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2011A Aluminum vs. EN 2.4668 Nickel

2011A aluminum belongs to the aluminum alloys classification, while EN 2.4668 nickel belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 2011A aluminum and the bottom bar is EN 2.4668 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 6.8 to 16
14
Fatigue Strength, MPa 75 to 100
590
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
75
Shear Strength, MPa 190 to 250
840
Tensile Strength: Ultimate (UTS), MPa 310 to 410
1390
Tensile Strength: Yield (Proof), MPa 140 to 310
1160

Thermal Properties

Latent Heat of Fusion, J/g 390
310
Maximum Temperature: Mechanical, °C 190
980
Melting Completion (Liquidus), °C 660
1460
Melting Onset (Solidus), °C 550
1410
Specific Heat Capacity, J/kg-K 870
450
Thermal Conductivity, W/m-K 130
13
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 96
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 11
75
Density, g/cm3 3.1
8.3
Embodied Carbon, kg CO2/kg material 7.9
13
Embodied Energy, MJ/kg 150
190
Embodied Water, L/kg 1150
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 20 to 40
180
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 670
3490
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 44
23
Strength to Weight: Axial, points 28 to 37
46
Strength to Weight: Bending, points 33 to 40
33
Thermal Diffusivity, mm2/s 49
3.5
Thermal Shock Resistance, points 14 to 18
40

Alloy Composition


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Aluminum (Al), % 91.5 to 95.1
0.3 to 0.7
Bismuth (Bi), % 0.2 to 0.6
0
Boron (B), % 0
0.0020 to 0.0060
Carbon (C), % 0
0.020 to 0.080
Chromium (Cr), % 0
17 to 21
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 4.5 to 6.0
0 to 0.3
Iron (Fe), % 0 to 0.5
11.2 to 24.6
Lead (Pb), % 0.2 to 0.6
0
Manganese (Mn), % 0
0 to 0.35
Molybdenum (Mo), % 0
2.8 to 3.3
Nickel (Ni), % 0
50 to 55
Niobium (Nb), % 0
4.7 to 5.5
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 0.4
0 to 0.35
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
0.6 to 1.2
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.15
0