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356.0 Aluminum vs. S21900 Stainless Steel

356.0 aluminum belongs to the aluminum alloys classification, while S21900 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, 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 356.0 aluminum and the bottom bar is S21900 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 55 to 75
220
Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.0 to 3.8
50
Fatigue Strength, MPa 55 to 75
380
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
78
Shear Strength, MPa 140 to 190
510
Tensile Strength: Ultimate (UTS), MPa 160 to 240
710
Tensile Strength: Yield (Proof), MPa 100 to 190
390

Thermal Properties

Latent Heat of Fusion, J/g 500
290
Maximum Temperature: Mechanical, °C 170
980
Melting Completion (Liquidus), °C 620
1400
Melting Onset (Solidus), °C 570
1350
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 150 to 170
14
Thermal Expansion, µm/m-K 21
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40 to 43
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 140 to 150
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
15
Density, g/cm3 2.6
7.7
Embodied Carbon, kg CO2/kg material 8.0
3.0
Embodied Energy, MJ/kg 150
43
Embodied Water, L/kg 1110
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.2 to 8.2
300
Resilience: Unit (Modulus of Resilience), kJ/m3 70 to 250
380
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
25
Strength to Weight: Axial, points 17 to 26
26
Strength to Weight: Bending, points 25 to 33
23
Thermal Diffusivity, mm2/s 64 to 71
3.8
Thermal Shock Resistance, points 7.6 to 11
15

Alloy Composition


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Aluminum (Al), % 90.1 to 93.3
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
19 to 21.5
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0 to 0.6
59.4 to 67.4
Magnesium (Mg), % 0.2 to 0.45
0
Manganese (Mn), % 0 to 0.35
8.0 to 10
Nickel (Ni), % 0
5.5 to 7.5
Nitrogen (N), % 0
0.15 to 0.4
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 6.5 to 7.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0