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S32654 Stainless Steel vs. 5657 Aluminum

S32654 stainless steel belongs to the iron alloys classification, while 5657 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 S32654 stainless steel and the bottom bar is 5657 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 220
40 to 50
Elastic (Young's, Tensile) Modulus, GPa 210
68
Elongation at Break, % 45
6.6 to 15
Fatigue Strength, MPa 450
74 to 88
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 82
26
Shear Strength, MPa 590
92 to 110
Tensile Strength: Ultimate (UTS), MPa 850
150 to 200
Tensile Strength: Yield (Proof), MPa 490
140 to 170

Thermal Properties

Latent Heat of Fusion, J/g 310
400
Maximum Temperature: Mechanical, °C 1100
180
Melting Completion (Liquidus), °C 1450
660
Melting Onset (Solidus), °C 1410
640
Specific Heat Capacity, J/kg-K 460
900
Thermal Conductivity, W/m-K 11
210
Thermal Expansion, µm/m-K 15
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
54
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
180

Otherwise Unclassified Properties

Base Metal Price, % relative 34
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 6.4
8.4
Embodied Energy, MJ/kg 87
160
Embodied Water, L/kg 220
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 330
9.7 to 27
Resilience: Unit (Modulus of Resilience), kJ/m3 570
140 to 200
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 29
15 to 20
Strength to Weight: Bending, points 25
23 to 28
Thermal Diffusivity, mm2/s 2.9
84
Thermal Shock Resistance, points 19
6.7 to 8.6

Alloy Composition


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Aluminum (Al), % 0
98.5 to 99.4
Carbon (C), % 0 to 0.020
0
Chromium (Cr), % 24 to 25
0
Copper (Cu), % 0.3 to 0.6
0 to 0.1
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 38.3 to 45.3
0 to 0.1
Magnesium (Mg), % 0
0.6 to 1.0
Manganese (Mn), % 2.0 to 4.0
0 to 0.030
Molybdenum (Mo), % 7.0 to 8.0
0
Nickel (Ni), % 21 to 23
0
Nitrogen (N), % 0.45 to 0.55
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.5
0 to 0.080
Sulfur (S), % 0 to 0.0050
0
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.050
Residuals, % 0
0 to 0.050