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EN 1.6554 Steel vs. 383.0 Aluminum

EN 1.6554 steel belongs to the iron alloys classification, while 383.0 aluminum belongs to the aluminum alloys. There are 31 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 EN 1.6554 steel and the bottom bar is 383.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 230 to 280
75
Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 17 to 21
3.5
Fatigue Strength, MPa 380 to 520
150
Impact Strength: V-Notched Charpy, J 30 to 45
4.0
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
28
Tensile Strength: Ultimate (UTS), MPa 780 to 930
280
Tensile Strength: Yield (Proof), MPa 550 to 790
150

Thermal Properties

Latent Heat of Fusion, J/g 250
540
Maximum Temperature: Mechanical, °C 420
170
Melting Completion (Liquidus), °C 1460
580
Melting Onset (Solidus), °C 1420
540
Specific Heat Capacity, J/kg-K 470
880
Thermal Conductivity, W/m-K 40
96
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.6
23
Electrical Conductivity: Equal Weight (Specific), % IACS 8.7
74

Otherwise Unclassified Properties

Base Metal Price, % relative 3.4
10
Density, g/cm3 7.9
2.8
Embodied Carbon, kg CO2/kg material 1.7
7.5
Embodied Energy, MJ/kg 22
140
Embodied Water, L/kg 53
1030

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 150
8.2
Resilience: Unit (Modulus of Resilience), kJ/m3 810 to 1650
150
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 27 to 33
28
Strength to Weight: Bending, points 24 to 27
34
Thermal Diffusivity, mm2/s 11
39
Thermal Shock Resistance, points 23 to 27
13

Alloy Composition

Aluminum (Al), % 0
79.7 to 88.5
Carbon (C), % 0.23 to 0.28
0
Chromium (Cr), % 0.7 to 0.9
0
Copper (Cu), % 0 to 0.3
2.0 to 3.0
Iron (Fe), % 94.6 to 97.3
0 to 1.3
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0.6 to 0.9
0 to 0.5
Molybdenum (Mo), % 0.2 to 0.3
0
Nickel (Ni), % 1.0 to 2.0
0 to 0.3
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.6
9.5 to 11.5
Sulfur (S), % 0 to 0.025
0
Tin (Sn), % 0
0 to 0.15
Vanadium (V), % 0 to 0.030
0
Zinc (Zn), % 0
0 to 3.0
Residuals, % 0
0 to 0.5