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6025 Aluminum vs. 8176 Aluminum

Both 6025 aluminum and 8176 aluminum are aluminum alloys. They have a moderately high 95% of their average alloy composition in common.

For each property being compared, the top bar is 6025 aluminum and the bottom bar is 8176 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
69
Elongation at Break, % 2.8 to 10
15
Fatigue Strength, MPa 67 to 110
59
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 110 to 140
70
Tensile Strength: Ultimate (UTS), MPa 190 to 240
160
Tensile Strength: Yield (Proof), MPa 68 to 210
95

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 160
170
Melting Completion (Liquidus), °C 650
660
Melting Onset (Solidus), °C 550
650
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 130
230
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
61
Electrical Conductivity: Equal Weight (Specific), % IACS 110
200

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.8
2.7
Embodied Carbon, kg CO2/kg material 8.5
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1160
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.0 to 15
21
Resilience: Unit (Modulus of Resilience), kJ/m3 33 to 310
66
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 19 to 24
16
Strength to Weight: Bending, points 26 to 31
24
Thermal Diffusivity, mm2/s 54
93
Thermal Shock Resistance, points 8.2 to 10
7.0

Alloy Composition

Aluminum (Al), % 91.7 to 96.3
98.6 to 99.6
Chromium (Cr), % 0 to 0.2
0
Copper (Cu), % 0.2 to 0.7
0
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 0 to 0.7
0.4 to 1.0
Magnesium (Mg), % 2.1 to 3.0
0
Manganese (Mn), % 0.6 to 1.4
0
Silicon (Si), % 0.8 to 1.5
0.030 to 0.15
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.5
0 to 0.1
Residuals, % 0
0 to 0.15