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5083 Aluminum vs. ASTM A182 Grade F3VCb

5083 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F3VCb belongs to the iron alloys. There are 31 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 5083 aluminum and the bottom bar is ASTM A182 grade F3VCb.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75 to 110
210
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 1.1 to 17
21
Fatigue Strength, MPa 93 to 190
320
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 170 to 220
420
Tensile Strength: Ultimate (UTS), MPa 290 to 390
670
Tensile Strength: Yield (Proof), MPa 110 to 340
460

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 190
470
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 580
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 96
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 8.9
2.4
Embodied Energy, MJ/kg 150
33
Embodied Water, L/kg 1170
64

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.2 to 42
120
Resilience: Unit (Modulus of Resilience), kJ/m3 95 to 860
570
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 29 to 40
24
Strength to Weight: Bending, points 36 to 44
22
Thermal Diffusivity, mm2/s 48
11
Thermal Shock Resistance, points 12 to 17
19

Alloy Composition

Aluminum (Al), % 92.4 to 95.6
0
Calcium (Ca), % 0
0.00050 to 0.015
Carbon (C), % 0
0.1 to 0.15
Chromium (Cr), % 0.050 to 0.25
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), % 4.0 to 4.9
0
Manganese (Mn), % 0.4 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 0.4
0 to 0.1
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.15
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