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N08020 Stainless Steel vs. 336.0 Aluminum

N08020 stainless steel belongs to the iron alloys classification, while 336.0 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 N08020 stainless steel and the bottom bar is 336.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
75
Elongation at Break, % 15 to 34
0.5
Fatigue Strength, MPa 210 to 240
80 to 93
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
28
Shear Strength, MPa 380 to 410
190 to 250
Tensile Strength: Ultimate (UTS), MPa 610 to 620
250 to 320
Tensile Strength: Yield (Proof), MPa 270 to 420
190 to 300

Thermal Properties

Latent Heat of Fusion, J/g 300
570
Maximum Temperature: Mechanical, °C 1100
210
Melting Completion (Liquidus), °C 1410
570
Melting Onset (Solidus), °C 1360
540
Specific Heat Capacity, J/kg-K 460
890
Thermal Conductivity, W/m-K 12
120
Thermal Expansion, µm/m-K 15
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.6
29
Electrical Conductivity: Equal Weight (Specific), % IACS 1.8
95

Otherwise Unclassified Properties

Base Metal Price, % relative 38
11
Density, g/cm3 8.2
2.8
Embodied Carbon, kg CO2/kg material 6.6
7.9
Embodied Energy, MJ/kg 92
140
Embodied Water, L/kg 220
1010

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 83 to 170
1.1 to 1.6
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 440
250 to 580
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 21
25 to 32
Strength to Weight: Bending, points 20
32 to 38
Thermal Diffusivity, mm2/s 3.2
48
Thermal Shock Resistance, points 15
12 to 16

Alloy Composition

Aluminum (Al), % 0
79.1 to 85.8
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 19 to 21
0
Copper (Cu), % 3.0 to 4.0
0.5 to 1.5
Iron (Fe), % 29.9 to 44
0 to 1.2
Magnesium (Mg), % 0
0.7 to 1.3
Manganese (Mn), % 0 to 2.0
0 to 0.35
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 32 to 38
2.0 to 3.0
Niobium (Nb), % 0 to 1.0
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
11 to 13
Sulfur (S), % 0 to 0.035
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.35