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383.0 Aluminum vs. EN 1.6579 Steel

383.0 aluminum belongs to the aluminum alloys classification, while EN 1.6579 steel belongs to the iron 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 383.0 aluminum and the bottom bar is EN 1.6579 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
260 to 290
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 3.5
11 to 14
Fatigue Strength, MPa 150
380 to 570
Impact Strength: V-Notched Charpy, J 4.0
35 to 41
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
73
Tensile Strength: Ultimate (UTS), MPa 280
850 to 980
Tensile Strength: Yield (Proof), MPa 150
600 to 910

Thermal Properties

Latent Heat of Fusion, J/g 540
250
Maximum Temperature: Mechanical, °C 170
440
Melting Completion (Liquidus), °C 580
1460
Melting Onset (Solidus), °C 540
1410
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 96
39
Thermal Expansion, µm/m-K 21
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 23
7.7
Electrical Conductivity: Equal Weight (Specific), % IACS 74
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 10
3.7
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 7.5
1.7
Embodied Energy, MJ/kg 140
22
Embodied Water, L/kg 1030
56

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.2
100 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 150
950 to 2210
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 28
30 to 35
Strength to Weight: Bending, points 34
25 to 28
Thermal Diffusivity, mm2/s 39
11
Thermal Shock Resistance, points 13
25 to 29

Alloy Composition


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Aluminum (Al), % 79.7 to 88.5
0
Carbon (C), % 0
0.32 to 0.38
Chromium (Cr), % 0
1.4 to 1.7
Copper (Cu), % 2.0 to 3.0
0
Iron (Fe), % 0 to 1.3
94.2 to 96.1
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0.6 to 1.0
Molybdenum (Mo), % 0
0.15 to 0.35
Nickel (Ni), % 0 to 0.3
1.4 to 1.7
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 9.5 to 11.5
0 to 0.6
Sulfur (S), % 0
0 to 0.030
Tin (Sn), % 0 to 0.15
0
Zinc (Zn), % 0 to 3.0
0
Residuals, % 0 to 0.5
0