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319.0 Aluminum vs. N08367 Stainless Steel

319.0 aluminum belongs to the aluminum alloys classification, while N08367 stainless steel belongs to the iron alloys. There are 31 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 319.0 aluminum and the bottom bar is N08367 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 78 to 84
210
Elastic (Young's, Tensile) Modulus, GPa 72
210
Elongation at Break, % 1.8 to 2.0
34
Fatigue Strength, MPa 76 to 80
280
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
80
Shear Strength, MPa 170 to 210
490
Tensile Strength: Ultimate (UTS), MPa 190 to 240
740
Tensile Strength: Yield (Proof), MPa 110 to 180
350

Thermal Properties

Latent Heat of Fusion, J/g 480
310
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 540
1410
Specific Heat Capacity, J/kg-K 880
460
Thermal Conductivity, W/m-K 110
12
Thermal Expansion, µm/m-K 22
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
1.8
Electrical Conductivity: Equal Weight (Specific), % IACS 84
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 10
33
Density, g/cm3 2.9
8.1
Embodied Carbon, kg CO2/kg material 7.7
6.2
Embodied Energy, MJ/kg 140
84
Embodied Water, L/kg 1080
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.3 to 3.9
210
Resilience: Unit (Modulus of Resilience), kJ/m3 88 to 220
290
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 48
24
Strength to Weight: Axial, points 18 to 24
25
Strength to Weight: Bending, points 25 to 30
22
Thermal Diffusivity, mm2/s 44
3.2
Thermal Shock Resistance, points 8.6 to 11
17

Alloy Composition

Aluminum (Al), % 85.8 to 91.5
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
20 to 22
Copper (Cu), % 3.0 to 4.0
0 to 0.75
Iron (Fe), % 0 to 1.0
41.4 to 50.3
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0 to 2.0
Molybdenum (Mo), % 0
6.0 to 7.0
Nickel (Ni), % 0 to 0.35
23.5 to 25.5
Nitrogen (N), % 0
0.18 to 0.25
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 5.5 to 6.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0