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AISI 201L Stainless Steel vs. 7022 Aluminum

AISI 201L stainless steel belongs to the iron alloys classification, while 7022 aluminum belongs to the aluminum alloys. There are 30 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 AISI 201L stainless steel and the bottom bar is 7022 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 22 to 46
6.3 to 8.0
Fatigue Strength, MPa 270 to 530
140 to 170
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 77
26
Shear Strength, MPa 520 to 660
290 to 320
Tensile Strength: Ultimate (UTS), MPa 740 to 1040
490 to 540
Tensile Strength: Yield (Proof), MPa 290 to 790
390 to 460

Thermal Properties

Latent Heat of Fusion, J/g 280
380
Maximum Temperature: Mechanical, °C 880
200
Melting Completion (Liquidus), °C 1410
640
Melting Onset (Solidus), °C 1370
480
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 15
140
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
21
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
65

Otherwise Unclassified Properties

Base Metal Price, % relative 12
10
Density, g/cm3 7.7
2.9
Embodied Carbon, kg CO2/kg material 2.6
8.5
Embodied Energy, MJ/kg 38
150
Embodied Water, L/kg 140
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210 to 300
29 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 1570
1100 to 1500
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
47
Strength to Weight: Axial, points 27 to 37
47 to 51
Strength to Weight: Bending, points 24 to 30
47 to 50
Thermal Diffusivity, mm2/s 4.0
54
Thermal Shock Resistance, points 16 to 23
21 to 23

Alloy Composition

Aluminum (Al), % 0
87.9 to 92.4
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 16 to 18
0.1 to 0.3
Copper (Cu), % 0
0.5 to 1.0
Iron (Fe), % 67.9 to 75
0 to 0.5
Magnesium (Mg), % 0
2.6 to 3.7
Manganese (Mn), % 5.5 to 7.5
0.1 to 0.4
Nickel (Ni), % 3.5 to 5.5
0
Nitrogen (N), % 0 to 0.25
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 0.75
0 to 0.5
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
4.3 to 5.2
Zirconium (Zr), % 0
0 to 0.2
Residuals, % 0
0 to 0.15