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5086 Aluminum vs. Grey Cast Iron

5086 aluminum belongs to the aluminum alloys classification, while grey cast iron 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 5086 aluminum and the bottom bar is grey cast iron.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 65 to 100
160 to 300
Elastic (Young's, Tensile) Modulus, GPa 68
180
Elongation at Break, % 1.7 to 20
9.6
Fatigue Strength, MPa 88 to 180
69 to 170
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
69
Shear Strength, MPa 160 to 230
180 to 610
Tensile Strength: Ultimate (UTS), MPa 270 to 390
160 to 450
Tensile Strength: Yield (Proof), MPa 110 to 320
98 to 290

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Melting Completion (Liquidus), °C 640
1380
Melting Onset (Solidus), °C 590
1180
Specific Heat Capacity, J/kg-K 900
490
Thermal Conductivity, W/m-K 130
46
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
7.4
Electrical Conductivity: Equal Weight (Specific), % IACS 100
8.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
1.9
Density, g/cm3 2.7
7.5
Embodied Carbon, kg CO2/kg material 8.8
1.5
Embodied Energy, MJ/kg 150
21
Embodied Water, L/kg 1180
44

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.8 to 42
13 to 37
Resilience: Unit (Modulus of Resilience), kJ/m3 86 to 770
27 to 240
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 28 to 40
5.8 to 17
Strength to Weight: Bending, points 34 to 44
8.7 to 17
Thermal Diffusivity, mm2/s 52
13
Thermal Shock Resistance, points 12 to 17
6.0 to 17

Alloy Composition

Aluminum (Al), % 93 to 96.3
0
Carbon (C), % 0
3.1 to 3.4
Chromium (Cr), % 0.050 to 0.25
0
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.5
92.1 to 93.9
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0.2 to 0.7
0.5 to 0.7
Phosphorus (P), % 0
0 to 0.9
Silicon (Si), % 0 to 0.4
2.5 to 2.8
Sulfur (S), % 0
0 to 0.15
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0