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ASTM A182 Grade F122 vs. 7204 Aluminum

ASTM A182 grade F122 belongs to the iron alloys classification, while 7204 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 7204 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 23
11 to 13
Fatigue Strength, MPa 320
110 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 450
130 to 220
Tensile Strength: Ultimate (UTS), MPa 710
220 to 380
Tensile Strength: Yield (Proof), MPa 450
120 to 310

Thermal Properties

Latent Heat of Fusion, J/g 270
380
Maximum Temperature: Mechanical, °C 600
210
Melting Completion (Liquidus), °C 1490
640
Melting Onset (Solidus), °C 1440
520
Specific Heat Capacity, J/kg-K 470
880
Thermal Conductivity, W/m-K 24
150
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
39
Electrical Conductivity: Equal Weight (Specific), % IACS 12
120

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 8.0
2.9
Embodied Carbon, kg CO2/kg material 3.0
8.4
Embodied Energy, MJ/kg 44
150
Embodied Water, L/kg 100
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
25 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 520
110 to 710
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
47
Strength to Weight: Axial, points 25
21 to 36
Strength to Weight: Bending, points 22
28 to 40
Thermal Diffusivity, mm2/s 6.4
58
Thermal Shock Resistance, points 19
9.4 to 16

Alloy Composition

Aluminum (Al), % 0 to 0.020
90.5 to 94.8
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.070 to 0.14
0
Chromium (Cr), % 10 to 11.5
0 to 0.3
Copper (Cu), % 0.3 to 1.7
0 to 0.2
Iron (Fe), % 81.3 to 87.7
0 to 0.35
Magnesium (Mg), % 0
1.0 to 2.0
Manganese (Mn), % 0 to 0.7
0.2 to 0.7
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 0.3
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 to 0.1
Zinc (Zn), % 0
4.0 to 5.0
Zirconium (Zr), % 0 to 0.010
0 to 0.25
Residuals, % 0
0 to 0.15