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EN AC-48100 Aluminum vs. EN 1.8872 Steel

EN AC-48100 aluminum belongs to the aluminum alloys classification, while EN 1.8872 steel belongs to the iron 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 AC-48100 aluminum and the bottom bar is EN 1.8872 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 100 to 140
180
Elastic (Young's, Tensile) Modulus, GPa 76
190
Elongation at Break, % 1.1
21
Fatigue Strength, MPa 120 to 130
310
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 29
73
Tensile Strength: Ultimate (UTS), MPa 240 to 330
610
Tensile Strength: Yield (Proof), MPa 190 to 300
450

Thermal Properties

Latent Heat of Fusion, J/g 640
250
Maximum Temperature: Mechanical, °C 170
410
Melting Completion (Liquidus), °C 580
1460
Melting Onset (Solidus), °C 470
1420
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 130
39
Thermal Expansion, µm/m-K 20
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 87
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 11
2.8
Density, g/cm3 2.8
7.9
Embodied Carbon, kg CO2/kg material 7.3
1.7
Embodied Energy, MJ/kg 130
22
Embodied Water, L/kg 940
50

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 3.6
120
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
530
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 24 to 33
22
Strength to Weight: Bending, points 31 to 38
20
Thermal Diffusivity, mm2/s 55
10
Thermal Shock Resistance, points 11 to 16
18

Alloy Composition


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Aluminum (Al), % 72.1 to 79.8
0
Boron (B), % 0
0 to 0.0050
Carbon (C), % 0
0 to 0.18
Chromium (Cr), % 0
0 to 0.5
Copper (Cu), % 4.0 to 5.0
0 to 0.3
Iron (Fe), % 0 to 1.3
95.1 to 100
Magnesium (Mg), % 0.25 to 0.65
0
Manganese (Mn), % 0 to 0.5
0 to 1.7
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0 to 0.3
0 to 1.0
Niobium (Nb), % 0
0 to 0.050
Nitrogen (N), % 0
0 to 0.015
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 16 to 18
0 to 0.5
Sulfur (S), % 0
0 to 0.0080
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0 to 0.25
0 to 0.030
Vanadium (V), % 0
0 to 0.080
Zinc (Zn), % 0 to 1.5
0
Zirconium (Zr), % 0
0 to 0.050
Residuals, % 0 to 0.25
0