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5051A-O Aluminum vs. 6351-O Aluminum

Both 5051A-O aluminum and 6351-O aluminum are aluminum alloys. Both are furnished in the annealed condition. They have a very high 99% of their average alloy composition in common.

For each property being compared, the top bar is 5051A-O aluminum and the bottom bar is 6351-O aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
69
Elongation at Break, % 21
16
Fatigue Strength, MPa 61
98
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 110
86
Tensile Strength: Ultimate (UTS), MPa 170
140
Tensile Strength: Yield (Proof), MPa 56
95

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 190
160
Melting Completion (Liquidus), °C 640
650
Melting Onset (Solidus), °C 610
570
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 150
180
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 39
46
Electrical Conductivity: Equal Weight (Specific), % IACS 130
150

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
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27
20
Resilience: Unit (Modulus of Resilience), kJ/m3 23
65
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 17
14
Strength to Weight: Bending, points 25
22
Thermal Diffusivity, mm2/s 63
72
Thermal Shock Resistance, points 7.6
6.2

Alloy Composition


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Aluminum (Al), % 96.1 to 98.6
96 to 98.5
Chromium (Cr), % 0 to 0.3
0
Copper (Cu), % 0 to 0.050
0 to 0.1
Iron (Fe), % 0 to 0.45
0 to 0.5
Magnesium (Mg), % 1.4 to 2.1
0.4 to 0.8
Manganese (Mn), % 0 to 0.25
0.4 to 0.8
Silicon (Si), % 0 to 0.3
0.7 to 1.3
Titanium (Ti), % 0 to 0.1
0 to 0.2
Zinc (Zn), % 0 to 0.2
0 to 0.2
Residuals, % 0 to 0.15
0 to 0.15