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355.0 Aluminum vs. C61000 Bronze

355.0 aluminum belongs to the aluminum alloys classification, while C61000 bronze belongs to the copper 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 355.0 aluminum and the bottom bar is C61000 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
110
Elongation at Break, % 1.5 to 2.6
29 to 50
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 27
42
Shear Strength, MPa 150 to 240
280 to 300
Tensile Strength: Ultimate (UTS), MPa 200 to 260
390 to 460
Tensile Strength: Yield (Proof), MPa 150 to 190
150 to 190

Thermal Properties

Latent Heat of Fusion, J/g 470
220
Maximum Temperature: Mechanical, °C 180
210
Melting Completion (Liquidus), °C 620
1040
Melting Onset (Solidus), °C 560
990
Specific Heat Capacity, J/kg-K 890
420
Thermal Conductivity, W/m-K 150 to 170
69
Thermal Expansion, µm/m-K 22
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38 to 43
15
Electrical Conductivity: Equal Weight (Specific), % IACS 120 to 140
16

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
29
Density, g/cm3 2.7
8.5
Embodied Carbon, kg CO2/kg material 8.0
3.0
Embodied Energy, MJ/kg 150
49
Embodied Water, L/kg 1120
370

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.7 to 5.9
110 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 150 to 250
100 to 160
Stiffness to Weight: Axial, points 14
7.4
Stiffness to Weight: Bending, points 51
19
Strength to Weight: Axial, points 20 to 27
13 to 15
Strength to Weight: Bending, points 28 to 33
14 to 16
Thermal Diffusivity, mm2/s 60 to 69
19
Thermal Shock Resistance, points 9.1 to 12
14 to 16

Alloy Composition

Aluminum (Al), % 90.3 to 94.1
6.0 to 8.5
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 1.0 to 1.5
90.2 to 94
Iron (Fe), % 0 to 0.6
0 to 0.5
Lead (Pb), % 0
0 to 0.020
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.5
0
Silicon (Si), % 4.5 to 5.5
0 to 0.1
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0 to 0.2
Residuals, % 0
0 to 0.5