MakeItFrom.com
Menu (ESC)

7050 Aluminum vs. S31266 Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while S31266 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 S31266 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 2.2 to 12
40
Fatigue Strength, MPa 130 to 210
400
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 280 to 330
590
Tensile Strength: Ultimate (UTS), MPa 490 to 570
860
Tensile Strength: Yield (Proof), MPa 390 to 500
470

Thermal Properties

Latent Heat of Fusion, J/g 370
310
Maximum Temperature: Mechanical, °C 190
1100
Melting Completion (Liquidus), °C 630
1470
Melting Onset (Solidus), °C 490
1420
Specific Heat Capacity, J/kg-K 860
460
Thermal Conductivity, W/m-K 140
12
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
1.8
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 10
37
Density, g/cm3 3.1
8.2
Embodied Carbon, kg CO2/kg material 8.2
6.5
Embodied Energy, MJ/kg 150
89
Embodied Water, L/kg 1120
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
290
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
540
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 45 to 51
29
Strength to Weight: Bending, points 45 to 50
24
Thermal Diffusivity, mm2/s 54
3.1
Thermal Shock Resistance, points 21 to 25
18

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.040
23 to 25
Copper (Cu), % 2.0 to 2.6
1.0 to 2.5
Iron (Fe), % 0 to 0.15
34.1 to 46
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
2.0 to 4.0
Molybdenum (Mo), % 0
5.2 to 6.2
Nickel (Ni), % 0
21 to 24
Nitrogen (N), % 0
0.35 to 0.6
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.12
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.060
0
Tungsten (W), % 0
1.5 to 2.5
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0