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5051A-O Aluminum vs. 5110A-O Aluminum

Both 5051A-O aluminum and 5110A-O aluminum are aluminum alloys. Both are furnished in the annealed condition. They have a very high 98% of their average alloy composition in common.

For each property being compared, the top bar is 5051A-O aluminum and the bottom bar is 5110A-O aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
68
Elongation at Break, % 21
28
Fatigue Strength, MPa 61
37
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 110
66
Tensile Strength: Ultimate (UTS), MPa 170
100
Tensile Strength: Yield (Proof), MPa 56
32

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 190
180
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 610
640
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 150
220
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 39
57
Electrical Conductivity: Equal Weight (Specific), % IACS 130
190

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 8.5
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27
22
Resilience: Unit (Modulus of Resilience), kJ/m3 23
7.6
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 17
10
Strength to Weight: Bending, points 25
18
Thermal Diffusivity, mm2/s 63
91
Thermal Shock Resistance, points 7.6
4.5

Alloy Composition


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Aluminum (Al), % 96.1 to 98.6
98.5 to 99.8
Chromium (Cr), % 0 to 0.3
0
Copper (Cu), % 0 to 0.050
0 to 0.2
Iron (Fe), % 0 to 0.45
0 to 0.25
Magnesium (Mg), % 1.4 to 2.1
0.2 to 0.6
Manganese (Mn), % 0 to 0.25
0 to 0.2
Silicon (Si), % 0 to 0.3
0 to 0.15
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.2
0 to 0.030
Residuals, % 0 to 0.15
0 to 0.1