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EN 1.5113 Steel vs. 6014 Aluminum

EN 1.5113 steel belongs to the iron alloys classification, while 6014 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 6014 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 11 to 18
9.1 to 17
Fatigue Strength, MPa 220 to 470
43 to 79
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
26
Shear Strength, MPa 360 to 540
96 to 150
Tensile Strength: Ultimate (UTS), MPa 580 to 900
160 to 260
Tensile Strength: Yield (Proof), MPa 320 to 770
80 to 200

Thermal Properties

Latent Heat of Fusion, J/g 260
400
Maximum Temperature: Mechanical, °C 400
180
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1410
620
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 52
200
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.2
53
Electrical Conductivity: Equal Weight (Specific), % IACS 8.4
180

Otherwise Unclassified Properties

Base Metal Price, % relative 2.0
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.4
8.6
Embodied Energy, MJ/kg 19
160
Embodied Water, L/kg 48
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 91 to 96
22
Resilience: Unit (Modulus of Resilience), kJ/m3 270 to 1570
46 to 300
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 21 to 32
16 to 26
Strength to Weight: Bending, points 20 to 27
24 to 33
Thermal Diffusivity, mm2/s 14
83
Thermal Shock Resistance, points 17 to 26
7.0 to 11

Alloy Composition

Aluminum (Al), % 0
97.1 to 99.2
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.2
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 97 to 97.5
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.8
Manganese (Mn), % 1.6 to 1.8
0.050 to 0.2
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.9 to 1.1
0.3 to 0.6
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.1
Vanadium (V), % 0
0.050 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15