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AISI 316 Stainless Steel vs. EN AC-51300 Aluminum

AISI 316 stainless steel belongs to the iron alloys classification, while EN AC-51300 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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 316 stainless steel and the bottom bar is EN AC-51300 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 160 to 360
65
Elastic (Young's, Tensile) Modulus, GPa 200
67
Elongation at Break, % 8.0 to 55
3.7
Fatigue Strength, MPa 210 to 430
78
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
25
Tensile Strength: Ultimate (UTS), MPa 520 to 1180
190
Tensile Strength: Yield (Proof), MPa 230 to 850
110

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Mechanical, °C 590
170
Melting Completion (Liquidus), °C 1400
640
Melting Onset (Solidus), °C 1380
600
Specific Heat Capacity, J/kg-K 470
910
Thermal Conductivity, W/m-K 15
110
Thermal Expansion, µm/m-K 16
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
31
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
100

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
9.1
Embodied Energy, MJ/kg 53
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 85 to 260
6.1
Resilience: Unit (Modulus of Resilience), kJ/m3 130 to 1820
87
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 18 to 41
20
Strength to Weight: Bending, points 18 to 31
28
Thermal Diffusivity, mm2/s 4.1
45
Thermal Shock Resistance, points 11 to 26
8.6

Alloy Composition

Aluminum (Al), % 0
91.4 to 95.5
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 16 to 18
0
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 62 to 72
0 to 0.55
Magnesium (Mg), % 0
4.5 to 6.5
Manganese (Mn), % 0 to 2.0
0 to 0.45
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 0.55
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15