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5026 Aluminum vs. EN 1.4659 Stainless Steel

5026 aluminum belongs to the aluminum alloys classification, while EN 1.4659 stainless steel belongs to the iron alloys. There are 30 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 5026 aluminum and the bottom bar is EN 1.4659 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 5.1 to 11
49
Fatigue Strength, MPa 94 to 140
460
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 150 to 180
640
Tensile Strength: Ultimate (UTS), MPa 260 to 320
900
Tensile Strength: Yield (Proof), MPa 120 to 250
480

Thermal Properties

Latent Heat of Fusion, J/g 400
300
Maximum Temperature: Mechanical, °C 210
1100
Melting Completion (Liquidus), °C 650
1480
Melting Onset (Solidus), °C 510
1430
Specific Heat Capacity, J/kg-K 890
460
Thermal Conductivity, W/m-K 130
12
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 99
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
37
Density, g/cm3 2.8
8.2
Embodied Carbon, kg CO2/kg material 8.9
6.5
Embodied Energy, MJ/kg 150
89
Embodied Water, L/kg 1150
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 29
370
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 440
550
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
24
Strength to Weight: Axial, points 26 to 32
31
Strength to Weight: Bending, points 33 to 37
25
Thermal Diffusivity, mm2/s 52
3.2
Thermal Shock Resistance, points 11 to 14
19

Alloy Composition

Aluminum (Al), % 88.2 to 94.7
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0 to 0.3
23 to 25
Copper (Cu), % 0.1 to 0.8
1.0 to 2.0
Iron (Fe), % 0.2 to 1.0
35.7 to 45.7
Magnesium (Mg), % 3.9 to 4.9
0
Manganese (Mn), % 0.6 to 1.8
2.0 to 4.0
Molybdenum (Mo), % 0
5.5 to 6.5
Nickel (Ni), % 0
21 to 23
Nitrogen (N), % 0
0.35 to 0.5
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0.55 to 1.4
0 to 0.7
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.2
0
Tungsten (W), % 0
1.5 to 2.5
Zinc (Zn), % 0 to 1.0
0
Zirconium (Zr), % 0 to 0.3
0
Residuals, % 0 to 0.15
0