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EN 1.4567 Stainless Steel vs. 511.0 Aluminum

EN 1.4567 stainless steel belongs to the iron alloys classification, while 511.0 aluminum belongs to the aluminum alloys. There are 31 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 1.4567 stainless steel and the bottom bar is 511.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190 to 240
50
Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 22 to 51
3.0
Fatigue Strength, MPa 190 to 260
55
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
25
Shear Strength, MPa 390 to 490
120
Tensile Strength: Ultimate (UTS), MPa 550 to 780
150
Tensile Strength: Yield (Proof), MPa 200 to 390
83

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Mechanical, °C 930
170
Melting Completion (Liquidus), °C 1410
640
Melting Onset (Solidus), °C 1370
590
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 11
140
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
36
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
120

Otherwise Unclassified Properties

Base Metal Price, % relative 16
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 3.1
8.8
Embodied Energy, MJ/kg 43
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 220
3.7
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 400
51
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 19 to 27
15
Strength to Weight: Bending, points 19 to 24
23
Thermal Diffusivity, mm2/s 3.0
59
Thermal Shock Resistance, points 12 to 17
6.5

Alloy Composition


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Aluminum (Al), % 0
93.3 to 96.2
Carbon (C), % 0 to 0.040
0
Chromium (Cr), % 17 to 19
0
Copper (Cu), % 3.0 to 4.0
0 to 0.15
Iron (Fe), % 63.3 to 71.5
0 to 0.5
Magnesium (Mg), % 0
3.5 to 4.5
Manganese (Mn), % 0 to 2.0
0 to 0.35
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
0.3 to 0.7
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.15
Residuals, % 0
0 to 0.15