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AISI 316L Stainless Steel vs. 512.0 Aluminum

AISI 316L stainless steel belongs to the iron alloys classification, while 512.0 aluminum belongs to the aluminum 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 AISI 316L stainless steel and the bottom bar is 512.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170 to 350
50
Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 9.0 to 50
2.0
Fatigue Strength, MPa 170 to 450
58
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
26
Tensile Strength: Ultimate (UTS), MPa 530 to 1160
130
Tensile Strength: Yield (Proof), MPa 190 to 870
83

Thermal Properties

Latent Heat of Fusion, J/g 290
420
Maximum Temperature: Mechanical, °C 870
180
Melting Completion (Liquidus), °C 1400
630
Melting Onset (Solidus), °C 1380
590
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 15
150
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
38
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
130

Otherwise Unclassified Properties

Base Metal Price, % relative 19
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 3.9
8.8
Embodied Energy, MJ/kg 53
150
Embodied Water, L/kg 150
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 77 to 230
2.3
Resilience: Unit (Modulus of Resilience), kJ/m3 93 to 1880
50
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 19 to 41
14
Strength to Weight: Bending, points 18 to 31
22
Thermal Diffusivity, mm2/s 4.1
60
Thermal Shock Resistance, points 12 to 25
6.1

Alloy Composition

Aluminum (Al), % 0
90.6 to 95.1
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 16 to 18
0 to 0.25
Copper (Cu), % 0
0 to 0.35
Iron (Fe), % 62 to 72
0 to 0.6
Magnesium (Mg), % 0
3.5 to 4.5
Manganese (Mn), % 0 to 2.0
0 to 0.8
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 10 to 14
0
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 0.75
1.4 to 2.2
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.35
Residuals, % 0
0 to 0.15