Mechanical Anisotropy and Fatigue Behavior of 3D-Printed Dentures: A Comparison with CAD/CAM Milled Bases After Thermomechanical Aging
Abstract
1. Introduction
2. Materials and Methods
2.1. Study Design
2.2. Sample Preparation
2.3. Thermomechanical Aging (Pre-Conditioning)
2.4. Flexural Strength Testing (Static Loading)
2.5. Accelerated Fatigue-to-Failure Testing (Cyclic Loading)
2.6. Fractography
2.7. Statistical Analysis
3. Results
3.1. Flexural Strength
3.2. Fatigue Resistance
3.3. Fractography
- •
- SEM features of flexural strength test samples: The fracture surfaces showed characteristic “stair-step” or corrugated appearance as the crack path deviated while cutting across the horizontal layers. Sometimes, crack origin beginning at the surface was seen, followed by a rough region indicating a high-energy, sudden, catastrophic failure. Also, isolated inherent microporosities, voids from the printing process, were spotted (Figure 10A).
- •
- SEM features of fatigue resistance test broken samples: The surfaces displayed distinct fatigue striations (arrest lines) indicating the slow, progressive growth of the crack over time. The crack path traversed the print layers, but with localized micro-cracking where the cyclic load repeatedly stressed the weak bonds between the resin layers before final fast fracture (Figure 10B).
- •
- SEM features of flexural strength test samples: Compared to Group I, the fracture edges appeared less “crisp” and more rounded due to resin plasticization. The layers showed signs of interlayer debonding near the fracture site, as thermocycling weakens the bond between consecutive print layers (Figure 10C).
- •
- SEM features of fatigue resistance test broken samples: The fatigue striations were present but highly irregular and “smeared” due to the softened matrix. Prominent secondary cracks branched off the main fracture line, with increased surface roughness or pitting where unreacted monomers were washed out during aging (Figure 10D).
- •
- SEM features of flexural strength test samples: The fracture surfaces displayed a mixed-mode failure characterized by a staggered, zig-zag pattern (white arrows). The crack propagation path deflected diagonally, transitioning between trans-layer fractures, cutting through the resin, with short segments of interlaminar cleavage traveling along the 45° layer interfaces (yellow arrows) (Figure 11A).
- •
- SEM features of fatigue resistance test broken samples: Under cyclic loading, fatigue striations appeared angled relative to the primary stress axis (black arrows). Localized areas of “structural unzipping” (shear-like sliding) along the 45° layer boundaries were visible prior to the fast fracture zone (yellow arrows) (Figure 11B).
- •
- SEM features of flexural strength test samples: The SEM showed more prominent interlaminar gaps compared to the unaged Group III (white arrows). The fractured edges looked more plasticized (yellow arrows) (Figure 11C).
- •
- SEM features of fatigue resistance test broken samples: The SEM showed pronounced striations of the degraded surface under cyclic loading (white arrows). The mechanical washout of unreacted monomers during aging resulted in more surface micro-cracks (yellow arrows) (Figure 11D).
- •
- SEM features of flexural strength test samples: The hallmark of this subgroup was the adhesive failure (delamination). The SEM showed a relatively smooth, “cleavage-like” fracture surface because the static load simply split or peeled the vertical layers apart along their interfaces. Hackle lines were minimal, indicating a low-energy failure (Figure 12A).
- •
- SEM features of fatigue resistance test broken samples: Pronounced layer separation. Under cyclic loading, the continuous flexing caused the vertical layers to “unzip.” And fatigue striations were strictly confined within the adhesive interface between layers, rather than across the bulk material (Figure 12B).
- •
- SEM features of flexural strength test samples: The SEM showed clear, wide fissures between the vertical layers, demonstrating that the thermocycling completely degraded the interlayer adhesion. The fracture surface will look like a separated deck of cards (Figure 12C).
- •
- SEM features of fatigue resistance test broken samples: The SEM showed multiple points of crack initiation. The matrix also showed signs of swelling, and the separation of layers was profound, with deep, branching secondary cracks traveling vertically down the denture base (Figure 12D).
- •
- SEM features of flexural strength test samples: The SEM revealed homogeneous brittle and semi-brittle polymer fracture, no layer lines and highly dense surfaces with virtually no porosity. The fracture sites featured clear “mirror” zones radiating outward to a “mist” and finally a rough “hackle” zone (Figure 13A).
- •
- SEM features of fatigue resistance test broken samples: The SEM revealed clear, uniform fatigue striations radiating in a fan-like pattern from a single initiation point. The surrounding matrix appeared highly intact and dense, with very few secondary cracks compared to the printed groups (Figure 13B).
