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713.0 Aluminum vs. C16200 Copper

713.0 aluminum belongs to the aluminum alloys classification, while C16200 copper belongs to the copper alloys. There are 30 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 713.0 aluminum and the bottom bar is C16200 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
120
Elongation at Break, % 3.9 to 4.3
2.0 to 56
Fatigue Strength, MPa 63 to 120
100 to 210
Poisson's Ratio 0.32
0.34
Shear Modulus, GPa 27
43
Shear Strength, MPa 180
190 to 390
Tensile Strength: Ultimate (UTS), MPa 240 to 260
240 to 550
Tensile Strength: Yield (Proof), MPa 170
48 to 470

Thermal Properties

Latent Heat of Fusion, J/g 370
210
Maximum Temperature: Mechanical, °C 180
370
Melting Completion (Liquidus), °C 630
1080
Melting Onset (Solidus), °C 610
1030
Specific Heat Capacity, J/kg-K 860
380
Thermal Conductivity, W/m-K 150
360
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
90
Electrical Conductivity: Equal Weight (Specific), % IACS 100
90

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
30
Density, g/cm3 3.1
9.0
Embodied Carbon, kg CO2/kg material 7.8
2.6
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 1110
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.7 to 9.9
10 to 99
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 220
10 to 970
Stiffness to Weight: Axial, points 13
7.2
Stiffness to Weight: Bending, points 45
18
Strength to Weight: Axial, points 22 to 23
7.4 to 17
Strength to Weight: Bending, points 28 to 29
9.6 to 17
Thermal Diffusivity, mm2/s 57
100
Thermal Shock Resistance, points 10 to 11
8.7 to 20

Alloy Composition


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Aluminum (Al), % 87.6 to 92.4
0
Cadmium (Cd), % 0
0.7 to 1.2
Chromium (Cr), % 0 to 0.35
0
Copper (Cu), % 0.4 to 1.0
98.6 to 99.3
Iron (Fe), % 0 to 1.1
0 to 0.2
Magnesium (Mg), % 0.2 to 0.5
0
Manganese (Mn), % 0 to 0.6
0
Nickel (Ni), % 0 to 0.15
0
Silicon (Si), % 0 to 0.25
0
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 7.0 to 8.0
0
Residuals, % 0 to 0.25
0