MakeItFrom.com
Menu (ESC)

C70600 Copper-nickel vs. 713.0 Aluminum

C70600 copper-nickel belongs to the copper alloys classification, while 713.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 C70600 copper-nickel and the bottom bar is 713.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
71
Elongation at Break, % 3.0 to 34
3.9 to 4.3
Poisson's Ratio 0.34
0.32
Shear Modulus, GPa 46
27
Shear Strength, MPa 190 to 330
180
Tensile Strength: Ultimate (UTS), MPa 290 to 570
240 to 260
Tensile Strength: Yield (Proof), MPa 63 to 270
170

Thermal Properties

Latent Heat of Fusion, J/g 220
370
Maximum Temperature: Mechanical, °C 220
180
Melting Completion (Liquidus), °C 1150
630
Melting Onset (Solidus), °C 1100
610
Specific Heat Capacity, J/kg-K 390
860
Thermal Conductivity, W/m-K 44
150
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.8
35
Electrical Conductivity: Equal Weight (Specific), % IACS 9.9
100

Otherwise Unclassified Properties

Base Metal Price, % relative 33
9.5
Density, g/cm3 8.9
3.1
Embodied Carbon, kg CO2/kg material 3.4
7.8
Embodied Energy, MJ/kg 51
150
Embodied Water, L/kg 300
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.5 to 160
8.7 to 9.9
Resilience: Unit (Modulus of Resilience), kJ/m3 16 to 290
210 to 220
Stiffness to Weight: Axial, points 7.7
13
Stiffness to Weight: Bending, points 19
45
Strength to Weight: Axial, points 9.1 to 18
22 to 23
Strength to Weight: Bending, points 11 to 17
28 to 29
Thermal Diffusivity, mm2/s 13
57
Thermal Shock Resistance, points 9.8 to 19
10 to 11

Alloy Composition

Aluminum (Al), % 0
87.6 to 92.4
Chromium (Cr), % 0
0 to 0.35
Copper (Cu), % 84.7 to 90
0.4 to 1.0
Iron (Fe), % 1.0 to 1.8
0 to 1.1
Lead (Pb), % 0 to 0.050
0
Magnesium (Mg), % 0
0.2 to 0.5
Manganese (Mn), % 0 to 1.0
0 to 0.6
Nickel (Ni), % 9.0 to 11
0 to 0.15
Silicon (Si), % 0
0 to 0.25
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0 to 1.0
7.0 to 8.0
Residuals, % 0
0 to 0.25