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A413.0 Aluminum vs. EN 1.5414 Steel

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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