| Literature DB >> 35012080 |
Tobias Graf1, Josef Schweiger2, Jan-Frederik Güth1, Thomas Sciuk3, Oliver Schubert2, Kurt-Jürgen Erdelt2.
Abstract
Data on the long-term behavior of computer-aided designed/computer-aided manufactured (CAD-CAM) resin-based composites are sparse. To achieve higher predictability on the mechanical behavior of these materials, the aim of the study was to establish a mathematical relationship between the material thickness of resin-based materials and their fracture load. The tested materials were Lava Ultimate (LU), Cerasmart (GC), Enamic (EN), and Telio CAD (TC). For this purpose, 60 specimens were prepared, each with five different material thicknesses between 0.4 mm and 1.6 mm (N = 60, n = 12). The fracture load of all specimens was determined using the biaxial flexural strength test (DIN EN ISO 6872). Regression curves were fitted to the results and their coefficient of determination (R2) was computed. Cubic regression curves showed the best R2 approximation (LU R2 = 0.947, GC R2 = 0.971, VE R2 = 0.981, TC R2 = 0.971) to the fracture load values. These findings imply that the fracture load of all tested resin-based materials has a cubic relationship to material thickness. By means of a cubic equation and material-specific fracture load coefficients, the fracture load can be calculated when material thickness is given. The approach enables a better predictability for resin-based restorations for the individual patient. Hence, the methodology might be reasonably applied to other restorative materials.Entities:
Keywords: CAD-CAM; PMMA; digital workflow; fracture strength; fracture strength equation; hybrid materials; mathematical analysis; polymer infiltrated ceramic network; resin nano ceramics
Year: 2021 PMID: 35012080 PMCID: PMC8747289 DOI: 10.3390/polym14010058
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.329
Figure 1Experimental setup.
Descriptive statistics of fracture load values including mean values, standard deviations (SD), and statistical significance (Scheffe’s post-hoc test). Same letters indicate no statistically significant differences concerning fracture load values (a, b).
| Material Thickness | Flexural Strength | |||||
|---|---|---|---|---|---|---|
| 0.4 mm | 0.7 mm | 1.0 mm | 1.3 mm | 1.6 mm | ||
| material | mean ± SD (N) | mean ± SD (N) | mean ± SD (N) | mean ± SD (N) | mean ± SD (N) | mean ± SD (MPa) |
| Lava | 21.3 ± 3.1 | 58.9 ± 9.3 | 132.1 ± 12.8 | 218.2 ± 35.0 | 289.8 ± 35.0 | 223.3 ± 20.0 |
| GC Smart (GC) | 27.7 ± 47.0 | 74.6 ± 10.2 | 162.1 ± 18.5 | 254.3 ± 35.1 | 408.2 ± 44.9 | 276.3 ± 41.0 |
| Vita Enamic (VE) | 13.3 ± 1.0 | 32,6 ± 7.9 | 88.8 ± 7.3 | 153.4 ± 14.7 | 230.0 ± 20.5 | 132.4 ± 10.2 |
| Telio CAD (TC) | 32.3 ± 16.9 | 69.2 ± 16.0 | 122.5 ± 19.1 | 204.0 ± 29.5 | 315.5 ± 22.5 | 187.8 ± 27.6 |
Figure 2Plotted regression curves (linear, quadratic, and cubic) for Lava Ultimate (LU) with specimens of five thicknesses.
Figure 3Plotted regression curves (linear, quadratic, and cubic) for Cerasmart (GC) with specimens of five thicknesses.
Figure 4Plotted regression curves (linear, quadratic, and cubic) for Enamic (EN) with specimens of five thicknesses.
Figure 5Plotted regression curves (linear, quadratic, and cubic) for Telio CAD (TC) with specimens of five thicknesses.
R2 values of the linear, quadratic, and cubic curves for all tested materials (* fracture load values that fit the curves best).
| Material | Linear | Quadratic | Cubic |
|---|---|---|---|
| Lava Ultimate (LU) | 0.886 | 0.944 | 0.947 * |
| GC Smart (GC) | 0.886 | 0.971 * | 0.971 * |
| Enamic (VE) | 0.888 | 0.981 * | 0.981 * |
| Telio CAD (TC) | 0.896 | 0.969 | 0.971 * |
Figure 6Cubic regression curves for all tested materials.
Material-specific “Fracture Load Coefficients” ‘b0’, ‘b1’, ‘b2’, and ‘b3’ with mean values and standard deviations.
| Material | Cubic “Fracture Load Coefficients” | |||
|---|---|---|---|---|
| b0 | b1 | b2 | b3 | |
| Lava Ultimate (LU) | 1.1 ± 0.5 | −45.1 ± 44.6 | 230.0 ± 70.0 | −53.1 ± 28.8 |
| GC Smart (GC) | −0.57 ± 7.2 | 31.0 ± 42.5 | 95.8 ± 66.7 | 27.3 ± 27.5 |
| Enamic (VE) | 1.0 ± 3.5 | −30.7 ± 20.1 | 129.7 ± 31.3 | −13.0 ± 12.9 |
| Telio CAD (TC) | 0.0 ± 5.5 | 69.9 ± 51.3 | 9.8 ± 21.2 | 43.7 ± 5.5 |
Calculated fracture load values (in N) for Cerasmart (GC), Lava Ultimate (LU), Enamic (VE), and Telio CAD (TC) using the “Fracture Load Equation” for given thicknesses.
| Material-Dependent Calculated Fracture Loads | Material Thickness (in mm) | |||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 0.3 | 0.4 | 0.5 | 0.6 | 0.7 | 0.8 | 0.9 | 1.0 | 1.1 | 1.2 | 1.3 | 1.4 | 1.5 | 1.6 | 1.7 | 1.8 | 1.9 | 2.0 | |
| Lava | 6.9 | 16.5 | 29.4 | 45.4 | 64.1 | 85.1 | 108.1 | 132.9 | 159.2 | 186.5 | 214.5 | 243.1 | 271.8 | 300.3 | 328.2 | 355.4 | 381.5 | 406.1 |
| GC Smart (GC) (in N) | 18.1 | 28.9 | 42.3 | 58.4 | 77.4 | 99.5 | 124.8 | 153.5 | 185.8 | 221.8 | 261.6 | 305.5 | 353.6 | 406.1 | 463.2 | 524.9 | 591.5 | 663.1 |
| Enamic (VE) (in N) | 3.2 | 8.7 | 16.5 | 26.5 | 38.7 | 52.9 | 69.0 | 87.1 | 107.0 | 128.6 | 151.8 | 176.7 | 203.0 | 230.8 | 259.9 | 290.3 | 321.9 | 354.6 |
| Telio CAD (TC) (in N) | 23.0 | 32.3 | 42.9 | 54.9 | 68.7 | 84.5 | 102.7 | 123.4 | 146.8 | 173.4 | 203.3 | 236.8 | 274.2 | 315.7 | 361.6 | 412.1 | 467.6 | 528.2 |