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6182 Aluminum vs. ASTM A182 Grade F23

6182 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F23 belongs to the iron 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 6182 aluminum and the bottom bar is ASTM A182 grade F23.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 6.8 to 13
22
Fatigue Strength, MPa 63 to 99
320
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 140 to 190
360
Tensile Strength: Ultimate (UTS), MPa 230 to 320
570
Tensile Strength: Yield (Proof), MPa 130 to 270
460

Thermal Properties

Latent Heat of Fusion, J/g 410
250
Maximum Temperature: Mechanical, °C 190
450
Melting Completion (Liquidus), °C 640
1500
Melting Onset (Solidus), °C 600
1450
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 160
41
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 130
8.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.0
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.4
2.5
Embodied Energy, MJ/kg 150
36
Embodied Water, L/kg 1170
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 21 to 26
120
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 520
550
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 23 to 32
20
Strength to Weight: Bending, points 30 to 38
19
Thermal Diffusivity, mm2/s 65
11
Thermal Shock Resistance, points 10 to 14
17

Alloy Composition

Aluminum (Al), % 95 to 97.9
0 to 0.030
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0 to 0.25
1.9 to 2.6
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.5
93.2 to 96.2
Magnesium (Mg), % 0.7 to 1.2
0
Manganese (Mn), % 0.5 to 1.0
0.1 to 0.6
Molybdenum (Mo), % 0
0.050 to 0.3
Nickel (Ni), % 0
0 to 0.4
Niobium (Nb), % 0
0.020 to 0.080
Nitrogen (N), % 0
0 to 0.015
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0.9 to 1.3
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.1
0.0050 to 0.060
Tungsten (W), % 0
1.5 to 1.8
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.050 to 0.2
0
Residuals, % 0 to 0.15
0