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4032 Aluminum vs. 5754 Aluminum

Both 4032 aluminum and 5754 aluminum are aluminum alloys. They have 86% of their average alloy composition in common.

For each property being compared, the top bar is 4032 aluminum and the bottom bar is 5754 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 120
52 to 88
Elastic (Young's, Tensile) Modulus, GPa 73
68
Elongation at Break, % 6.7
2.0 to 19
Fatigue Strength, MPa 110
66 to 140
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 28
26
Shear Strength, MPa 260
120 to 190
Tensile Strength: Ultimate (UTS), MPa 390
200 to 330
Tensile Strength: Yield (Proof), MPa 320
80 to 280

Thermal Properties

Latent Heat of Fusion, J/g 570
400
Maximum Temperature: Mechanical, °C 180
190
Melting Completion (Liquidus), °C 570
650
Melting Onset (Solidus), °C 530
600
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 140
130
Thermal Expansion, µm/m-K 19
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
33
Electrical Conductivity: Equal Weight (Specific), % IACS 120
110

Otherwise Unclassified Properties

Base Metal Price, % relative 10
9.5
Density, g/cm3 2.6
2.7
Embodied Carbon, kg CO2/kg material 7.8
8.7
Embodied Energy, MJ/kg 140
150
Embodied Water, L/kg 1030
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 25
6.1 to 32
Resilience: Unit (Modulus of Resilience), kJ/m3 700
47 to 580
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
50
Strength to Weight: Axial, points 41
21 to 34
Strength to Weight: Bending, points 45
28 to 39
Thermal Diffusivity, mm2/s 59
54
Thermal Shock Resistance, points 20
8.9 to 14

Alloy Composition

Aluminum (Al), % 81.1 to 87.2
94.2 to 97.4
Chromium (Cr), % 0 to 0.1
0 to 0.3
Copper (Cu), % 0.5 to 1.3
0 to 0.1
Iron (Fe), % 0 to 1.0
0 to 0.4
Magnesium (Mg), % 0.8 to 1.3
2.6 to 3.6
Manganese (Mn), % 0
0 to 0.5
Nickel (Ni), % 0.5 to 1.3
0
Silicon (Si), % 11 to 13.5
0 to 0.4
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0 to 0.25
0 to 0.2
Residuals, % 0
0 to 0.15