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C61500 Bronze vs. 333.0 Aluminum

C61500 bronze belongs to the copper alloys classification, while 333.0 aluminum belongs to the aluminum alloys. There are 29 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 C61500 bronze and the bottom bar is 333.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
73
Elongation at Break, % 3.0 to 55
1.0 to 2.0
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 42
28
Shear Strength, MPa 350 to 550
190 to 230
Tensile Strength: Ultimate (UTS), MPa 480 to 970
230 to 280
Tensile Strength: Yield (Proof), MPa 150 to 720
130 to 210

Thermal Properties

Latent Heat of Fusion, J/g 220
520
Maximum Temperature: Mechanical, °C 220
170
Melting Completion (Liquidus), °C 1040
590
Melting Onset (Solidus), °C 1030
530
Specific Heat Capacity, J/kg-K 430
880
Thermal Conductivity, W/m-K 58
100 to 140
Thermal Expansion, µm/m-K 18
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 13
26 to 35
Electrical Conductivity: Equal Weight (Specific), % IACS 13
83 to 110

Otherwise Unclassified Properties

Base Metal Price, % relative 29
10
Density, g/cm3 8.4
2.8
Embodied Carbon, kg CO2/kg material 3.2
7.6
Embodied Energy, MJ/kg 52
140
Embodied Water, L/kg 380
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 200
2.1 to 4.6
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 2310
120 to 290
Stiffness to Weight: Axial, points 7.5
14
Stiffness to Weight: Bending, points 19
49
Strength to Weight: Axial, points 16 to 32
22 to 27
Strength to Weight: Bending, points 16 to 26
29 to 34
Thermal Diffusivity, mm2/s 16
42 to 57
Thermal Shock Resistance, points 17 to 34
11 to 13

Alloy Composition

Aluminum (Al), % 7.7 to 8.3
81.8 to 89
Copper (Cu), % 89 to 90.5
3.0 to 4.0
Iron (Fe), % 0
0 to 1.0
Lead (Pb), % 0 to 0.015
0
Magnesium (Mg), % 0
0.050 to 0.5
Manganese (Mn), % 0
0 to 0.5
Nickel (Ni), % 1.8 to 2.2
0 to 0.5
Silicon (Si), % 0
8.0 to 10
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5