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C95300 Bronze vs. 6016 Aluminum

C95300 bronze belongs to the copper alloys classification, while 6016 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 C95300 bronze and the bottom bar is 6016 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 120 to 170
55 to 80
Elastic (Young's, Tensile) Modulus, GPa 110
69
Elongation at Break, % 14 to 25
11 to 27
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 42
26
Tensile Strength: Ultimate (UTS), MPa 520 to 610
200 to 280
Tensile Strength: Yield (Proof), MPa 190 to 310
110 to 210

Thermal Properties

Latent Heat of Fusion, J/g 230
410
Maximum Temperature: Mechanical, °C 220
160
Melting Completion (Liquidus), °C 1050
660
Melting Onset (Solidus), °C 1040
610
Specific Heat Capacity, J/kg-K 440
900
Thermal Conductivity, W/m-K 63
190 to 210
Thermal Expansion, µm/m-K 18
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 13
48 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 14
160 to 180

Otherwise Unclassified Properties

Base Metal Price, % relative 28
9.5
Density, g/cm3 8.3
2.7
Embodied Carbon, kg CO2/kg material 3.1
8.2
Embodied Energy, MJ/kg 52
150
Embodied Water, L/kg 390
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 73 to 100
29 to 47
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 420
82 to 340
Stiffness to Weight: Axial, points 7.5
14
Stiffness to Weight: Bending, points 19
51
Strength to Weight: Axial, points 17 to 21
21 to 29
Strength to Weight: Bending, points 17 to 19
29 to 35
Thermal Diffusivity, mm2/s 17
77 to 86
Thermal Shock Resistance, points 19 to 22
9.1 to 12

Alloy Composition


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Aluminum (Al), % 9.0 to 11
96.4 to 98.8
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 86.5 to 90.2
0 to 0.2
Iron (Fe), % 0.8 to 1.5
0 to 0.5
Magnesium (Mg), % 0
0.25 to 0.6
Manganese (Mn), % 0
0 to 0.2
Silicon (Si), % 0
1.0 to 1.5
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0 to 1.0
0 to 0.15