 to 27
26
Thermal Shock Resistance, points 4.5 to 8.4
18

Alloy Composition

Aluminum (Al), % 98.5 to 99.8
0 to 0.25
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
58 to 62
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.25
0 to 1.0
Magnesium (Mg), % 0.2 to 0.6
0
Manganese (Mn), % 0 to 0.2
0 to 0.3
Nickel (Ni), % 0
34.5 to 42
Nitrogen (N), % 0
0 to 0.3
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.15
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0
0 to 0.5
Zinc (Zn), % 0 to 0.030
0
Residuals, % 0 to 0.1
0