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328.0 Aluminum vs. S66286 Stainless Steel

328.0 aluminum belongs to the aluminum alloys classification, while S66286 stainless steel belongs to the iron alloys. There are 29 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 328.0 aluminum and the bottom bar is S66286 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 1.6 to 2.1
17 to 40
Fatigue Strength, MPa 55 to 80
240 to 410
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
75
Tensile Strength: Ultimate (UTS), MPa 200 to 270
620 to 1020
Tensile Strength: Yield (Proof), MPa 120 to 170
280 to 670

Thermal Properties

Latent Heat of Fusion, J/g 510
300
Maximum Temperature: Mechanical, °C 180
920
Melting Completion (Liquidus), °C 620
1430
Melting Onset (Solidus), °C 560
1370
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 120
15
Thermal Expansion, µm/m-K 22
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 99
2.2

Otherwise Unclassified Properties

Base Metal Price, % relative 10
26
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 7.8
6.0
Embodied Energy, MJ/kg 140
87
Embodied Water, L/kg 1070
170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.8 to 5.0
150 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 92 to 200
190 to 1150
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 21 to 28
22 to 36
Strength to Weight: Bending, points 28 to 34
20 to 28
Thermal Diffusivity, mm2/s 50
4.0
Thermal Shock Resistance, points 9.2 to 12
13 to 22

Alloy Composition


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Aluminum (Al), % 84.5 to 91.1
0 to 0.35
Boron (B), % 0
0.0010 to 0.010
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0 to 0.35
13.5 to 16
Copper (Cu), % 1.0 to 2.0
0
Iron (Fe), % 0 to 1.0
49.1 to 59.5
Magnesium (Mg), % 0.2 to 0.6
0
Manganese (Mn), % 0.2 to 0.6
0 to 2.0
Molybdenum (Mo), % 0
1.0 to 1.5
Nickel (Ni), % 0 to 0.25
24 to 27
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 7.5 to 8.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
1.9 to 2.4
Vanadium (V), % 0
0.1 to 0.5
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0 to 0.5
0