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5110A Aluminum vs. 2124 Aluminum

Both 5110A aluminum and 2124 aluminum are aluminum alloys. They have a moderately high 94% of their average alloy composition in common.

For each property being compared, the top bar is 5110A aluminum and the bottom bar is 2124 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
71
Elongation at Break, % 4.5 to 28
5.7
Fatigue Strength, MPa 37 to 77
130
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
27
Shear Strength, MPa 66 to 110
280
Tensile Strength: Ultimate (UTS), MPa 100 to 190
490
Tensile Strength: Yield (Proof), MPa 32 to 170
430

Thermal Properties

Latent Heat of Fusion, J/g 400
390
Maximum Temperature: Mechanical, °C 180
190
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 640
500
Specific Heat Capacity, J/kg-K 900
880
Thermal Conductivity, W/m-K 220
150
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 57
38
Electrical Conductivity: Equal Weight (Specific), % IACS 190
110

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
10
Density, g/cm3 2.7
3.0
Embodied Carbon, kg CO2/kg material 8.3
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.8 to 22
27
Resilience: Unit (Modulus of Resilience), kJ/m3 7.6 to 200
1290
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
46
Strength to Weight: Axial, points 10 to 19
45
Strength to Weight: Bending, points 18 to 27
46
Thermal Diffusivity, mm2/s 91
58
Thermal Shock Resistance, points 4.5 to 8.4
21

Alloy Composition

Aluminum (Al), % 98.5 to 99.8
91.3 to 94.7
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0 to 0.2
3.8 to 4.9
Iron (Fe), % 0 to 0.25
0 to 0.3
Magnesium (Mg), % 0.2 to 0.6
1.2 to 1.8
Manganese (Mn), % 0 to 0.2
0.3 to 0.9
Silicon (Si), % 0 to 0.15
0 to 0.2
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0 to 0.030
0 to 0.25
Residuals, % 0
0 to 0.15