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S21904 Stainless Steel vs. 328.0 Aluminum

S21904 stainless steel belongs to the iron alloys classification, while 328.0 aluminum belongs to the aluminum alloys. There are 30 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 S21904 stainless steel and the bottom bar is 328.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210 to 300
60 to 82
Elastic (Young's, Tensile) Modulus, GPa 200
72
Elongation at Break, % 17 to 51
1.6 to 2.1
Fatigue Strength, MPa 380 to 550
55 to 80
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
27
Tensile Strength: Ultimate (UTS), MPa 700 to 1000
200 to 270
Tensile Strength: Yield (Proof), MPa 390 to 910
120 to 170

Thermal Properties

Latent Heat of Fusion, J/g 290
510
Maximum Temperature: Mechanical, °C 980
180
Melting Completion (Liquidus), °C 1400
620
Melting Onset (Solidus), °C 1350
560
Specific Heat Capacity, J/kg-K 480
890
Thermal Conductivity, W/m-K 14
120
Thermal Expansion, µm/m-K 17
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
30
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
99

Otherwise Unclassified Properties

Base Metal Price, % relative 15
10
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 3.0
7.8
Embodied Energy, MJ/kg 43
140
Embodied Water, L/kg 160
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 160 to 310
2.8 to 5.0
Resilience: Unit (Modulus of Resilience), kJ/m3 380 to 2070
92 to 200
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 25 to 36
21 to 28
Strength to Weight: Bending, points 23 to 29
28 to 34
Thermal Diffusivity, mm2/s 3.8
50
Thermal Shock Resistance, points 15 to 21
9.2 to 12

Alloy Composition


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Aluminum (Al), % 0
84.5 to 91.1
Carbon (C), % 0 to 0.040
0
Chromium (Cr), % 19 to 21.5
0 to 0.35
Copper (Cu), % 0
1.0 to 2.0
Iron (Fe), % 59.5 to 67.4
0 to 1.0
Magnesium (Mg), % 0
0.2 to 0.6
Manganese (Mn), % 8.0 to 10
0.2 to 0.6
Nickel (Ni), % 5.5 to 7.5
0 to 0.25
Nitrogen (N), % 0.15 to 0.4
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
7.5 to 8.5
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 1.5
Residuals, % 0
0 to 0.5