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4032 Aluminum vs. 5154A Aluminum

Both 4032 aluminum and 5154A 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 5154A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 120
58 to 100
Elastic (Young's, Tensile) Modulus, GPa 73
68
Elongation at Break, % 6.7
1.1 to 19
Fatigue Strength, MPa 110
83 to 160
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 28
26
Shear Strength, MPa 260
140 to 210
Tensile Strength: Ultimate (UTS), MPa 390
230 to 370
Tensile Strength: Yield (Proof), MPa 320
96 to 320

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
32
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
8.8
Embodied Energy, MJ/kg 140
150
Embodied Water, L/kg 1030
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 25
4.0 to 36
Resilience: Unit (Modulus of Resilience), kJ/m3 700
68 to 760
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
51
Strength to Weight: Axial, points 41
24 to 38
Strength to Weight: Bending, points 45
31 to 43
Thermal Diffusivity, mm2/s 59
53
Thermal Shock Resistance, points 20
10 to 16

Alloy Composition

Aluminum (Al), % 81.1 to 87.2
93.7 to 96.9
Chromium (Cr), % 0 to 0.1
0 to 0.25
Copper (Cu), % 0.5 to 1.3
0 to 0.1
Iron (Fe), % 0 to 1.0
0 to 0.5
Magnesium (Mg), % 0.8 to 1.3
3.1 to 3.9
Manganese (Mn), % 0
0 to 0.5
Nickel (Ni), % 0.5 to 1.3
0
Silicon (Si), % 11 to 13.5
0 to 0.5
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0 to 0.25
0 to 0.2
Residuals, % 0
0 to 0.15