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512.0 Aluminum vs. 8011A Aluminum

Both 512.0 aluminum and 8011A 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 512.0 aluminum and the bottom bar is 8011A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 50
25 to 50
Elastic (Young's, Tensile) Modulus, GPa 69
69
Elongation at Break, % 2.0
1.7 to 28
Fatigue Strength, MPa 58
33 to 76
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Tensile Strength: Ultimate (UTS), MPa 130
100 to 180
Tensile Strength: Yield (Proof), MPa 83
34 to 170

Thermal Properties

Latent Heat of Fusion, J/g 420
400
Maximum Temperature: Mechanical, °C 180
170
Melting Completion (Liquidus), °C 630
650
Melting Onset (Solidus), °C 590
630
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 150
210
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
56
Electrical Conductivity: Equal Weight (Specific), % IACS 130
180

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.0
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 8.8
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1160
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3
3.0 to 22
Resilience: Unit (Modulus of Resilience), kJ/m3 50
8.2 to 200
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
50
Strength to Weight: Axial, points 14
11 to 18
Strength to Weight: Bending, points 22
18 to 26
Thermal Diffusivity, mm2/s 60
86
Thermal Shock Resistance, points 6.1
4.6 to 8.1

Alloy Composition

Aluminum (Al), % 90.6 to 95.1
97.5 to 99.1
Chromium (Cr), % 0 to 0.25
0 to 0.1
Copper (Cu), % 0 to 0.35
0 to 0.1
Iron (Fe), % 0 to 0.6
0.5 to 1.0
Magnesium (Mg), % 3.5 to 4.5
0 to 0.1
Manganese (Mn), % 0 to 0.8
0 to 0.1
Silicon (Si), % 1.4 to 2.2
0.4 to 0.8
Titanium (Ti), % 0 to 0.25
0 to 0.050
Zinc (Zn), % 0 to 0.35
0 to 0.1
Residuals, % 0
0 to 0.15