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2618A Aluminum vs. SAE-AISI 1140 Steel

2618A aluminum belongs to the aluminum alloys classification, while SAE-AISI 1140 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 2618A aluminum and the bottom bar is SAE-AISI 1140 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 4.5
14 to 18
Fatigue Strength, MPa 120
230 to 370
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
72
Shear Strength, MPa 260
370 to 420
Tensile Strength: Ultimate (UTS), MPa 440
600 to 700
Tensile Strength: Yield (Proof), MPa 410
340 to 570

Thermal Properties

Latent Heat of Fusion, J/g 390
250
Maximum Temperature: Mechanical, °C 230
400
Melting Completion (Liquidus), °C 670
1460
Melting Onset (Solidus), °C 560
1420
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 150
51
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
7.0
Electrical Conductivity: Equal Weight (Specific), % IACS 110
8.1

Otherwise Unclassified Properties

Base Metal Price, % relative 11
1.8
Density, g/cm3 3.0
7.8
Embodied Carbon, kg CO2/kg material 8.4
1.4
Embodied Energy, MJ/kg 150
18
Embodied Water, L/kg 1150
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19
89 to 93
Resilience: Unit (Modulus of Resilience), kJ/m3 1180
310 to 870
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 41
21 to 25
Strength to Weight: Bending, points 44
20 to 22
Thermal Diffusivity, mm2/s 59
14
Thermal Shock Resistance, points 19
18 to 21

Alloy Composition

Aluminum (Al), % 91.5 to 95.2
0
Carbon (C), % 0
0.37 to 0.44
Copper (Cu), % 1.8 to 2.7
0
Iron (Fe), % 0.9 to 1.4
98.4 to 98.9
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.25
0.7 to 1.0
Nickel (Ni), % 0.8 to 1.4
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.15 to 0.25
0
Sulfur (S), % 0
0.080 to 0.13
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.15
0
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0