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355.0 Aluminum vs. S20161 Stainless Steel

355.0 aluminum belongs to the aluminum alloys classification, while S20161 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, 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 355.0 aluminum and the bottom bar is S20161 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 72 to 83
250
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 1.5 to 2.6
46
Fatigue Strength, MPa 55 to 70
360
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
76
Shear Strength, MPa 150 to 240
690
Tensile Strength: Ultimate (UTS), MPa 200 to 260
980
Tensile Strength: Yield (Proof), MPa 150 to 190
390

Thermal Properties

Latent Heat of Fusion, J/g 470
330
Maximum Temperature: Mechanical, °C 180
870
Melting Completion (Liquidus), °C 620
1380
Melting Onset (Solidus), °C 560
1330
Specific Heat Capacity, J/kg-K 890
490
Thermal Conductivity, W/m-K 150 to 170
15
Thermal Expansion, µm/m-K 22
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38 to 43
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 120 to 140
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
7.5
Embodied Carbon, kg CO2/kg material 8.0
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1120
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.7 to 5.9
360
Resilience: Unit (Modulus of Resilience), kJ/m3 150 to 250
390
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
26
Strength to Weight: Axial, points 20 to 27
36
Strength to Weight: Bending, points 28 to 33
29
Thermal Diffusivity, mm2/s 60 to 69
4.0
Thermal Shock Resistance, points 9.1 to 12
22

Alloy Composition

Aluminum (Al), % 90.3 to 94.1
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0 to 0.25
15 to 18
Copper (Cu), % 1.0 to 1.5
0
Iron (Fe), % 0 to 0.6
65.6 to 73.9
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.5
4.0 to 6.0
Nickel (Ni), % 0
4.0 to 6.0
Nitrogen (N), % 0
0.080 to 0.2
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 4.5 to 5.5
3.0 to 4.0
Sulfur (S), % 0
0 to 0.040
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0