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5657 Aluminum vs. S32050 Stainless Steel

5657 aluminum belongs to the aluminum alloys classification, while S32050 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 5657 aluminum and the bottom bar is S32050 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 40 to 50
220
Elastic (Young's, Tensile) Modulus, GPa 68
210
Elongation at Break, % 6.6 to 15
46
Fatigue Strength, MPa 74 to 88
340
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 92 to 110
540
Tensile Strength: Ultimate (UTS), MPa 150 to 200
770
Tensile Strength: Yield (Proof), MPa 140 to 170
370

Thermal Properties

Latent Heat of Fusion, J/g 400
310
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 660
1460
Melting Onset (Solidus), °C 640
1410
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 210
12
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 180
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
31
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.4
6.0
Embodied Energy, MJ/kg 160
81
Embodied Water, L/kg 1200
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.7 to 27
290
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 200
330
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 15 to 20
27
Strength to Weight: Bending, points 23 to 28
23
Thermal Diffusivity, mm2/s 84
3.3
Thermal Shock Resistance, points 6.7 to 8.6
17

Alloy Composition

Aluminum (Al), % 98.5 to 99.4
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
22 to 24
Copper (Cu), % 0 to 0.1
0 to 0.4
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.1
43.1 to 51.8
Magnesium (Mg), % 0.6 to 1.0
0
Manganese (Mn), % 0 to 0.030
0 to 1.5
Molybdenum (Mo), % 0
6.0 to 6.6
Nickel (Ni), % 0
20 to 23
Nitrogen (N), % 0
0.21 to 0.32
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.080
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.050
0