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5088 Aluminum vs. 6110 Aluminum

Both 5088 aluminum and 6110 aluminum are aluminum alloys. They have a very high 96% of their average alloy composition in common.

For each property being compared, the top bar is 5088 aluminum and the bottom bar is 6110 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
70
Elongation at Break, % 29
2.2
Fatigue Strength, MPa 180
120
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 25
26
Shear Strength, MPa 200
290
Tensile Strength: Ultimate (UTS), MPa 310
500
Tensile Strength: Yield (Proof), MPa 150
500

Thermal Properties

Latent Heat of Fusion, J/g 390
410
Maximum Temperature: Mechanical, °C 200
170
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 540
600
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 120
170
Thermal Expansion, µm/m-K 24
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
42
Electrical Conductivity: Equal Weight (Specific), % IACS 98
140

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.8
Embodied Carbon, kg CO2/kg material 9.0
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1180
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 76
11
Resilience: Unit (Modulus of Resilience), kJ/m3 170
1770
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 32
51
Strength to Weight: Bending, points 38
51
Thermal Diffusivity, mm2/s 51
67
Thermal Shock Resistance, points 14
22

Alloy Composition

Aluminum (Al), % 92.4 to 94.8
94.4 to 98.4
Chromium (Cr), % 0 to 0.15
0.040 to 0.25
Copper (Cu), % 0 to 0.25
0.2 to 0.7
Iron (Fe), % 0.1 to 0.35
0 to 0.8
Magnesium (Mg), % 4.7 to 5.5
0.5 to 1.1
Manganese (Mn), % 0.2 to 0.5
0.2 to 0.7
Silicon (Si), % 0 to 0.2
0.7 to 1.5
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0.2 to 0.4
0 to 0.3
Zirconium (Zr), % 0 to 0.15
0
Residuals, % 0
0 to 0.15