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5051A Aluminum vs. 6151 Aluminum

Both 5051A aluminum and 6151 aluminum are aluminum alloys. They have a very high 99% of their average alloy composition in common.

For each property being compared, the top bar is 5051A aluminum and the bottom bar is 6151 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
69
Elongation at Break, % 18 to 21
1.1 to 5.7
Fatigue Strength, MPa 51 to 61
80 to 100
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 110
190 to 200
Tensile Strength: Ultimate (UTS), MPa 170
330 to 340
Tensile Strength: Yield (Proof), MPa 56
270 to 280

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 190
170
Melting Completion (Liquidus), °C 640
650
Melting Onset (Solidus), °C 610
590
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 150
170
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 39
45
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
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 27
3.5 to 18
Resilience: Unit (Modulus of Resilience), kJ/m3 23
520 to 580
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 17 to 18
34
Strength to Weight: Bending, points 25
39
Thermal Diffusivity, mm2/s 63
70
Thermal Shock Resistance, points 7.6
15

Alloy Composition

Aluminum (Al), % 96.1 to 98.6
95.6 to 98.8
Chromium (Cr), % 0 to 0.3
0.15 to 0.35
Copper (Cu), % 0 to 0.050
0 to 0.35
Iron (Fe), % 0 to 0.45
0 to 1.0
Magnesium (Mg), % 1.4 to 2.1
0.45 to 0.8
Manganese (Mn), % 0 to 0.25
0 to 0.2
Silicon (Si), % 0 to 0.3
0.6 to 1.2
Titanium (Ti), % 0 to 0.1
0 to 0.15
Zinc (Zn), % 0 to 0.2
0 to 0.25
Residuals, % 0
0 to 0.15