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5056 Aluminum vs. SAE-AISI 5160 Steel

5056 aluminum belongs to the aluminum alloys classification, while SAE-AISI 5160 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 5056 aluminum and the bottom bar is SAE-AISI 5160 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
190
Elongation at Break, % 4.9 to 31
12 to 18
Fatigue Strength, MPa 140 to 200
180 to 650
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 25
73
Shear Strength, MPa 170 to 240
390 to 700
Tensile Strength: Ultimate (UTS), MPa 290 to 460
660 to 1150
Tensile Strength: Yield (Proof), MPa 150 to 410
280 to 1010

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 190
420
Melting Completion (Liquidus), °C 640
1450
Melting Onset (Solidus), °C 570
1410
Specific Heat Capacity, J/kg-K 910
470
Thermal Conductivity, W/m-K 130
43
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 99
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.1
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.0
1.4
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 1180
50

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 140
73 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 1220
200 to 2700
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 30 to 48
23 to 41
Strength to Weight: Bending, points 36 to 50
22 to 31
Thermal Diffusivity, mm2/s 53
12
Thermal Shock Resistance, points 13 to 20
19 to 34

Alloy Composition

Aluminum (Al), % 93 to 95.4
0
Carbon (C), % 0
0.56 to 0.61
Chromium (Cr), % 0.050 to 0.2
0.7 to 0.9
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.4
97.1 to 97.8
Magnesium (Mg), % 4.5 to 5.6
0
Manganese (Mn), % 0.050 to 0.2
0.75 to 1.0
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.3
0.15 to 0.35
Sulfur (S), % 0
0 to 0.040
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0

Comparable Variants