MakeItFrom.com
Menu (ESC)

7022 Aluminum vs. N08926 Stainless Steel

7022 aluminum belongs to the aluminum alloys classification, while N08926 stainless steel belongs to the iron alloys. There are 30 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 7022 aluminum and the bottom bar is N08926 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 6.3 to 8.0
40
Fatigue Strength, MPa 140 to 170
290
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
80
Shear Strength, MPa 290 to 320
500
Tensile Strength: Ultimate (UTS), MPa 490 to 540
740
Tensile Strength: Yield (Proof), MPa 390 to 460
330

Thermal Properties

Latent Heat of Fusion, J/g 380
300
Maximum Temperature: Mechanical, °C 200
1100
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 480
1410
Specific Heat Capacity, J/kg-K 870
460
Thermal Conductivity, W/m-K 140
12
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 21
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 65
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 10
33
Density, g/cm3 2.9
8.1
Embodied Carbon, kg CO2/kg material 8.5
6.2
Embodied Energy, MJ/kg 150
84
Embodied Water, L/kg 1130
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 40
240
Resilience: Unit (Modulus of Resilience), kJ/m3 1100 to 1500
270
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 47 to 51
25
Strength to Weight: Bending, points 47 to 50
22
Thermal Diffusivity, mm2/s 54
3.2
Thermal Shock Resistance, points 21 to 23
16

Alloy Composition

Aluminum (Al), % 87.9 to 92.4
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0.1 to 0.3
19 to 21
Copper (Cu), % 0.5 to 1.0
0.5 to 1.5
Iron (Fe), % 0 to 0.5
41.7 to 50.4
Magnesium (Mg), % 2.6 to 3.7
0
Manganese (Mn), % 0.1 to 0.4
0 to 2.0
Molybdenum (Mo), % 0
6.0 to 7.0
Nickel (Ni), % 0
24 to 26
Nitrogen (N), % 0
0.15 to 0.25
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.5
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 4.3 to 5.2
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0