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333.0 Aluminum vs. EN 1.4515 Stainless Steel

333.0 aluminum belongs to the aluminum alloys classification, while EN 1.4515 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 333.0 aluminum and the bottom bar is EN 1.4515 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
200
Elongation at Break, % 1.0 to 2.0
25
Fatigue Strength, MPa 83 to 100
380
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 28
80
Tensile Strength: Ultimate (UTS), MPa 230 to 280
730
Tensile Strength: Yield (Proof), MPa 130 to 210
550

Thermal Properties

Latent Heat of Fusion, J/g 520
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 590
1440
Melting Onset (Solidus), °C 530
1390
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 100 to 140
16
Thermal Expansion, µm/m-K 21
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26 to 35
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 83 to 110
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 10
19
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 7.6
3.8
Embodied Energy, MJ/kg 140
53
Embodied Water, L/kg 1040
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.1 to 4.6
170
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 290
730
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 49
25
Strength to Weight: Axial, points 22 to 27
26
Strength to Weight: Bending, points 29 to 34
23
Thermal Diffusivity, mm2/s 42 to 57
4.3
Thermal Shock Resistance, points 11 to 13
20

Alloy Composition

Aluminum (Al), % 81.8 to 89
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
24.5 to 26.5
Copper (Cu), % 3.0 to 4.0
0.8 to 1.3
Iron (Fe), % 0 to 1.0
58.4 to 66.6
Magnesium (Mg), % 0.050 to 0.5
0
Manganese (Mn), % 0 to 0.5
0 to 2.0
Molybdenum (Mo), % 0
2.5 to 3.5
Nickel (Ni), % 0 to 0.5
5.5 to 7.0
Nitrogen (N), % 0
0.12 to 0.25
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 8.0 to 10
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0