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EN AC-48100 Aluminum vs. SAE-AISI D2 Steel

EN AC-48100 aluminum belongs to the aluminum alloys classification, while SAE-AISI D2 steel belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (4, 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 D2 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 76
190
Elongation at Break, % 1.1
5.0 to 16
Fatigue Strength, MPa 120 to 130
310 to 860
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 29
75
Tensile Strength: Ultimate (UTS), MPa 240 to 330
760 to 2000
Tensile Strength: Yield (Proof), MPa 190 to 300
470 to 1510

Thermal Properties

Latent Heat of Fusion, J/g 640
270
Melting Completion (Liquidus), °C 580
1440
Melting Onset (Solidus), °C 470
1390
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 130
31
Thermal Expansion, µm/m-K 20
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
4.3
Electrical Conductivity: Equal Weight (Specific), % IACS 87
5.1

Otherwise Unclassified Properties

Base Metal Price, % relative 11
8.0
Density, g/cm3 2.8
7.7
Embodied Carbon, kg CO2/kg material 7.3
3.4
Embodied Energy, MJ/kg 130
50
Embodied Water, L/kg 940
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 3.6
92 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
570 to 5940
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 24 to 33
27 to 72
Strength to Weight: Bending, points 31 to 38
24 to 46
Thermal Diffusivity, mm2/s 55
8.3
Thermal Shock Resistance, points 11 to 16
25 to 67

Alloy Composition


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Aluminum (Al), % 72.1 to 79.8
0
Carbon (C), % 0
1.4 to 1.6
Chromium (Cr), % 0
11 to 13
Copper (Cu), % 4.0 to 5.0
0 to 0.25
Iron (Fe), % 0 to 1.3
81.3 to 86.9
Magnesium (Mg), % 0.25 to 0.65
0
Manganese (Mn), % 0 to 0.5
0 to 0.6
Molybdenum (Mo), % 0
0.7 to 1.2
Nickel (Ni), % 0 to 0.3
0 to 0.3
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 16 to 18
0 to 0.6
Sulfur (S), % 0
0 to 0.030
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0 to 1.1
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0 to 0.25
0