319.0 Aluminum vs. SAE-AISI 1108 Steel
319.0 aluminum belongs to the aluminum alloys classification, while SAE-AISI 1108 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 319.0 aluminum and the bottom bar is SAE-AISI 1108 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 78 to 84 | |
| 110 to 140 |
| Elastic (Young's, Tensile) Modulus, GPa | 72 | |
| 190 |
| Elongation at Break, % | 1.8 to 2.0 | |
| 23 to 34 |
| Fatigue Strength, MPa | 76 to 80 | |
| 170 to 260 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 27 | |
| 73 |
| Shear Strength, MPa | 170 to 210 | |
| 250 to 280 |
| Tensile Strength: Ultimate (UTS), MPa | 190 to 240 | |
| 380 to 440 |
| Tensile Strength: Yield (Proof), MPa | 110 to 180 | |
| 220 to 360 |
Thermal Properties
| Latent Heat of Fusion, J/g | 480 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 400 |
| Melting Completion (Liquidus), °C | 600 | |
| 1460 |
| Melting Onset (Solidus), °C | 540 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 880 | |
| 470 |
| Thermal Conductivity, W/m-K | 110 | |
| 52 |
| Thermal Expansion, µm/m-K | 22 | |
| 12 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 27 | |
| 7.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 84 | |
| 8.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 10 | |
| 1.8 |
| Density, g/cm3 | 2.9 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 7.7 | |
| 1.4 |
| Embodied Energy, MJ/kg | 140 | |
| 18 |
| Embodied Water, L/kg | 1080 | |
| 46 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 3.3 to 3.9 | |
| 95 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 88 to 220 | |
| 130 to 340 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 48 | |
| 24 |
| Strength to Weight: Axial, points | 18 to 24 | |
| 13 to 16 |
| Strength to Weight: Bending, points | 25 to 30 | |
| 15 to 16 |
| Thermal Diffusivity, mm2/s | 44 | |
| 14 |
| Thermal Shock Resistance, points | 8.6 to 11 | |
| 12 to 14 |
Alloy Composition
| Aluminum (Al), % | 85.8 to 91.5 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.080 to 0.13 |
| Copper (Cu), % | 3.0 to 4.0 | |
| 0 |
| Iron (Fe), % | 0 to 1.0 | |
| 98.9 to 99.24 |
| Magnesium (Mg), % | 0 to 0.1 | |
| 0 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0.6 to 0.8 |
| Nickel (Ni), % | 0 to 0.35 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 5.5 to 6.5 | |
| 0 |
| Sulfur (S), % | 0 | |
| 0.080 to 0.13 |
| Titanium (Ti), % | 0 to 0.25 | |
| 0 |
| Zinc (Zn), % | 0 to 1.0 | |
| 0 |
| Residuals, % | 0 to 0.5 | |
| 0 |