Shear bond strength of zirconia to resin: The effects of specimen preparation and loading procedure

The bonding of zirconia has been the subject of increasing attention over the last decade for the definitive approach, but optimal resin bonding to zirconia has yet to be realized. In order to evaluate new bonding strategy developments, bond strength tests are needed.1 Available bond strength tests include the macro/micro tensile bond strength test, macro/micro shear bond strength (SBS) test, push-out test, and four point bending test,2, 3, 4 of which SBS test is the most commonly used one for the evaluation of resin bond strength of zirconia. However, SBS results vary among many studies even when evaluating the same bonding strategy. Shortcomings of the SBS test have been recognized, and it is difficult to draw reliable conclusions from comparing the results of different SBS experiments. A large number of the same or similar experiments have to be performed in order to accurately evaluate newly developed bonding strategy, which leads to wasteful repetition.

To clarify the key factors that affect the SBS results, the structure of the bonding specimens used for SBS test should be known first. The most commonly used SBS test specimens for the evaluation of bonding between zirconia and composite resin exhibit a sandwich-type structure, with a pretreated zirconia end that is cemented under constant load on the other end (usually be composite resin, or ceramic glass, or the same pretreated zirconia) by a layer of resin cement.5 This kind of structure resembles the cantilever beam when an end of the bonding specimen is loaded with a shear force during the SBS test process. Based on the theory of cantilever beam bending moment,6 the bending moment of the cantilever beam is positively correlated with the load and the length of the cantilever beam, when it is under a vertical uniform load. If the load distribution is not uniform, the bending moment of unloaded unit is 0. During the loading process, with the increase of internal bending moment of the cantilever beam, the structure will fracture when its mechanical strength is not strong enough to resist the bending moment.7 This principle is expected to be helpful for explaining the main reason for the variation of shear bond test results.

In the structure of SBS bonding specimen, the thickness of the resin cement layer and the load bearing end can be considered as the length of the cantilever beam. It has been reported previously that an increase in resin cement thickness led to decreased flexural strength between the glass-based ceramics and resin.8 Another study found that a resin cement layer thickness of 50 – 150 µm did not affect the SBS of dentine, while 200 µm cement layer thickness led to decreased SBS.9 Therefore, the resin cement layer thickness would affect SBS values. In addition, a previous study adopted three stress models to evaluate failure behavior of shear bond strength specimens when bonded to dentin, and found that failures of specimens originated from loaded cylinder surface and were unrelated to the bonded surface area.6 Both the conclusions of these in vitro studies matched the cantilever theory.

As the most commonly used material to build the load bearing end of a SBS bonding specimen,7, 10 the composite resin has been recommend by ISO that should have a flexural modulus greater than 9 GPa to reduce its deformation during the SBS test.11, 12, 13 However, unfortunately, there is not much detail. According to Hooke's law, stress is equal to the product of elastic modulus and shape variable; therefore, for same deformation, the higher the elastic modulus, the greater the stress is.14 Chiba et al.15 demonstrated through 3D FE analysis that the shear stress on the cervical surface of resin core decreased as the elastic modulus of resin composites increased.

The resin core materials with higher elastic moduli could restrain the elastic deformation and hold larger stress internally. Another study found that von Mises stresses for composites with lower elastic moduli spread over a large area, and high elastic modulus composite material accumulated stresses at the bonded interface.16 These above studies suggested that composite resin of different elastic moduli may be another key factor that affects the SBS values.

In this study, zirconia/resin cement/composite resin structure bonding specimens were built with three-dimensional finite element (3D FE) molds, and SBS test simulation was performed for stress distribution analysis. In vitro SBS test was also performed to validate the results of 3D FE analysis. We inferred based on cantilevered beam theory that the load flat width, the resin cement thickness, and different composite resins mechanical properties would affect the SBS results.

