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EN 1.5414 Steel vs. 713.0 Aluminum

EN 1.5414 steel belongs to the iron alloys classification, while 713.0 aluminum belongs to the aluminum alloys. There are 31 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 EN 1.5414 steel and the bottom bar is 713.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170 to 180
74 to 75
Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 22
3.9 to 4.3
Fatigue Strength, MPa 250 to 270
63 to 120
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 73
27
Shear Strength, MPa 350 to 370
180
Tensile Strength: Ultimate (UTS), MPa 550 to 580
240 to 260
Tensile Strength: Yield (Proof), MPa 350 to 380
170

Thermal Properties

Latent Heat of Fusion, J/g 250
370
Maximum Temperature: Mechanical, °C 410
180
Melting Completion (Liquidus), °C 1470
630
Melting Onset (Solidus), °C 1420
610
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 44
150
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.3
35
Electrical Conductivity: Equal Weight (Specific), % IACS 8.4
100

Otherwise Unclassified Properties

Base Metal Price, % relative 2.6
9.5
Density, g/cm3 7.9
3.1
Embodied Carbon, kg CO2/kg material 1.6
7.8
Embodied Energy, MJ/kg 21
150
Embodied Water, L/kg 50
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
8.7 to 9.9
Resilience: Unit (Modulus of Resilience), kJ/m3 320 to 370
210 to 220
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 19 to 20
22 to 23
Strength to Weight: Bending, points 19 to 20
28 to 29
Thermal Diffusivity, mm2/s 12
57
Thermal Shock Resistance, points 16 to 17
10 to 11

Alloy Composition

Aluminum (Al), % 0
87.6 to 92.4
Carbon (C), % 0 to 0.2
0
Chromium (Cr), % 0 to 0.3
0 to 0.35
Copper (Cu), % 0 to 0.3
0.4 to 1.0
Iron (Fe), % 96.4 to 98.7
0 to 1.1
Magnesium (Mg), % 0
0.2 to 0.5
Manganese (Mn), % 0.9 to 1.5
0 to 0.6
Molybdenum (Mo), % 0.45 to 0.6
0
Nickel (Ni), % 0 to 0.3
0 to 0.15
Nitrogen (N), % 0 to 0.012
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.4
0 to 0.25
Sulfur (S), % 0 to 0.0050
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
7.0 to 8.0
Residuals, % 0
0 to 0.25