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EN AC-51400 Aluminum vs. AISI 316L Stainless Steel

EN AC-51400 aluminum belongs to the aluminum alloys classification, while AISI 316L stainless steel belongs to the iron alloys. There are 30 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 EN AC-51400 aluminum and the bottom bar is AISI 316L stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 71
170 to 350
Elastic (Young's, Tensile) Modulus, GPa 67
200
Elongation at Break, % 3.4
9.0 to 50
Fatigue Strength, MPa 85
170 to 450
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
78
Tensile Strength: Ultimate (UTS), MPa 190
530 to 1160
Tensile Strength: Yield (Proof), MPa 120
190 to 870

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 170
870
Melting Completion (Liquidus), °C 640
1400
Melting Onset (Solidus), °C 600
1380
Specific Heat Capacity, J/kg-K 910
470
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
19
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 9.1
3.9
Embodied Energy, MJ/kg 150
53
Embodied Water, L/kg 1170
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.6
77 to 230
Resilience: Unit (Modulus of Resilience), kJ/m3 110
93 to 1880
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 20
19 to 41
Strength to Weight: Bending, points 28
18 to 31
Thermal Diffusivity, mm2/s 46
4.1
Thermal Shock Resistance, points 8.6
12 to 25

Alloy Composition

Aluminum (Al), % 90.5 to 95.5
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
16 to 18
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.55
62 to 72
Magnesium (Mg), % 4.5 to 6.5
0
Manganese (Mn), % 0 to 0.45
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 3.0
Nickel (Ni), % 0
10 to 14
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 1.5
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0