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B535.0 Aluminum vs. EN 1.7380 Steel

B535.0 aluminum belongs to the aluminum alloys classification, while EN 1.7380 steel belongs to the iron alloys. There are 31 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 B535.0 aluminum and the bottom bar is EN 1.7380 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 65
160 to 170
Elastic (Young's, Tensile) Modulus, GPa 66
190
Elongation at Break, % 10
19 to 20
Fatigue Strength, MPa 62
200 to 230
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 25
74
Shear Strength, MPa 210
330 to 350
Tensile Strength: Ultimate (UTS), MPa 260
540 to 550
Tensile Strength: Yield (Proof), MPa 130
290 to 330

Thermal Properties

Latent Heat of Fusion, J/g 390
260
Maximum Temperature: Mechanical, °C 170
460
Melting Completion (Liquidus), °C 630
1470
Melting Onset (Solidus), °C 550
1430
Specific Heat Capacity, J/kg-K 910
470
Thermal Conductivity, W/m-K 96
39
Thermal Expansion, µm/m-K 25
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 24
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 82
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.8
Density, g/cm3 2.6
7.9
Embodied Carbon, kg CO2/kg material 9.4
1.8
Embodied Energy, MJ/kg 160
23
Embodied Water, L/kg 1180
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 22
87 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 130
230 to 280
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 28
19 to 20
Strength to Weight: Bending, points 35
19
Thermal Diffusivity, mm2/s 40
11
Thermal Shock Resistance, points 11
15 to 16

Alloy Composition

Aluminum (Al), % 91.7 to 93.4
0
Carbon (C), % 0
0.080 to 0.14
Chromium (Cr), % 0
2.0 to 2.5
Copper (Cu), % 0 to 0.1
0 to 0.3
Iron (Fe), % 0 to 0.15
94.6 to 96.6
Magnesium (Mg), % 6.5 to 7.5
0
Manganese (Mn), % 0 to 0.050
0.4 to 0.8
Molybdenum (Mo), % 0
0.9 to 1.1
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.15
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0.1 to 0.25
0
Residuals, % 0 to 0.15
0