- •
- SEM features of flexural strength test samples: The SEM revealed similar morphology to group V, but the “mirror” zones were smaller, indicating that less energy was required to initiate fast fracture due to aging. Slight surface degradation and microscopic shallow pitting were visible due to water sorption (Figure 13C).
- •
- SEM features of fatigue resistance test broken samples: The SEM showed clear fatigue striations but were accompanied by surface micro-cracking and roughening caused by the chewing simulation’s localized stresses. The crack propagation zones showed slightly more texturing and matrix yielding compared to the unaged control (Figure 13D).
4. Discussion
5. Conclusions
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Acknowledgments
Conflicts of Interest
Abbreviations
| CAD/CAM | Computer aided design/computer aided manufacturing |
| SEM | Scanning electron microscope |
| PMMA | polymethyl methacrylate |
| CAD file | Computer-aided design file |
| kN | Kilo newton |
| MPa | Mega pascal |
| N | Newton |
| Hz | Hertz |
| Au | gold |
| kV | Kilo volt |
| ART | Aligned Rank Transform |
| η2p | Partial Eta Squared |
| Tukey’s HSD | Tukey’s Honestly Significant Difference test |
| Mean ± SD | mean ± standard deviation |
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| Group | Fabrication Method/Printing Direction | Aging Condition | Flexural Strength Testing Samples | Fatigue Testing Samples |
|---|---|---|---|---|
| I | 0° (Horizontal) | Non-Aged | 20 | 20 |
| II | 0° (Horizontal) | Aged | 20 | 20 |
| III | 45° (Oblique) | Non-Aged | 20 | 20 |
| IV | 45° (Oblique) | Aged | 20 | 20 |
| V | 90° (Vertical) | Non-Aged | 20 | 20 |
| VI | 90° (Vertical) | Aged | 20 | 20 |
| VII | CADCAM | Non-Aged | 20 | 20 |
| VIII | CADCAM | Aged | 20 | 20 |
| Group | Method/Aging | Mean ± SD (Mpa) | Min | Max |
|---|---|---|---|---|
| Group I (N = 20) | 0° (Horizontal) Non-Aged | 101.14 ± 4.80 | 92.43 | 109.90 |
| Group II (N = 20) | 0° (Horizontal) Aged | 90.40 ± 5.81 | 80.24 | 103.11 |
| Group III (N = 20) | 45° (Oblique) Non-Aged | 93.84 ± 4.93 | 83.42 | 100.34 |
| Group IV (N = 20) | 45° (Oblique) Aged | 80.78 ± 7.78 | 62.66 | 91.95 |
| Group V (N = 20) | 90° (Vertical) Non-Aged | 84.83 ± 4.84 | 74.76 | 95.35 |
| Group VI (N = 20) | 90° (Vertical) Aged | 70.35 ± 8.18 | 54.65 | 89.71 |
| Group VII (N = 20) | CADCAM Non-Aged | 149.43 ± 5.35 | 142.25 | 160.95 |
| Group VIII (N = 20) | CADCAM Aged | 140.28 ± 5.42 | 130.36 | 151.19 |
| Source | F | p | Partial η2p |
|---|---|---|---|
| Orientation | 988.13 | <0.001 * | 0.9512 |
| Conditioning | 155.20 | <0.001 * | 0.5052 |
| Orientation × Conditioning | 1.55 | 0.203 | 0.0298 |
| 45° (Oblique) | 90° (Vertical) | CADCAM Milled | |
|---|---|---|---|
| 0° (Horizontal) | <0.001 * | <0.001 * | <0.001 * |
| 45° (Oblique) | <0.001 * | <0.001 * | |
| 90° (Vertical) | <0.001 * |
| 0° Aged | 45° Non-Aged | 45° Aged | 90° Non-Aged | 90° Aged | CADCAM Non-Aged | CADCAM Aged | |
|---|---|---|---|---|---|---|---|
| 0° Non-Aged | <0.001 * | 0.004 * | <0.001 * | <0.001 * | <0.001 * | <0.001 * | <0.001 * |
| 0° Aged | 0.618 | <0.001 * | 0.075 | <0.001 * | <0.001 * | <0.001 * | |
| 45° Non-Aged | <0.001 * | 0.401 | <0.001 * | <0.001 * | <0.001 * | ||
