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1350 Aluminum vs. EN 1.7711 Steel

1350 aluminum belongs to the aluminum alloys classification, while EN 1.7711 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 1350 aluminum and the bottom bar is EN 1.7711 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 20 to 45
210 to 280
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 1.4 to 30
16 to 22
Fatigue Strength, MPa 24 to 50
290 to 520
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 44 to 110
440 to 570
Tensile Strength: Ultimate (UTS), MPa 68 to 190
690 to 930
Tensile Strength: Yield (Proof), MPa 25 to 170
400 to 800

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 170
430
Melting Completion (Liquidus), °C 660
1460
Melting Onset (Solidus), °C 650
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 230
33
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61 to 62
7.4
Electrical Conductivity: Equal Weight (Specific), % IACS 200 to 210
8.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.0
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
2.3
Embodied Energy, MJ/kg 160
32
Embodied Water, L/kg 1200
54

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 0.77 to 54
130 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 4.4 to 200
430 to 1690
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 7.0 to 19
24 to 33
Strength to Weight: Bending, points 14 to 27
22 to 27
Thermal Diffusivity, mm2/s 96
8.9
Thermal Shock Resistance, points 3.0 to 8.2
24 to 32

Alloy Composition

Aluminum (Al), % 99.5 to 100
0 to 0.015
Boron (B), % 0 to 0.050
0
Carbon (C), % 0
0.36 to 0.44
Chromium (Cr), % 0 to 0.010
0.9 to 1.2
Copper (Cu), % 0 to 0.050
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.4
96 to 97.5
Manganese (Mn), % 0 to 0.010
0.45 to 0.85
Molybdenum (Mo), % 0
0.5 to 0.65
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.1
0 to 0.4
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.020
0
Vanadium (V), % 0 to 0.020
0.25 to 0.35
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.1
0

Comparable Variants