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2219 Aluminum vs. EN 1.4568 Stainless Steel

2219 aluminum belongs to the aluminum alloys classification, while EN 1.4568 stainless 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 2219 aluminum and the bottom bar is EN 1.4568 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 2.2 to 20
2.3 to 21
Fatigue Strength, MPa 90 to 130
220 to 670
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
76
Shear Strength, MPa 110 to 280
520 to 930
Tensile Strength: Ultimate (UTS), MPa 180 to 480
830 to 1620
Tensile Strength: Yield (Proof), MPa 88 to 390
330 to 1490

Thermal Properties

Latent Heat of Fusion, J/g 390
280
Maximum Temperature: Mechanical, °C 230
890
Melting Completion (Liquidus), °C 640
1420
Melting Onset (Solidus), °C 540
1380
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 110 to 170
16
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28 to 44
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 81 to 130
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 11
13
Density, g/cm3 3.1
7.7
Embodied Carbon, kg CO2/kg material 8.2
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1130
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.6 to 60
36 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 54 to 1060
290 to 5710
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 44
25
Strength to Weight: Axial, points 16 to 43
30 to 58
Strength to Weight: Bending, points 23 to 44
25 to 40
Thermal Diffusivity, mm2/s 42 to 63
4.3
Thermal Shock Resistance, points 8.2 to 22
23 to 46

Alloy Composition

Aluminum (Al), % 91.5 to 93.8
0.7 to 1.5
Carbon (C), % 0
0 to 0.090
Chromium (Cr), % 0
16 to 18
Copper (Cu), % 5.8 to 6.8
0
Iron (Fe), % 0 to 0.3
70.9 to 76.8
Magnesium (Mg), % 0 to 0.020
0
Manganese (Mn), % 0.2 to 0.4
0 to 1.0
Nickel (Ni), % 0
6.5 to 7.8
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
0 to 0.7
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0.020 to 0.1
0
Vanadium (V), % 0.050 to 0.15
0
Zinc (Zn), % 0 to 0.1
0
Zirconium (Zr), % 0.1 to 0.25
0
Residuals, % 0 to 0.15
0