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5456 Aluminum vs. ASTM A182 Grade F3VCb

5456 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F3VCb belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 5456 aluminum and the bottom bar is ASTM A182 grade F3VCb.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 11 to 18
21
Fatigue Strength, MPa 130 to 210
320
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 190 to 210
420
Tensile Strength: Ultimate (UTS), MPa 320 to 340
670
Tensile Strength: Yield (Proof), MPa 150 to 250
460

Thermal Properties

Latent Heat of Fusion, J/g 390
250
Maximum Temperature: Mechanical, °C 190
470
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 570
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 120
40
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.7
Electrical Conductivity: Equal Weight (Specific), % IACS 97
8.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.5
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 9.0
2.4
Embodied Energy, MJ/kg 150
33
Embodied Water, L/kg 1170
64

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 33 to 46
120
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 470
570
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 33 to 35
24
Strength to Weight: Bending, points 38 to 40
22
Thermal Diffusivity, mm2/s 48
11
Thermal Shock Resistance, points 14 to 15
19

Alloy Composition

Aluminum (Al), % 92 to 94.8
0
Calcium (Ca), % 0
0.00050 to 0.015
Carbon (C), % 0
0.1 to 0.15
Chromium (Cr), % 0.050 to 0.2
2.7 to 3.3
Copper (Cu), % 0 to 0.1
0 to 0.25
Iron (Fe), % 0 to 0.4
93.8 to 95.8
Magnesium (Mg), % 4.7 to 5.5
0
Manganese (Mn), % 0.5 to 1.0
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0
0 to 0.25
Niobium (Nb), % 0
0.015 to 0.070
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.25
0 to 0.1
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.2
0 to 0.015
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0