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C72900 Copper-nickel vs. 7049 Aluminum

C72900 copper-nickel belongs to the copper alloys classification, while 7049 aluminum belongs to the aluminum 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 C72900 copper-nickel and the bottom bar is 7049 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
70
Elongation at Break, % 6.0 to 20
6.2 to 7.0
Poisson's Ratio 0.34
0.32
Shear Modulus, GPa 45
27
Shear Strength, MPa 540 to 630
300 to 310
Tensile Strength: Ultimate (UTS), MPa 870 to 1080
510 to 530
Tensile Strength: Yield (Proof), MPa 700 to 920
420 to 450

Thermal Properties

Latent Heat of Fusion, J/g 210
370
Maximum Temperature: Mechanical, °C 210
180
Melting Completion (Liquidus), °C 1120
640
Melting Onset (Solidus), °C 950
480
Specific Heat Capacity, J/kg-K 380
860
Thermal Conductivity, W/m-K 29
130
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.8
36
Electrical Conductivity: Equal Weight (Specific), % IACS 8.0
110

Otherwise Unclassified Properties

Base Metal Price, % relative 39
10
Density, g/cm3 8.8
3.1
Embodied Carbon, kg CO2/kg material 4.6
8.1
Embodied Energy, MJ/kg 72
140
Embodied Water, L/kg 360
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 49 to 210
31 to 34
Resilience: Unit (Modulus of Resilience), kJ/m3 2030 to 3490
1270 to 1440
Stiffness to Weight: Axial, points 7.6
13
Stiffness to Weight: Bending, points 19
45
Strength to Weight: Axial, points 27 to 34
46 to 47
Strength to Weight: Bending, points 23 to 27
46 to 47
Thermal Diffusivity, mm2/s 8.6
51
Thermal Shock Resistance, points 31 to 38
22 to 23

Alloy Composition


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Aluminum (Al), % 0
85.7 to 89.5
Chromium (Cr), % 0
0.1 to 0.22
Copper (Cu), % 74.1 to 78
1.2 to 1.9
Iron (Fe), % 0 to 0.5
0 to 0.35
Lead (Pb), % 0 to 0.020
0
Magnesium (Mg), % 0 to 0.15
2.0 to 2.9
Manganese (Mn), % 0 to 0.3
0 to 0.2
Nickel (Ni), % 14.5 to 15.5
0
Niobium (Nb), % 0 to 0.1
0
Silicon (Si), % 0
0 to 0.25
Tin (Sn), % 7.5 to 8.5
0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0 to 0.5
7.2 to 8.2
Residuals, % 0 to 0.3
0 to 0.15