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5088 Aluminum vs. 6106 Aluminum

Both 5088 aluminum and 6106 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 5088 aluminum and the bottom bar is 6106 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
69
Elongation at Break, % 29
9.1
Fatigue Strength, MPa 180
88
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 25
26
Shear Strength, MPa 200
170
Tensile Strength: Ultimate (UTS), MPa 310
290
Tensile Strength: Yield (Proof), MPa 150
220

Thermal Properties

Latent Heat of Fusion, J/g 390
400
Maximum Temperature: Mechanical, °C 200
160
Melting Completion (Liquidus), °C 640
660
Melting Onset (Solidus), °C 540
610
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 120
190
Thermal Expansion, µm/m-K 24
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
49
Electrical Conductivity: Equal Weight (Specific), % IACS 98
160

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 9.0
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1180
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 76
24
Resilience: Unit (Modulus of Resilience), kJ/m3 170
370
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 32
29
Strength to Weight: Bending, points 38
35
Thermal Diffusivity, mm2/s 51
78
Thermal Shock Resistance, points 14
13

Alloy Composition

Aluminum (Al), % 92.4 to 94.8
97.2 to 99.3
Chromium (Cr), % 0 to 0.15
0 to 0.2
Copper (Cu), % 0 to 0.25
0 to 0.25
Iron (Fe), % 0.1 to 0.35
0 to 0.35
Magnesium (Mg), % 4.7 to 5.5
0.4 to 0.8
Manganese (Mn), % 0.2 to 0.5
0.050 to 0.2
Silicon (Si), % 0 to 0.2
0.3 to 0.6
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0.2 to 0.4
0 to 0.15
Zirconium (Zr), % 0 to 0.15
0
Residuals, % 0
0 to 0.15