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EN 1.5113 Steel vs. 6110A Aluminum

EN 1.5113 steel belongs to the iron alloys classification, while 6110A aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 1.5113 steel and the bottom bar is 6110A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 11 to 18
11 to 18
Fatigue Strength, MPa 220 to 470
140 to 210
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
26
Shear Strength, MPa 360 to 540
220 to 280
Tensile Strength: Ultimate (UTS), MPa 580 to 900
360 to 470
Tensile Strength: Yield (Proof), MPa 320 to 770
250 to 430

Thermal Properties

Latent Heat of Fusion, J/g 260
410
Maximum Temperature: Mechanical, °C 400
190
Melting Completion (Liquidus), °C 1450
650
Melting Onset (Solidus), °C 1410
600
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 52
160
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.2
42
Electrical Conductivity: Equal Weight (Specific), % IACS 8.4
140

Otherwise Unclassified Properties

Base Metal Price, % relative 2.0
9.5
Density, g/cm3 7.8
2.8
Embodied Carbon, kg CO2/kg material 1.4
8.4
Embodied Energy, MJ/kg 19
150
Embodied Water, L/kg 48
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 91 to 96
47 to 58
Resilience: Unit (Modulus of Resilience), kJ/m3 270 to 1570
450 to 1300
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 21 to 32
36 to 47
Strength to Weight: Bending, points 20 to 27
41 to 48
Thermal Diffusivity, mm2/s 14
65
Thermal Shock Resistance, points 17 to 26
16 to 21

Alloy Composition

Aluminum (Al), % 0
94.8 to 98
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0.050 to 0.25
Copper (Cu), % 0
0.3 to 0.8
Iron (Fe), % 97 to 97.5
0 to 0.5
Magnesium (Mg), % 0
0.7 to 1.1
Manganese (Mn), % 1.6 to 1.8
0.3 to 0.9
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.9 to 1.1
0.7 to 1.1
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0 to 0.2
Residuals, % 0
0 to 0.15