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5082 Aluminum vs. C42200 Brass

5082 aluminum belongs to the aluminum alloys classification, while C42200 brass belongs to the copper 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 5082 aluminum and the bottom bar is C42200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
110
Elongation at Break, % 1.1
2.0 to 46
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 25
42
Shear Strength, MPa 210 to 230
210 to 350
Tensile Strength: Ultimate (UTS), MPa 380 to 400
300 to 610
Tensile Strength: Yield (Proof), MPa 300 to 340
100 to 570

Thermal Properties

Latent Heat of Fusion, J/g 400
200
Maximum Temperature: Mechanical, °C 180
170
Melting Completion (Liquidus), °C 640
1040
Melting Onset (Solidus), °C 560
1020
Specific Heat Capacity, J/kg-K 910
380
Thermal Conductivity, W/m-K 130
130
Thermal Expansion, µm/m-K 24
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
31
Electrical Conductivity: Equal Weight (Specific), % IACS 110
32

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
29
Density, g/cm3 2.7
8.6
Embodied Carbon, kg CO2/kg material 8.9
2.7
Embodied Energy, MJ/kg 150
44
Embodied Water, L/kg 1180
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 4.3
12 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 670 to 870
49 to 1460
Stiffness to Weight: Axial, points 14
7.2
Stiffness to Weight: Bending, points 51
19
Strength to Weight: Axial, points 39 to 41
9.5 to 19
Strength to Weight: Bending, points 43 to 45
11 to 18
Thermal Diffusivity, mm2/s 54
39
Thermal Shock Resistance, points 17 to 18
10 to 21

Alloy Composition

Aluminum (Al), % 93.5 to 96
0
Chromium (Cr), % 0 to 0.15
0
Copper (Cu), % 0 to 0.15
86 to 89
Iron (Fe), % 0 to 0.35
0 to 0.050
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 4.0 to 5.0
0
Manganese (Mn), % 0 to 0.15
0
Phosphorus (P), % 0
0 to 0.35
Silicon (Si), % 0 to 0.2
0
Tin (Sn), % 0
0.8 to 1.4
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.25
8.7 to 13.2
Residuals, % 0
0 to 0.5