C55/67 vs C90/105
C90/105 is 1.2 times as stiff as C55/67. Their densities are about the same. Per unit mass C90/105 is 1.2 times as stiff. Strength: f_ck = 55 MPa for C55/67, f_ck = 90 MPa for C90/105.
Side by side
ratio = C90/105 / C55/67 · log scale| Property | C55/67 | C90/105 | Unit | Ratio | ¼×1×4× |
|---|---|---|---|---|---|
| E Young's modulus | 38 | 44 | GPa | 1.16× | |
| G Shear modulus | 15.83 | 18.33 | GPa | 1.16× | |
| 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 | 55 | 90 | MPa | 1.64× | |
| f_ck,cube Characteristic cube strength | 67 | 105 | MPa | 1.57× | |
| f_cm Mean cylinder strength | 63 | 98 | MPa | 1.56× | |
| f_ctm Mean tensile strength | 4.2 | 5 | MPa | 1.19× | |
| f_ctk,0.05 Tensile strength, 5 % fractile | 3 | 3.5 | MPa | 1.17× | |
| f_ctk,0.95 Tensile strength, 95 % fractile | 5.5 | 6.6 | MPa | 1.2× | |
| ε_c1 Strain at peak stress | 2.5 | 2.8 | ‰ | 1.12× | |
| ε_cu1 Ultimate strain | 3.2 | 2.8 | ‰ | 0.875× | |
| ε_c2 Strain at peak, parabola–rectangle | 2.2 | 2.6 | ‰ | 1.18× | |
| ε_cu2 Ultimate strain, parabola–rectangle | 3.1 | 2.6 | ‰ | 0.839× | |
| n Exponent, parabola–rectangle | 1.75 | 1.4 | – | 0.8× | |
| ε_c3 Strain at peak, bilinear | 1.8 | 2.3 | ‰ | 1.28× | |
| ε_cu3 Ultimate strain, bilinear | 3.1 | 2.6 | ‰ | 0.839× | |
| E/ρ Specific stiffness E/ρ · derived | 15.53 | 17.98 | MJ/kg | 1.16× | |
| c₀ Bar wave speed √(E/ρ) · derived | 3940 | 4240 | m/s | 1.08× | |
| f/ρ Specific strength f/ρ · derived | 22.47 | 36.78 | kJ/kg | 1.64× |
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.