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384.0 Aluminum vs. SAE-AISI 1552 Steel

384.0 aluminum belongs to the aluminum alloys classification, while SAE-AISI 1552 steel belongs to the iron alloys. There are 31 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 384.0 aluminum and the bottom bar is SAE-AISI 1552 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85
220 to 250
Elastic (Young's, Tensile) Modulus, GPa 74
190
Elongation at Break, % 2.5
11 to 14
Fatigue Strength, MPa 140
290 to 400
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
72
Shear Strength, MPa 200
460 to 510
Tensile Strength: Ultimate (UTS), MPa 330
760 to 840
Tensile Strength: Yield (Proof), MPa 170
460 to 650

Thermal Properties

Latent Heat of Fusion, J/g 550
250
Maximum Temperature: Mechanical, °C 170
400
Melting Completion (Liquidus), °C 580
1460
Melting Onset (Solidus), °C 530
1420
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 96
51
Thermal Expansion, µm/m-K 21
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 22
11
Electrical Conductivity: Equal Weight (Specific), % IACS 69
12

Otherwise Unclassified Properties

Base Metal Price, % relative 11
1.8
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 7.4
1.4
Embodied Energy, MJ/kg 140
19
Embodied Water, L/kg 1010
47

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.9
81 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 190
560 to 1130
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 49
24
Strength to Weight: Axial, points 32
27 to 30
Strength to Weight: Bending, points 37
24 to 25
Thermal Diffusivity, mm2/s 39
14
Thermal Shock Resistance, points 15
26 to 29

Alloy Composition


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Aluminum (Al), % 77.3 to 86.5
0
Carbon (C), % 0
0.47 to 0.55
Copper (Cu), % 3.0 to 4.5
0
Iron (Fe), % 0 to 1.3
97.9 to 98.3
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
1.2 to 1.5
Nickel (Ni), % 0 to 0.5
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 10.5 to 12
0
Sulfur (S), % 0
0 to 0.050
Tin (Sn), % 0 to 0.35
0
Zinc (Zn), % 0 to 3.0
0
Residuals, % 0 to 0.5
0