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328.0 Aluminum vs. S15500 Stainless Steel

328.0 aluminum belongs to the aluminum alloys classification, while S15500 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (7, 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 S15500 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 60 to 82
290 to 430
Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 1.6 to 2.1
6.8 to 16
Fatigue Strength, MPa 55 to 80
350 to 650
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
75
Tensile Strength: Ultimate (UTS), MPa 200 to 270
890 to 1490
Tensile Strength: Yield (Proof), MPa 120 to 170
590 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 510
280
Maximum Temperature: Mechanical, °C 180
820
Melting Completion (Liquidus), °C 620
1430
Melting Onset (Solidus), °C 560
1380
Specific Heat Capacity, J/kg-K 890
480
Thermal Conductivity, W/m-K 120
17
Thermal Expansion, µm/m-K 22
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 99
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 10
13
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 7.8
2.7
Embodied Energy, MJ/kg 140
39
Embodied Water, L/kg 1070
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.8 to 5.0
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 92 to 200
890 to 4460
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 21 to 28
32 to 53
Strength to Weight: Bending, points 28 to 34
26 to 37
Thermal Diffusivity, mm2/s 50
4.6
Thermal Shock Resistance, points 9.2 to 12
30 to 50

Alloy Composition


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Aluminum (Al), % 84.5 to 91.1
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0 to 0.35
14 to 15.5
Copper (Cu), % 1.0 to 2.0
2.5 to 4.5
Iron (Fe), % 0 to 1.0
71.9 to 79.9
Magnesium (Mg), % 0.2 to 0.6
0
Manganese (Mn), % 0.2 to 0.6
0 to 1.0
Nickel (Ni), % 0 to 0.25
3.5 to 5.5
Niobium (Nb), % 0
0.15 to 0.45
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
0
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0 to 0.5
0