Finite element modeling was carried out and analyzed using Abaqus software (Dassault Systemes S.A, boulevard de Verdun, Courbevoie, France). The mechanical parameters used in the bond strength test models followed the manufacturers' recommendation (Table 1). The model was composed of 22857-33477 hexahedral elements that represented the isotropic materials for the model. All the materials were assumed to be homogeneous and isotropic. In order to simulate the SBS test, the boundary nodes of the zirconia cuboid were fixed with no movement in any direction. Forces were loaded at the top of the cylinder using a rectangular rigid rod of 2 mm × 3 mm to mimic the practical situations. The von Mises stress (VMS) distribution was analyzed in each specimen and the von Mises strain distribution of the cement layer, and calculated the peak values of the principal shear stress in the different portions of the cement layer.

Table 1
Mechanical properties and dimensions of the components of SBS specimens models

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To evaluate the different stress distribution under uniform and non-uniform load, the resin-composite Filtek Z250 was chosen as the resin-composite cylinder and its thickness was set to typical 1 mm,15 2 mm,17 3 mm,18 and 4 mm19 according to the previous literature. The load flat width was set to 1 mm, 2 mm, 3 mm, 4 mm and 5 mm in order to simulate the SBS test under uniform or non-uniform load. The thickness of the cement layer was set to typical 50 µm.20 Stress forced was 50 N.21

To evaluate the different stress distribution with different resin cement thickness, the models were designed as 3 mm width of load flat and 3 mm thickness of Filtek Z250 resin-composite cylinder according to the dimensions of the specimens used in the SBS tests. The thickness of the cement layer were set to typical 50 µm,20 80 µm,22 100 µm23, 24 and 180 µm24 reported in the previous literatures. Stresses forced were 50 N and 300 N.21

To evaluate the different stress distribution with different elastic modulus of resin composite, the models were designed as 3 mm width of load flat and 3 mm thickness of three kinds of resin-composite cylinder, including Filtek Z100, Filtek Z250, and Filtek Z350, according to the dimensions of the specimens used in the SBS tests. The thickness of the cement layer was set to 50 µm.20 Stresses forced were 50 N and 300 N.21

Shear bond strength (SBS) test was then performed to verify the results of 3D FE simulation. Industrially manufactured Y-TZP (yttrium-stabilized tetragonal zirconia) plates (94% ZrO₂, 6% Y₂O₃, Shenzhen Santo Industry Technology Development Company Limited, ShenZhen, China), with dimensions of 10 × 10 × 0.9 mm³, were subjected to air particle abrasion with 50 µm alumina particles from a distance of 10 mm for 20 s at 0.25 MPa. The 375 Y-TZP plates were randomly assigned to five groups (n = 75 per group) according to the conditioning methods applied (Table 2). A total of 375 prepolymerized resin composite cylinders (6 mm inner diameter; 3 mm height) were made from a light-cured composite resin (Filtek Z250, 3M ESPE, St. Paul, MN, USA). The above 375 pretreated Y-TZP plates was then further divided into five subgroups (n = 15) according to the load applied (0.49, 1.96, 4.90, 9.80, or 19.60 N) during cementation of zirconia to the resin cement. Prepolymerized resin composite cylinders were cemented on pretreated Y-TZP plates by a layer of conventional MDP-free resin cement (RelyX Veneer, 3M ESPE, St. Paul, MN, USA) or MDP-containing resin cement (Clearfil SA Luting, Panavia SA Luting Plus) under a corresponding constant load for 5 minutes.

Table 2
Conditioning methods for groups under five different cementation loads in shear bond strength test

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Another 180 air-abraded Y-TZP plates were prepared and assigned to three groups (n = 60 per group) according to three kinds of resin composites used. The resin composites chosen were Filtek Z100, Filtek Z250 and Filtek Z350, produced by the same manufacturer, to avoid the interference of mechanical properties except Young's modulus. The 180 pretreated Y-TZP plates were then further divided into three subgroups (n = 20) according to the primers applied, Z-Prime Plus and Clearfil Ceramic Primer, and group without any further treatment (Ctr) as control. The conditioning methods applied were same as described in Table 2. The load applied was 9.80 N when preparing SBS specimens.

