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7050 Aluminum vs. AISI 201L Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while AISI 201L stainless steel belongs to the iron 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 7050 aluminum and the bottom bar is AISI 201L stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.2 to 12
22 to 46
Fatigue Strength, MPa 130 to 210
270 to 530
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 280 to 330
520 to 660
Tensile Strength: Ultimate (UTS), MPa 490 to 570
740 to 1040
Tensile Strength: Yield (Proof), MPa 390 to 500
290 to 790

Thermal Properties

Latent Heat of Fusion, J/g 370
280
Maximum Temperature: Mechanical, °C 190
880
Melting Completion (Liquidus), °C 630
1410
Melting Onset (Solidus), °C 490
1370
Specific Heat Capacity, J/kg-K 860
480
Thermal Conductivity, W/m-K 140
15
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 10
12
Density, g/cm3 3.1
7.7
Embodied Carbon, kg CO2/kg material 8.2
2.6
Embodied Energy, MJ/kg 150
38
Embodied Water, L/kg 1120
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
210 to 300
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
220 to 1570
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
27 to 37
Strength to Weight: Bending, points 45 to 50
24 to 30
Thermal Diffusivity, mm2/s 54
4.0
Thermal Shock Resistance, points 21 to 25
16 to 23

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.040
16 to 18
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
67.9 to 75
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
5.5 to 7.5
Nickel (Ni), % 0
3.5 to 5.5
Nitrogen (N), % 0
0 to 0.25
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.12
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.060
0
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0