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EN 1.4567 Stainless Steel vs. 2011A Aluminum

EN 1.4567 stainless steel belongs to the iron alloys classification, while 2011A aluminum belongs to the aluminum 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 EN 1.4567 stainless steel and the bottom bar is 2011A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 22 to 51
6.8 to 16
Fatigue Strength, MPa 190 to 260
75 to 100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 390 to 490
190 to 250
Tensile Strength: Ultimate (UTS), MPa 550 to 780
310 to 410
Tensile Strength: Yield (Proof), MPa 200 to 390
140 to 310

Thermal Properties

Latent Heat of Fusion, J/g 290
390
Maximum Temperature: Mechanical, °C 930
190
Melting Completion (Liquidus), °C 1410
660
Melting Onset (Solidus), °C 1370
550
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 11
130
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
33
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
96

Otherwise Unclassified Properties

Base Metal Price, % relative 16
11
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 3.1
7.9
Embodied Energy, MJ/kg 43
150
Embodied Water, L/kg 150
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 220
20 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 400
140 to 670
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
44
Strength to Weight: Axial, points 19 to 27
28 to 37
Strength to Weight: Bending, points 19 to 24
33 to 40
Thermal Diffusivity, mm2/s 3.0
49
Thermal Shock Resistance, points 12 to 17
14 to 18

Alloy Composition

Aluminum (Al), % 0
91.5 to 95.1
Bismuth (Bi), % 0
0.2 to 0.6
Carbon (C), % 0 to 0.040
0
Chromium (Cr), % 17 to 19
0
Copper (Cu), % 3.0 to 4.0
4.5 to 6.0
Iron (Fe), % 63.3 to 71.5
0 to 0.5
Lead (Pb), % 0
0.2 to 0.6
Manganese (Mn), % 0 to 2.0
0
Nickel (Ni), % 8.5 to 10.5
0
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0 to 0.4
Sulfur (S), % 0 to 0.015
0
Zinc (Zn), % 0
0 to 0.3
Residuals, % 0
0 to 0.15