Chromium 33 vs. 50Cr-50Ni Alloy
Both chromium 33 and 50Cr-50Ni alloy are otherwise unclassified metals. They have 66% of their average alloy composition in common.
For each property being compared, the top bar is chromium 33 and the bottom bar is 50Cr-50Ni alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
210 |
Elongation at Break, % | 45 | |
5.7 |
Poisson's Ratio | 0.27 | |
0.26 |
Shear Modulus, GPa | 81 | |
84 |
Tensile Strength: Ultimate (UTS), MPa | 850 | |
620 |
Tensile Strength: Yield (Proof), MPa | 430 | |
390 |
Thermal Properties
Latent Heat of Fusion, J/g | 320 | |
350 |
Specific Heat Capacity, J/kg-K | 480 | |
490 |
Thermal Expansion, µm/m-K | 14 | |
15 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 36 | |
50 |
Density, g/cm3 | 7.9 | |
8.0 |
Embodied Carbon, kg CO2/kg material | 6.0 | |
7.9 |
Embodied Energy, MJ/kg | 84 | |
110 |
Embodied Water, L/kg | 250 | |
350 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 320 | |
31 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 450 | |
350 |
Stiffness to Weight: Axial, points | 14 | |
15 |
Stiffness to Weight: Bending, points | 25 | |
25 |
Strength to Weight: Axial, points | 30 | |
21 |
Strength to Weight: Bending, points | 25 | |
20 |
Thermal Shock Resistance, points | 21 | |
14 |
Alloy Composition
Aluminum (Al), % | 0 | |
0 to 0.25 |
Carbon (C), % | 0 to 0.015 | |
0 to 0.1 |
Chromium (Cr), % | 31 to 35 | |
48 to 52 |
Copper (Cu), % | 0.3 to 1.2 | |
0 |
Iron (Fe), % | 25.7 to 37.9 | |
0 to 1.0 |
Manganese (Mn), % | 0 to 2.0 | |
0 to 0.3 |
Molybdenum (Mo), % | 0.5 to 2.0 | |
0 |
Nickel (Ni), % | 30 to 33 | |
44.5 to 52 |
Nitrogen (N), % | 0.35 to 0.6 | |
0 to 0.3 |
Phosphorus (P), % | 0 to 0.020 | |
0 to 0.020 |
Silicon (Si), % | 0 to 0.5 | |
0 to 1.0 |
Sulfur (S), % | 0 to 0.010 | |
0 to 0.020 |
Titanium (Ti), % | 0 | |
0 to 0.5 |