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ASTM A387 Grade 21L Class 1 vs. A360.0 Aluminum

ASTM A387 grade 21L class 1 belongs to the iron alloys classification, while A360.0 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 21L class 1 and the bottom bar is A360.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 150
75
Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 21
1.6 to 5.0
Fatigue Strength, MPa 160
82 to 150
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
27
Shear Strength, MPa 310
180
Tensile Strength: Ultimate (UTS), MPa 500
180 to 320
Tensile Strength: Yield (Proof), MPa 230
170 to 260

Thermal Properties

Latent Heat of Fusion, J/g 260
530
Maximum Temperature: Mechanical, °C 480
170
Melting Completion (Liquidus), °C 1470
680
Melting Onset (Solidus), °C 1430
590
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 41
110
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.6
30
Electrical Conductivity: Equal Weight (Specific), % IACS 8.8
100

Otherwise Unclassified Properties

Base Metal Price, % relative 4.1
9.5
Density, g/cm3 7.9
2.6
Embodied Carbon, kg CO2/kg material 1.8
7.8
Embodied Energy, MJ/kg 23
150
Embodied Water, L/kg 62
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 84
4.6 to 13
Resilience: Unit (Modulus of Resilience), kJ/m3 140
190 to 470
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 24
53
Strength to Weight: Axial, points 18
19 to 34
Strength to Weight: Bending, points 18
27 to 39
Thermal Diffusivity, mm2/s 11
48
Thermal Shock Resistance, points 14
8.5 to 15

Alloy Composition

Aluminum (Al), % 0
85.8 to 90.6
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 2.8 to 3.3
0
Copper (Cu), % 0
0 to 0.6
Iron (Fe), % 94.4 to 96.1
0 to 1.3
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0.3 to 0.6
0 to 0.35
Molybdenum (Mo), % 0.9 to 1.1
0
Nickel (Ni), % 0
0 to 0.5
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
9.0 to 10
Sulfur (S), % 0 to 0.025
0
Tin (Sn), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.25