| 45° Aged | <0.001 * | <0.001 * | <0.001 * | <0.001 * | |||
| 90° Non-Aged | <0.001 * | <0.001 * | <0.001 * | ||||
| 90° Aged | <0.001 * | <0.001 * | |||||
| CADCAM Non-Aged | <0.001 * |
| Group | Method/Aging | Fractured | Runout | Fracture Rate | All (Mean ± SD) | Fractured Only (Mean ± SD) |
|---|---|---|---|---|---|---|
| Group I (N = 20) | 0° (Horizontal) Non-Aged | 4 | 16 | 20% | 97,764 ± 5244 | 88,820 ± 6389 |
| Group II (N = 20) | 0° (Horizontal) Aged | 9 | 11 | 45% | 88,865 ± 13,236 | 75,256 ± 6101 |
| Group III (N = 20) | 45° (Oblique) Non-Aged | 3 | 17 | 15% | 98,748 ± 3100 | 91,653 ± 1565 |
| Group IV (N = 20) | 45° (Oblique) Aged | 8 | 12 | 40% | 91,828 ± 11,607 | 79,571 ± 8917 |
| Group V (N = 20) | 90° (Vertical) Non-Aged | 7 | 13 | 35% | 92,830 ± 10,451 | 79,513 ± 5252 |
| Group VI (N = 20) | 90° (Vertical) Aged | 14 | 6 | 70% | 73,887 ± 18,459 | 62,696 ± 6958 |
| Group VII (N = 20) | CADCAM Non-Aged | 0 | 20 | 0% | 100,000 ± 0 | — |
| Group VIII (N = 20) | CADCAM Aged | 2 | 18 | 10% | 99,158 ± 2767 | 91,580 ± 4228 |
| Source | F | p | Partial η2 |
|---|---|---|---|
| Orientation | 17.07 | <0.001 *** | 0.252 |
| Conditioning | 48.54 | <0.001 *** | 0.242 |
| Orientation × Conditioning | 9.85 | <0.001 *** | 0.163 |
| 45° (Oblique) | 90° (Vertical) | CADCAM | |
|---|---|---|---|
| 0° (Horizontal) | 0.682 | 0.003 * | 0.004 * |
| 45° (Oblique) | <0.001 * | 0.089 | |
| 90° (Vertical) | <0.001 * |
| 0° Aged | 45° Non-Aged | 45° Aged | 90° Non-Aged | 90° Aged | CADCAM Non-Aged | CADCAM Aged | |
|---|---|---|---|---|---|---|---|
| 0° Non-Aged | 0.591 | 1.000 | 1.000 | 1.000 | <0.001 * | 1.000 | 1.000 |
| 0° Aged | 0.222 | 1.000 | 1.000 | 0.092 | 0.012 * | 0.089 | |
| 45° Non-Aged | 1.000 | 1.000 | <0.001 * | 1.000 | 1.000 | ||
| 45° Aged | 1.000 | 0.012 * | 1.000 | 0.526 | |||
| 90° Non-Aged | 0.003 * | 1.000 | 1.000 | ||||
| 90° Aged | <0.001 * | <0.001 * | |||||
| CADCAM Non-Aged | 1.000 |
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Alkhodary, M.A.; Elmoazen, R.; Alresheedi, B.A.; Alenezi, A.; Alharethi, N.; Alrethia, R. Mechanical Anisotropy and Fatigue Behavior of 3D-Printed Dentures: A Comparison with CAD/CAM Milled Bases After Thermomechanical Aging. J. Funct. Biomater. 2026, 17, 297. https://doi.org/10.3390/jfb17060297
Alkhodary MA, Elmoazen R, Alresheedi BA, Alenezi A, Alharethi N, Alrethia R. Mechanical Anisotropy and Fatigue Behavior of 3D-Printed Dentures: A Comparison with CAD/CAM Milled Bases After Thermomechanical Aging. Journal of Functional Biomaterials. 2026; 17(6):297. https://doi.org/10.3390/jfb17060297
Chicago/Turabian StyleAlkhodary, Mohamed Ahmed, Ramy Elmoazen, Bandar Awadh Alresheedi, Ali Alenezi, Naji Alharethi, and Rawan Alrethia. 2026. "Mechanical Anisotropy and Fatigue Behavior of 3D-Printed Dentures: A Comparison with CAD/CAM Milled Bases After Thermomechanical Aging" Journal of Functional Biomaterials 17, no. 6: 297. https://doi.org/10.3390/jfb17060297
APA StyleAlkhodary, M. A., Elmoazen, R., Alresheedi, B. A., Alenezi, A., Alharethi, N., & Alrethia, R. (2026). Mechanical Anisotropy and Fatigue Behavior of 3D-Printed Dentures: A Comparison with CAD/CAM Milled Bases After Thermomechanical Aging. Journal of Functional Biomaterials, 17(6), 297. https://doi.org/10.3390/jfb17060297

