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359.0 Aluminum vs. EN 1.4655 Stainless Steel

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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