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EN 1.4655 Stainless Steel vs. 359.0 Aluminum

EN 1.4655 stainless steel belongs to the iron alloys classification, while 359.0 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 1.4655 stainless steel and the bottom bar is 359.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 23 to 25
3.8 to 4.9
Fatigue Strength, MPa 320
100
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 78
27
Shear Strength, MPa 460
220 to 230
Tensile Strength: Ultimate (UTS), MPa 720 to 730
340 to 350
Tensile Strength: Yield (Proof), MPa 450 to 480
250 to 280

Thermal Properties

Latent Heat of Fusion, J/g 290
530
Maximum Temperature: Mechanical, °C 1050
170
Melting Completion (Liquidus), °C 1420
600
Melting Onset (Solidus), °C 1370
570
Specific Heat Capacity, J/kg-K 480
910
Thermal Conductivity, W/m-K 15
140
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
35
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
120

Otherwise Unclassified Properties

Base Metal Price, % relative 15
9.5
Density, g/cm3 7.7
2.6
Embodied Carbon, kg CO2/kg material 2.9
8.0
Embodied Energy, MJ/kg 41
150
Embodied Water, L/kg 160
1090

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 160
12 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 510 to 580
450 to 540
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
54
Strength to Weight: Axial, points 26
37 to 38
Strength to Weight: Bending, points 23
42 to 43
Thermal Diffusivity, mm2/s 4.0
59
Thermal Shock Resistance, points 20
16 to 17

Alloy Composition


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Aluminum (Al), % 0
88.9 to 91
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 22 to 24
0
Copper (Cu), % 1.0 to 3.0
0 to 0.2
Iron (Fe), % 63.6 to 73.4
0 to 0.2
Magnesium (Mg), % 0
0.5 to 0.7
Manganese (Mn), % 0 to 2.0
0 to 0.1
Molybdenum (Mo), % 0.1 to 0.6
0
Nickel (Ni), % 3.5 to 5.5
0
Nitrogen (N), % 0.050 to 0.2
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 1.0
8.5 to 9.5
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15