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ASTM A182 Grade F23 vs. 6110A Aluminum

ASTM A182 grade F23 belongs to the iron alloys classification, while 6110A 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 F23 and the bottom bar is 6110A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 22
11 to 18
Fatigue Strength, MPa 320
140 to 210
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
26
Shear Strength, MPa 360
220 to 280
Tensile Strength: Ultimate (UTS), MPa 570
360 to 470
Tensile Strength: Yield (Proof), MPa 460
250 to 430

Thermal Properties

Latent Heat of Fusion, J/g 250
410
Maximum Temperature: Mechanical, °C 450
190
Melting Completion (Liquidus), °C 1500
650
Melting Onset (Solidus), °C 1450
600
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 41
160
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.8
42
Electrical Conductivity: Equal Weight (Specific), % IACS 8.9
140

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
9.5
Density, g/cm3 8.0
2.8
Embodied Carbon, kg CO2/kg material 2.5
8.4
Embodied Energy, MJ/kg 36
150
Embodied Water, L/kg 59
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
47 to 58
Resilience: Unit (Modulus of Resilience), kJ/m3 550
450 to 1300
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 20
36 to 47
Strength to Weight: Bending, points 19
41 to 48
Thermal Diffusivity, mm2/s 11
65
Thermal Shock Resistance, points 17
16 to 21

Alloy Composition


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Aluminum (Al), % 0 to 0.030
94.8 to 98
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.040 to 0.1
0
Chromium (Cr), % 1.9 to 2.6
0.050 to 0.25
Copper (Cu), % 0
0.3 to 0.8
Iron (Fe), % 93.2 to 96.2
0 to 0.5
Magnesium (Mg), % 0
0.7 to 1.1
Manganese (Mn), % 0.1 to 0.6
0.3 to 0.9
Molybdenum (Mo), % 0.050 to 0.3
0
Nickel (Ni), % 0 to 0.4
0
Niobium (Nb), % 0.020 to 0.080
0
Nitrogen (N), % 0 to 0.015
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.5
0.7 to 1.1
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0.0050 to 0.060
0 to 0.2
Tungsten (W), % 1.5 to 1.8
0
Vanadium (V), % 0.2 to 0.3
0
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0 to 0.2
Residuals, % 0
0 to 0.15