After removal of excess resin cement with a probe, the resin composite cylinders were light-cured at 6 different locations for 40 s each using a LED lamp (1000 mW/cm², Elipar FreeLight 2, 3M ESPE, St. Paul, MN, USA). All the specimens were submitted to SBS test after 24 h water storage at 37℃ by a universal testing machine (Instron Model 3365, Electropuls, Norwood, MA, USA). During the SBS test, a load was applied with a crosshead speed of 1 mm/min perpendicularly to the adhesive interface using a metal flat rod until failure. The maximum load was recorded and the SBS values were calculated according to the following formula: SBS (MPa) = the maximum load (N) / area (mm²).

After testing, all debonded specimens were examined under a stereomicroscope (C-DSS230, Nikon, Tokyo, Japan). Fracture modes were classified as: adhesive failures, fracture sites entirely located between the resin/cement and zirconia surface; cohesive failures, fractures occurring exclusively within the resin/cement; or mixed failures, partial resin/resin cement fractures and partial Y-TZP surface exposure.

Another batch of air-abraded Y-TZP plates were prepared (size error less than 0.02 mm) and assigned to three groups (n = 25 per group), similar to SBS test, to receive surface treatments. These pretreated Y-TZP plates was then divided into five subgroups (n = 5) to build bi-layered specimens according to the load applied during cementation.

Bi-layered specimens in each group were built through bonding two identically pretreated Y-TZP plates to each other with a layer of resin cement (RelyX Veneer, Clearfil SA Luting, Panavia SA Luting Plus) under constant loads of 0.49, 1.96, 4.90, 9.80, or 19.60 N. After light-curing for 80 s from two sides, four lateral sides of the bi-layered specimens were wet-polished with silicon carbide papers of increasing fineness (800, 1000, 1200 grit) using a metallographic polisher (PG-1, BiaoYu instrument, ShangHai, China). Thickness of the cement layer was then measured at 40× magnification under a stereomicroscope (C-DSS230, Nikon, Tokyo, Japan).

After satisfying the normality and homogeneity of the data sets, two-way ANOVA and post hoc tests (Tukey HSD test) were performed to statistically examine the influences of the bonding strategies and loads on SBS values, and examine the influences of resin cement types and loads on the thickness of resin cement. Statistical significance was set at α = 0.05. The relationships between thickness and different loading conditions, and between SBS values and different load conditions were assessed by Pearson correlation analysis.

3D FE analysis of ceramic-composite combinations showing stress accumulation areas is presented in Fig. 1. When the thickness of resin-composite cylinder was set to be 1 or 2 mm, the load flat width that range from 1 mm to 5 mm had no effect on the peak value of maximum principal stress and the area of stress distribution. When the composite resin thickness was up to 3 and 4 mm, the area of stress distribution increased along with the increasing of the load flat width. When the load flat width was not beyond the cylinder thickness, the maximum principal stress appeared at the top of the interface between the cylinder and the cement layer, and along with the increase of the load flat width, the peak value of the maximum principal stress and the distribution area decreased. When the load flat width was beyond the cylinder thickness, the location of the maximum principal stress changed to the top of the cylinder free-end, and with the increase of the load flat width, the peak value of the maximum principal stress and the distribution area increased. When the cylinder thickness was 3 mm, the value of the maximum principal stress was the minimum when load flat width was 4 mm; when the cylinder thickness was 4 mm, the value of the maximum principal stress was the minimum when load flat width was 5 mm.

