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771.0 Aluminum vs. Automotive Malleable Cast Iron

771.0 aluminum belongs to the aluminum alloys classification, while automotive malleable cast iron belongs to the iron alloys. There are 28 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 771.0 aluminum and the bottom bar is automotive malleable cast iron.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85 to 120
130 to 290
Elastic (Young's, Tensile) Modulus, GPa 70
180
Elongation at Break, % 1.7 to 6.5
1.0 to 10
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
70
Tensile Strength: Ultimate (UTS), MPa 250 to 370
350 to 720
Tensile Strength: Yield (Proof), MPa 210 to 350
220 to 590

Thermal Properties

Latent Heat of Fusion, J/g 380
260
Melting Completion (Liquidus), °C 630
1410
Melting Onset (Solidus), °C 620
1370
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 140 to 150
41
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
7.4
Electrical Conductivity: Equal Weight (Specific), % IACS 82
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
1.9
Density, g/cm3 3.0
7.6
Embodied Carbon, kg CO2/kg material 8.0
1.5
Embodied Energy, MJ/kg 150
20
Embodied Water, L/kg 1130
45

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.4 to 20
6.8 to 30
Resilience: Unit (Modulus of Resilience), kJ/m3 310 to 900
130 to 950
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 23 to 35
13 to 26
Strength to Weight: Bending, points 29 to 39
14 to 24
Thermal Diffusivity, mm2/s 54 to 58
11
Thermal Shock Resistance, points 11 to 16
9.9 to 21

Alloy Composition


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Aluminum (Al), % 90.5 to 92.5
0
Carbon (C), % 0
2.2 to 2.9
Chromium (Cr), % 0.060 to 0.2
0
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.15
93.6 to 96.7
Magnesium (Mg), % 0.8 to 1.0
0
Manganese (Mn), % 0 to 0.1
0.15 to 1.3
Phosphorus (P), % 0
0.020 to 0.15
Silicon (Si), % 0 to 0.15
0.9 to 1.9
Sulfur (S), % 0
0.020 to 0.2
Titanium (Ti), % 0.1 to 0.2
0
Zinc (Zn), % 6.5 to 7.5
0
Residuals, % 0 to 0.15
0