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EN 1.7386 Steel vs. 2219 Aluminum

EN 1.7386 steel belongs to the iron alloys classification, while 2219 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 EN 1.7386 steel and the bottom bar is 2219 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 18 to 21
2.2 to 20
Fatigue Strength, MPa 170 to 290
90 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Shear Strength, MPa 340 to 410
110 to 280
Tensile Strength: Ultimate (UTS), MPa 550 to 670
180 to 480
Tensile Strength: Yield (Proof), MPa 240 to 440
88 to 390

Thermal Properties

Latent Heat of Fusion, J/g 270
390
Maximum Temperature: Mechanical, °C 600
230
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1410
540
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 26
110 to 170
Thermal Expansion, µm/m-K 13
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.0
28 to 44
Electrical Conductivity: Equal Weight (Specific), % IACS 10
81 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 6.5
11
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 2.0
8.2
Embodied Energy, MJ/kg 28
150
Embodied Water, L/kg 88
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 92 to 110
9.6 to 60
Resilience: Unit (Modulus of Resilience), kJ/m3 150 to 490
54 to 1060
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
44
Strength to Weight: Axial, points 20 to 24
16 to 43
Strength to Weight: Bending, points 19 to 22
23 to 44
Thermal Diffusivity, mm2/s 6.9
42 to 63
Thermal Shock Resistance, points 15 to 18
8.2 to 22

Alloy Composition

Aluminum (Al), % 0 to 0.040
91.5 to 93.8
Carbon (C), % 0.080 to 0.15
0
Chromium (Cr), % 8.0 to 10
0
Copper (Cu), % 0 to 0.3
5.8 to 6.8
Iron (Fe), % 86.8 to 90.5
0 to 0.3
Magnesium (Mg), % 0
0 to 0.020
Manganese (Mn), % 0.3 to 0.6
0.2 to 0.4
Molybdenum (Mo), % 0.9 to 1.1
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.25 to 1.0
0 to 0.2
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0.020 to 0.1
Vanadium (V), % 0
0.050 to 0.15
Zinc (Zn), % 0
0 to 0.1
Zirconium (Zr), % 0
0.1 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants