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ACI-ASTM CG8M Steel vs. 5083 Aluminum

ACI-ASTM CG8M steel belongs to the iron alloys classification, while 5083 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, 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 ACI-ASTM CG8M steel and the bottom bar is 5083 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 180
75 to 110
Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 45
1.1 to 17
Fatigue Strength, MPa 280
93 to 190
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 79
26
Tensile Strength: Ultimate (UTS), MPa 550
290 to 390
Tensile Strength: Yield (Proof), MPa 300
110 to 340

Thermal Properties

Latent Heat of Fusion, J/g 300
400
Maximum Temperature: Corrosion, °C 420
65
Maximum Temperature: Mechanical, °C 1020
190
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1400
580
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 16
120
Thermal Expansion, µm/m-K 16
24

Electrical Properties

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

Otherwise Unclassified Properties

Base Metal Price, % relative 20
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 4.1
8.9
Embodied Energy, MJ/kg 56
150
Embodied Water, L/kg 160
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
4.2 to 42
Resilience: Unit (Modulus of Resilience), kJ/m3 220
95 to 860
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 19
29 to 40
Strength to Weight: Bending, points 19
36 to 44
Thermal Diffusivity, mm2/s 4.3
48
Thermal Shock Resistance, points 12
12 to 17

Alloy Composition

Aluminum (Al), % 0
92.4 to 95.6
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 18 to 21
0.050 to 0.25
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 58.8 to 70
0 to 0.4
Magnesium (Mg), % 0
4.0 to 4.9
Manganese (Mn), % 0 to 1.5
0.4 to 1.0
Molybdenum (Mo), % 3.0 to 4.0
0
Nickel (Ni), % 9.0 to 13
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.5
0 to 0.4
Sulfur (S), % 0 to 0.040
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15