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6110 Aluminum vs. 2124 Aluminum

Both 6110 aluminum and 2124 aluminum are aluminum alloys. They have a very high 95% of their average alloy composition in common.

For each property being compared, the top bar is 6110 aluminum and the bottom bar is 2124 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
71
Elongation at Break, % 2.2
5.7
Fatigue Strength, MPa 120
130
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
27
Shear Strength, MPa 290
280
Tensile Strength: Ultimate (UTS), MPa 500
490
Tensile Strength: Yield (Proof), MPa 500
430

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 170
190
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 600
500
Specific Heat Capacity, J/kg-K 900
880
Thermal Conductivity, W/m-K 170
150
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
38
Electrical Conductivity: Equal Weight (Specific), % IACS 140
110

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
10
Density, g/cm3 2.8
3.0
Embodied Carbon, kg CO2/kg material 8.2
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1170
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
27
Resilience: Unit (Modulus of Resilience), kJ/m3 1770
1290
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
46
Strength to Weight: Axial, points 51
45
Strength to Weight: Bending, points 51
46
Thermal Diffusivity, mm2/s 67
58
Thermal Shock Resistance, points 22
21

Alloy Composition

Aluminum (Al), % 94.4 to 98.4
91.3 to 94.7
Chromium (Cr), % 0.040 to 0.25
0 to 0.1
Copper (Cu), % 0.2 to 0.7
3.8 to 4.9
Iron (Fe), % 0 to 0.8
0 to 0.3
Magnesium (Mg), % 0.5 to 1.1
1.2 to 1.8
Manganese (Mn), % 0.2 to 0.7
0.3 to 0.9
Silicon (Si), % 0.7 to 1.5
0 to 0.2
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