AWS E320LR vs. C21000 Brass
AWS E320LR belongs to the iron alloys classification, while C21000 brass belongs to the copper alloys. There are 20 material properties with values for both materials. Properties with values for just one material (12, in this case) are not shown.
For each property being compared, the top bar is AWS E320LR and the bottom bar is C21000 brass.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
110 |
Elongation at Break, % | 34 | |
2.9 to 50 |
Poisson's Ratio | 0.28 | |
0.34 |
Shear Modulus, GPa | 77 | |
43 |
Tensile Strength: Ultimate (UTS), MPa | 580 | |
240 to 450 |
Thermal Properties
Latent Heat of Fusion, J/g | 300 | |
200 |
Melting Completion (Liquidus), °C | 1410 | |
1070 |
Melting Onset (Solidus), °C | 1360 | |
1050 |
Specific Heat Capacity, J/kg-K | 460 | |
390 |
Thermal Expansion, µm/m-K | 14 | |
18 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 36 | |
30 |
Density, g/cm3 | 8.2 | |
8.8 |
Embodied Carbon, kg CO2/kg material | 6.2 | |
2.6 |
Embodied Energy, MJ/kg | 87 | |
42 |
Embodied Water, L/kg | 220 | |
310 |
Common Calculations
Stiffness to Weight: Axial, points | 13 | |
7.2 |
Stiffness to Weight: Bending, points | 24 | |
18 |
Strength to Weight: Axial, points | 20 | |
7.4 to 14 |
Strength to Weight: Bending, points | 19 | |
9.6 to 15 |
Thermal Shock Resistance, points | 15 | |
8.1 to 15 |
Alloy Composition
Carbon (C), % | 0 to 0.030 | |
0 |
Chromium (Cr), % | 19 to 21 | |
0 |
Copper (Cu), % | 3.0 to 4.0 | |
94 to 96 |
Iron (Fe), % | 32.7 to 42.5 | |
0 to 0.050 |
Lead (Pb), % | 0 | |
0 to 0.030 |
Manganese (Mn), % | 1.5 to 2.5 | |
0 |
Molybdenum (Mo), % | 2.0 to 3.0 | |
0 |
Nickel (Ni), % | 32 to 36 | |
0 |
Niobium (Nb), % | 0 to 0.4 | |
0 |
Phosphorus (P), % | 0 to 0.020 | |
0 |
Silicon (Si), % | 0 to 0.3 | |
0 |
Sulfur (S), % | 0 to 0.015 | |
0 |
Zinc (Zn), % | 0 | |
3.7 to 6.0 |
Residuals, % | 0 | |
0 to 0.2 |