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518.0 Aluminum vs. SAE-AISI 1151 Steel

518.0 aluminum belongs to the aluminum alloys classification, while SAE-AISI 1151 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 518.0 aluminum and the bottom bar is SAE-AISI 1151 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 80
210 to 220
Elastic (Young's, Tensile) Modulus, GPa 67
190
Elongation at Break, % 5.0
11 to 17
Fatigue Strength, MPa 140
260 to 410
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 25
72
Shear Strength, MPa 200
430 to 480
Tensile Strength: Ultimate (UTS), MPa 310
710 to 800
Tensile Strength: Yield (Proof), MPa 190
390 to 660

Thermal Properties

Latent Heat of Fusion, J/g 390
250
Maximum Temperature: Mechanical, °C 170
400
Melting Completion (Liquidus), °C 620
1460
Melting Onset (Solidus), °C 560
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 98
51
Thermal Expansion, µm/m-K 24
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 24
10
Electrical Conductivity: Equal Weight (Specific), % IACS 81
12

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
1.8
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.4
1.4
Embodied Energy, MJ/kg 150
18
Embodied Water, L/kg 1160
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14
86 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 270
400 to 1170
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 32
25 to 28
Strength to Weight: Bending, points 38
22 to 24
Thermal Diffusivity, mm2/s 40
14
Thermal Shock Resistance, points 14
22 to 25

Alloy Composition


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Aluminum (Al), % 88.1 to 92.5
0
Carbon (C), % 0
0.48 to 0.55
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0 to 1.8
98.3 to 98.7
Magnesium (Mg), % 7.5 to 8.5
0
Manganese (Mn), % 0 to 0.35
0.7 to 1.0
Nickel (Ni), % 0 to 0.15
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.35
0
Sulfur (S), % 0
0.080 to 0.13
Tin (Sn), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0 to 0.25
0