C12/15 vs C55/67
C55/67 is 1.4 times as stiff as C12/15. Their densities are about the same. Per unit mass C55/67 is 1.4 times as stiff. Strength: f_ck = 12 MPa for C12/15, f_ck = 55 MPa for C55/67.
Side by side
ratio = C55/67 / C12/15 · log scale| Property | C12/15 | C55/67 | Unit | Ratio | ¼×1×4× |
|---|---|---|---|---|---|
| E Young's modulus | 27 | 38 | GPa | 1.41× | |
| G Shear modulus | 11.25 | 15.83 | GPa | 1.41× | |
| 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 | 12 | 55 | MPa | 4.58× | |
| f_ck,cube Characteristic cube strength | 15 | 67 | MPa | 4.47× | |
| f_cm Mean cylinder strength | 20 | 63 | MPa | 3.15× | |
| f_ctm Mean tensile strength | 1.6 | 4.2 | MPa | 2.62× | |
| f_ctk,0.05 Tensile strength, 5 % fractile | 1.1 | 3 | MPa | 2.73× | |
| f_ctk,0.95 Tensile strength, 95 % fractile | 2 | 5.5 | MPa | 2.75× | |
| ε_c1 Strain at peak stress | 1.8 | 2.5 | ‰ | 1.39× | |
| 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 | 11.03 | 15.53 | MJ/kg | 1.41× | |
| c₀ Bar wave speed √(E/ρ) · derived | 3322 | 3940 | m/s | 1.19× | |
| f/ρ Specific strength f/ρ · derived | 4.903 | 22.47 | kJ/kg | 4.58× |
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.