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S35315 Stainless Steel vs. 319.0 Aluminum

S35315 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 S35315 stainless steel and the bottom bar is 319.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190
78 to 84
Elastic (Young's, Tensile) Modulus, GPa 200
72
Elongation at Break, % 46
1.8 to 2.0
Fatigue Strength, MPa 280
76 to 80
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
27
Shear Strength, MPa 520
170 to 210
Tensile Strength: Ultimate (UTS), MPa 740
190 to 240
Tensile Strength: Yield (Proof), MPa 300
110 to 180

Thermal Properties

Latent Heat of Fusion, J/g 330
480
Maximum Temperature: Mechanical, °C 1100
170
Melting Completion (Liquidus), °C 1370
600
Melting Onset (Solidus), °C 1330
540
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 12
110
Thermal Expansion, µm/m-K 16
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
27
Electrical Conductivity: Equal Weight (Specific), % IACS 2.0
84

Otherwise Unclassified Properties

Base Metal Price, % relative 34
10
Density, g/cm3 7.9
2.9
Embodied Carbon, kg CO2/kg material 5.7
7.7
Embodied Energy, MJ/kg 81
140
Embodied Water, L/kg 220
1080

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 270
3.3 to 3.9
Resilience: Unit (Modulus of Resilience), kJ/m3 230
88 to 220
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
48
Strength to Weight: Axial, points 26
18 to 24
Strength to Weight: Bending, points 23
25 to 30
Thermal Diffusivity, mm2/s 3.1
44
Thermal Shock Resistance, points 17
8.6 to 11

Alloy Composition

Aluminum (Al), % 0
85.8 to 91.5
Carbon (C), % 0.040 to 0.080
0
Cerium (Ce), % 0.030 to 0.1
0
Chromium (Cr), % 24 to 26
0
Copper (Cu), % 0
3.0 to 4.0
Iron (Fe), % 33.6 to 40.6
0 to 1.0
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0 to 2.0
0 to 0.5
Nickel (Ni), % 34 to 36
0 to 0.35
Nitrogen (N), % 0.12 to 0.18
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 1.2 to 2.0
5.5 to 6.5
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5