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EN 1.4415 Stainless Steel vs. 8176 Aluminum

EN 1.4415 stainless steel belongs to the iron alloys classification, while 8176 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 1.4415 stainless steel and the bottom bar is 8176 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 17 to 20
15
Fatigue Strength, MPa 470 to 510
59
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 520 to 570
70
Tensile Strength: Ultimate (UTS), MPa 830 to 930
160
Tensile Strength: Yield (Proof), MPa 730 to 840
95

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 790
170
Melting Completion (Liquidus), °C 1460
660
Melting Onset (Solidus), °C 1420
650
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 19
230
Thermal Expansion, µm/m-K 9.9
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
61
Electrical Conductivity: Equal Weight (Specific), % IACS 2.8
200

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 3.6
8.2
Embodied Energy, MJ/kg 51
150
Embodied Water, L/kg 120
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 160
21
Resilience: Unit (Modulus of Resilience), kJ/m3 1350 to 1790
66
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 29 to 33
16
Strength to Weight: Bending, points 25 to 27
24
Thermal Diffusivity, mm2/s 5.1
93
Thermal Shock Resistance, points 30 to 34
7.0

Alloy Composition

Aluminum (Al), % 0
98.6 to 99.6
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 11.5 to 13.5
0
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 75.9 to 82.4
0.4 to 1.0
Manganese (Mn), % 0 to 0.5
0
Molybdenum (Mo), % 1.5 to 2.5
0
Nickel (Ni), % 4.5 to 6.5
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 0.5
0.030 to 0.15
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.010
0
Vanadium (V), % 0.1 to 0.5
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15