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EN 1.7366 Steel vs. 5059 Aluminum

EN 1.7366 steel belongs to the iron alloys classification, while 5059 aluminum belongs to the aluminum 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 EN 1.7366 steel and the bottom bar is 5059 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 17 to 19
11 to 25
Fatigue Strength, MPa 160 to 320
170 to 240
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
26
Shear Strength, MPa 290 to 440
220 to 250
Tensile Strength: Ultimate (UTS), MPa 460 to 710
350 to 410
Tensile Strength: Yield (Proof), MPa 230 to 480
170 to 300

Thermal Properties

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

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.1
29
Electrical Conductivity: Equal Weight (Specific), % IACS 9.3
95

Otherwise Unclassified Properties

Base Metal Price, % relative 4.3
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.7
9.1
Embodied Energy, MJ/kg 23
160
Embodied Water, L/kg 69
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 74 to 110
42 to 75
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 600
220 to 650
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 16 to 25
36 to 42
Strength to Weight: Bending, points 17 to 23
41 to 45
Thermal Diffusivity, mm2/s 11
44
Thermal Shock Resistance, points 13 to 20
16 to 18

Alloy Composition

Aluminum (Al), % 0
89.9 to 94
Carbon (C), % 0 to 0.18
0
Chromium (Cr), % 4.0 to 6.0
0 to 0.25
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 91.9 to 95.3
0 to 0.5
Magnesium (Mg), % 0
5.0 to 6.0
Manganese (Mn), % 0.3 to 0.8
0.6 to 1.2
Molybdenum (Mo), % 0.45 to 0.65
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.4
0 to 0.45
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0.4 to 0.9
Zirconium (Zr), % 0
0.050 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants