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296.0 Aluminum vs. N06230 Nickel

296.0 aluminum belongs to the aluminum alloys classification, while N06230 nickel belongs to the nickel alloys. There are 29 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 296.0 aluminum and the bottom bar is N06230 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
210
Elongation at Break, % 3.2 to 7.1
38 to 48
Fatigue Strength, MPa 47 to 70
250 to 360
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
83
Tensile Strength: Ultimate (UTS), MPa 260 to 270
620 to 840
Tensile Strength: Yield (Proof), MPa 120 to 180
330 to 400

Thermal Properties

Latent Heat of Fusion, J/g 420
310
Maximum Temperature: Mechanical, °C 170
990
Melting Completion (Liquidus), °C 630
1370
Melting Onset (Solidus), °C 540
1300
Specific Heat Capacity, J/kg-K 870
420
Thermal Conductivity, W/m-K 130 to 150
8.9
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 37
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 99 to 110
1.3

Otherwise Unclassified Properties

Base Metal Price, % relative 11
85
Density, g/cm3 3.0
9.5
Embodied Carbon, kg CO2/kg material 7.8
11
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1110
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.6 to 15
200 to 330
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 220
250 to 380
Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 46
21
Strength to Weight: Axial, points 24 to 25
18 to 25
Strength to Weight: Bending, points 30 to 31
17 to 21
Thermal Diffusivity, mm2/s 51 to 56
2.3
Thermal Shock Resistance, points 12
17 to 23

Alloy Composition

Aluminum (Al), % 89 to 94
0.2 to 0.5
Boron (B), % 0
0 to 0.015
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
20 to 24
Cobalt (Co), % 0
0 to 5.0
Copper (Cu), % 4.0 to 5.0
0
Iron (Fe), % 0 to 1.2
0 to 3.0
Lanthanum (La), % 0
0.0050 to 0.050
Magnesium (Mg), % 0 to 0.050
0
Manganese (Mn), % 0 to 0.35
0.3 to 1.0
Molybdenum (Mo), % 0
1.0 to 3.0
Nickel (Ni), % 0 to 0.35
47.5 to 65.2
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 2.0 to 3.0
0.25 to 0.75
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0
Tungsten (W), % 0
13 to 15
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.35
0