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ASTM A182 Grade F122 vs. 2007 Aluminum

ASTM A182 grade F122 belongs to the iron alloys classification, while 2007 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 2007 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 23
5.6 to 8.0
Fatigue Strength, MPa 320
91 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
27
Shear Strength, MPa 450
220 to 250
Tensile Strength: Ultimate (UTS), MPa 710
370 to 420
Tensile Strength: Yield (Proof), MPa 450
240 to 270

Thermal Properties

Latent Heat of Fusion, J/g 270
390
Maximum Temperature: Mechanical, °C 600
190
Melting Completion (Liquidus), °C 1490
640
Melting Onset (Solidus), °C 1440
510
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
47
Electrical Conductivity: Equal Weight (Specific), % IACS 12
140

Otherwise Unclassified Properties

Base Metal Price, % relative 12
11
Density, g/cm3 8.0
3.1
Embodied Carbon, kg CO2/kg material 3.0
8.0
Embodied Energy, MJ/kg 44
150
Embodied Water, L/kg 100
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
21 to 26
Resilience: Unit (Modulus of Resilience), kJ/m3 520
390 to 530
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
44
Strength to Weight: Axial, points 25
33 to 38
Strength to Weight: Bending, points 22
37 to 40
Thermal Diffusivity, mm2/s 6.4
48
Thermal Shock Resistance, points 19
16 to 19

Alloy Composition

Aluminum (Al), % 0 to 0.020
87.5 to 95
Bismuth (Bi), % 0
0 to 0.2
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.070 to 0.14
0
Chromium (Cr), % 10 to 11.5
0 to 0.1
Copper (Cu), % 0.3 to 1.7
3.3 to 4.6
Iron (Fe), % 81.3 to 87.7
0 to 0.8
Lead (Pb), % 0
0.8 to 1.5
Magnesium (Mg), % 0
0.4 to 1.8
Manganese (Mn), % 0 to 0.7
0.5 to 1.0
Molybdenum (Mo), % 0.25 to 0.6
0
Nickel (Ni), % 0 to 0.5
0 to 0.2
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 0.8
Sulfur (S), % 0 to 0.010
0
Tin (Sn), % 0
0 to 0.2
Titanium (Ti), % 0 to 0.010
0 to 0.2
Tungsten (W), % 1.5 to 2.5
0
Vanadium (V), % 0.15 to 0.3
0
Zinc (Zn), % 0
0 to 0.8
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.3