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2014A Aluminum vs. EN 1.5508 Steel

2014A aluminum belongs to the aluminum alloys classification, while EN 1.5508 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 2014A aluminum and the bottom bar is EN 1.5508 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 6.2 to 16
11 to 20
Fatigue Strength, MPa 93 to 150
210 to 320
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
73
Shear Strength, MPa 130 to 290
300 to 360
Tensile Strength: Ultimate (UTS), MPa 210 to 490
420 to 1460
Tensile Strength: Yield (Proof), MPa 110 to 430
310 to 490

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 210
400
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 510
1420
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 150
51
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
7.1
Electrical Conductivity: Equal Weight (Specific), % IACS 110
8.2

Otherwise Unclassified Properties

Base Metal Price, % relative 11
1.9
Density, g/cm3 3.0
7.8
Embodied Carbon, kg CO2/kg material 8.1
1.4
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 1140
47

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 49
44 to 230
Resilience: Unit (Modulus of Resilience), kJ/m3 85 to 1300
260 to 640
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 46
24
Strength to Weight: Axial, points 19 to 45
15 to 52
Strength to Weight: Bending, points 26 to 46
16 to 36
Thermal Diffusivity, mm2/s 55
14
Thermal Shock Resistance, points 9.0 to 22
12 to 43

Alloy Composition

Aluminum (Al), % 90.8 to 95
0
Boron (B), % 0
0.00080 to 0.0050
Carbon (C), % 0
0.2 to 0.25
Chromium (Cr), % 0 to 0.1
0 to 0.3
Copper (Cu), % 3.9 to 5.0
0 to 0.25
Iron (Fe), % 0 to 0.5
97.9 to 99.199
Magnesium (Mg), % 0.2 to 0.8
0
Manganese (Mn), % 0.4 to 1.2
0.6 to 0.9
Nickel (Ni), % 0 to 0.1
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0.5 to 0.9
0 to 0.3
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0