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358.0 Aluminum vs. EN 1.1181 Steel

358.0 aluminum belongs to the aluminum alloys classification, while EN 1.1181 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 1.1181 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 3.5 to 6.0
19 to 20
Fatigue Strength, MPa 100 to 110
190 to 260
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
73
Shear Strength, MPa 300 to 320
350 to 390
Tensile Strength: Ultimate (UTS), MPa 350 to 370
560 to 620
Tensile Strength: Yield (Proof), MPa 290 to 320
280 to 380

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
42
Thermal Expansion, µm/m-K 21
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 130
8.3

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
1.4
Embodied Energy, MJ/kg 160
19
Embodied Water, L/kg 1090
47

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 20
90 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 590 to 710
210 to 380
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 53
24
Strength to Weight: Axial, points 37 to 39
20 to 22
Strength to Weight: Bending, points 42 to 44
19 to 21
Thermal Diffusivity, mm2/s 63
11
Thermal Shock Resistance, points 16 to 17
19 to 21

Alloy Composition

Aluminum (Al), % 89.1 to 91.8
0
Beryllium (Be), % 0.1 to 0.3
0
Carbon (C), % 0
0.32 to 0.39
Chromium (Cr), % 0 to 0.2
0 to 0.4
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.3
97.4 to 99.18
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.2
0.5 to 0.8
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