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ASTM A182 Grade F6b vs. 1100 Aluminum

ASTM A182 grade F6b belongs to the iron alloys classification, while 1100 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 F6b and the bottom bar is 1100 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 18
1.1 to 32
Fatigue Strength, MPa 440
32 to 71
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 530
54 to 95
Tensile Strength: Ultimate (UTS), MPa 850
86 to 170
Tensile Strength: Yield (Proof), MPa 710
28 to 150

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 750
180
Melting Completion (Liquidus), °C 1450
660
Melting Onset (Solidus), °C 1400
640
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 25
220
Thermal Expansion, µm/m-K 10
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.8
59
Electrical Conductivity: Equal Weight (Specific), % IACS 3.2
190

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
9.0
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.2
8.2
Embodied Energy, MJ/kg 30
150
Embodied Water, L/kg 100
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
0.76 to 52
Resilience: Unit (Modulus of Resilience), kJ/m3 1280
5.7 to 170
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 30
8.7 to 17
Strength to Weight: Bending, points 26
16 to 25
Thermal Diffusivity, mm2/s 6.7
90
Thermal Shock Resistance, points 31
3.7 to 7.4

Alloy Composition

Aluminum (Al), % 0
99 to 99.95
Carbon (C), % 0 to 0.15
0
Chromium (Cr), % 11.5 to 13.5
0
Copper (Cu), % 0 to 0.5
0.050 to 0.2
Iron (Fe), % 81.2 to 87.1
0 to 1.0
Manganese (Mn), % 0 to 1.0
0 to 0.050
Molybdenum (Mo), % 0.4 to 0.6
0
Nickel (Ni), % 1.0 to 2.0
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 1.0
0 to 1.0
Sulfur (S), % 0 to 0.020
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15