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336.0 Aluminum vs. EN 1.6554 Steel

336.0 aluminum belongs to the aluminum alloys classification, while EN 1.6554 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 336.0 aluminum and the bottom bar is EN 1.6554 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 110 to 130
230 to 280
Elastic (Young's, Tensile) Modulus, GPa 75
190
Elongation at Break, % 0.5
17 to 21
Fatigue Strength, MPa 80 to 93
380 to 520
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
73
Tensile Strength: Ultimate (UTS), MPa 250 to 320
780 to 930
Tensile Strength: Yield (Proof), MPa 190 to 300
550 to 790

Thermal Properties

Latent Heat of Fusion, J/g 570
250
Maximum Temperature: Mechanical, °C 210
420
Melting Completion (Liquidus), °C 570
1460
Melting Onset (Solidus), °C 540
1420
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 120
40
Thermal Expansion, µm/m-K 19
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 95
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 11
3.4
Density, g/cm3 2.8
7.9
Embodied Carbon, kg CO2/kg material 7.9
1.7
Embodied Energy, MJ/kg 140
22
Embodied Water, L/kg 1010
53

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.1 to 1.6
140 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
810 to 1650
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 25 to 32
27 to 33
Strength to Weight: Bending, points 32 to 38
24 to 27
Thermal Diffusivity, mm2/s 48
11
Thermal Shock Resistance, points 12 to 16
23 to 27

Alloy Composition

Aluminum (Al), % 79.1 to 85.8
0
Carbon (C), % 0
0.23 to 0.28
Chromium (Cr), % 0
0.7 to 0.9
Copper (Cu), % 0.5 to 1.5
0 to 0.3
Iron (Fe), % 0 to 1.2
94.6 to 97.3
Magnesium (Mg), % 0.7 to 1.3
0
Manganese (Mn), % 0 to 0.35
0.6 to 0.9
Molybdenum (Mo), % 0
0.2 to 0.3
Nickel (Ni), % 2.0 to 3.0
1.0 to 2.0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 11 to 13
0 to 0.6
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0 to 0.030
Zinc (Zn), % 0 to 0.35
0

Comparable Variants