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5154A Aluminum vs. 2618 Aluminum

Both 5154A aluminum and 2618 aluminum are aluminum alloys. They have a very high 96% of their average alloy composition in common.

For each property being compared, the top bar is 5154A aluminum and the bottom bar is 2618 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 58 to 100
120
Elastic (Young's, Tensile) Modulus, GPa 68
71
Elongation at Break, % 1.1 to 19
5.8
Fatigue Strength, MPa 83 to 160
110
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
27
Shear Strength, MPa 140 to 210
260
Tensile Strength: Ultimate (UTS), MPa 230 to 370
420
Tensile Strength: Yield (Proof), MPa 96 to 320
350

Thermal Properties

Latent Heat of Fusion, J/g 400
390
Maximum Temperature: Mechanical, °C 190
210
Melting Completion (Liquidus), °C 650
640
Melting Onset (Solidus), °C 600
550
Specific Heat Capacity, J/kg-K 900
880
Thermal Conductivity, W/m-K 130
160
Thermal Expansion, µm/m-K 24
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
37
Electrical Conductivity: Equal Weight (Specific), % IACS 110
110

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
11
Density, g/cm3 2.7
2.9
Embodied Carbon, kg CO2/kg material 8.8
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1180
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 36
23
Resilience: Unit (Modulus of Resilience), kJ/m3 68 to 760
850
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
47
Strength to Weight: Axial, points 24 to 38
40
Strength to Weight: Bending, points 31 to 43
42
Thermal Diffusivity, mm2/s 53
62
Thermal Shock Resistance, points 10 to 16
19

Alloy Composition

Aluminum (Al), % 93.7 to 96.9
92.4 to 94.9
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 0 to 0.1
1.9 to 2.7
Iron (Fe), % 0 to 0.5
0.9 to 1.3
Magnesium (Mg), % 3.1 to 3.9
1.3 to 1.8
Manganese (Mn), % 0 to 0.5
0
Nickel (Ni), % 0
0.9 to 1.2
Silicon (Si), % 0 to 0.5
0.1 to 0.25
Titanium (Ti), % 0 to 0.2
0.040 to 0.1
Zinc (Zn), % 0 to 0.2
0 to 0.1
Residuals, % 0
0 to 0.15