MakeItFrom.com
Menu (ESC)

206.0 Aluminum vs. N06985 Nickel

206.0 aluminum belongs to the aluminum alloys classification, while N06985 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 206.0 aluminum and the bottom bar is N06985 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
210
Elongation at Break, % 8.4 to 12
45
Fatigue Strength, MPa 88 to 210
220
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
80
Shear Strength, MPa 260
480
Tensile Strength: Ultimate (UTS), MPa 330 to 440
690
Tensile Strength: Yield (Proof), MPa 190 to 350
260

Thermal Properties

Latent Heat of Fusion, J/g 390
320
Maximum Temperature: Mechanical, °C 170
990
Melting Completion (Liquidus), °C 650
1350
Melting Onset (Solidus), °C 570
1260
Specific Heat Capacity, J/kg-K 880
450
Thermal Conductivity, W/m-K 120
10
Thermal Expansion, µm/m-K 19
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 99
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 11
55
Density, g/cm3 3.0
8.4
Embodied Carbon, kg CO2/kg material 8.0
8.8
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1150
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 49
250
Resilience: Unit (Modulus of Resilience), kJ/m3 270 to 840
160
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
23
Strength to Weight: Axial, points 30 to 40
23
Strength to Weight: Bending, points 35 to 42
21
Thermal Diffusivity, mm2/s 46
2.6
Thermal Shock Resistance, points 17 to 23
16

Alloy Composition

Aluminum (Al), % 93.3 to 95.3
0
Carbon (C), % 0
0 to 0.015
Chromium (Cr), % 0
21 to 23.5
Cobalt (Co), % 0
0 to 5.0
Copper (Cu), % 4.2 to 5.0
1.5 to 2.5
Iron (Fe), % 0 to 0.15
18 to 21
Magnesium (Mg), % 0.15 to 0.35
0
Manganese (Mn), % 0.2 to 0.5
0 to 1.0
Molybdenum (Mo), % 0
6.0 to 8.0
Nickel (Ni), % 0 to 0.050
35.9 to 53.5
Niobium (Nb), % 0
0 to 0.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Tin (Sn), % 0 to 0.050
0
Titanium (Ti), % 0.15 to 0.3
0
Tungsten (W), % 0
0 to 1.5
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0