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8176 Aluminum vs. 6025 Aluminum

Both 8176 aluminum and 6025 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 8176 aluminum and the bottom bar is 6025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61
33
Electrical Conductivity: Equal Weight (Specific), % IACS 200
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 8.2
8.5
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1160

Common Calculations

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

Alloy Composition


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