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C27200 Brass vs. 6016 Aluminum

C27200 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 (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 C27200 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, % 10 to 50
11 to 27
Poisson's Ratio 0.31
0.33
Shear Modulus, GPa 40
26
Shear Strength, MPa 230 to 320
130 to 170
Tensile Strength: Ultimate (UTS), MPa 370 to 590
200 to 280
Tensile Strength: Yield (Proof), MPa 150 to 410
110 to 210

Thermal Properties

Latent Heat of Fusion, J/g 170
410
Maximum Temperature: Mechanical, °C 130
160
Melting Completion (Liquidus), °C 920
660
Melting Onset (Solidus), °C 870
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 28
48 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 31
160 to 180

Otherwise Unclassified Properties

Base Metal Price, % relative 24
9.5
Density, g/cm3 8.1
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 30 to 270
29 to 47
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 810
82 to 340
Stiffness to Weight: Axial, points 7.2
14
Stiffness to Weight: Bending, points 19
51
Strength to Weight: Axial, points 13 to 20
21 to 29
Strength to Weight: Bending, points 14 to 19
29 to 35
Thermal Diffusivity, mm2/s 37
77 to 86
Thermal Shock Resistance, points 12 to 20
9.1 to 12

Alloy Composition

Aluminum (Al), % 0
96.4 to 98.8
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 62 to 65
0 to 0.2
Iron (Fe), % 0 to 0.070
0 to 0.5
Lead (Pb), % 0 to 0.070
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), % 34.6 to 38
0 to 0.2
Residuals, % 0
0 to 0.15