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ASTM A182 Grade F122 vs. 3104 Aluminum

ASTM A182 grade F122 belongs to the iron alloys classification, while 3104 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 3104 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 23
1.1 to 20
Fatigue Strength, MPa 320
74 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 450
110 to 180
Tensile Strength: Ultimate (UTS), MPa 710
170 to 310
Tensile Strength: Yield (Proof), MPa 450
68 to 270

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 600
180
Melting Completion (Liquidus), °C 1490
650
Melting Onset (Solidus), °C 1440
600
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 24
160
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
41
Electrical Conductivity: Equal Weight (Specific), % IACS 12
130

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 8.0
2.8
Embodied Carbon, kg CO2/kg material 3.0
8.4
Embodied Energy, MJ/kg 44
150
Embodied Water, L/kg 100
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
1.6 to 60
Resilience: Unit (Modulus of Resilience), kJ/m3 520
34 to 540
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 25
17 to 31
Strength to Weight: Bending, points 22
25 to 37
Thermal Diffusivity, mm2/s 6.4
64
Thermal Shock Resistance, points 19
7.6 to 13

Alloy Composition


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Aluminum (Al), % 0 to 0.020
95.1 to 98.4
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
0.050 to 0.25
Gallium (Ga), % 0
0 to 0.050
Iron (Fe), % 81.3 to 87.7
0 to 0.8
Magnesium (Mg), % 0
0.8 to 1.3
Manganese (Mn), % 0 to 0.7
0.8 to 1.4
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 to 0.6
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0 to 0.1
Tungsten (W), % 1.5 to 2.5
0
Vanadium (V), % 0.15 to 0.3
0 to 0.050
Zinc (Zn), % 0
0 to 0.25
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15