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C61900 Bronze vs. 356.0 Aluminum

C61900 bronze belongs to the copper alloys classification, while 356.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 C61900 bronze and the bottom bar is 356.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
70
Elongation at Break, % 21 to 32
2.0 to 3.8
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 43
27
Shear Strength, MPa 370 to 410
140 to 190
Tensile Strength: Ultimate (UTS), MPa 570 to 650
160 to 240
Tensile Strength: Yield (Proof), MPa 230 to 310
100 to 190

Thermal Properties

Latent Heat of Fusion, J/g 230
500
Maximum Temperature: Mechanical, °C 220
170
Melting Completion (Liquidus), °C 1050
620
Melting Onset (Solidus), °C 1040
570
Specific Heat Capacity, J/kg-K 440
900
Thermal Conductivity, W/m-K 79
150 to 170
Thermal Expansion, µm/m-K 18
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
40 to 43
Electrical Conductivity: Equal Weight (Specific), % IACS 11
140 to 150

Otherwise Unclassified Properties

Base Metal Price, % relative 28
9.5
Density, g/cm3 8.3
2.6
Embodied Carbon, kg CO2/kg material 3.1
8.0
Embodied Energy, MJ/kg 51
150
Embodied Water, L/kg 380
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 150
3.2 to 8.2
Resilience: Unit (Modulus of Resilience), kJ/m3 230 to 430
70 to 250
Stiffness to Weight: Axial, points 7.6
15
Stiffness to Weight: Bending, points 19
53
Strength to Weight: Axial, points 19 to 22
17 to 26
Strength to Weight: Bending, points 18 to 20
25 to 33
Thermal Diffusivity, mm2/s 22
64 to 71
Thermal Shock Resistance, points 20 to 23
7.6 to 11

Alloy Composition


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Aluminum (Al), % 8.5 to 10
90.1 to 93.3
Copper (Cu), % 83.6 to 88.5
0 to 0.25
Iron (Fe), % 3.0 to 4.5
0 to 0.6
Lead (Pb), % 0 to 0.020
0
Magnesium (Mg), % 0
0.2 to 0.45
Manganese (Mn), % 0
0 to 0.35
Silicon (Si), % 0
6.5 to 7.5
Tin (Sn), % 0 to 0.6
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0 to 0.8
0 to 0.35
Residuals, % 0 to 0.5
0 to 0.15