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6014 Aluminum vs. ASTM A182 Grade F122

6014 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 6014 aluminum and the bottom bar is ASTM A182 grade F122.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 9.1 to 17
23
Fatigue Strength, MPa 43 to 79
320
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 96 to 150
450
Tensile Strength: Ultimate (UTS), MPa 160 to 260
710
Tensile Strength: Yield (Proof), MPa 80 to 200
450

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 180
600
Melting Completion (Liquidus), °C 640
1490
Melting Onset (Solidus), °C 620
1440
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 200
24
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 53
10
Electrical Conductivity: Equal Weight (Specific), % IACS 180
12

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.6
3.0
Embodied Energy, MJ/kg 160
44
Embodied Water, L/kg 1190
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 22
140
Resilience: Unit (Modulus of Resilience), kJ/m3 46 to 300
520
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 16 to 26
25
Strength to Weight: Bending, points 24 to 33
22
Thermal Diffusivity, mm2/s 83
6.4
Thermal Shock Resistance, points 7.0 to 11
19

Alloy Composition

Aluminum (Al), % 97.1 to 99.2
0 to 0.020
Boron (B), % 0
0 to 0.0050
Carbon (C), % 0
0.070 to 0.14
Chromium (Cr), % 0 to 0.2
10 to 11.5
Copper (Cu), % 0 to 0.25
0.3 to 1.7
Iron (Fe), % 0 to 0.35
81.3 to 87.7
Magnesium (Mg), % 0.4 to 0.8
0
Manganese (Mn), % 0.050 to 0.2
0 to 0.7
Molybdenum (Mo), % 0
0.25 to 0.6
Nickel (Ni), % 0
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), % 0.3 to 0.6
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.1
0 to 0.010
Tungsten (W), % 0
1.5 to 2.5
Vanadium (V), % 0.050 to 0.2
0.15 to 0.3
Zinc (Zn), % 0 to 0.1
0
Zirconium (Zr), % 0
0 to 0.010
Residuals, % 0 to 0.15
0