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5457 Aluminum vs. 4032 Aluminum

Both 5457 aluminum and 4032 aluminum are aluminum alloys. They have 85% of their average alloy composition in common.

For each property being compared, the top bar is 5457 aluminum and the bottom bar is 4032 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 32 to 55
120
Elastic (Young's, Tensile) Modulus, GPa 68
73
Elongation at Break, % 6.0 to 22
6.7
Fatigue Strength, MPa 55 to 98
110
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
28
Shear Strength, MPa 85 to 130
260
Tensile Strength: Ultimate (UTS), MPa 130 to 210
390
Tensile Strength: Yield (Proof), MPa 50 to 190
320

Thermal Properties

Latent Heat of Fusion, J/g 400
570
Maximum Temperature: Mechanical, °C 180
180
Melting Completion (Liquidus), °C 660
570
Melting Onset (Solidus), °C 630
530
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 180
140
Thermal Expansion, µm/m-K 24
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 46
34
Electrical Conductivity: Equal Weight (Specific), % IACS 150
120

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
10
Density, g/cm3 2.7
2.6
Embodied Carbon, kg CO2/kg material 8.4
7.8
Embodied Energy, MJ/kg 160
140
Embodied Water, L/kg 1190
1030

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 23
25
Resilience: Unit (Modulus of Resilience), kJ/m3 18 to 250
700
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
53
Strength to Weight: Axial, points 13 to 21
41
Strength to Weight: Bending, points 21 to 28
45
Thermal Diffusivity, mm2/s 72
59
Thermal Shock Resistance, points 5.7 to 9.0
20

Alloy Composition


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Aluminum (Al), % 97.8 to 99.05
81.1 to 87.2
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0 to 0.2
0.5 to 1.3
Iron (Fe), % 0 to 0.1
0 to 1.0
Magnesium (Mg), % 0.8 to 1.2
0.8 to 1.3
Manganese (Mn), % 0.15 to 0.45
0
Nickel (Ni), % 0
0.5 to 1.3
Silicon (Si), % 0 to 0.080
11 to 13.5
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.050
0 to 0.25
Residuals, % 0 to 0.1
0 to 0.15