Fig. 1
Sectional views of von Mises stress of the finite element model simulating the shear bond test. Thickness of the resin composite was 1 mm (A), 2 mm (B), 3 mm (C – G) and 4 mm (D – H). The load flat applied on the cylinder was 1 mm (C, H), 2 mm (D, I), 3 mm (E, J), 4 mm (F, K) and 5 mm (G, H). The sectional views were derived from the entire view. When cylinder thickness was 1 mm or 2 mm, different loading area resulted in same maximum principal stress.

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The load flat width and the resin-composite cylinder thickness of 3D FE models were designed to be 3 mm. The thickness of resin cement, the elastic modulus, and Poisson's ratio of resin-composite cylinder were changed respectively for simulation and analysis. For these models (Fig. 2 and Fig. 3), the 3D FE simulation indicated that the maximum principal stress was located at the interface between the resin composite and the resin cement, which decreased quickly in the resin cement and slowly in the resin composite. The principal stress was larger and more widely distributed in the resin composite cylinder than in the cement layer and Y-TZP plate. Independent and enlarged sectional views of von Mises stress (VMS) of the finite element model were shown in supplementary information. The distribution areas under 50 N and 300 N load conditions were similar, while the maximum principal stress values were different.

Fig. 2
Sectional views of von Mises stress of the finite element model simulating the shear bond test. Thickness of the resin cement was 50 µm (A, E), 80 µm (B, F), 100 µm (C, G) and 180 µm (D, H). The force applied on the cylinder was 50 N (A, B, C, D) and 300 N (E, F, G, H). The sectional views were derived from the entire view. Among the modeled thicknesses, the peak value of maximum principal stress was found in the 50 µm thick cement simulation, followed by 80, 100, and 180 µm, which occurred at the top of the resin cement/resin composite interface in all cases. The stress distribution areas for either the 50 or 300 N loads were similar, with the exception of the principal stress values.

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Fig. 3
Sectional views of von Mises stress of the finite element model simulating the shear bond test. The resin composite was Filtek Z100 (A, D), Filtek Z250 (B, E) and Filtek Z350 (C, F). The force applied on the cylinder was 50 N (A, B, C) and 300 N (D, E, F). The sectional views were derived from the entire view. Among the modeled resin composites, the peak value of maximum principal stress was found in the Filtek Z250 simulation, followed by Filtek Z350 and Filtek Z100, which occurred at the top of the resin cement/resin composite interface in all cases. The stress distribution areas for either the 50 or 300 N loads were similar, with the exception of the principal stress values.

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When the thickness of the cement layer was set to be 50 µm, 80 µm, 100 µm and 180 µm, as shown in Fig. 2, the peak value of the principal stress decreased as the thickness of the cement layer increased, and occurred at the top of the interface between resin cement and resin composite in each thickness. For models consisting of different resin composites, as shown in Fig. 3, the peak value of the principal stress decreased as the elastic modulus of the cylinder increased, and the maximum appears in Filtek Z250, followed by Filtek Z350 and Filtek Z100.

For specimens prepared under five different loads, the SBS values were significantly affected by the bonding strategy (F = 21.78, P < .05) and loads (F = 141.78, P < .05) during preparing the SBS bonding specimens, but there were no significant interactions between these two factors (F = 1.13, P > .05). Means and standard deviations of the SBS values of all the groups were shown in Fig. 4A. Regardless of the bonding strategies used, the SBS values of the 0.49 N groups were the lowest, and those of 19.60 N groups were the highest (P < .05). Moreover, 1.96, 4.90, and 9.80 N groups showed product dependent significance. In the ZP and CCP groups, the differences in the SBS values after preparation in 4.90 N and 9.80 N conditions were insignificant, and were less than those prepared in 9.80 N conditions (P < .05). In the Ctr, CSL, and PSLP groups, no significant differences were found among specimens prepared under 1.96, 4.90, or 9.80 N conditions.

Fig. 4
(A) Means and standard deviations of the SBS values of all the groups in result 2.1. Different superscript letters represent group means that were significantly different (P < .05). Regardless of the loads factor, the SBS values of the control group were the lowest. (B) Failure modes observed in groups of SBS test in result 2.1. Adhesive, failure at the ceramic surface; mixed, combination of adhesive failure at ceramic surface and cohesive failure in luting resin or composite cylinder.

