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C75400 Nickel Silver vs. 2011 Aluminum

C75400 nickel silver belongs to the copper alloys classification, while 2011 aluminum belongs to the aluminum 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 C75400 nickel silver and the bottom bar is 2011 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
71
Elongation at Break, % 2.0 to 43
8.5 to 18
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 46
27
Shear Strength, MPa 250 to 370
190 to 250
Tensile Strength: Ultimate (UTS), MPa 370 to 630
310 to 420
Tensile Strength: Yield (Proof), MPa 130 to 590
140 to 310

Thermal Properties

Latent Heat of Fusion, J/g 200
390
Maximum Temperature: Mechanical, °C 190
190
Melting Completion (Liquidus), °C 1080
640
Melting Onset (Solidus), °C 1040
540
Specific Heat Capacity, J/kg-K 390
870
Thermal Conductivity, W/m-K 36
140 to 170
Thermal Expansion, µm/m-K 18
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.0
35 to 45
Electrical Conductivity: Equal Weight (Specific), % IACS 7.4
100 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 32
11
Density, g/cm3 8.5
3.1
Embodied Carbon, kg CO2/kg material 3.8
7.9
Embodied Energy, MJ/kg 59
150
Embodied Water, L/kg 300
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 120
29 to 52
Resilience: Unit (Modulus of Resilience), kJ/m3 75 to 1450
140 to 680
Stiffness to Weight: Axial, points 7.9
13
Stiffness to Weight: Bending, points 19
44
Strength to Weight: Axial, points 12 to 21
27 to 37
Strength to Weight: Bending, points 13 to 19
32 to 40
Thermal Diffusivity, mm2/s 11
51 to 64
Thermal Shock Resistance, points 12 to 21
14 to 19

Alloy Composition

Aluminum (Al), % 0
91.3 to 94.6
Bismuth (Bi), % 0
0.2 to 0.6
Copper (Cu), % 63.5 to 66.5
5.0 to 6.0
Iron (Fe), % 0 to 0.25
0 to 0.7
Lead (Pb), % 0 to 0.1
0.2 to 0.6
Manganese (Mn), % 0 to 0.5
0
Nickel (Ni), % 14 to 16
0
Silicon (Si), % 0
0 to 0.4
Zinc (Zn), % 16.2 to 22.5
0 to 0.3
Residuals, % 0
0 to 0.15