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5059 Aluminum vs. SAE-AISI 6150 Steel

5059 aluminum belongs to the aluminum alloys classification, while SAE-AISI 6150 steel belongs to the iron 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 5059 aluminum and the bottom bar is SAE-AISI 6150 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 11 to 25
15 to 23
Fatigue Strength, MPa 170 to 240
300 to 750
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 220 to 250
400 to 730
Tensile Strength: Ultimate (UTS), MPa 350 to 410
630 to 1200
Tensile Strength: Yield (Proof), MPa 170 to 300
420 to 1160

Thermal Properties

Latent Heat of Fusion, J/g 390
250
Maximum Temperature: Mechanical, °C 210
420
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 510
1410
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 110
46
Thermal Expansion, µm/m-K 24
12 to 13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 95
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.3
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.1
2.0
Embodied Energy, MJ/kg 160
28
Embodied Water, L/kg 1160
51

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 75
130 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 650
460 to 3590
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 36 to 42
22 to 43
Strength to Weight: Bending, points 41 to 45
21 to 32
Thermal Diffusivity, mm2/s 44
13
Thermal Shock Resistance, points 16 to 18
20 to 38

Alloy Composition

Aluminum (Al), % 89.9 to 94
0
Carbon (C), % 0
0.48 to 0.53
Chromium (Cr), % 0 to 0.25
0.8 to 1.1
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0 to 0.5
96.7 to 97.7
Magnesium (Mg), % 5.0 to 6.0
0
Manganese (Mn), % 0.6 to 1.2
0.7 to 0.9
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.45
0.15 to 0.35
Sulfur (S), % 0
0 to 0.040
Titanium (Ti), % 0 to 0.2
0
Vanadium (V), % 0
0.15 to 0.3
Zinc (Zn), % 0.4 to 0.9
0
Zirconium (Zr), % 0.050 to 0.25
0
Residuals, % 0 to 0.15
0

Comparable Variants