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2011 Aluminum vs. ASTM A387 Grade 22L Class 1

2011 aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 22L class 1 belongs to the iron alloys. There are 30 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 2011 aluminum and the bottom bar is ASTM A387 grade 22L class 1.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 8.5 to 18
20
Fatigue Strength, MPa 74 to 120
160
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
74
Shear Strength, MPa 190 to 250
310
Tensile Strength: Ultimate (UTS), MPa 310 to 420
500
Tensile Strength: Yield (Proof), MPa 140 to 310
230

Thermal Properties

Latent Heat of Fusion, J/g 390
260
Maximum Temperature: Mechanical, °C 190
460
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 540
1430
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 140 to 170
40
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35 to 45
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 100 to 130
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 11
3.8
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 7.9
1.7
Embodied Energy, MJ/kg 150
23
Embodied Water, L/kg 1150
58

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 52
83
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 680
140
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 44
24
Strength to Weight: Axial, points 27 to 37
18
Strength to Weight: Bending, points 32 to 40
18
Thermal Diffusivity, mm2/s 51 to 64
11
Thermal Shock Resistance, points 14 to 19
14

Alloy Composition

Aluminum (Al), % 91.3 to 94.6
0
Bismuth (Bi), % 0.2 to 0.6
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
2.0 to 2.5
Copper (Cu), % 5.0 to 6.0
0
Iron (Fe), % 0 to 0.7
95.2 to 96.8
Lead (Pb), % 0.2 to 0.6
0
Manganese (Mn), % 0
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.4
0 to 0.5
Sulfur (S), % 0
0 to 0.025
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.15
0