C25/30 vs C45/55
C45/55 is 1.2 times as stiff as C25/30. Their densities are about the same. Per unit mass C45/55 is 1.2 times as stiff. Strength: f_ck = 25 MPa for C25/30, f_ck = 45 MPa for C45/55.
Side by side
ratio = C45/55 / C25/30 · log scale| Property | C25/30 | C45/55 | Unit | Ratio | ¼×1×4× |
|---|---|---|---|---|---|
| E Young's modulus | 31 | 36 | GPa | 1.16× | |
| G Shear modulus | 12.92 | 15 | 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 | 25 | 45 | MPa | 1.8× | |
| f_ck,cube Characteristic cube strength | 30 | 55 | MPa | 1.83× | |
| f_cm Mean cylinder strength | 33 | 53 | MPa | 1.61× | |
| f_ctm Mean tensile strength | 2.6 | 3.8 | MPa | 1.46× | |
| f_ctk,0.05 Tensile strength, 5 % fractile | 1.8 | 2.7 | MPa | 1.5× | |
| f_ctk,0.95 Tensile strength, 95 % fractile | 3.3 | 4.9 | MPa | 1.48× | |
| ε_c1 Strain at peak stress | 2.1 | 2.4 | ‰ | 1.14× | |
| ε_cu1 Ultimate strain | 3.5 | 3.5 | ‰ | 1× | |
| ε_c2 Strain at peak, parabola–rectangle | 2 | 2 | ‰ | 1× | |
| ε_cu2 Ultimate strain, parabola–rectangle | 3.5 | 3.5 | ‰ | 1× | |
| n Exponent, parabola–rectangle | 2 | 2 | – | 1× | |
| ε_c3 Strain at peak, bilinear | 1.75 | 1.75 | ‰ | 1× | |
| ε_cu3 Ultimate strain, bilinear | 3.5 | 3.5 | ‰ | 1× | |
| E/ρ Specific stiffness E/ρ · derived | 12.67 | 14.71 | MJ/kg | 1.16× | |
| c₀ Bar wave speed √(E/ρ) · derived | 3559 | 3835 | m/s | 1.08× | |
| f/ρ Specific strength f/ρ · derived | 10.22 | 18.39 | kJ/kg | 1.8× |
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.