C50/60 vs C60/75
C60/75 and C50/60 are about equally stiff. Their densities are about the same. Per unit mass they are about equally stiff (15.12 and 15.94 MJ/kg). Strength: f_ck = 50 MPa for C50/60, f_ck = 60 MPa for C60/75.
Side by side
ratio = C60/75 / C50/60 · log scale| Property | C50/60 | C60/75 | Unit | Ratio | ¼×1×4× |
|---|---|---|---|---|---|
| E Young's modulus | 37 | 39 | GPa | 1.05× | |
| G Shear modulus | 15.42 | 16.25 | GPa | 1.05× | |
| 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 | 50 | 60 | MPa | 1.2× | |
| f_ck,cube Characteristic cube strength | 60 | 75 | MPa | 1.25× | |
| f_cm Mean cylinder strength | 58 | 68 | MPa | 1.17× | |
| f_ctm Mean tensile strength | 4.1 | 4.4 | MPa | 1.07× | |
| f_ctk,0.05 Tensile strength, 5 % fractile | 2.9 | 3.1 | MPa | 1.07× | |
| f_ctk,0.95 Tensile strength, 95 % fractile | 5.3 | 5.7 | MPa | 1.08× | |
| ε_c1 Strain at peak stress | 2.45 | 2.6 | ‰ | 1.06× | |
| ε_cu1 Ultimate strain | 3.5 | 3 | ‰ | 0.857× | |
| ε_c2 Strain at peak, parabola–rectangle | 2 | 2.3 | ‰ | 1.15× | |
| ε_cu2 Ultimate strain, parabola–rectangle | 3.5 | 2.9 | ‰ | 0.829× | |
| n Exponent, parabola–rectangle | 2 | 1.6 | – | 0.8× | |
| ε_c3 Strain at peak, bilinear | 1.75 | 1.9 | ‰ | 1.09× | |
| ε_cu3 Ultimate strain, bilinear | 3.5 | 2.9 | ‰ | 0.829× | |
| E/ρ Specific stiffness E/ρ · derived | 15.12 | 15.94 | MJ/kg | 1.05× | |
| c₀ Bar wave speed √(E/ρ) · derived | 3888 | 3992 | m/s | 1.03× | |
| f/ρ Specific strength f/ρ · derived | 20.43 | 24.52 | kJ/kg | 1.2× |
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.