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5086 Aluminum vs. ACI-ASTM CA40 Steel

5086 aluminum belongs to the aluminum alloys classification, while ACI-ASTM CA40 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 5086 aluminum and the bottom bar is ACI-ASTM CA40 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 65 to 100
310
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 1.7 to 20
10
Fatigue Strength, MPa 88 to 180
460
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Tensile Strength: Ultimate (UTS), MPa 270 to 390
910
Tensile Strength: Yield (Proof), MPa 110 to 320
860

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Corrosion, °C 65
390
Maximum Temperature: Mechanical, °C 190
750
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 590
1500
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 130
25
Thermal Expansion, µm/m-K 24
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
3.0
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.5
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.8
2.0
Embodied Energy, MJ/kg 150
28
Embodied Water, L/kg 1180
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.8 to 42
89
Resilience: Unit (Modulus of Resilience), kJ/m3 86 to 770
1910
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 28 to 40
33
Strength to Weight: Bending, points 34 to 44
27
Thermal Diffusivity, mm2/s 52
6.7
Thermal Shock Resistance, points 12 to 17
33

Alloy Composition

Aluminum (Al), % 93 to 96.3
0
Carbon (C), % 0
0.2 to 0.4
Chromium (Cr), % 0.050 to 0.25
11.5 to 14
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.5
81.5 to 88.3
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0.2 to 0.7
0 to 1.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0
0 to 1.0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.4
0 to 1.5
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