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4032 Aluminum vs. 1050A Aluminum

Both 4032 aluminum and 1050A aluminum are aluminum alloys. They have 85% of their average alloy composition in common.

For each property being compared, the top bar is 4032 aluminum and the bottom bar is 1050A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 120
20 to 45
Elastic (Young's, Tensile) Modulus, GPa 73
68
Elongation at Break, % 6.7
1.1 to 33
Fatigue Strength, MPa 110
22 to 55
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 28
26
Shear Strength, MPa 260
44 to 97
Tensile Strength: Ultimate (UTS), MPa 390
68 to 170
Tensile Strength: Yield (Proof), MPa 320
22 to 150

Thermal Properties

Latent Heat of Fusion, J/g 570
400
Maximum Temperature: Mechanical, °C 180
170
Melting Completion (Liquidus), °C 570
660
Melting Onset (Solidus), °C 530
650
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 140
230
Thermal Expansion, µm/m-K 19
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
59
Electrical Conductivity: Equal Weight (Specific), % IACS 120
200

Otherwise Unclassified Properties

Base Metal Price, % relative 10
9.0
Density, g/cm3 2.6
2.7
Embodied Carbon, kg CO2/kg material 7.8
8.2
Embodied Energy, MJ/kg 140
150
Embodied Water, L/kg 1030
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 25
1.9 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 700
3.7 to 160
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
50
Strength to Weight: Axial, points 41
6.9 to 18
Strength to Weight: Bending, points 45
14 to 25
Thermal Diffusivity, mm2/s 59
94
Thermal Shock Resistance, points 20
3.0 to 7.6

Alloy Composition


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Aluminum (Al), % 81.1 to 87.2
99.5 to 100
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0.5 to 1.3
0 to 0.050
Iron (Fe), % 0 to 1.0
0 to 0.4
Magnesium (Mg), % 0.8 to 1.3
0 to 0.050
Manganese (Mn), % 0
0 to 0.050
Nickel (Ni), % 0.5 to 1.3
0
Silicon (Si), % 11 to 13.5
0 to 0.25
Titanium (Ti), % 0
0 to 0.050
Zinc (Zn), % 0 to 0.25
0 to 0.070
Residuals, % 0 to 0.15
0