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5086 Aluminum vs. C65100 Bronze

5086 aluminum belongs to the aluminum alloys classification, while C65100 bronze belongs to the copper alloys. There are 30 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 5086 aluminum and the bottom bar is C65100 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
120
Elongation at Break, % 1.7 to 20
2.4 to 50
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 26
43
Shear Strength, MPa 160 to 230
200 to 350
Tensile Strength: Ultimate (UTS), MPa 270 to 390
280 to 560
Tensile Strength: Yield (Proof), MPa 110 to 320
95 to 440

Thermal Properties

Latent Heat of Fusion, J/g 400
230
Maximum Temperature: Mechanical, °C 190
200
Melting Completion (Liquidus), °C 640
1060
Melting Onset (Solidus), °C 590
1030
Specific Heat Capacity, J/kg-K 900
390
Thermal Conductivity, W/m-K 130
57
Thermal Expansion, µm/m-K 24
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
12
Electrical Conductivity: Equal Weight (Specific), % IACS 100
12

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
30
Calomel Potential, mV -760
-280
Density, g/cm3 2.7
8.8
Embodied Carbon, kg CO2/kg material 8.8
2.6
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 1180
300

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.8 to 42
12 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 86 to 770
39 to 820
Stiffness to Weight: Axial, points 14
7.3
Stiffness to Weight: Bending, points 50
18
Strength to Weight: Axial, points 28 to 40
8.7 to 18
Strength to Weight: Bending, points 34 to 44
11 to 17
Thermal Diffusivity, mm2/s 52
16
Thermal Shock Resistance, points 12 to 17
9.5 to 19

Alloy Composition

Aluminum (Al), % 93 to 96.3
0
Chromium (Cr), % 0.050 to 0.25
0
Copper (Cu), % 0 to 0.1
94.5 to 99.2
Iron (Fe), % 0 to 0.5
0 to 0.8
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0.2 to 0.7
0 to 0.7
Silicon (Si), % 0 to 0.4
0.8 to 2.0
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0 to 1.5
Residuals, % 0
0 to 0.5