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2218 Aluminum vs. S35140 Stainless Steel

2218 aluminum belongs to the aluminum alloys classification, while S35140 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 2218 aluminum and the bottom bar is S35140 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 95 to 110
210
Elastic (Young's, Tensile) Modulus, GPa 73
200
Elongation at Break, % 6.8 to 10
34
Fatigue Strength, MPa 110
250
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
78
Shear Strength, MPa 210 to 250
460
Tensile Strength: Ultimate (UTS), MPa 330 to 430
690
Tensile Strength: Yield (Proof), MPa 260 to 310
310

Thermal Properties

Latent Heat of Fusion, J/g 390
300
Maximum Temperature: Mechanical, °C 220
1100
Melting Completion (Liquidus), °C 640
1420
Melting Onset (Solidus), °C 510
1370
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 140
14
Thermal Expansion, µm/m-K 22
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 110
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 11
31
Density, g/cm3 3.1
8.0
Embodied Carbon, kg CO2/kg material 8.2
5.5
Embodied Energy, MJ/kg 150
78
Embodied Water, L/kg 1130
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 31
190
Resilience: Unit (Modulus of Resilience), kJ/m3 450 to 650
250
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 30 to 39
24
Strength to Weight: Bending, points 34 to 41
22
Thermal Diffusivity, mm2/s 52
3.7
Thermal Shock Resistance, points 15 to 19
16

Alloy Composition


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Aluminum (Al), % 88.8 to 93.6
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 to 0.1
20 to 22
Copper (Cu), % 3.5 to 4.5
0
Iron (Fe), % 0 to 1.0
44.1 to 52.7
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.2
1.0 to 3.0
Molybdenum (Mo), % 0
1.0 to 2.0
Nickel (Ni), % 1.7 to 2.3
25 to 27
Niobium (Nb), % 0
0.25 to 0.75
Nitrogen (N), % 0
0.080 to 0.2
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.9
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0