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EN 1.7366 Steel vs. 6110A Aluminum

EN 1.7366 steel belongs to the iron alloys classification, while 6110A aluminum belongs to the aluminum 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 EN 1.7366 steel and the bottom bar is 6110A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 17 to 19
11 to 18
Fatigue Strength, MPa 160 to 320
140 to 210
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
26
Shear Strength, MPa 290 to 440
220 to 280
Tensile Strength: Ultimate (UTS), MPa 460 to 710
360 to 470
Tensile Strength: Yield (Proof), MPa 230 to 480
250 to 430

Thermal Properties

Latent Heat of Fusion, J/g 260
410
Maximum Temperature: Mechanical, °C 510
190
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1420
600
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 40
160
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.1
42
Electrical Conductivity: Equal Weight (Specific), % IACS 9.3
140

Otherwise Unclassified Properties

Base Metal Price, % relative 4.3
9.5
Density, g/cm3 7.8
2.8
Embodied Carbon, kg CO2/kg material 1.7
8.4
Embodied Energy, MJ/kg 23
150
Embodied Water, L/kg 69
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 74 to 110
47 to 58
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 600
450 to 1300
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 16 to 25
36 to 47
Strength to Weight: Bending, points 17 to 23
41 to 48
Thermal Diffusivity, mm2/s 11
65
Thermal Shock Resistance, points 13 to 20
16 to 21

Alloy Composition

Aluminum (Al), % 0
94.8 to 98
Carbon (C), % 0 to 0.18
0
Chromium (Cr), % 4.0 to 6.0
0.050 to 0.25
Copper (Cu), % 0
0.3 to 0.8
Iron (Fe), % 91.9 to 95.3
0 to 0.5
Magnesium (Mg), % 0
0.7 to 1.1
Manganese (Mn), % 0.3 to 0.8
0.3 to 0.9
Molybdenum (Mo), % 0.45 to 0.65
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.4
0.7 to 1.1
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0 to 0.2
Residuals, % 0
0 to 0.15