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N08020 Stainless Steel vs. 6351 Aluminum

N08020 stainless steel belongs to the iron alloys classification, while 6351 aluminum belongs to the aluminum 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 N08020 stainless steel and the bottom bar is 6351 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 15 to 34
7.8 to 18
Fatigue Strength, MPa 210 to 240
79 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 380 to 410
84 to 200
Tensile Strength: Ultimate (UTS), MPa 610 to 620
140 to 310
Tensile Strength: Yield (Proof), MPa 270 to 420
95 to 270

Thermal Properties

Latent Heat of Fusion, J/g 300
410
Maximum Temperature: Mechanical, °C 1100
160
Melting Completion (Liquidus), °C 1410
650
Melting Onset (Solidus), °C 1360
570
Specific Heat Capacity, J/kg-K 460
900
Thermal Conductivity, W/m-K 12
180
Thermal Expansion, µm/m-K 15
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.6
46
Electrical Conductivity: Equal Weight (Specific), % IACS 1.8
150

Otherwise Unclassified Properties

Base Metal Price, % relative 38
9.5
Density, g/cm3 8.2
2.7
Embodied Carbon, kg CO2/kg material 6.6
8.3
Embodied Energy, MJ/kg 92
150
Embodied Water, L/kg 220
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 83 to 170
20 to 38
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 440
65 to 540
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 21
14 to 32
Strength to Weight: Bending, points 20
22 to 38
Thermal Diffusivity, mm2/s 3.2
72
Thermal Shock Resistance, points 15
6.1 to 14

Alloy Composition

Aluminum (Al), % 0
96 to 98.5
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 19 to 21
0
Copper (Cu), % 3.0 to 4.0
0 to 0.1
Iron (Fe), % 29.9 to 44
0 to 0.5
Magnesium (Mg), % 0
0.4 to 0.8
Manganese (Mn), % 0 to 2.0
0.4 to 0.8
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 32 to 38
0
Niobium (Nb), % 0 to 1.0
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0.7 to 1.3
Sulfur (S), % 0 to 0.035
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15

Comparable Variants