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SAE-AISI 1080 Steel vs. 2007 Aluminum

SAE-AISI 1080 steel belongs to the iron alloys classification, while 2007 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 SAE-AISI 1080 steel and the bottom bar is 2007 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 11
5.6 to 8.0
Fatigue Strength, MPa 300 to 360
91 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
27
Shear Strength, MPa 460 to 520
220 to 250
Tensile Strength: Ultimate (UTS), MPa 770 to 870
370 to 420
Tensile Strength: Yield (Proof), MPa 480 to 590
240 to 270

Thermal Properties

Latent Heat of Fusion, J/g 250
390
Maximum Temperature: Mechanical, °C 400
190
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1410
510
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 51
130
Thermal Expansion, µm/m-K 12
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.6
47
Electrical Conductivity: Equal Weight (Specific), % IACS 11
140

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
11
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 1.4
8.0
Embodied Energy, MJ/kg 19
150
Embodied Water, L/kg 46
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 80 to 84
21 to 26
Resilience: Unit (Modulus of Resilience), kJ/m3 610 to 920
390 to 530
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
44
Strength to Weight: Axial, points 27 to 31
33 to 38
Strength to Weight: Bending, points 24 to 26
37 to 40
Thermal Diffusivity, mm2/s 14
48
Thermal Shock Resistance, points 25 to 29
16 to 19

Alloy Composition

Aluminum (Al), % 0
87.5 to 95
Bismuth (Bi), % 0
0 to 0.2
Carbon (C), % 0.75 to 0.88
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0
3.3 to 4.6
Iron (Fe), % 98.1 to 98.7
0 to 0.8
Lead (Pb), % 0
0.8 to 1.5
Magnesium (Mg), % 0
0.4 to 1.8
Manganese (Mn), % 0.6 to 0.9
0.5 to 1.0
Nickel (Ni), % 0
0 to 0.2
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0
0 to 0.8
Sulfur (S), % 0 to 0.050
0
Tin (Sn), % 0
0 to 0.2
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.8
Residuals, % 0
0 to 0.3