MakeItFrom.com
Menu (ESC)

N08020 Stainless Steel vs. 2011A Aluminum

N08020 stainless steel belongs to the iron alloys classification, while 2011A 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 2011A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 15 to 34
6.8 to 16
Fatigue Strength, MPa 210 to 240
75 to 100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 380 to 410
190 to 250
Tensile Strength: Ultimate (UTS), MPa 610 to 620
310 to 410
Tensile Strength: Yield (Proof), MPa 270 to 420
140 to 310

Thermal Properties

Latent Heat of Fusion, J/g 300
390
Maximum Temperature: Mechanical, °C 1100
190
Melting Completion (Liquidus), °C 1410
660
Melting Onset (Solidus), °C 1360
550
Specific Heat Capacity, J/kg-K 460
870
Thermal Conductivity, W/m-K 12
130
Thermal Expansion, µm/m-K 15
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.6
33
Electrical Conductivity: Equal Weight (Specific), % IACS 1.8
96

Otherwise Unclassified Properties

Base Metal Price, % relative 38
11
Density, g/cm3 8.2
3.1
Embodied Carbon, kg CO2/kg material 6.6
7.9
Embodied Energy, MJ/kg 92
150
Embodied Water, L/kg 220
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 83 to 170
20 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 440
140 to 670
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
44
Strength to Weight: Axial, points 21
28 to 37
Strength to Weight: Bending, points 20
33 to 40
Thermal Diffusivity, mm2/s 3.2
49
Thermal Shock Resistance, points 15
14 to 18

Alloy Composition

Aluminum (Al), % 0
91.5 to 95.1
Bismuth (Bi), % 0
0.2 to 0.6
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 19 to 21
0
Copper (Cu), % 3.0 to 4.0
4.5 to 6.0
Iron (Fe), % 29.9 to 44
0 to 0.5
Lead (Pb), % 0
0.2 to 0.6
Manganese (Mn), % 0 to 2.0
0
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 to 0.4
Sulfur (S), % 0 to 0.035
0
Zinc (Zn), % 0
0 to 0.3
Residuals, % 0
0 to 0.15