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Grey Cast Iron vs. 5383 Aluminum

Grey cast iron belongs to the iron alloys classification, while 5383 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 grey cast iron and the bottom bar is 5383 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 160 to 300
85 to 110
Elastic (Young's, Tensile) Modulus, GPa 180
68
Elongation at Break, % 9.6
6.7 to 15
Fatigue Strength, MPa 69 to 170
130 to 200
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 69
26
Shear Strength, MPa 180 to 610
190 to 220
Tensile Strength: Ultimate (UTS), MPa 160 to 450
310 to 370
Tensile Strength: Yield (Proof), MPa 98 to 290
150 to 310

Thermal Properties

Latent Heat of Fusion, J/g 280
390
Melting Completion (Liquidus), °C 1380
650
Melting Onset (Solidus), °C 1180
540
Specific Heat Capacity, J/kg-K 490
900
Thermal Conductivity, W/m-K 46
130
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.4
29
Electrical Conductivity: Equal Weight (Specific), % IACS 8.9
97

Otherwise Unclassified Properties

Base Metal Price, % relative 1.9
9.5
Density, g/cm3 7.5
2.7
Embodied Carbon, kg CO2/kg material 1.5
9.0
Embodied Energy, MJ/kg 21
160
Embodied Water, L/kg 44
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 37
23 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 27 to 240
170 to 690
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 5.8 to 17
32 to 38
Strength to Weight: Bending, points 8.7 to 17
38 to 42
Thermal Diffusivity, mm2/s 13
51
Thermal Shock Resistance, points 6.0 to 17
14 to 16

Alloy Composition


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Aluminum (Al), % 0
92 to 95.3
Carbon (C), % 3.1 to 3.4
0
Chromium (Cr), % 0
0 to 0.25
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 92.1 to 93.9
0 to 0.25
Magnesium (Mg), % 0
4.0 to 5.2
Manganese (Mn), % 0.5 to 0.7
0.7 to 1.0
Phosphorus (P), % 0 to 0.9
0
Silicon (Si), % 2.5 to 2.8
0 to 0.25
Sulfur (S), % 0 to 0.15
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