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EN AC-48100 Aluminum vs. SAE-AISI 52100 Steel

EN AC-48100 aluminum belongs to the aluminum alloys classification, while SAE-AISI 52100 steel belongs to the iron alloys. There are 30 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 AC-48100 aluminum and the bottom bar is SAE-AISI 52100 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 100 to 140
180 to 210
Elastic (Young's, Tensile) Modulus, GPa 76
190
Elongation at Break, % 1.1
10 to 20
Fatigue Strength, MPa 120 to 130
250 to 340
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 29
72
Tensile Strength: Ultimate (UTS), MPa 240 to 330
590 to 2010
Tensile Strength: Yield (Proof), MPa 190 to 300
360 to 560

Thermal Properties

Latent Heat of Fusion, J/g 640
250
Maximum Temperature: Mechanical, °C 170
430
Melting Completion (Liquidus), °C 580
1450
Melting Onset (Solidus), °C 470
1410
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 130
47
Thermal Expansion, µm/m-K 20
12 to 13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 87
8.5

Otherwise Unclassified Properties

Base Metal Price, % relative 11
2.4
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 7.3
1.5
Embodied Energy, MJ/kg 130
20
Embodied Water, L/kg 940
51

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 3.6
54 to 310
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
350 to 840
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 24 to 33
21 to 72
Strength to Weight: Bending, points 31 to 38
20 to 45
Thermal Diffusivity, mm2/s 55
13
Thermal Shock Resistance, points 11 to 16
19 to 61

Alloy Composition

Aluminum (Al), % 72.1 to 79.8
0
Carbon (C), % 0
0.93 to 1.1
Chromium (Cr), % 0
1.4 to 1.6
Copper (Cu), % 4.0 to 5.0
0
Iron (Fe), % 0 to 1.3
96.5 to 97.3
Magnesium (Mg), % 0.25 to 0.65
0
Manganese (Mn), % 0 to 0.5
0.25 to 0.45
Nickel (Ni), % 0 to 0.3
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 16 to 18
0.15 to 0.35
Sulfur (S), % 0
0 to 0.015
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0 to 0.25
0