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6070 Aluminum vs. EN 1.5113 Steel

6070 aluminum belongs to the aluminum alloys classification, while EN 1.5113 steel belongs to the iron alloys. There are 30 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 6070 aluminum and the bottom bar is EN 1.5113 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 5.6 to 8.6
11 to 18
Fatigue Strength, MPa 95 to 130
220 to 470
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 220 to 240
360 to 540
Tensile Strength: Ultimate (UTS), MPa 370 to 380
580 to 900
Tensile Strength: Yield (Proof), MPa 350
320 to 770

Thermal Properties

Latent Heat of Fusion, J/g 410
260
Maximum Temperature: Mechanical, °C 160
400
Melting Completion (Liquidus), °C 650
1450
Melting Onset (Solidus), °C 570
1410
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 160
52
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 140
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.0
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.4
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 1170
48

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 20 to 32
91 to 96
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 900
270 to 1570
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 38
21 to 32
Strength to Weight: Bending, points 42 to 43
20 to 27
Thermal Diffusivity, mm2/s 65
14
Thermal Shock Resistance, points 16 to 17
17 to 26

Alloy Composition

Aluminum (Al), % 94.6 to 98
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0.15 to 0.4
0
Iron (Fe), % 0 to 0.5
97 to 97.5
Magnesium (Mg), % 0.5 to 1.2
0
Manganese (Mn), % 0.4 to 1.0
1.6 to 1.8
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 1.0 to 1.7
0.9 to 1.1
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0