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SAE-AISI 1086 Steel vs. 6151 Aluminum

SAE-AISI 1086 steel belongs to the iron alloys classification, while 6151 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 1086 steel and the bottom bar is 6151 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 11
1.1 to 5.7
Fatigue Strength, MPa 300 to 360
80 to 100
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
26
Shear Strength, MPa 450 to 520
190 to 200
Tensile Strength: Ultimate (UTS), MPa 760 to 870
330 to 340
Tensile Strength: Yield (Proof), MPa 480 to 580
270 to 280

Thermal Properties

Latent Heat of Fusion, J/g 240
410
Maximum Temperature: Mechanical, °C 400
170
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1410
590
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 50
170
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.0
45
Electrical Conductivity: Equal Weight (Specific), % IACS 8.1
150

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.4
8.2
Embodied Energy, MJ/kg 19
150
Embodied Water, L/kg 45
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 79 to 84
3.5 to 18
Resilience: Unit (Modulus of Resilience), kJ/m3 610 to 890
520 to 580
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 27 to 31
34
Strength to Weight: Bending, points 24 to 26
39
Thermal Diffusivity, mm2/s 14
70
Thermal Shock Resistance, points 26 to 30
15

Alloy Composition

Aluminum (Al), % 0
95.6 to 98.8
Carbon (C), % 0.8 to 0.93
0
Chromium (Cr), % 0
0.15 to 0.35
Copper (Cu), % 0
0 to 0.35
Iron (Fe), % 98.5 to 98.9
0 to 1.0
Magnesium (Mg), % 0
0.45 to 0.8
Manganese (Mn), % 0.3 to 0.5
0 to 0.2
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0
0.6 to 1.2
Sulfur (S), % 0 to 0.050
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15