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C65500 Bronze vs. 5050 Aluminum

C65500 bronze belongs to the copper alloys classification, while 5050 aluminum belongs to the aluminum 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 C65500 bronze and the bottom bar is 5050 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
68
Elongation at Break, % 4.0 to 70
1.7 to 22
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 43
26
Shear Strength, MPa 260 to 440
91 to 140
Tensile Strength: Ultimate (UTS), MPa 360 to 760
140 to 250
Tensile Strength: Yield (Proof), MPa 120 to 430
50 to 210

Thermal Properties

Latent Heat of Fusion, J/g 260
400
Maximum Temperature: Mechanical, °C 200
180
Melting Completion (Liquidus), °C 1030
650
Melting Onset (Solidus), °C 970
630
Specific Heat Capacity, J/kg-K 400
900
Thermal Conductivity, W/m-K 36
190
Thermal Expansion, µm/m-K 18
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.0
50
Electrical Conductivity: Equal Weight (Specific), % IACS 7.3
170

Otherwise Unclassified Properties

Base Metal Price, % relative 29
9.5
Calomel Potential, mV -270
-760
Density, g/cm3 8.6
2.7
Embodied Carbon, kg CO2/kg material 2.7
8.4
Embodied Energy, MJ/kg 42
150
Embodied Water, L/kg 300
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11 to 450
4.1 to 24
Resilience: Unit (Modulus of Resilience), kJ/m3 62 to 790
18 to 330
Stiffness to Weight: Axial, points 7.5
14
Stiffness to Weight: Bending, points 19
50
Strength to Weight: Axial, points 12 to 24
15 to 26
Strength to Weight: Bending, points 13 to 21
22 to 33
Thermal Diffusivity, mm2/s 10
79
Thermal Shock Resistance, points 12 to 26
6.3 to 11

Alloy Composition


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Aluminum (Al), % 0
96.3 to 98.9
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 91.5 to 96.7
0 to 0.2
Iron (Fe), % 0 to 0.8
0 to 0.7
Lead (Pb), % 0 to 0.050
0
Magnesium (Mg), % 0
1.1 to 1.8
Manganese (Mn), % 0.5 to 1.3
0 to 0.1
Nickel (Ni), % 0 to 0.6
0
Silicon (Si), % 2.8 to 3.8
0 to 0.4
Zinc (Zn), % 0 to 1.5
0 to 0.25
Residuals, % 0 to 0.5
0 to 0.15