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5456 Aluminum vs. EN 1.7336 Steel

5456 aluminum belongs to the aluminum alloys classification, while EN 1.7336 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 5456 aluminum and the bottom bar is EN 1.7336 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 11 to 18
22
Fatigue Strength, MPa 130 to 210
240 to 310
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 190 to 210
370
Tensile Strength: Ultimate (UTS), MPa 320 to 340
590
Tensile Strength: Yield (Proof), MPa 150 to 250
340 to 440

Thermal Properties

Latent Heat of Fusion, J/g 390
260
Maximum Temperature: Mechanical, °C 190
430
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 570
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 120
40
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 97
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.1
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.0
1.6
Embodied Energy, MJ/kg 150
21
Embodied Water, L/kg 1170
53

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 33 to 46
110 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 470
310 to 510
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 33 to 35
21
Strength to Weight: Bending, points 38 to 40
20
Thermal Diffusivity, mm2/s 48
11
Thermal Shock Resistance, points 14 to 15
17

Alloy Composition

Aluminum (Al), % 92 to 94.8
0
Carbon (C), % 0
0 to 0.17
Chromium (Cr), % 0.050 to 0.2
1.0 to 1.5
Copper (Cu), % 0 to 0.1
0 to 0.3
Iron (Fe), % 0 to 0.4
95.6 to 97.7
Magnesium (Mg), % 4.7 to 5.5
0
Manganese (Mn), % 0.5 to 1.0
0.4 to 0.65
Molybdenum (Mo), % 0
0.45 to 0.65
Nickel (Ni), % 0
0 to 0.3
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 0.25
0.5 to 0.8
Sulfur (S), % 0
0 to 0.0050
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0