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B535.0 Aluminum vs. AISI 422 Stainless Steel

B535.0 aluminum belongs to the aluminum alloys classification, while AISI 422 stainless steel belongs to the iron alloys. There are 31 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 B535.0 aluminum and the bottom bar is AISI 422 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 65
260 to 330
Elastic (Young's, Tensile) Modulus, GPa 66
200
Elongation at Break, % 10
15 to 17
Fatigue Strength, MPa 62
410 to 500
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
76
Shear Strength, MPa 210
560 to 660
Tensile Strength: Ultimate (UTS), MPa 260
910 to 1080
Tensile Strength: Yield (Proof), MPa 130
670 to 870

Thermal Properties

Latent Heat of Fusion, J/g 390
270
Maximum Temperature: Mechanical, °C 170
650
Melting Completion (Liquidus), °C 630
1480
Melting Onset (Solidus), °C 550
1470
Specific Heat Capacity, J/kg-K 910
470
Thermal Conductivity, W/m-K 96
24
Thermal Expansion, µm/m-K 25
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 24
4.7
Electrical Conductivity: Equal Weight (Specific), % IACS 82
5.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
11
Density, g/cm3 2.6
7.9
Embodied Carbon, kg CO2/kg material 9.4
3.1
Embodied Energy, MJ/kg 160
44
Embodied Water, L/kg 1180
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 22
140 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 130
1140 to 1910
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 28
32 to 38
Strength to Weight: Bending, points 35
26 to 30
Thermal Diffusivity, mm2/s 40
6.4
Thermal Shock Resistance, points 11
33 to 39

Alloy Composition

Aluminum (Al), % 91.7 to 93.4
0
Carbon (C), % 0
0.2 to 0.25
Chromium (Cr), % 0
11 to 12.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.15
81.9 to 85.8
Magnesium (Mg), % 6.5 to 7.5
0
Manganese (Mn), % 0 to 0.050
0.5 to 1.0
Molybdenum (Mo), % 0
0.9 to 1.3
Nickel (Ni), % 0
0.5 to 1.0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.15
0 to 0.5
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0.1 to 0.25
0
Tungsten (W), % 0
0.9 to 1.3
Vanadium (V), % 0
0.2 to 0.3
Residuals, % 0 to 0.15
0