C20/25 vs C55/67
C55/67 is 1.3 times as stiff as C20/25. Their densities are about the same. Per unit mass C55/67 is 1.3 times as stiff. Strength: f_ck = 20 MPa for C20/25, f_ck = 55 MPa for C55/67.
Side by side
ratio = C55/67 / C20/25 · log scale| Property | C20/25 | C55/67 | Unit | Ratio | ¼×1×4× |
|---|---|---|---|---|---|
| E Young's modulus | 30 | 38 | GPa | 1.27× | |
| G Shear modulus | 12.5 | 15.83 | GPa | 1.27× | |
| ν Poisson's ratio | 0.2 | 0.2 | – | 1× | |
| ρ Density | 2447 | 2447 | kg/m³ | 1× | |
| γ Weight density | 24 | 24 | kN/m³ | 1× | |
| α Coefficient of thermal expansion | 10 | 10 | 10⁻⁶/K | 1× | |
| f_ck Characteristic cylinder strength | 20 | 55 | MPa | 2.75× | |
| f_ck,cube Characteristic cube strength | 25 | 67 | MPa | 2.68× | |
| f_cm Mean cylinder strength | 28 | 63 | MPa | 2.25× | |
| f_ctm Mean tensile strength | 2.2 | 4.2 | MPa | 1.91× | |
| f_ctk,0.05 Tensile strength, 5 % fractile | 1.5 | 3 | MPa | 2× | |
| f_ctk,0.95 Tensile strength, 95 % fractile | 2.9 | 5.5 | MPa | 1.9× | |
| ε_c1 Strain at peak stress | 2 | 2.5 | ‰ | 1.25× | |
| ε_cu1 Ultimate strain | 3.5 | 3.2 | ‰ | 0.914× | |
| ε_c2 Strain at peak, parabola–rectangle | 2 | 2.2 | ‰ | 1.1× | |
| ε_cu2 Ultimate strain, parabola–rectangle | 3.5 | 3.1 | ‰ | 0.886× | |
| n Exponent, parabola–rectangle | 2 | 1.75 | – | 0.875× | |
| ε_c3 Strain at peak, bilinear | 1.75 | 1.8 | ‰ | 1.03× | |
| ε_cu3 Ultimate strain, bilinear | 3.5 | 3.1 | ‰ | 0.886× | |
| E/ρ Specific stiffness E/ρ · derived | 12.26 | 15.53 | MJ/kg | 1.27× | |
| c₀ Bar wave speed √(E/ρ) · derived | 3501 | 3940 | m/s | 1.13× | |
| f/ρ Specific strength f/ρ · derived | 8.172 | 22.47 | kJ/kg | 2.75× |
Values at the first thickness band or product form of each material (EN 1992-1-1; EN 1992-1-1). A minimum and a characteristic value are not the same kind of number — read the ratio as a guide. Each material's page lists every band and every source.