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EN 1.7383 Steel vs. 518.0 Aluminum

EN 1.7383 steel belongs to the iron alloys classification, while 518.0 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 1.7383 steel and the bottom bar is 518.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170 to 180
80
Elastic (Young's, Tensile) Modulus, GPa 190
67
Elongation at Break, % 20 to 23
5.0
Fatigue Strength, MPa 210 to 270
140
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
25
Shear Strength, MPa 350 to 380
200
Tensile Strength: Ultimate (UTS), MPa 560 to 610
310
Tensile Strength: Yield (Proof), MPa 300 to 400
190

Thermal Properties

Latent Heat of Fusion, J/g 260
390
Maximum Temperature: Mechanical, °C 460
170
Melting Completion (Liquidus), °C 1470
620
Melting Onset (Solidus), °C 1430
560
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 39
98
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.7
24
Electrical Conductivity: Equal Weight (Specific), % IACS 8.8
81

Otherwise Unclassified Properties

Base Metal Price, % relative 3.9
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 1.8
9.4
Embodied Energy, MJ/kg 23
150
Embodied Water, L/kg 59
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
14
Resilience: Unit (Modulus of Resilience), kJ/m3 240 to 420
270
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 20 to 22
32
Strength to Weight: Bending, points 19 to 20
38
Thermal Diffusivity, mm2/s 11
40
Thermal Shock Resistance, points 16 to 18
14

Alloy Composition

Aluminum (Al), % 0 to 0.040
88.1 to 92.5
Carbon (C), % 0.080 to 0.15
0
Chromium (Cr), % 2.0 to 2.5
0
Copper (Cu), % 0 to 0.3
0 to 0.25
Iron (Fe), % 94.3 to 96.6
0 to 1.8
Magnesium (Mg), % 0
7.5 to 8.5
Manganese (Mn), % 0.4 to 0.8
0 to 0.35
Molybdenum (Mo), % 0.9 to 1.1
0
Nickel (Ni), % 0 to 0.3
0 to 0.15
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 0.35
Sulfur (S), % 0 to 0.010
0
Tin (Sn), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.15
Residuals, % 0
0 to 0.25