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6110 Aluminum vs. 5019 Aluminum

Both 6110 aluminum and 5019 aluminum are aluminum alloys. They have a very high 95% of their average alloy composition in common.

For each property being compared, the top bar is 6110 aluminum and the bottom bar is 5019 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
68
Elongation at Break, % 2.2
2.2 to 18
Fatigue Strength, MPa 120
100 to 160
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 290
170 to 210
Tensile Strength: Ultimate (UTS), MPa 500
280 to 360
Tensile Strength: Yield (Proof), MPa 500
120 to 300

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 170
180
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 600
540
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 170
130
Thermal Expansion, µm/m-K 23
24

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
7.6 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 1770
110 to 650
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
51
Strength to Weight: Axial, points 51
29 to 38
Strength to Weight: Bending, points 51
35 to 42
Thermal Diffusivity, mm2/s 67
52
Thermal Shock Resistance, points 22
13 to 16

Alloy Composition

Aluminum (Al), % 94.4 to 98.4
91.5 to 95.3
Chromium (Cr), % 0.040 to 0.25
0 to 0.2
Copper (Cu), % 0.2 to 0.7
0 to 0.1
Iron (Fe), % 0 to 0.8
0 to 0.5
Magnesium (Mg), % 0.5 to 1.1
4.5 to 5.6
Manganese (Mn), % 0.2 to 0.7
0.1 to 0.6
Silicon (Si), % 0.7 to 1.5
0 to 0.4
Titanium (Ti), % 0 to 0.15
0 to 0.2
Zinc (Zn), % 0 to 0.3
0 to 0.2
Residuals, % 0 to 0.15
0 to 0.15