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1350 Aluminum vs. N10675 Nickel

1350 aluminum belongs to the aluminum alloys classification, while N10675 nickel 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 1350 aluminum and the bottom bar is N10675 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
220
Elongation at Break, % 1.4 to 30
47
Fatigue Strength, MPa 24 to 50
350
Poisson's Ratio 0.33
0.31
Shear Modulus, GPa 26
85
Shear Strength, MPa 44 to 110
610
Tensile Strength: Ultimate (UTS), MPa 68 to 190
860
Tensile Strength: Yield (Proof), MPa 25 to 170
400

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 170
910
Melting Completion (Liquidus), °C 660
1420
Melting Onset (Solidus), °C 650
1370
Specific Heat Capacity, J/kg-K 900
380
Thermal Conductivity, W/m-K 230
11
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61 to 62
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 200 to 210
1.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
80
Density, g/cm3 2.7
9.3
Embodied Carbon, kg CO2/kg material 8.3
16
Embodied Energy, MJ/kg 160
210
Embodied Water, L/kg 1200
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 0.77 to 54
330
Resilience: Unit (Modulus of Resilience), kJ/m3 4.4 to 200
350
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
22
Strength to Weight: Axial, points 7.0 to 19
26
Strength to Weight: Bending, points 14 to 27
22
Thermal Diffusivity, mm2/s 96
3.1
Thermal Shock Resistance, points 3.0 to 8.2
26

Alloy Composition

Aluminum (Al), % 99.5 to 100
0 to 0.5
Boron (B), % 0 to 0.050
0
Carbon (C), % 0
0 to 0.010
Chromium (Cr), % 0 to 0.010
1.0 to 3.0
Cobalt (Co), % 0
0 to 3.0
Copper (Cu), % 0 to 0.050
0 to 0.2
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.4
1.0 to 3.0
Manganese (Mn), % 0 to 0.010
0 to 3.0
Molybdenum (Mo), % 0
27 to 32
Nickel (Ni), % 0
51.3 to 71
Niobium (Nb), % 0
0 to 0.2
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.1
0 to 0.1
Sulfur (S), % 0
0 to 0.010
Tantalum (Ta), % 0
0 to 0.2
Titanium (Ti), % 0 to 0.020
0 to 0.2
Tungsten (W), % 0
0 to 3.0
Vanadium (V), % 0 to 0.020
0 to 0.2
Zinc (Zn), % 0 to 0.050
0 to 0.1
Residuals, % 0 to 0.1
0