MakeItFrom.com
Menu (ESC)

2036 Aluminum vs. AISI 317 Stainless Steel

2036 aluminum belongs to the aluminum alloys classification, while AISI 317 stainless steel belongs to the iron 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 2036 aluminum and the bottom bar is AISI 317 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 24
35 to 55
Fatigue Strength, MPa 130
250 to 330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
79
Shear Strength, MPa 210
420 to 470
Tensile Strength: Ultimate (UTS), MPa 340
580 to 710
Tensile Strength: Yield (Proof), MPa 200
250 to 420

Thermal Properties

Latent Heat of Fusion, J/g 390
290
Maximum Temperature: Mechanical, °C 190
590
Melting Completion (Liquidus), °C 650
1400
Melting Onset (Solidus), °C 560
1380
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 160
15
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 10
21
Density, g/cm3 2.9
7.9
Embodied Carbon, kg CO2/kg material 8.1
4.3
Embodied Energy, MJ/kg 150
59
Embodied Water, L/kg 1160
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 70
210 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 270
150 to 430
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 48
25
Strength to Weight: Axial, points 33
20 to 25
Strength to Weight: Bending, points 38
20 to 22
Thermal Diffusivity, mm2/s 62
4.1
Thermal Shock Resistance, points 15
12 to 15

Alloy Composition

Aluminum (Al), % 94.4 to 97.4
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0 to 0.1
18 to 20
Copper (Cu), % 2.2 to 3.0
0
Iron (Fe), % 0 to 0.5
58 to 68
Magnesium (Mg), % 0.3 to 0.6
0
Manganese (Mn), % 0.1 to 0.4
0 to 2.0
Molybdenum (Mo), % 0
3.0 to 4.0
Nickel (Ni), % 0
11 to 15
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.5
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0