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EN AC-51400 Aluminum vs. AISI 410Cb Stainless Steel

EN AC-51400 aluminum belongs to the aluminum alloys classification, while AISI 410Cb stainless steel belongs to the iron 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 EN AC-51400 aluminum and the bottom bar is AISI 410Cb stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 71
200 to 270
Elastic (Young's, Tensile) Modulus, GPa 67
190
Elongation at Break, % 3.4
15
Fatigue Strength, MPa 85
180 to 460
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
76
Tensile Strength: Ultimate (UTS), MPa 190
550 to 960
Tensile Strength: Yield (Proof), MPa 120
310 to 790

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 170
730
Melting Completion (Liquidus), °C 640
1450
Melting Onset (Solidus), °C 600
1400
Specific Heat Capacity, J/kg-K 910
480
Thermal Conductivity, W/m-K 110
27
Thermal Expansion, µm/m-K 23
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 110
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.5
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 9.1
2.0
Embodied Energy, MJ/kg 150
29
Embodied Water, L/kg 1170
97

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.6
70 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 110
240 to 1600
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 20
20 to 35
Strength to Weight: Bending, points 28
19 to 28
Thermal Diffusivity, mm2/s 46
7.3
Thermal Shock Resistance, points 8.6
20 to 35

Alloy Composition


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Aluminum (Al), % 90.5 to 95.5
0
Carbon (C), % 0
0 to 0.18
Chromium (Cr), % 0
11 to 13
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.55
84.5 to 89
Magnesium (Mg), % 4.5 to 6.5
0
Manganese (Mn), % 0 to 0.45
0 to 1.0
Niobium (Nb), % 0
0.050 to 0.3
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 1.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0