50Cr-50Ni Alloy vs. EV31A Magnesium
50Cr-50Ni alloy belongs to the otherwise unclassified metals classification, while EV31A magnesium belongs to the magnesium alloys. There are 16 material properties with values for both materials. Properties with values for just one material (16, 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 50Cr-50Ni alloy and the bottom bar is EV31A magnesium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 44 |
| Elongation at Break, % | 5.7 | |
| 3.5 |
| Poisson's Ratio | 0.26 | |
| 0.27 |
| Shear Modulus, GPa | 84 | |
| 17 |
| Tensile Strength: Ultimate (UTS), MPa | 620 | |
| 260 |
| Tensile Strength: Yield (Proof), MPa | 390 | |
| 170 |
Thermal Properties
| Specific Heat Capacity, J/kg-K | 490 | |
| 1000 |
| Thermal Expansion, µm/m-K | 15 | |
| 27 |
Otherwise Unclassified Properties
| Density, g/cm3 | 8.0 | |
| 1.8 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 31 | |
| 8.1 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 350 | |
| 330 |
| Stiffness to Weight: Axial, points | 15 | |
| 13 |
| Stiffness to Weight: Bending, points | 25 | |
| 65 |
| Strength to Weight: Axial, points | 21 | |
| 40 |
| Strength to Weight: Bending, points | 20 | |
| 50 |
| Thermal Shock Resistance, points | 14 | |
| 16 |