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EN 1.5414 Steel vs. A413.0 Aluminum

EN 1.5414 steel belongs to the iron alloys classification, while A413.0 aluminum belongs to the aluminum alloys. There are 31 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 1.5414 steel and the bottom bar is A413.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170 to 180
80
Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 22
3.5
Fatigue Strength, MPa 250 to 270
130
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
27
Shear Strength, MPa 350 to 370
170
Tensile Strength: Ultimate (UTS), MPa 550 to 580
240
Tensile Strength: Yield (Proof), MPa 350 to 380
130

Thermal Properties

Latent Heat of Fusion, J/g 250
570
Maximum Temperature: Mechanical, °C 410
170
Melting Completion (Liquidus), °C 1470
590
Melting Onset (Solidus), °C 1420
580
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 44
120
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.3
31
Electrical Conductivity: Equal Weight (Specific), % IACS 8.4
110

Otherwise Unclassified Properties

Base Metal Price, % relative 2.6
9.5
Density, g/cm3 7.9
2.6
Embodied Carbon, kg CO2/kg material 1.6
7.6
Embodied Energy, MJ/kg 21
140
Embodied Water, L/kg 50
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
7.1
Resilience: Unit (Modulus of Resilience), kJ/m3 320 to 370
120
Stiffness to Weight: Axial, points 13
16
Stiffness to Weight: Bending, points 24
54
Strength to Weight: Axial, points 19 to 20
25
Strength to Weight: Bending, points 19 to 20
33
Thermal Diffusivity, mm2/s 12
52
Thermal Shock Resistance, points 16 to 17
11

Alloy Composition

Aluminum (Al), % 0
82.9 to 89
Carbon (C), % 0 to 0.2
0
Chromium (Cr), % 0 to 0.3
0
Copper (Cu), % 0 to 0.3
0 to 1.0
Iron (Fe), % 96.4 to 98.7
0 to 1.3
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0.9 to 1.5
0 to 0.35
Molybdenum (Mo), % 0.45 to 0.6
0
Nickel (Ni), % 0 to 0.3
0 to 0.5
Nitrogen (N), % 0 to 0.012
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.4
11 to 13
Sulfur (S), % 0 to 0.0050
0
Tin (Sn), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.25