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N08800 Stainless Steel vs. 6106 Aluminum

N08800 stainless steel belongs to the iron alloys classification, while 6106 aluminum belongs to the aluminum 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 N08800 stainless steel and the bottom bar is 6106 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 4.5 to 34
9.1
Fatigue Strength, MPa 150 to 390
88
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 340 to 580
170
Tensile Strength: Ultimate (UTS), MPa 500 to 1000
290
Tensile Strength: Yield (Proof), MPa 190 to 830
220

Thermal Properties

Latent Heat of Fusion, J/g 300
400
Maximum Temperature: Mechanical, °C 1100
160
Melting Completion (Liquidus), °C 1390
660
Melting Onset (Solidus), °C 1360
610
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 12
190
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
49
Electrical Conductivity: Equal Weight (Specific), % IACS 1.9
160

Otherwise Unclassified Properties

Base Metal Price, % relative 30
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 5.3
8.3
Embodied Energy, MJ/kg 76
150
Embodied Water, L/kg 200
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 160
24
Resilience: Unit (Modulus of Resilience), kJ/m3 96 to 1740
370
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 18 to 35
29
Strength to Weight: Bending, points 18 to 28
35
Thermal Diffusivity, mm2/s 3.0
78
Thermal Shock Resistance, points 13 to 25
13

Alloy Composition

Aluminum (Al), % 0.15 to 0.6
97.2 to 99.3
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 19 to 23
0 to 0.2
Copper (Cu), % 0 to 0.75
0 to 0.25
Iron (Fe), % 39.5 to 50.7
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.8
Manganese (Mn), % 0 to 1.5
0.050 to 0.2
Nickel (Ni), % 30 to 35
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0.3 to 0.6
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0.15 to 0.6
0 to 0.1
Zinc (Zn), % 0
0 to 0.15
Residuals, % 0
0 to 0.15