ASTM A182 Grade F10 vs. 356.0 Aluminum
ASTM A182 grade F10 belongs to the iron alloys classification, while 356.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is ASTM A182 grade F10 and the bottom bar is 356.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 190 | |
| 55 to 75 |
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 70 |
| Elongation at Break, % | 34 | |
| 2.0 to 3.8 |
| Fatigue Strength, MPa | 180 | |
| 55 to 75 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 74 | |
| 27 |
| Shear Strength, MPa | 420 | |
| 140 to 190 |
| Tensile Strength: Ultimate (UTS), MPa | 630 | |
| 160 to 240 |
| Tensile Strength: Yield (Proof), MPa | 230 | |
| 100 to 190 |
Thermal Properties
| Latent Heat of Fusion, J/g | 290 | |
| 500 |
| Maximum Temperature: Mechanical, °C | 600 | |
| 170 |
| Melting Completion (Liquidus), °C | 1420 | |
| 620 |
| Melting Onset (Solidus), °C | 1370 | |
| 570 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 900 |
| Thermal Expansion, µm/m-K | 13 | |
| 21 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 15 | |
| 40 to 43 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 17 | |
| 140 to 150 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 18 | |
| 9.5 |
| Density, g/cm3 | 7.9 | |
| 2.6 |
| Embodied Carbon, kg CO2/kg material | 3.6 | |
| 8.0 |
| Embodied Energy, MJ/kg | 51 | |
| 150 |
| Embodied Water, L/kg | 120 | |
| 1110 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 170 | |
| 3.2 to 8.2 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 140 | |
| 70 to 250 |
| Stiffness to Weight: Axial, points | 13 | |
| 15 |
| Stiffness to Weight: Bending, points | 24 | |
| 53 |
| Strength to Weight: Axial, points | 22 | |
| 17 to 26 |
| Strength to Weight: Bending, points | 21 | |
| 25 to 33 |
| Thermal Shock Resistance, points | 18 | |
| 7.6 to 11 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 90.1 to 93.3 |
| Carbon (C), % | 0.1 to 0.2 | |
| 0 |
| Chromium (Cr), % | 7.0 to 9.0 | |
| 0 |
| Copper (Cu), % | 0 | |
| 0 to 0.25 |
| Iron (Fe), % | 66.5 to 72.4 | |
| 0 to 0.6 |
| Magnesium (Mg), % | 0 | |
| 0.2 to 0.45 |
| Manganese (Mn), % | 0.5 to 0.8 | |
| 0 to 0.35 |
| Nickel (Ni), % | 19 to 22 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 |
| Silicon (Si), % | 1.0 to 1.4 | |
| 6.5 to 7.5 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.25 |
| Zinc (Zn), % | 0 | |
| 0 to 0.35 |
| Residuals, % | 0 | |
| 0 to 0.15 |