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713.0 Aluminum vs. EN 1.5410 Steel

713.0 aluminum belongs to the aluminum alloys classification, while EN 1.5410 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 713.0 aluminum and the bottom bar is EN 1.5410 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 74 to 75
170 to 190
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 3.9 to 4.3
20 to 25
Fatigue Strength, MPa 63 to 120
290 to 330
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 27
73
Tensile Strength: Ultimate (UTS), MPa 240 to 260
560 to 620
Tensile Strength: Yield (Proof), MPa 170
400 to 480

Thermal Properties

Latent Heat of Fusion, J/g 370
250
Maximum Temperature: Mechanical, °C 180
400
Melting Completion (Liquidus), °C 630
1460
Melting Onset (Solidus), °C 610
1420
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 150
51
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 100
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.3
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 7.8
1.7
Embodied Energy, MJ/kg 150
22
Embodied Water, L/kg 1110
49

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.7 to 9.9
120 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 220
430 to 610
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 22 to 23
20 to 22
Strength to Weight: Bending, points 28 to 29
19 to 21
Thermal Diffusivity, mm2/s 57
14
Thermal Shock Resistance, points 10 to 11
16 to 18

Alloy Composition

Aluminum (Al), % 87.6 to 92.4
0
Carbon (C), % 0
0 to 0.12
Chromium (Cr), % 0 to 0.35
0
Copper (Cu), % 0.4 to 1.0
0
Iron (Fe), % 0 to 1.1
96.9 to 98.6
Magnesium (Mg), % 0.2 to 0.5
0
Manganese (Mn), % 0 to 0.6
1.2 to 1.8
Molybdenum (Mo), % 0
0.2 to 0.4
Nickel (Ni), % 0 to 0.15
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.25
0 to 0.6
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 7.0 to 8.0
0
Residuals, % 0 to 0.25
0