1235-H111 Aluminum vs. 8011A-H111 Aluminum
Both 1235-H111 aluminum and 8011A-H111 aluminum are aluminum alloys. Both are furnished in the H111 temper. Their average alloy composition is basically identical. There are 29 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is 1235-H111 aluminum and the bottom bar is 8011A-H111 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 69 | |
| 69 |
| Elongation at Break, % | 34 | |
| 28 |
| Fatigue Strength, MPa | 58 | |
| 33 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 26 | |
| 26 |
| Tensile Strength: Ultimate (UTS), MPa | 84 | |
| 100 |
| Tensile Strength: Yield (Proof), MPa | 57 | |
| 34 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 170 |
| Melting Completion (Liquidus), °C | 640 | |
| 650 |
| Melting Onset (Solidus), °C | 640 | |
| 630 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 900 |
| Thermal Conductivity, W/m-K | 230 | |
| 210 |
| Thermal Expansion, µm/m-K | 23 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 60 | |
| 56 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 200 | |
| 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 | 8.3 | |
| 8.2 |
| Embodied Energy, MJ/kg | 160 | |
| 150 |
| Embodied Water, L/kg | 1190 | |
| 1180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 25 | |
| 22 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 24 | |
| 8.2 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 50 | |
| 50 |
| Strength to Weight: Axial, points | 8.6 | |
| 11 |
| Strength to Weight: Bending, points | 16 | |
| 18 |
| Thermal Diffusivity, mm2/s | 93 | |
| 86 |
| Thermal Shock Resistance, points | 3.7 | |
| 4.6 |
Alloy Composition
| Aluminum (Al), % | 99.35 to 100 | |
| 97.5 to 99.1 |
| Chromium (Cr), % | 0 | |
| 0 to 0.1 |
| Copper (Cu), % | 0 to 0.050 | |
| 0 to 0.1 |
| Iron (Fe), % | 0 to 0.65 | |
| 0.5 to 1.0 |
| Magnesium (Mg), % | 0 to 0.050 | |
| 0 to 0.1 |
| Manganese (Mn), % | 0 to 0.050 | |
| 0 to 0.1 |
| Silicon (Si), % | 0 to 0.65 | |
| 0.4 to 0.8 |
| Titanium (Ti), % | 0 to 0.060 | |
| 0 to 0.050 |
| Vanadium (V), % | 0 to 0.050 | |
| 0 |
| Zinc (Zn), % | 0 to 0.1 | |
| 0 to 0.1 |
| Residuals, % | 0 | |
| 0 to 0.15 |