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6016 Aluminum vs. S20432 Stainless Steel

6016 aluminum belongs to the aluminum alloys classification, while S20432 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 6016 aluminum and the bottom bar is S20432 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 55 to 80
170
Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 11 to 27
45
Fatigue Strength, MPa 68 to 89
210
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 130 to 170
400
Tensile Strength: Ultimate (UTS), MPa 200 to 280
580
Tensile Strength: Yield (Proof), MPa 110 to 210
230

Thermal Properties

Latent Heat of Fusion, J/g 410
280
Maximum Temperature: Mechanical, °C 160
900
Melting Completion (Liquidus), °C 660
1410
Melting Onset (Solidus), °C 610
1370
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 190 to 210
15
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 48 to 54
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 160 to 180
2.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.2
2.7
Embodied Energy, MJ/kg 150
38
Embodied Water, L/kg 1180
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 47
210
Resilience: Unit (Modulus of Resilience), kJ/m3 82 to 340
140
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 21 to 29
21
Strength to Weight: Bending, points 29 to 35
20
Thermal Diffusivity, mm2/s 77 to 86
4.0
Thermal Shock Resistance, points 9.1 to 12
13

Alloy Composition

Aluminum (Al), % 96.4 to 98.8
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0 to 0.1
17 to 18
Copper (Cu), % 0 to 0.2
2.0 to 3.0
Iron (Fe), % 0 to 0.5
66.7 to 74
Magnesium (Mg), % 0.25 to 0.6
0
Manganese (Mn), % 0 to 0.2
3.0 to 5.0
Nickel (Ni), % 0
4.0 to 6.0
Nitrogen (N), % 0
0.050 to 0.2
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 1.0 to 1.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0