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EN 1.0456 Steel vs. 2017 Aluminum

EN 1.0456 steel belongs to the iron alloys classification, while 2017 aluminum belongs to the aluminum alloys. There are 30 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 1.0456 steel and the bottom bar is 2017 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 24 to 26
12 to 18
Fatigue Strength, MPa 210 to 220
90 to 130
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
27
Shear Strength, MPa 270 to 280
130 to 260
Tensile Strength: Ultimate (UTS), MPa 420 to 450
190 to 430
Tensile Strength: Yield (Proof), MPa 290 to 300
76 to 260

Thermal Properties

Latent Heat of Fusion, J/g 250
390
Maximum Temperature: Mechanical, °C 400
190
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1420
510
Specific Heat Capacity, J/kg-K 470
880
Thermal Conductivity, W/m-K 48
150
Thermal Expansion, µm/m-K 12
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.3
38
Electrical Conductivity: Equal Weight (Specific), % IACS 8.4
110

Otherwise Unclassified Properties

Base Metal Price, % relative 2.2
10
Density, g/cm3 7.8
3.0
Embodied Carbon, kg CO2/kg material 1.5
8.0
Embodied Energy, MJ/kg 20
150
Embodied Water, L/kg 49
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 93 to 99
24 to 66
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 230
41 to 470
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
46
Strength to Weight: Axial, points 15 to 16
17 to 40
Strength to Weight: Bending, points 16 to 17
24 to 42
Thermal Diffusivity, mm2/s 13
56
Thermal Shock Resistance, points 13 to 14
7.9 to 18

Alloy Composition

Aluminum (Al), % 0.020 to 0.060
91.6 to 95.5
Carbon (C), % 0 to 0.2
0
Chromium (Cr), % 0 to 0.3
0 to 0.1
Copper (Cu), % 0 to 0.35
3.5 to 4.5
Iron (Fe), % 96.7 to 99.48
0 to 0.7
Magnesium (Mg), % 0
0.4 to 0.8
Manganese (Mn), % 0.5 to 1.4
0.4 to 1.0
Molybdenum (Mo), % 0 to 0.1
0
Nickel (Ni), % 0 to 0.3
0
Niobium (Nb), % 0 to 0.050
0
Nitrogen (N), % 0 to 0.015
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.4
0.2 to 0.8
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0 to 0.030
0 to 0.15
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15