MakeItFrom.com
Menu (ESC)

5056 Aluminum vs. SAE-AISI 5140 Steel

5056 aluminum belongs to the aluminum alloys classification, while SAE-AISI 5140 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 5140 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
190
Elongation at Break, % 4.9 to 31
12 to 29
Fatigue Strength, MPa 140 to 200
220 to 570
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 25
73
Shear Strength, MPa 170 to 240
360 to 600
Tensile Strength: Ultimate (UTS), MPa 290 to 460
560 to 970
Tensile Strength: Yield (Proof), MPa 150 to 410
290 to 840

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 190
420
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 570
1420
Specific Heat Capacity, J/kg-K 910
470
Thermal Conductivity, W/m-K 130
45
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
49

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 140
76 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 1220
220 to 1880
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 30 to 48
20 to 34
Strength to Weight: Bending, points 36 to 50
19 to 28
Thermal Diffusivity, mm2/s 53
12
Thermal Shock Resistance, points 13 to 20
16 to 29

Alloy Composition

Aluminum (Al), % 93 to 95.4
0
Carbon (C), % 0
0.38 to 0.43
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
97.3 to 98.1
Magnesium (Mg), % 4.5 to 5.6
0
Manganese (Mn), % 0.050 to 0.2
0.7 to 0.9
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