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6014 Aluminum vs. Nickel 690

6014 aluminum belongs to the aluminum alloys classification, while nickel 690 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 6014 aluminum and the bottom bar is nickel 690.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 9.1 to 17
3.4 to 34
Fatigue Strength, MPa 43 to 79
180 to 300
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
79
Shear Strength, MPa 96 to 150
420 to 570
Tensile Strength: Ultimate (UTS), MPa 160 to 260
640 to 990
Tensile Strength: Yield (Proof), MPa 80 to 200
250 to 760

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 180
1010
Melting Completion (Liquidus), °C 640
1380
Melting Onset (Solidus), °C 620
1340
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 200
14
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 53
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 180
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Density, g/cm3 2.7
8.3
Embodied Carbon, kg CO2/kg material 8.6
8.2
Embodied Energy, MJ/kg 160
120
Embodied Water, L/kg 1190
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 22
31 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 46 to 300
160 to 1440
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 16 to 26
21 to 33
Strength to Weight: Bending, points 24 to 33
20 to 27
Thermal Diffusivity, mm2/s 83
3.5
Thermal Shock Resistance, points 7.0 to 11
16 to 25

Alloy Composition

Aluminum (Al), % 97.1 to 99.2
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.2
27 to 31
Copper (Cu), % 0 to 0.25
0 to 0.5
Iron (Fe), % 0 to 0.35
7.0 to 11
Magnesium (Mg), % 0.4 to 0.8
0
Manganese (Mn), % 0.050 to 0.2
0 to 0.5
Nickel (Ni), % 0
58 to 66
Silicon (Si), % 0.3 to 0.6
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0
Vanadium (V), % 0.050 to 0.2
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0