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A360.0 Aluminum vs. C23000 Brass

A360.0 aluminum belongs to the aluminum alloys classification, while C23000 brass belongs to the copper alloys. There are 30 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 A360.0 aluminum and the bottom bar is C23000 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
110
Elongation at Break, % 1.6 to 5.0
2.9 to 47
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 27
42
Shear Strength, MPa 180
220 to 340
Tensile Strength: Ultimate (UTS), MPa 180 to 320
280 to 590
Tensile Strength: Yield (Proof), MPa 170 to 260
83 to 480

Thermal Properties

Latent Heat of Fusion, J/g 530
190
Maximum Temperature: Mechanical, °C 170
170
Melting Completion (Liquidus), °C 680
1030
Melting Onset (Solidus), °C 590
990
Specific Heat Capacity, J/kg-K 900
390
Thermal Conductivity, W/m-K 110
160
Thermal Expansion, µm/m-K 21
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
37
Electrical Conductivity: Equal Weight (Specific), % IACS 100
39

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
28
Calomel Potential, mV -700
-350
Density, g/cm3 2.6
8.6
Embodied Carbon, kg CO2/kg material 7.8
2.6
Embodied Energy, MJ/kg 150
43
Embodied Water, L/kg 1070
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 13
6.2 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 470
31 to 1040
Stiffness to Weight: Axial, points 15
7.2
Stiffness to Weight: Bending, points 53
19
Strength to Weight: Axial, points 19 to 34
8.9 to 19
Strength to Weight: Bending, points 27 to 39
11 to 18
Thermal Diffusivity, mm2/s 48
48
Thermal Shock Resistance, points 8.5 to 15
9.4 to 20

Alloy Composition

Aluminum (Al), % 85.8 to 90.6
0
Copper (Cu), % 0 to 0.6
84 to 86
Iron (Fe), % 0 to 1.3
0 to 0.050
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.35
0
Nickel (Ni), % 0 to 0.5
0
Silicon (Si), % 9.0 to 10
0
Tin (Sn), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.5
13.7 to 16
Residuals, % 0
0 to 0.2