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S31655 Stainless Steel vs. 319.0 Aluminum

S31655 stainless steel belongs to the iron alloys classification, while 319.0 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 S31655 stainless steel and the bottom bar is 319.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210
78 to 84
Elastic (Young's, Tensile) Modulus, GPa 200
72
Elongation at Break, % 39
1.8 to 2.0
Fatigue Strength, MPa 300
76 to 80
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
27
Shear Strength, MPa 490
170 to 210
Tensile Strength: Ultimate (UTS), MPa 710
190 to 240
Tensile Strength: Yield (Proof), MPa 350
110 to 180

Thermal Properties

Latent Heat of Fusion, J/g 290
480
Maximum Temperature: Mechanical, °C 1010
170
Melting Completion (Liquidus), °C 1430
600
Melting Onset (Solidus), °C 1380
540
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 15
110
Thermal Expansion, µm/m-K 16
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
27
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
84

Otherwise Unclassified Properties

Base Metal Price, % relative 17
10
Density, g/cm3 7.8
2.9
Embodied Carbon, kg CO2/kg material 3.3
7.7
Embodied Energy, MJ/kg 46
140
Embodied Water, L/kg 160
1080

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 230
3.3 to 3.9
Resilience: Unit (Modulus of Resilience), kJ/m3 310
88 to 220
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
48
Strength to Weight: Axial, points 25
18 to 24
Strength to Weight: Bending, points 23
25 to 30
Thermal Diffusivity, mm2/s 4.0
44
Thermal Shock Resistance, points 16
8.6 to 11

Alloy Composition

Aluminum (Al), % 0
85.8 to 91.5
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 19.5 to 21.5
0
Copper (Cu), % 0 to 1.0
3.0 to 4.0
Iron (Fe), % 63.2 to 71.9
0 to 1.0
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0 to 2.0
0 to 0.5
Molybdenum (Mo), % 0.5 to 1.5
0
Nickel (Ni), % 8.0 to 9.5
0 to 0.35
Nitrogen (N), % 0.14 to 0.25
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
5.5 to 6.5
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5