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6082 Aluminum vs. 4032 Aluminum

Both 6082 aluminum and 4032 aluminum are aluminum alloys. They have 87% of their average alloy composition in common.

For each property being compared, the top bar is 6082 aluminum and the bottom bar is 4032 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 40 to 95
120
Elastic (Young's, Tensile) Modulus, GPa 69
73
Elongation at Break, % 6.3 to 18
6.7
Fatigue Strength, MPa 55 to 130
110
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
28
Shear Strength, MPa 84 to 220
260
Tensile Strength: Ultimate (UTS), MPa 140 to 340
390
Tensile Strength: Yield (Proof), MPa 85 to 320
320

Thermal Properties

Latent Heat of Fusion, J/g 410
570
Maximum Temperature: Mechanical, °C 170
180
Melting Completion (Liquidus), °C 650
570
Melting Onset (Solidus), °C 580
530
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 160
140
Thermal Expansion, µm/m-K 23
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
34
Electrical Conductivity: Equal Weight (Specific), % IACS 140
120

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
10
Density, g/cm3 2.7
2.6
Embodied Carbon, kg CO2/kg material 8.3
7.8
Embodied Energy, MJ/kg 150
140
Embodied Water, L/kg 1170
1030

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19 to 43
25
Resilience: Unit (Modulus of Resilience), kJ/m3 52 to 710
700
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
53
Strength to Weight: Axial, points 14 to 35
41
Strength to Weight: Bending, points 21 to 40
45
Thermal Diffusivity, mm2/s 67
59
Thermal Shock Resistance, points 6.0 to 15
20

Alloy Composition


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Aluminum (Al), % 95.2 to 98.3
81.1 to 87.2
Chromium (Cr), % 0 to 0.25
0 to 0.1
Copper (Cu), % 0 to 0.1
0.5 to 1.3
Iron (Fe), % 0 to 0.5
0 to 1.0
Magnesium (Mg), % 0.6 to 1.2
0.8 to 1.3
Manganese (Mn), % 0.4 to 1.0
0
Nickel (Ni), % 0
0.5 to 1.3
Silicon (Si), % 0.7 to 1.3
11 to 13.5
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.2
0 to 0.25
Residuals, % 0 to 0.15
0 to 0.15