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EN 1.0565 Steel vs. 201.0 Aluminum

EN 1.0565 steel belongs to the iron alloys classification, while 201.0 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 1.0565 steel and the bottom bar is 201.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 160
95 to 140
Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 24
4.4 to 20
Fatigue Strength, MPa 260
120 to 150
Impact Strength: V-Notched Charpy, J 71
10 to 22
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
27
Shear Strength, MPa 350
290
Tensile Strength: Ultimate (UTS), MPa 550
370 to 470
Tensile Strength: Yield (Proof), MPa 360
220 to 400

Thermal Properties

Latent Heat of Fusion, J/g 250
390
Maximum Temperature: Mechanical, °C 400
170
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1420
570
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 50
120
Thermal Expansion, µm/m-K 12
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.4
30 to 33
Electrical Conductivity: Equal Weight (Specific), % IACS 8.5
87 to 97

Otherwise Unclassified Properties

Base Metal Price, % relative 2.3
38
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 1.6
8.7
Embodied Energy, MJ/kg 22
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
19 to 63
Resilience: Unit (Modulus of Resilience), kJ/m3 340
330 to 1160
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 19
33 to 42
Strength to Weight: Bending, points 19
37 to 44
Thermal Diffusivity, mm2/s 14
45
Thermal Shock Resistance, points 17
19 to 25

Alloy Composition


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Aluminum (Al), % 0 to 0.060
92.1 to 95.1
Carbon (C), % 0 to 0.2
0
Chromium (Cr), % 0 to 0.3
0
Copper (Cu), % 0 to 0.3
4.0 to 5.2
Iron (Fe), % 96.2 to 99
0 to 0.15
Magnesium (Mg), % 0
0.15 to 0.55
Manganese (Mn), % 0.9 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 0.020
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 0.1
Silver (Ag), % 0
0.4 to 1.0
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.030
0.15 to 0.35
Vanadium (V), % 0 to 0.1
0
Residuals, % 0
0 to 0.1