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ASTM A182 Grade F122 vs. 2011A Aluminum

ASTM A182 grade F122 belongs to the iron alloys classification, while 2011A aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 A182 grade F122 and the bottom bar is 2011A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 23
6.8 to 16
Fatigue Strength, MPa 320
75 to 100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 450
190 to 250
Tensile Strength: Ultimate (UTS), MPa 710
310 to 410
Tensile Strength: Yield (Proof), MPa 450
140 to 310

Thermal Properties

Latent Heat of Fusion, J/g 270
390
Maximum Temperature: Mechanical, °C 600
190
Melting Completion (Liquidus), °C 1490
660
Melting Onset (Solidus), °C 1440
550
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 24
130
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
33
Electrical Conductivity: Equal Weight (Specific), % IACS 12
96

Otherwise Unclassified Properties

Base Metal Price, % relative 12
11
Density, g/cm3 8.0
3.1
Embodied Carbon, kg CO2/kg material 3.0
7.9
Embodied Energy, MJ/kg 44
150
Embodied Water, L/kg 100
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
20 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 520
140 to 670
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
44
Strength to Weight: Axial, points 25
28 to 37
Strength to Weight: Bending, points 22
33 to 40
Thermal Diffusivity, mm2/s 6.4
49
Thermal Shock Resistance, points 19
14 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.020
91.5 to 95.1
Bismuth (Bi), % 0
0.2 to 0.6
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.070 to 0.14
0
Chromium (Cr), % 10 to 11.5
0
Copper (Cu), % 0.3 to 1.7
4.5 to 6.0
Iron (Fe), % 81.3 to 87.7
0 to 0.5
Lead (Pb), % 0
0.2 to 0.6
Manganese (Mn), % 0 to 0.7
0
Molybdenum (Mo), % 0.25 to 0.6
0
Nickel (Ni), % 0 to 0.5
0
Niobium (Nb), % 0.040 to 0.1
0
Nitrogen (N), % 0.040 to 0.1
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0 to 0.4
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0
Tungsten (W), % 1.5 to 2.5
0
Vanadium (V), % 0.15 to 0.3
0
Zinc (Zn), % 0
0 to 0.3
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15