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2618 Aluminum vs. 4032 Aluminum

Both 2618 aluminum and 4032 aluminum are aluminum alloys. They have 88% of their average alloy composition in common.

For each property being compared, the top bar is 2618 aluminum and the bottom bar is 4032 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 120
120
Elastic (Young's, Tensile) Modulus, GPa 71
73
Elongation at Break, % 5.8
6.7
Fatigue Strength, MPa 110
110
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 27
28
Shear Strength, MPa 260
260
Tensile Strength: Ultimate (UTS), MPa 420
390
Tensile Strength: Yield (Proof), MPa 350
320

Thermal Properties

Latent Heat of Fusion, J/g 390
570
Maximum Temperature: Mechanical, °C 210
180
Melting Completion (Liquidus), °C 640
570
Melting Onset (Solidus), °C 550
530
Specific Heat Capacity, J/kg-K 880
900
Thermal Conductivity, W/m-K 160
140
Thermal Expansion, µm/m-K 22
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
34
Electrical Conductivity: Equal Weight (Specific), % IACS 110
120

Otherwise Unclassified Properties

Base Metal Price, % relative 11
10
Density, g/cm3 2.9
2.6
Embodied Carbon, kg CO2/kg material 8.3
7.8
Embodied Energy, MJ/kg 150
140
Embodied Water, L/kg 1150
1030

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23
25
Resilience: Unit (Modulus of Resilience), kJ/m3 850
700
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 47
53
Strength to Weight: Axial, points 40
41
Strength to Weight: Bending, points 42
45
Thermal Diffusivity, mm2/s 62
59
Thermal Shock Resistance, points 19
20

Alloy Composition

Aluminum (Al), % 92.4 to 94.9
81.1 to 87.2
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 1.9 to 2.7
0.5 to 1.3
Iron (Fe), % 0.9 to 1.3
0 to 1.0
Magnesium (Mg), % 1.3 to 1.8
0.8 to 1.3
Nickel (Ni), % 0.9 to 1.2
0.5 to 1.3
Silicon (Si), % 0.1 to 0.25
11 to 13.5
Titanium (Ti), % 0.040 to 0.1
0
Zinc (Zn), % 0 to 0.1
0 to 0.25
Residuals, % 0
0 to 0.15