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EN 1.4107 Stainless Steel vs. EN AC-51500 Aluminum

EN 1.4107 stainless steel belongs to the iron alloys classification, while EN AC-51500 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 1.4107 stainless steel and the bottom bar is EN AC-51500 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 18 to 21
5.6
Fatigue Strength, MPa 260 to 350
120
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Tensile Strength: Ultimate (UTS), MPa 620 to 700
280
Tensile Strength: Yield (Proof), MPa 400 to 570
160

Thermal Properties

Latent Heat of Fusion, J/g 270
430
Maximum Temperature: Mechanical, °C 740
170
Melting Completion (Liquidus), °C 1450
630
Melting Onset (Solidus), °C 1410
590
Specific Heat Capacity, J/kg-K 480
910
Thermal Conductivity, W/m-K 27
120
Thermal Expansion, µm/m-K 10
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
26
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
88

Otherwise Unclassified Properties

Base Metal Price, % relative 7.5
9.5
Density, g/cm3 7.8
2.6
Embodied Carbon, kg CO2/kg material 2.1
9.0
Embodied Energy, MJ/kg 30
150
Embodied Water, L/kg 100
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 120
13
Resilience: Unit (Modulus of Resilience), kJ/m3 420 to 840
190
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
52
Strength to Weight: Axial, points 22 to 25
29
Strength to Weight: Bending, points 21 to 22
36
Thermal Diffusivity, mm2/s 7.2
49
Thermal Shock Resistance, points 22 to 25
13

Alloy Composition

Aluminum (Al), % 0
89.8 to 93.1
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 11.5 to 12.5
0
Copper (Cu), % 0 to 0.3
0 to 0.050
Iron (Fe), % 83.8 to 87.2
0 to 0.25
Magnesium (Mg), % 0
4.7 to 6.0
Manganese (Mn), % 0.5 to 0.8
0.4 to 0.8
Molybdenum (Mo), % 0 to 0.5
0
Nickel (Ni), % 0.8 to 1.5
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.4
1.8 to 2.6
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
0 to 0.25
Vanadium (V), % 0 to 0.080
0
Zinc (Zn), % 0
0 to 0.070
Residuals, % 0
0 to 0.15