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2618A Aluminum vs. N08020 Stainless Steel

2618A aluminum belongs to the aluminum alloys classification, while N08020 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 2618A aluminum and the bottom bar is N08020 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 4.5
15 to 34
Fatigue Strength, MPa 120
210 to 240
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
77
Shear Strength, MPa 260
380 to 410
Tensile Strength: Ultimate (UTS), MPa 440
610 to 620
Tensile Strength: Yield (Proof), MPa 410
270 to 420

Thermal Properties

Latent Heat of Fusion, J/g 390
300
Maximum Temperature: Mechanical, °C 230
1100
Melting Completion (Liquidus), °C 670
1410
Melting Onset (Solidus), °C 560
1360
Specific Heat Capacity, J/kg-K 880
460
Thermal Conductivity, W/m-K 150
12
Thermal Expansion, µm/m-K 23
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
1.6
Electrical Conductivity: Equal Weight (Specific), % IACS 110
1.8

Otherwise Unclassified Properties

Base Metal Price, % relative 11
38
Density, g/cm3 3.0
8.2
Embodied Carbon, kg CO2/kg material 8.4
6.6
Embodied Energy, MJ/kg 150
92
Embodied Water, L/kg 1150
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19
83 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 1180
180 to 440
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 41
21
Strength to Weight: Bending, points 44
20
Thermal Diffusivity, mm2/s 59
3.2
Thermal Shock Resistance, points 19
15

Alloy Composition

Aluminum (Al), % 91.5 to 95.2
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0
19 to 21
Copper (Cu), % 1.8 to 2.7
3.0 to 4.0
Iron (Fe), % 0.9 to 1.4
29.9 to 44
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.25
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 3.0
Nickel (Ni), % 0.8 to 1.4
32 to 38
Niobium (Nb), % 0
0 to 1.0
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0.15 to 0.25
0 to 1.0
Sulfur (S), % 0
0 to 0.035
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.15
0
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0