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ASTM A182 Grade F122 vs. 6351 Aluminum

ASTM A182 grade F122 belongs to the iron alloys classification, while 6351 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 6351 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 23
7.8 to 18
Fatigue Strength, MPa 320
79 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 450
84 to 200
Tensile Strength: Ultimate (UTS), MPa 710
140 to 310
Tensile Strength: Yield (Proof), MPa 450
95 to 270

Thermal Properties

Latent Heat of Fusion, J/g 270
410
Maximum Temperature: Mechanical, °C 600
160
Melting Completion (Liquidus), °C 1490
650
Melting Onset (Solidus), °C 1440
570
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 24
180
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
46
Electrical Conductivity: Equal Weight (Specific), % IACS 12
150

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 3.0
8.3
Embodied Energy, MJ/kg 44
150
Embodied Water, L/kg 100
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
20 to 38
Resilience: Unit (Modulus of Resilience), kJ/m3 520
65 to 540
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 25
14 to 32
Strength to Weight: Bending, points 22
22 to 38
Thermal Diffusivity, mm2/s 6.4
72
Thermal Shock Resistance, points 19
6.1 to 14

Alloy Composition

Aluminum (Al), % 0 to 0.020
96 to 98.5
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
0 to 0.1
Iron (Fe), % 81.3 to 87.7
0 to 0.5
Magnesium (Mg), % 0
0.4 to 0.8
Manganese (Mn), % 0 to 0.7
0.4 to 0.8
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
0.7 to 1.3
Sulfur (S), % 0 to 0.010
0
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 0.2
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15