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C33000 Brass vs. 6016 Aluminum

C33000 brass 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 (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 C33000 brass and the bottom bar is 6016 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
69
Elongation at Break, % 7.0 to 60
11 to 27
Poisson's Ratio 0.31
0.33
Shear Modulus, GPa 40
26
Shear Strength, MPa 240 to 300
130 to 170
Tensile Strength: Ultimate (UTS), MPa 320 to 520
200 to 280
Tensile Strength: Yield (Proof), MPa 110 to 450
110 to 210

Thermal Properties

Latent Heat of Fusion, J/g 180
410
Maximum Temperature: Mechanical, °C 130
160
Melting Completion (Liquidus), °C 940
660
Melting Onset (Solidus), °C 900
610
Specific Heat Capacity, J/kg-K 390
900
Thermal Conductivity, W/m-K 120
190 to 210
Thermal Expansion, µm/m-K 20
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
48 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 29
160 to 180

Otherwise Unclassified Properties

Base Metal Price, % relative 24
9.5
Density, g/cm3 8.2
2.7
Embodied Carbon, kg CO2/kg material 2.7
8.2
Embodied Energy, MJ/kg 45
150
Embodied Water, L/kg 320
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 35 to 150
29 to 47
Resilience: Unit (Modulus of Resilience), kJ/m3 60 to 950
82 to 340
Stiffness to Weight: Axial, points 7.2
14
Stiffness to Weight: Bending, points 19
51
Strength to Weight: Axial, points 11 to 18
21 to 29
Strength to Weight: Bending, points 13 to 18
29 to 35
Thermal Diffusivity, mm2/s 37
77 to 86
Thermal Shock Resistance, points 11 to 17
9.1 to 12

Alloy Composition

Aluminum (Al), % 0
96.4 to 98.8
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 65 to 68
0 to 0.2
Iron (Fe), % 0 to 0.070
0 to 0.5
Lead (Pb), % 0.25 to 0.7
0
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), % 30.8 to 34.8
0 to 0.2
Residuals, % 0
0 to 0.15