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5059 Aluminum vs. EN 1.7362 Steel

5059 aluminum belongs to the aluminum alloys classification, while EN 1.7362 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 5059 aluminum and the bottom bar is EN 1.7362 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 11 to 25
21 to 22
Fatigue Strength, MPa 170 to 240
140 to 250
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 220 to 250
320 to 370
Tensile Strength: Ultimate (UTS), MPa 350 to 410
510 to 600
Tensile Strength: Yield (Proof), MPa 170 to 300
200 to 360

Thermal Properties

Latent Heat of Fusion, J/g 390
260
Maximum Temperature: Mechanical, °C 210
510
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 510
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 110
40
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
8.1
Electrical Conductivity: Equal Weight (Specific), % IACS 95
9.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.5
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.1
1.8
Embodied Energy, MJ/kg 160
23
Embodied Water, L/kg 1160
69

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 75
90 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 650
100 to 340
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 36 to 42
18 to 21
Strength to Weight: Bending, points 41 to 45
18 to 20
Thermal Diffusivity, mm2/s 44
11
Thermal Shock Resistance, points 16 to 18
14 to 17

Alloy Composition


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Aluminum (Al), % 89.9 to 94
0
Carbon (C), % 0
0.1 to 0.15
Chromium (Cr), % 0 to 0.25
4.0 to 6.0
Copper (Cu), % 0 to 0.25
0 to 0.3
Iron (Fe), % 0 to 0.5
91.5 to 95.2
Magnesium (Mg), % 5.0 to 6.0
0
Manganese (Mn), % 0.6 to 1.2
0.3 to 0.6
Molybdenum (Mo), % 0
0.45 to 0.65
Nickel (Ni), % 0
0 to 0.3
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.45
0 to 0.5
Sulfur (S), % 0
0 to 0.0050
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0.4 to 0.9
0
Zirconium (Zr), % 0.050 to 0.25
0
Residuals, % 0 to 0.15
0

Comparable Variants