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4006 Aluminum vs. ASTM A182 Grade F12 Class 2

4006 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F12 class 2 belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 4006 aluminum and the bottom bar is ASTM A182 grade F12 class 2.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 28 to 45
180
Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 3.4 to 24
22
Fatigue Strength, MPa 35 to 110
220
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 70 to 91
340
Tensile Strength: Ultimate (UTS), MPa 110 to 160
540
Tensile Strength: Yield (Proof), MPa 62 to 140
310

Thermal Properties

Latent Heat of Fusion, J/g 410
250
Maximum Temperature: Mechanical, °C 160
430
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 620
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 220
43
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 56
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 180
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
2.8
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.1
1.6
Embodied Energy, MJ/kg 150
21
Embodied Water, L/kg 1180
52

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.1 to 26
100
Resilience: Unit (Modulus of Resilience), kJ/m3 28 to 130
260
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 11 to 16
19
Strength to Weight: Bending, points 19 to 24
19
Thermal Diffusivity, mm2/s 89
12
Thermal Shock Resistance, points 4.9 to 7.0
16

Alloy Composition

Aluminum (Al), % 97.4 to 98.7
0
Carbon (C), % 0
0.1 to 0.2
Chromium (Cr), % 0 to 0.2
0.8 to 1.3
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0.5 to 0.8
96.4 to 98.3
Magnesium (Mg), % 0 to 0.010
0
Manganese (Mn), % 0 to 0.050
0.3 to 0.8
Molybdenum (Mo), % 0
0.44 to 0.65
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.8 to 1.2
0.1 to 0.6
Sulfur (S), % 0
0 to 0.040
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.15
0