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8011A Aluminum vs. EN AC-51300 Aluminum

Both 8011A aluminum and EN AC-51300 aluminum are aluminum alloys. They have a moderately high 94% of their average alloy composition in common.

For each property being compared, the top bar is 8011A aluminum and the bottom bar is EN AC-51300 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 25 to 50
65
Elastic (Young's, Tensile) Modulus, GPa 69
67
Elongation at Break, % 1.7 to 28
3.7
Fatigue Strength, MPa 33 to 76
78
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
25
Tensile Strength: Ultimate (UTS), MPa 100 to 180
190
Tensile Strength: Yield (Proof), MPa 34 to 170
110

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 170
170
Melting Completion (Liquidus), °C 650
640
Melting Onset (Solidus), °C 630
600
Specific Heat Capacity, J/kg-K 900
910
Thermal Conductivity, W/m-K 210
110
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 56
31
Electrical Conductivity: Equal Weight (Specific), % IACS 180
100

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
9.5
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 8.2
9.1
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1180
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.0 to 22
6.1
Resilience: Unit (Modulus of Resilience), kJ/m3 8.2 to 200
87
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
51
Strength to Weight: Axial, points 11 to 18
20
Strength to Weight: Bending, points 18 to 26
28
Thermal Diffusivity, mm2/s 86
45
Thermal Shock Resistance, points 4.6 to 8.1
8.6

Alloy Composition

Aluminum (Al), % 97.5 to 99.1
91.4 to 95.5
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0 to 0.1
0 to 0.1
Iron (Fe), % 0.5 to 1.0
0 to 0.55
Magnesium (Mg), % 0 to 0.1
4.5 to 6.5
Manganese (Mn), % 0 to 0.1
0 to 0.45
Silicon (Si), % 0.4 to 0.8
0 to 0.55
Titanium (Ti), % 0 to 0.050
0 to 0.2
Zinc (Zn), % 0 to 0.1
0 to 0.1
Residuals, % 0
0 to 0.15