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ASTM A182 Grade F6b vs. 5383 Aluminum

ASTM A182 grade F6b belongs to the iron alloys classification, while 5383 aluminum belongs to the aluminum alloys. There are 32 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 ASTM A182 grade F6b and the bottom bar is 5383 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 260
85 to 110
Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 18
6.7 to 15
Fatigue Strength, MPa 440
130 to 200
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 530
190 to 220
Tensile Strength: Ultimate (UTS), MPa 850
310 to 370
Tensile Strength: Yield (Proof), MPa 710
150 to 310

Thermal Properties

Latent Heat of Fusion, J/g 280
390
Maximum Temperature: Corrosion, °C 390
65
Maximum Temperature: Mechanical, °C 750
200
Melting Completion (Liquidus), °C 1450
650
Melting Onset (Solidus), °C 1400
540
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 25
130
Thermal Expansion, µm/m-K 10
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.8
29
Electrical Conductivity: Equal Weight (Specific), % IACS 3.2
97

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.2
9.0
Embodied Energy, MJ/kg 30
160
Embodied Water, L/kg 100
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
23 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 1280
170 to 690
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 30
32 to 38
Strength to Weight: Bending, points 26
38 to 42
Thermal Diffusivity, mm2/s 6.7
51
Thermal Shock Resistance, points 31
14 to 16

Alloy Composition

Aluminum (Al), % 0
92 to 95.3
Carbon (C), % 0 to 0.15
0
Chromium (Cr), % 11.5 to 13.5
0 to 0.25
Copper (Cu), % 0 to 0.5
0 to 0.2
Iron (Fe), % 81.2 to 87.1
0 to 0.25
Magnesium (Mg), % 0
4.0 to 5.2
Manganese (Mn), % 0 to 1.0
0.7 to 1.0
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 0.25
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.4
Zirconium (Zr), % 0
0 to 0.2
Residuals, % 0
0 to 0.15