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ASTM A387 Grade 22L Class 1 vs. 2218 Aluminum

ASTM A387 grade 22L class 1 belongs to the iron alloys classification, while 2218 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 22L class 1 and the bottom bar is 2218 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 150
95 to 110
Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 20
6.8 to 10
Fatigue Strength, MPa 160
110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
27
Shear Strength, MPa 310
210 to 250
Tensile Strength: Ultimate (UTS), MPa 500
330 to 430
Tensile Strength: Yield (Proof), MPa 230
260 to 310

Thermal Properties

Latent Heat of Fusion, J/g 260
390
Maximum Temperature: Mechanical, °C 460
220
Melting Completion (Liquidus), °C 1470
640
Melting Onset (Solidus), °C 1430
510
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 40
140
Thermal Expansion, µm/m-K 13
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.5
37
Electrical Conductivity: Equal Weight (Specific), % IACS 8.6
110

Otherwise Unclassified Properties

Base Metal Price, % relative 3.8
11
Density, g/cm3 7.9
3.1
Embodied Carbon, kg CO2/kg material 1.7
8.2
Embodied Energy, MJ/kg 23
150
Embodied Water, L/kg 58
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 83
27 to 31
Resilience: Unit (Modulus of Resilience), kJ/m3 140
450 to 650
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 18
30 to 39
Strength to Weight: Bending, points 18
34 to 41
Thermal Diffusivity, mm2/s 11
52
Thermal Shock Resistance, points 14
15 to 19

Alloy Composition


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Aluminum (Al), % 0
88.8 to 93.6
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 2.0 to 2.5
0 to 0.1
Copper (Cu), % 0
3.5 to 4.5
Iron (Fe), % 95.2 to 96.8
0 to 1.0
Magnesium (Mg), % 0
1.2 to 1.8
Manganese (Mn), % 0.3 to 0.6
0 to 0.2
Molybdenum (Mo), % 0.9 to 1.1
0
Nickel (Ni), % 0
1.7 to 2.3
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 0.9
Sulfur (S), % 0 to 0.025
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15