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AISI 316L Stainless Steel vs. 1060 Aluminum

AISI 316L stainless steel belongs to the iron alloys classification, while 1060 aluminum belongs to the aluminum alloys. There are 31 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 AISI 316L stainless steel and the bottom bar is 1060 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 9.0 to 50
1.1 to 30
Fatigue Strength, MPa 170 to 450
15 to 50
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
26
Shear Strength, MPa 370 to 690
42 to 75
Tensile Strength: Ultimate (UTS), MPa 530 to 1160
67 to 130
Tensile Strength: Yield (Proof), MPa 190 to 870
17 to 110

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Mechanical, °C 870
170
Melting Completion (Liquidus), °C 1400
660
Melting Onset (Solidus), °C 1380
650
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 15
230
Thermal Expansion, µm/m-K 16
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
62
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
210

Otherwise Unclassified Properties

Base Metal Price, % relative 19
9.5
Calomel Potential, mV -50
-750
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 3.9
8.3
Embodied Energy, MJ/kg 53
160
Embodied Water, L/kg 150
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 77 to 230
0.57 to 37
Resilience: Unit (Modulus of Resilience), kJ/m3 93 to 1880
2.1 to 89
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 19 to 41
6.9 to 13
Strength to Weight: Bending, points 18 to 31
14 to 21
Thermal Diffusivity, mm2/s 4.1
96
Thermal Shock Resistance, points 12 to 25
3.0 to 5.6

Alloy Composition

Aluminum (Al), % 0
99.6 to 100
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 16 to 18
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 62 to 72
0 to 0.35
Magnesium (Mg), % 0
0 to 0.030
Manganese (Mn), % 0 to 2.0
0 to 0.030
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
0 to 0.25
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.030
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.050

Comparable Variants