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358.0 Aluminum vs. EN 1.1170 Steel

358.0 aluminum belongs to the aluminum alloys classification, while EN 1.1170 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 358.0 aluminum and the bottom bar is EN 1.1170 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 3.5 to 6.0
16 to 17
Fatigue Strength, MPa 100 to 110
220 to 330
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
73
Shear Strength, MPa 300 to 320
390 to 450
Tensile Strength: Ultimate (UTS), MPa 350 to 370
640 to 730
Tensile Strength: Yield (Proof), MPa 290 to 320
330 to 500

Thermal Properties

Latent Heat of Fusion, J/g 520
250
Maximum Temperature: Mechanical, °C 170
400
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 560
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 150
50
Thermal Expansion, µm/m-K 21
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 130
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 19
2.1
Density, g/cm3 2.6
7.8
Embodied Carbon, kg CO2/kg material 8.7
1.5
Embodied Energy, MJ/kg 160
19
Embodied Water, L/kg 1090
49

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 20
91 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 590 to 710
290 to 670
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 53
24
Strength to Weight: Axial, points 37 to 39
23 to 26
Strength to Weight: Bending, points 42 to 44
21 to 23
Thermal Diffusivity, mm2/s 63
13
Thermal Shock Resistance, points 16 to 17
20 to 23

Alloy Composition

Aluminum (Al), % 89.1 to 91.8
0
Beryllium (Be), % 0.1 to 0.3
0
Carbon (C), % 0
0.25 to 0.32
Chromium (Cr), % 0 to 0.2
0 to 0.4
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.3
96.7 to 98.5
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.2
1.3 to 1.7
Molybdenum (Mo), % 0
0 to 0.1
Nickel (Ni), % 0
0 to 0.4
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 7.6 to 8.6
0 to 0.4
Sulfur (S), % 0
0 to 0.035
Titanium (Ti), % 0.1 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0