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5051A-O Aluminum vs. 6025-O Aluminum

Both 5051A-O aluminum and 6025-O aluminum are aluminum alloys. Both are furnished in the annealed condition. They have a very high 97% of their average alloy composition in common.

For each property being compared, the top bar is 5051A-O aluminum and the bottom bar is 6025-O aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
70
Elongation at Break, % 21
10
Fatigue Strength, MPa 61
67
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 110
110
Tensile Strength: Ultimate (UTS), MPa 170
190
Tensile Strength: Yield (Proof), MPa 56
68

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
550
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 150
130
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 39
33
Electrical Conductivity: Equal Weight (Specific), % IACS 130
110

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.8
Embodied Carbon, kg CO2/kg material 8.5
8.5
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27
15
Resilience: Unit (Modulus of Resilience), kJ/m3 23
33
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 17
19
Strength to Weight: Bending, points 25
26
Thermal Diffusivity, mm2/s 63
54
Thermal Shock Resistance, points 7.6
8.2

Alloy Composition


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Aluminum (Al), % 96.1 to 98.6
91.7 to 96.3
Chromium (Cr), % 0 to 0.3
0 to 0.2
Copper (Cu), % 0 to 0.050
0.2 to 0.7
Iron (Fe), % 0 to 0.45
0 to 0.7
Magnesium (Mg), % 1.4 to 2.1
2.1 to 3.0
Manganese (Mn), % 0 to 0.25
0.6 to 1.4
Silicon (Si), % 0 to 0.3
0.8 to 1.5
Titanium (Ti), % 0 to 0.1
0 to 0.2
Zinc (Zn), % 0 to 0.2
0 to 0.5
Residuals, % 0 to 0.15
0 to 0.15