MakeItFrom.com
Menu (ESC)

354.0 Aluminum vs. Nickel 600

354.0 aluminum belongs to the aluminum alloys classification, while nickel 600 belongs to the nickel alloys. There are 29 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 354.0 aluminum and the bottom bar is nickel 600.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 2.4 to 3.0
3.4 to 35
Fatigue Strength, MPa 92 to 120
220 to 300
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
75
Tensile Strength: Ultimate (UTS), MPa 360 to 380
650 to 990
Tensile Strength: Yield (Proof), MPa 280 to 310
270 to 760

Thermal Properties

Latent Heat of Fusion, J/g 530
310
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 600
1410
Melting Onset (Solidus), °C 550
1350
Specific Heat Capacity, J/kg-K 900
460
Thermal Conductivity, W/m-K 130
14
Thermal Expansion, µm/m-K 21
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 110
1.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
55
Density, g/cm3 2.7
8.5
Embodied Carbon, kg CO2/kg material 7.8
9.0
Embodied Energy, MJ/kg 150
130
Embodied Water, L/kg 1070
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.6 to 9.8
31 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 540 to 670
190 to 1490
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 52
23
Strength to Weight: Axial, points 37 to 39
21 to 32
Strength to Weight: Bending, points 42 to 44
20 to 26
Thermal Diffusivity, mm2/s 52
3.6
Thermal Shock Resistance, points 17 to 18
19 to 29

Alloy Composition

Aluminum (Al), % 87.3 to 89.4
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0
14 to 17
Copper (Cu), % 1.6 to 2.0
0 to 0.5
Iron (Fe), % 0 to 0.2
6.0 to 10
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.1
0 to 1.0
Nickel (Ni), % 0
72 to 80
Silicon (Si), % 8.6 to 9.4
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0