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6013 Aluminum vs. Nickel 625

6013 aluminum belongs to the aluminum alloys classification, while nickel 625 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 6013 aluminum and the bottom bar is nickel 625.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 3.4 to 22
33 to 34
Fatigue Strength, MPa 98 to 140
240 to 320
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
79
Shear Strength, MPa 190 to 240
530 to 600
Tensile Strength: Ultimate (UTS), MPa 310 to 410
790 to 910
Tensile Strength: Yield (Proof), MPa 170 to 350
320 to 450

Thermal Properties

Latent Heat of Fusion, J/g 410
330
Maximum Temperature: Mechanical, °C 160
980
Melting Completion (Liquidus), °C 650
1350
Melting Onset (Solidus), °C 580
1290
Specific Heat Capacity, J/kg-K 900
440
Thermal Conductivity, W/m-K 150
11
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 120
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
80
Density, g/cm3 2.8
8.6
Embodied Carbon, kg CO2/kg material 8.3
14
Embodied Energy, MJ/kg 150
190
Embodied Water, L/kg 1170
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 58
220 to 250
Resilience: Unit (Modulus of Resilience), kJ/m3 200 to 900
260 to 490
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 49
23
Strength to Weight: Axial, points 31 to 41
26 to 29
Strength to Weight: Bending, points 37 to 44
22 to 24
Thermal Diffusivity, mm2/s 60
2.9
Thermal Shock Resistance, points 14 to 18
22 to 25

Alloy Composition


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Aluminum (Al), % 94.8 to 97.8
0 to 0.4
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 to 0.1
20 to 23
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0.6 to 1.1
0
Iron (Fe), % 0 to 0.5
0 to 5.0
Magnesium (Mg), % 0.8 to 1.2
0
Manganese (Mn), % 0.2 to 0.8
0 to 0.5
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0
58 to 68.9
Niobium (Nb), % 0
3.2 to 4.2
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0.6 to 1.0
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0 to 0.4
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0