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ASTM A387 Grade 11 Steel vs. 2018 Aluminum

ASTM A387 grade 11 steel belongs to the iron alloys classification, while 2018 aluminum belongs to the aluminum 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 ASTM A387 grade 11 steel and the bottom bar is 2018 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 150 to 180
120
Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 25
9.6
Fatigue Strength, MPa 200 to 250
120
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
27
Shear Strength, MPa 320 to 390
270
Tensile Strength: Ultimate (UTS), MPa 500 to 600
420
Tensile Strength: Yield (Proof), MPa 270 to 350
310

Thermal Properties

Latent Heat of Fusion, J/g 260
390
Maximum Temperature: Mechanical, °C 430
220
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1420
510
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 39
150
Thermal Expansion, µm/m-K 13
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.4
40
Electrical Conductivity: Equal Weight (Specific), % IACS 8.5
120

Otherwise Unclassified Properties

Base Metal Price, % relative 2.9
11
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 1.6
8.1
Embodied Energy, MJ/kg 21
150
Embodied Water, L/kg 53
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 100 to 130
37
Resilience: Unit (Modulus of Resilience), kJ/m3 200 to 320
670
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 18 to 21
38
Strength to Weight: Bending, points 18 to 20
41
Thermal Diffusivity, mm2/s 11
57
Thermal Shock Resistance, points 15 to 18
19

Alloy Composition


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Aluminum (Al), % 0
89.7 to 94.4
Carbon (C), % 0.050 to 0.17
0
Chromium (Cr), % 1.0 to 1.5
0 to 0.1
Copper (Cu), % 0
3.5 to 4.5
Iron (Fe), % 96.2 to 97.6
0 to 1.0
Magnesium (Mg), % 0
0.45 to 0.9
Manganese (Mn), % 0.4 to 0.65
0 to 0.2
Molybdenum (Mo), % 0.45 to 0.65
0
Nickel (Ni), % 0
1.7 to 2.3
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.5 to 0.8
0 to 0.9
Sulfur (S), % 0 to 0.025
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15