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2124 Aluminum vs. 5110A Aluminum

Both 2124 aluminum and 5110A 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 2124 aluminum and the bottom bar is 5110A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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