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EN AC-48100 Aluminum vs. EN 1.7365 Steel

EN AC-48100 aluminum belongs to the aluminum alloys classification, while EN 1.7365 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 1.7365 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 100 to 140
210
Elastic (Young's, Tensile) Modulus, GPa 76
190
Elongation at Break, % 1.1
18
Fatigue Strength, MPa 120 to 130
320
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 29
74
Tensile Strength: Ultimate (UTS), MPa 240 to 330
700
Tensile Strength: Yield (Proof), MPa 190 to 300
470

Thermal Properties

Latent Heat of Fusion, J/g 640
260
Maximum Temperature: Mechanical, °C 170
510
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
40
Thermal Expansion, µm/m-K 20
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
8.2
Electrical Conductivity: Equal Weight (Specific), % IACS 87
9.4

Otherwise Unclassified Properties

Base Metal Price, % relative 11
4.4
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 7.3
1.8
Embodied Energy, MJ/kg 130
24
Embodied Water, L/kg 940
70

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 3.6
110
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
580
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 24 to 33
25
Strength to Weight: Bending, points 31 to 38
22
Thermal Diffusivity, mm2/s 55
11
Thermal Shock Resistance, points 11 to 16
20

Alloy Composition


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Aluminum (Al), % 72.1 to 79.8
0
Carbon (C), % 0
0.12 to 0.19
Chromium (Cr), % 0
4.0 to 6.0
Copper (Cu), % 4.0 to 5.0
0 to 0.3
Iron (Fe), % 0 to 1.3
91.2 to 94.9
Magnesium (Mg), % 0.25 to 0.65
0
Manganese (Mn), % 0 to 0.5
0.5 to 0.8
Molybdenum (Mo), % 0
0.45 to 0.65
Nickel (Ni), % 0 to 0.3
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 16 to 18
0 to 0.8
Sulfur (S), % 0
0 to 0.025
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0 to 0.25
0