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5059 Aluminum vs. EN 1.7380 Steel

5059 aluminum belongs to the aluminum alloys classification, while EN 1.7380 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 1.7380 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 11 to 25
19 to 20
Fatigue Strength, MPa 170 to 240
200 to 230
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 220 to 250
330 to 350
Tensile Strength: Ultimate (UTS), MPa 350 to 410
540 to 550
Tensile Strength: Yield (Proof), MPa 170 to 300
290 to 330

Thermal Properties

Latent Heat of Fusion, J/g 390
260
Maximum Temperature: Mechanical, °C 210
460
Melting Completion (Liquidus), °C 650
1470
Melting Onset (Solidus), °C 510
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 110
39
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 95
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.8
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 9.1
1.8
Embodied Energy, MJ/kg 160
23
Embodied Water, L/kg 1160
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 75
87 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 650
230 to 280
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 36 to 42
19 to 20
Strength to Weight: Bending, points 41 to 45
19
Thermal Diffusivity, mm2/s 44
11
Thermal Shock Resistance, points 16 to 18
15 to 16

Alloy Composition

Aluminum (Al), % 89.9 to 94
0
Carbon (C), % 0
0.080 to 0.14
Chromium (Cr), % 0 to 0.25
2.0 to 2.5
Copper (Cu), % 0 to 0.25
0 to 0.3
Iron (Fe), % 0 to 0.5
94.6 to 96.6
Magnesium (Mg), % 5.0 to 6.0
0
Manganese (Mn), % 0.6 to 1.2
0.4 to 0.8
Molybdenum (Mo), % 0
0.9 to 1.1
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 0.010
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