50Cr-50Ni Alloy vs. Class 4 Tungsten
Both 50Cr-50Ni alloy and class 4 tungsten are otherwise unclassified metals. Both are furnished in the as-fabricated (no temper or treatment) condition. There are 20 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is 50Cr-50Ni alloy and the bottom bar is class 4 tungsten.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
270 |
Elongation at Break, % | 5.7 | |
2.3 |
Poisson's Ratio | 0.26 | |
0.28 |
Shear Modulus, GPa | 84 | |
110 |
Tensile Strength: Ultimate (UTS), MPa | 620 | |
790 |
Tensile Strength: Yield (Proof), MPa | 390 | |
580 |
Thermal Properties
Latent Heat of Fusion, J/g | 350 | |
170 |
Specific Heat Capacity, J/kg-K | 490 | |
130 |
Thermal Expansion, µm/m-K | 15 | |
4.5 |
Otherwise Unclassified Properties
Density, g/cm3 | 8.0 | |
16 |
Embodied Carbon, kg CO2/kg material | 7.9 | |
24 |
Embodied Energy, MJ/kg | 110 | |
360 |
Embodied Water, L/kg | 350 | |
150 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 31 | |
16 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 350 | |
620 |
Stiffness to Weight: Axial, points | 15 | |
9.6 |
Stiffness to Weight: Bending, points | 25 | |
14 |
Strength to Weight: Axial, points | 21 | |
14 |
Strength to Weight: Bending, points | 20 | |
12 |
Thermal Shock Resistance, points | 14 | |
46 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0 |
Chromium (Cr), % | 48 to 52 | |
0 |
Iron (Fe), % | 0 to 1.0 | |
0 |
Manganese (Mn), % | 0 to 0.3 | |
0 |
Nickel (Ni), % | 44.5 to 52 | |
0 |
Nitrogen (N), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.020 | |
0 |
Silicon (Si), % | 0 to 1.0 | |
0 |
Sulfur (S), % | 0 to 0.020 | |
0 |
Titanium (Ti), % | 0 to 0.5 | |
0 |
Tungsten (W), % | 0 | |
97 |
Residuals, % | 0 | |
3.0 |