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5383 Aluminum vs. ACI-ASTM CH20 Steel

5383 aluminum belongs to the aluminum alloys classification, while ACI-ASTM CH20 steel belongs to the iron alloys. There are 31 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 5383 aluminum and the bottom bar is ACI-ASTM CH20 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85 to 110
190
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 6.7 to 15
38
Fatigue Strength, MPa 130 to 200
290
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 26
78
Tensile Strength: Ultimate (UTS), MPa 310 to 370
610
Tensile Strength: Yield (Proof), MPa 150 to 310
350

Thermal Properties

Latent Heat of Fusion, J/g 390
310
Maximum Temperature: Corrosion, °C 65
440
Maximum Temperature: Mechanical, °C 200
1100
Melting Completion (Liquidus), °C 650
1410
Melting Onset (Solidus), °C 540
1430
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 130
14
Thermal Expansion, µm/m-K 24
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
2.0
Electrical Conductivity: Equal Weight (Specific), % IACS 97
2.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
20
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.0
3.7
Embodied Energy, MJ/kg 160
53
Embodied Water, L/kg 1170
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 40
200
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 690
300
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 32 to 38
22
Strength to Weight: Bending, points 38 to 42
21
Thermal Diffusivity, mm2/s 51
3.7
Thermal Shock Resistance, points 14 to 16
15

Alloy Composition


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Aluminum (Al), % 92 to 95.3
0
Carbon (C), % 0
0 to 0.2
Chromium (Cr), % 0 to 0.25
22 to 26
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.25
54.7 to 66
Magnesium (Mg), % 4.0 to 5.2
0
Manganese (Mn), % 0.7 to 1.0
0 to 1.5
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0
12 to 15
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.25
0 to 2.0
Sulfur (S), % 0
0 to 0.040
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.4
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0