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328.0 Aluminum vs. ASTM A182 Grade F122

328.0 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F122 belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 328.0 aluminum and the bottom bar is ASTM A182 grade F122.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 60 to 82
220
Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 1.6 to 2.1
23
Fatigue Strength, MPa 55 to 80
320
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
76
Tensile Strength: Ultimate (UTS), MPa 200 to 270
710
Tensile Strength: Yield (Proof), MPa 120 to 170
450

Thermal Properties

Latent Heat of Fusion, J/g 510
270
Maximum Temperature: Mechanical, °C 180
600
Melting Completion (Liquidus), °C 620
1490
Melting Onset (Solidus), °C 560
1440
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 120
24
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
10
Electrical Conductivity: Equal Weight (Specific), % IACS 99
12

Otherwise Unclassified Properties

Base Metal Price, % relative 10
12
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 7.8
3.0
Embodied Energy, MJ/kg 140
44
Embodied Water, L/kg 1070
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.8 to 5.0
140
Resilience: Unit (Modulus of Resilience), kJ/m3 92 to 200
520
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 21 to 28
25
Strength to Weight: Bending, points 28 to 34
22
Thermal Diffusivity, mm2/s 50
6.4
Thermal Shock Resistance, points 9.2 to 12
19

Alloy Composition


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Aluminum (Al), % 84.5 to 91.1
0 to 0.020
Boron (B), % 0
0 to 0.0050
Carbon (C), % 0
0.070 to 0.14
Chromium (Cr), % 0 to 0.35
10 to 11.5
Copper (Cu), % 1.0 to 2.0
0.3 to 1.7
Iron (Fe), % 0 to 1.0
81.3 to 87.7
Magnesium (Mg), % 0.2 to 0.6
0
Manganese (Mn), % 0.2 to 0.6
0 to 0.7
Molybdenum (Mo), % 0
0.25 to 0.6
Nickel (Ni), % 0 to 0.25
0 to 0.5
Niobium (Nb), % 0
0.040 to 0.1
Nitrogen (N), % 0
0.040 to 0.1
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 7.5 to 8.5
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.25
0 to 0.010
Tungsten (W), % 0
1.5 to 2.5
Vanadium (V), % 0
0.15 to 0.3
Zinc (Zn), % 0 to 1.5
0
Zirconium (Zr), % 0
0 to 0.010
Residuals, % 0 to 0.5
0