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383.0 Aluminum vs. EN 1.6554 Steel

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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