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6063A Aluminum vs. 8176 Aluminum

Both 6063A aluminum and 8176 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 6063A aluminum and the bottom bar is 8176 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
69
Elongation at Break, % 6.7 to 18
15
Fatigue Strength, MPa 53 to 80
59
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 78 to 150
70
Tensile Strength: Ultimate (UTS), MPa 130 to 260
160
Tensile Strength: Yield (Proof), MPa 55 to 200
95

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 160
170
Melting Completion (Liquidus), °C 640
660
Melting Onset (Solidus), °C 620
650
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 200
230
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 49 to 54
61
Electrical Conductivity: Equal Weight (Specific), % IACS 160 to 180
200

Otherwise Unclassified Properties

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

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 21
21
Resilience: Unit (Modulus of Resilience), kJ/m3 22 to 280
66
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 13 to 26
16
Strength to Weight: Bending, points 21 to 33
24
Thermal Diffusivity, mm2/s 83
93
Thermal Shock Resistance, points 5.6 to 11
7.0

Alloy Composition


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Aluminum (Al), % 97.5 to 99
98.6 to 99.6
Chromium (Cr), % 0 to 0.050
0
Copper (Cu), % 0 to 0.1
0
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 0.15 to 0.35
0.4 to 1.0
Magnesium (Mg), % 0.6 to 0.9
0
Manganese (Mn), % 0 to 0.15
0
Silicon (Si), % 0.3 to 0.6
0.030 to 0.15
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.15
0 to 0.1
Residuals, % 0 to 0.15
0 to 0.15