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5383 Aluminum vs. S82031 Stainless Steel

5383 aluminum belongs to the aluminum alloys classification, while S82031 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 5383 aluminum and the bottom bar is S82031 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 6.7 to 15
39
Fatigue Strength, MPa 130 to 200
490
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Shear Strength, MPa 190 to 220
540
Tensile Strength: Ultimate (UTS), MPa 310 to 370
780
Tensile Strength: Yield (Proof), MPa 150 to 310
570

Thermal Properties

Latent Heat of Fusion, J/g 390
290
Maximum Temperature: Corrosion, °C 65
430
Maximum Temperature: Mechanical, °C 200
980
Melting Completion (Liquidus), °C 650
1430
Melting Onset (Solidus), °C 540
1390
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 130
15
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 97
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 9.0
2.8
Embodied Energy, MJ/kg 160
39
Embodied Water, L/kg 1170
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 40
280
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 690
820
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 32 to 38
28
Strength to Weight: Bending, points 38 to 42
24
Thermal Diffusivity, mm2/s 51
3.9
Thermal Shock Resistance, points 14 to 16
22

Alloy Composition

Aluminum (Al), % 92 to 95.3
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.25
19 to 22
Copper (Cu), % 0 to 0.2
0 to 1.0
Iron (Fe), % 0 to 0.25
68 to 78.3
Magnesium (Mg), % 4.0 to 5.2
0
Manganese (Mn), % 0.7 to 1.0
0 to 2.5
Molybdenum (Mo), % 0
0.6 to 1.4
Nickel (Ni), % 0
2.0 to 4.0
Nitrogen (N), % 0
0.14 to 0.24
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.25
0 to 0.8
Sulfur (S), % 0
0 to 0.0050
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.4
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0