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S17400 Stainless Steel vs. 324.0 Aluminum

S17400 stainless steel belongs to the iron alloys classification, while 324.0 aluminum belongs to the aluminum alloys. There are 29 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 S17400 stainless steel and the bottom bar is 324.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 11 to 21
3.0 to 4.0
Fatigue Strength, MPa 380 to 670
77 to 89
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Tensile Strength: Ultimate (UTS), MPa 910 to 1390
210 to 310
Tensile Strength: Yield (Proof), MPa 580 to 1250
110 to 270

Thermal Properties

Latent Heat of Fusion, J/g 280
500
Maximum Temperature: Mechanical, °C 850
170
Melting Completion (Liquidus), °C 1440
610
Melting Onset (Solidus), °C 1400
550
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 17
150
Thermal Expansion, µm/m-K 11
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
34
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
120

Otherwise Unclassified Properties

Base Metal Price, % relative 14
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.7
7.9
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1090

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 160
6.8 to 8.9
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 4060
85 to 510
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
52
Strength to Weight: Axial, points 32 to 49
22 to 32
Strength to Weight: Bending, points 27 to 35
29 to 38
Thermal Diffusivity, mm2/s 4.5
62
Thermal Shock Resistance, points 30 to 46
9.7 to 14

Alloy Composition


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Aluminum (Al), % 0
87.3 to 92.2
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 15 to 17
0
Copper (Cu), % 3.0 to 5.0
0.4 to 0.6
Iron (Fe), % 70.4 to 78.9
0 to 1.2
Magnesium (Mg), % 0
0.4 to 0.7
Manganese (Mn), % 0 to 1.0
0 to 0.5
Nickel (Ni), % 3.0 to 5.0
0 to 0.3
Niobium (Nb), % 0.15 to 0.45
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
7.0 to 8.0
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.2