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5083 Aluminum vs. EN 1.4006 Stainless Steel

5083 aluminum belongs to the aluminum alloys classification, while EN 1.4006 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 5083 aluminum and the bottom bar is EN 1.4006 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 1.1 to 17
16 to 23
Fatigue Strength, MPa 93 to 190
150 to 300
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 170 to 220
370 to 460
Tensile Strength: Ultimate (UTS), MPa 290 to 390
590 to 750
Tensile Strength: Yield (Proof), MPa 110 to 340
230 to 510

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Corrosion, °C 65
390
Maximum Temperature: Mechanical, °C 190
740
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 580
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 120
30
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 96
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.0
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.9
1.9
Embodied Energy, MJ/kg 150
27
Embodied Water, L/kg 1170
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.2 to 42
99 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 95 to 860
140 to 660
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 29 to 40
21 to 27
Strength to Weight: Bending, points 36 to 44
20 to 24
Thermal Diffusivity, mm2/s 48
8.1
Thermal Shock Resistance, points 12 to 17
21 to 26

Alloy Composition


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Aluminum (Al), % 92.4 to 95.6
0
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0.050 to 0.25
11.5 to 13.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.4
83.1 to 88.4
Magnesium (Mg), % 4.0 to 4.9
0
Manganese (Mn), % 0.4 to 1.0
0 to 1.5
Nickel (Ni), % 0
0 to 0.75
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.4
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0

Comparable Variants