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ASTM A182 Grade F122 vs. 7178 Aluminum

ASTM A182 grade F122 belongs to the iron alloys classification, while 7178 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 7178 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 23
4.5 to 12
Fatigue Strength, MPa 320
120 to 210
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 76
27
Shear Strength, MPa 450
140 to 380
Tensile Strength: Ultimate (UTS), MPa 710
240 to 640
Tensile Strength: Yield (Proof), MPa 450
120 to 560

Thermal Properties

Latent Heat of Fusion, J/g 270
370
Maximum Temperature: Mechanical, °C 600
180
Melting Completion (Liquidus), °C 1490
630
Melting Onset (Solidus), °C 1440
480
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 24
130
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
31
Electrical Conductivity: Equal Weight (Specific), % IACS 12
91

Otherwise Unclassified Properties

Base Metal Price, % relative 12
10
Density, g/cm3 8.0
3.1
Embodied Carbon, kg CO2/kg material 3.0
8.2
Embodied Energy, MJ/kg 44
150
Embodied Water, L/kg 100
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
24 to 52
Resilience: Unit (Modulus of Resilience), kJ/m3 520
110 to 2220
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 25
21 to 58
Strength to Weight: Bending, points 22
28 to 54
Thermal Diffusivity, mm2/s 6.4
47
Thermal Shock Resistance, points 19
10 to 28

Alloy Composition

Aluminum (Al), % 0 to 0.020
85.4 to 89.5
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.070 to 0.14
0
Chromium (Cr), % 10 to 11.5
0.18 to 0.28
Copper (Cu), % 0.3 to 1.7
1.6 to 2.4
Iron (Fe), % 81.3 to 87.7
0 to 0.5
Magnesium (Mg), % 0
2.4 to 3.1
Manganese (Mn), % 0 to 0.7
0 to 0.3
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 0.4
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
6.3 to 7.3
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15