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EN 2.4851 Nickel vs. 356.0 Aluminum

EN 2.4851 nickel belongs to the nickel alloys classification, while 356.0 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 EN 2.4851 nickel and the bottom bar is 356.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190
55 to 75
Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 34
2.0 to 3.8
Fatigue Strength, MPa 170
55 to 75
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
27
Shear Strength, MPa 430
140 to 190
Tensile Strength: Ultimate (UTS), MPa 650
160 to 240
Tensile Strength: Yield (Proof), MPa 230
100 to 190

Thermal Properties

Latent Heat of Fusion, J/g 320
500
Maximum Temperature: Mechanical, °C 1200
170
Melting Completion (Liquidus), °C 1360
620
Melting Onset (Solidus), °C 1310
570
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 11
150 to 170
Thermal Expansion, µm/m-K 14
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
40 to 43
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
140 to 150

Otherwise Unclassified Properties

Base Metal Price, % relative 49
9.5
Density, g/cm3 8.2
2.6
Embodied Carbon, kg CO2/kg material 8.1
8.0
Embodied Energy, MJ/kg 120
150
Embodied Water, L/kg 280
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 170
3.2 to 8.2
Resilience: Unit (Modulus of Resilience), kJ/m3 130
70 to 250
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 23
53
Strength to Weight: Axial, points 22
17 to 26
Strength to Weight: Bending, points 20
25 to 33
Thermal Diffusivity, mm2/s 2.9
64 to 71
Thermal Shock Resistance, points 17
7.6 to 11

Alloy Composition

Aluminum (Al), % 1.0 to 1.7
90.1 to 93.3
Boron (B), % 0 to 0.0060
0
Carbon (C), % 0.030 to 0.1
0
Chromium (Cr), % 21 to 25
0
Copper (Cu), % 0 to 0.5
0 to 0.25
Iron (Fe), % 7.7 to 18
0 to 0.6
Magnesium (Mg), % 0
0.2 to 0.45
Manganese (Mn), % 0 to 1.0
0 to 0.35
Nickel (Ni), % 58 to 63
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
6.5 to 7.5
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.5
0 to 0.25
Zinc (Zn), % 0
0 to 0.35
Residuals, % 0
0 to 0.15