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5026-H111 Aluminum vs. 5449-H111 Aluminum

Both 5026-H111 aluminum and 5449-H111 aluminum are aluminum alloys. Both are furnished in the H111 temper. They have a very high 96% of their average alloy composition in common.

For each property being compared, the top bar is 5026-H111 aluminum and the bottom bar is 5449-H111 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
69
Elongation at Break, % 10
17
Fatigue Strength, MPa 94
78
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 150
130
Tensile Strength: Ultimate (UTS), MPa 260
210
Tensile Strength: Yield (Proof), MPa 120
91

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 210
190
Melting Completion (Liquidus), °C 650
650
Melting Onset (Solidus), °C 510
590
Specific Heat Capacity, J/kg-K 890
900
Thermal Conductivity, W/m-K 130
140
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
35
Electrical Conductivity: Equal Weight (Specific), % IACS 99
110

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.8
2.8
Embodied Carbon, kg CO2/kg material 8.9
8.5
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 22
29
Resilience: Unit (Modulus of Resilience), kJ/m3 100
60
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
50
Strength to Weight: Axial, points 26
22
Strength to Weight: Bending, points 33
29
Thermal Diffusivity, mm2/s 52
56
Thermal Shock Resistance, points 11
9.4

Alloy Composition


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Aluminum (Al), % 88.2 to 94.7
94.1 to 97.8
Chromium (Cr), % 0 to 0.3
0 to 0.3
Copper (Cu), % 0.1 to 0.8
0 to 0.3
Iron (Fe), % 0.2 to 1.0
0 to 0.7
Magnesium (Mg), % 3.9 to 4.9
1.6 to 2.6
Manganese (Mn), % 0.6 to 1.8
0.6 to 1.1
Silicon (Si), % 0.55 to 1.4
0 to 0.4
Titanium (Ti), % 0 to 0.2
0 to 0.1
Zinc (Zn), % 0 to 1.0
0 to 0.3
Zirconium (Zr), % 0 to 0.3
0
Residuals, % 0 to 0.15
0 to 0.15