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6110 Aluminum vs. 2036 Aluminum

Both 6110 aluminum and 2036 aluminum are aluminum alloys. They have a very high 98% of their average alloy composition in common.

For each property being compared, the top bar is 6110 aluminum and the bottom bar is 2036 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
70
Elongation at Break, % 2.2
24
Fatigue Strength, MPa 120
130
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 290
210
Tensile Strength: Ultimate (UTS), MPa 500
340
Tensile Strength: Yield (Proof), MPa 500
200

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 170
190
Melting Completion (Liquidus), °C 640
650
Melting Onset (Solidus), °C 600
560
Specific Heat Capacity, J/kg-K 900
890
Thermal Conductivity, W/m-K 170
160
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
41
Electrical Conductivity: Equal Weight (Specific), % IACS 140
130

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
10
Density, g/cm3 2.8
2.9
Embodied Carbon, kg CO2/kg material 8.2
8.1
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1170
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
70
Resilience: Unit (Modulus of Resilience), kJ/m3 1770
270
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
48
Strength to Weight: Axial, points 51
33
Strength to Weight: Bending, points 51
38
Thermal Diffusivity, mm2/s 67
62
Thermal Shock Resistance, points 22
15

Alloy Composition

Aluminum (Al), % 94.4 to 98.4
94.4 to 97.4
Chromium (Cr), % 0.040 to 0.25
0 to 0.1
Copper (Cu), % 0.2 to 0.7
2.2 to 3.0
Iron (Fe), % 0 to 0.8
0 to 0.5
Magnesium (Mg), % 0.5 to 1.1
0.3 to 0.6
Manganese (Mn), % 0.2 to 0.7
0.1 to 0.4
Silicon (Si), % 0.7 to 1.5
0 to 0.5
Titanium (Ti), % 0 to 0.15
0 to 0.15
Zinc (Zn), % 0 to 0.3
0 to 0.25
Residuals, % 0
0 to 0.15