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520.0 Aluminum vs. SAE-AISI 5160 Steel

520.0 aluminum belongs to the aluminum alloys classification, while SAE-AISI 5160 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 520.0 aluminum and the bottom bar is SAE-AISI 5160 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
200 to 340
Elastic (Young's, Tensile) Modulus, GPa 66
190
Elongation at Break, % 14
12 to 18
Fatigue Strength, MPa 55
180 to 650
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 25
73
Shear Strength, MPa 230
390 to 700
Tensile Strength: Ultimate (UTS), MPa 330
660 to 1150
Tensile Strength: Yield (Proof), MPa 170
280 to 1010

Thermal Properties

Latent Heat of Fusion, J/g 390
250
Maximum Temperature: Mechanical, °C 170
420
Melting Completion (Liquidus), °C 600
1450
Melting Onset (Solidus), °C 480
1410
Specific Heat Capacity, J/kg-K 910
470
Thermal Conductivity, W/m-K 87
43
Thermal Expansion, µm/m-K 25
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 21
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 72
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.1
Density, g/cm3 2.6
7.8
Embodied Carbon, kg CO2/kg material 9.8
1.4
Embodied Energy, MJ/kg 160
19
Embodied Water, L/kg 1170
50

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 39
73 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 230
200 to 2700
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 52
24
Strength to Weight: Axial, points 35
23 to 41
Strength to Weight: Bending, points 41
22 to 31
Thermal Diffusivity, mm2/s 37
12
Thermal Shock Resistance, points 14
19 to 34

Alloy Composition

Aluminum (Al), % 87.9 to 90.5
0
Carbon (C), % 0
0.56 to 0.61
Chromium (Cr), % 0
0.7 to 0.9
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0 to 0.3
97.1 to 97.8
Magnesium (Mg), % 9.5 to 10.6
0
Manganese (Mn), % 0 to 0.15
0.75 to 1.0
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.25
0.15 to 0.35
Sulfur (S), % 0
0 to 0.040
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0 to 0.15
0