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5083 Aluminum vs. ACI-ASTM CF8C Steel

5083 aluminum belongs to the aluminum alloys classification, while ACI-ASTM CF8C steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 5083 aluminum and the bottom bar is ACI-ASTM CF8C steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75 to 110
150
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 1.1 to 17
40
Fatigue Strength, MPa 93 to 190
220
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Tensile Strength: Ultimate (UTS), MPa 290 to 390
530
Tensile Strength: Yield (Proof), MPa 110 to 340
260

Thermal Properties

Latent Heat of Fusion, J/g 400
300
Maximum Temperature: Corrosion, °C 65
490
Maximum Temperature: Mechanical, °C 190
980
Melting Completion (Liquidus), °C 640
1420
Melting Onset (Solidus), °C 580
1430
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 120
16
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
2.0
Electrical Conductivity: Equal Weight (Specific), % IACS 96
2.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
19
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.9
3.7
Embodied Energy, MJ/kg 150
53
Embodied Water, L/kg 1170
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.2 to 42
180
Resilience: Unit (Modulus of Resilience), kJ/m3 95 to 860
170
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 29 to 40
19
Strength to Weight: Bending, points 36 to 44
19
Thermal Diffusivity, mm2/s 48
4.3
Thermal Shock Resistance, points 12 to 17
11

Alloy Composition

Aluminum (Al), % 92.4 to 95.6
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0.050 to 0.25
18 to 21
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.4
61.8 to 73
Magnesium (Mg), % 4.0 to 4.9
0
Manganese (Mn), % 0.4 to 1.0
0 to 1.5
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0
9.0 to 12
Niobium (Nb), % 0
0 to 1.0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.4
0 to 2.0
Sulfur (S), % 0
0 to 0.040
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0