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2014A Aluminum vs. ASTM A182 Grade F122

2014A 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 (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 2014A aluminum and the bottom bar is ASTM A182 grade F122.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 6.2 to 16
23
Fatigue Strength, MPa 93 to 150
320
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
76
Shear Strength, MPa 130 to 290
450
Tensile Strength: Ultimate (UTS), MPa 210 to 490
710
Tensile Strength: Yield (Proof), MPa 110 to 430
450

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 210
600
Melting Completion (Liquidus), °C 640
1490
Melting Onset (Solidus), °C 510
1440
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 150
24
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
10
Electrical Conductivity: Equal Weight (Specific), % IACS 110
12

Otherwise Unclassified Properties

Base Metal Price, % relative 11
12
Density, g/cm3 3.0
8.0
Embodied Carbon, kg CO2/kg material 8.1
3.0
Embodied Energy, MJ/kg 150
44
Embodied Water, L/kg 1140
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 49
140
Resilience: Unit (Modulus of Resilience), kJ/m3 85 to 1300
520
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
24
Strength to Weight: Axial, points 19 to 45
25
Strength to Weight: Bending, points 26 to 46
22
Thermal Diffusivity, mm2/s 55
6.4
Thermal Shock Resistance, points 9.0 to 22
19

Alloy Composition

Aluminum (Al), % 90.8 to 95
0 to 0.020
Boron (B), % 0
0 to 0.0050
Carbon (C), % 0
0.070 to 0.14
Chromium (Cr), % 0 to 0.1
10 to 11.5
Copper (Cu), % 3.9 to 5.0
0.3 to 1.7
Iron (Fe), % 0 to 0.5
81.3 to 87.7
Magnesium (Mg), % 0.2 to 0.8
0
Manganese (Mn), % 0.4 to 1.2
0 to 0.7
Molybdenum (Mo), % 0
0.25 to 0.6
Nickel (Ni), % 0 to 0.1
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), % 0.5 to 0.9
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.15
0 to 0.010
Tungsten (W), % 0
1.5 to 2.5
Vanadium (V), % 0
0.15 to 0.3
Zinc (Zn), % 0 to 0.25
0
Zirconium (Zr), % 0 to 0.2
0 to 0.010
Residuals, % 0 to 0.15
0