MakeItFrom.com
Menu (ESC)

EN 1.0566 Steel vs. 5042 Aluminum

EN 1.0566 steel belongs to the iron alloys classification, while 5042 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 EN 1.0566 steel and the bottom bar is 5042 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 24
1.1 to 3.4
Fatigue Strength, MPa 270
97 to 120
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
26
Shear Strength, MPa 350
200
Tensile Strength: Ultimate (UTS), MPa 550
340 to 360
Tensile Strength: Yield (Proof), MPa 370
270 to 310

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 400
180
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1420
570
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 50
130
Thermal Expansion, µm/m-K 12
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.4
33
Electrical Conductivity: Equal Weight (Specific), % IACS 8.5
110

Otherwise Unclassified Properties

Base Metal Price, % relative 2.3
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.6
8.8
Embodied Energy, MJ/kg 22
150
Embodied Water, L/kg 50
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
3.6 to 12
Resilience: Unit (Modulus of Resilience), kJ/m3 360
550 to 720
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 19
35 to 37
Strength to Weight: Bending, points 19
40 to 42
Thermal Diffusivity, mm2/s 14
53
Thermal Shock Resistance, points 17
15 to 16

Alloy Composition


Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
Aluminum (Al), % 0.020 to 0.024
94.2 to 96.8
Carbon (C), % 0 to 0.18
0
Chromium (Cr), % 0 to 0.3
0 to 0.1
Copper (Cu), % 0 to 0.3
0 to 0.15
Iron (Fe), % 96.2 to 98.9
0 to 0.35
Magnesium (Mg), % 0
3.0 to 4.0
Manganese (Mn), % 1.1 to 1.7
0.2 to 0.5
Molybdenum (Mo), % 0 to 0.080
0
Nickel (Ni), % 0 to 0.5
0
Niobium (Nb), % 0 to 0.050
0
Nitrogen (N), % 0 to 0.012
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 0.2
Sulfur (S), % 0 to 0.0080
0
Titanium (Ti), % 0 to 0.030
0 to 0.1
Vanadium (V), % 0 to 0.1
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15