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2218 Aluminum vs. S32654 Stainless Steel

2218 aluminum belongs to the aluminum alloys classification, while S32654 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 S32654 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 95 to 110
220
Elastic (Young's, Tensile) Modulus, GPa 73
210
Elongation at Break, % 6.8 to 10
45
Fatigue Strength, MPa 110
450
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
82
Shear Strength, MPa 210 to 250
590
Tensile Strength: Ultimate (UTS), MPa 330 to 430
850
Tensile Strength: Yield (Proof), MPa 260 to 310
490

Thermal Properties

Latent Heat of Fusion, J/g 390
310
Maximum Temperature: Mechanical, °C 220
1100
Melting Completion (Liquidus), °C 640
1450
Melting Onset (Solidus), °C 510
1410
Specific Heat Capacity, J/kg-K 870
460
Thermal Conductivity, W/m-K 140
11
Thermal Expansion, µm/m-K 22
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 11
34
Density, g/cm3 3.1
8.0
Embodied Carbon, kg CO2/kg material 8.2
6.4
Embodied Energy, MJ/kg 150
87
Embodied Water, L/kg 1130
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 31
330
Resilience: Unit (Modulus of Resilience), kJ/m3 450 to 650
570
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 30 to 39
29
Strength to Weight: Bending, points 34 to 41
25
Thermal Diffusivity, mm2/s 52
2.9
Thermal Shock Resistance, points 15 to 19
19

Alloy Composition

Aluminum (Al), % 88.8 to 93.6
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0 to 0.1
24 to 25
Copper (Cu), % 3.5 to 4.5
0.3 to 0.6
Iron (Fe), % 0 to 1.0
38.3 to 45.3
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.2
2.0 to 4.0
Molybdenum (Mo), % 0
7.0 to 8.0
Nickel (Ni), % 1.7 to 2.3
21 to 23
Nitrogen (N), % 0
0.45 to 0.55
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.9
0 to 0.5
Sulfur (S), % 0
0 to 0.0050
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0