EN 1.6526 Steel vs. AWS E320LR
Both EN 1.6526 steel and AWS E320LR are iron alloys. They have 40% of their average alloy composition in common. There are 19 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.
For each property being compared, the top bar is EN 1.6526 steel and the bottom bar is AWS E320LR.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 200 |
| Poisson's Ratio | 0.29 | |
| 0.28 |
| Shear Modulus, GPa | 73 | |
| 77 |
| Tensile Strength: Ultimate (UTS), MPa | 520 to 1460 | |
| 580 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 300 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1410 |
| Melting Onset (Solidus), °C | 1420 | |
| 1360 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 460 |
| Thermal Expansion, µm/m-K | 13 | |
| 14 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 2.6 | |
| 36 |
| Density, g/cm3 | 7.9 | |
| 8.2 |
| Embodied Carbon, kg CO2/kg material | 1.5 | |
| 6.2 |
| Embodied Energy, MJ/kg | 20 | |
| 87 |
| Embodied Water, L/kg | 50 | |
| 220 |
Common Calculations
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 | |
| 24 |
| Strength to Weight: Axial, points | 18 to 52 | |
| 20 |
| Strength to Weight: Bending, points | 18 to 36 | |
| 19 |
| Thermal Shock Resistance, points | 15 to 43 | |
| 15 |
Alloy Composition
| Carbon (C), % | 0.17 to 0.23 | |
| 0 to 0.030 |
| Chromium (Cr), % | 0.35 to 0.7 | |
| 19 to 21 |
| Copper (Cu), % | 0 to 0.25 | |
| 3.0 to 4.0 |
| Iron (Fe), % | 96.6 to 98.3 | |
| 32.7 to 42.5 |
| Manganese (Mn), % | 0.65 to 1.0 | |
| 1.5 to 2.5 |
| Molybdenum (Mo), % | 0.15 to 0.25 | |
| 2.0 to 3.0 |
| Nickel (Ni), % | 0.4 to 0.7 | |
| 32 to 36 |
| Niobium (Nb), % | 0 | |
| 0 to 0.4 |
| Phosphorus (P), % | 0 to 0.025 | |
| 0 to 0.020 |
| Silicon (Si), % | 0 to 0.3 | |
| 0 to 0.3 |
| Sulfur (S), % | 0.020 to 0.040 | |
| 0 to 0.015 |