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The failure mode results of all the groups were shown in Fig. 4B. For the Ctr group, 0.49, 1.96, and 4.90 N loads all resulted in adhesive failures, and 9.80 and 19.60 N loads mainly resulted in adhesive failures and a small number of mixed failure modes. For the 9.80 N groups, adhesive failures accounted for 94.33% of the total, with only one mixed failure, which accounted for 6.67% of the total failures. In the 19.60 N groups, adhesive failures accounted for 80% and mixed failures accounted for 20% of the total. The other groups except Ctr presented mixed failure modes or mainly mixed failure modes, with small amounts of adhesive damage under 0.49, 1.96, 4.90 N load conditions (P > .05).

Two-way ANOVA showed that loads applied for cementing during preparing the SBS bonding specimens affected the resin cement thickness (F = 106.78, P < .05), while resin cement types did not (F = 2.14, P = .126), and there was interaction between the two factors (F = 2.29, P = .032) (Table 3). Regardless of the type of resin cement used, the thickness of the resin cement layer was maximum under 0.49 N load and minimum under 19.60 N load (P < .05). There was no significant difference in resin cement thickness under 1.96 and 4.90 N loading conditions (P > .05). Under 4.90 and 9.80 N load, a significant difference in thickness between Panavia SA Luting Plus and Relyx Veneer resin cements was observed (P < .05).

Table 3
Mean (standard deviation) of thickness of three kinds of resin cement in bi-layered Y-TZP bonded specimens

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Correlation analysis results revealed that there was a strong correlation between load and resin cement layer thickness and between load and SBS values (Fig. 5). With increases in load, SBS values gradually increased and the resin cement layer thickness decreased.

Fig. 5
(A) Correlation results between thickness and different load conditions, (B) Correlation results between SBS values and different load conditions.

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For specimens made of three different resin composites, two-way ANOVA and Post-Hoc test of the SBS data revealed that SBS values were significantly affected by the bonding strategies and different composite resins used (P < .01) for preparing SBS bonding specimens, while there were no significant interactions between bonding strategies and different composite resins (P = 0.892). Means and standard deviations of the SBS values were shown in Fig. 6A.

Fig. 6
(A) Means and standard deviations of the SBS values of the groups in result 3.1. Different superscript letters represent group means that were significantly different (P < .05). Regardless of the composite resins factor, the SBS values of the control group were the lowest. (B) Failure modes observed in groups of SBS test in result 3.2.

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Regardless of the composite resin factor, the SBS values of the control group were lower than that of the primers applied groups. Regardless of the bonding strategies, the SBS values of the Z100 group were the lowest. Z350 group showed slightly higher SBS date than Z250 in group ZP, but Z350 group showed slightly lower SBS date than Z250 when applied with CCP. No statistical difference in SBS was found between group ZP and CCP (P = .596) nor between group Z250 and Z350 (P = .961).

According to results of failure mode analysis, for the control groups, Z100 and Z350 group presented pure adhesive failures, and Z250 group presented mainly adhesive failures and a small number mixed failure modes. For group ZP and CCP, Z100 group presented pure mixed failures. For Z250 group, adhesive failures accounted for 10% in group ZP. 5% adhesive failures were found in group CCP. In group ZP of Z350, adhesive failures also accounted for 5%. No cohesive failure was found in all the groups. The fracture mode details were presented in Fig. 6B.

There was no available standard to specify the loading area, shape, and size of the load bearing end for SBS test in evaluating bond strength of zirconia. The widely used shape of load bearing end in SBS test is cylinder, and the thickness is usually within 1 – 4 mm.15, 17, 18, 19 3D FE models were established of 1 – 4 mm thickness cylinder with 1 mm interval in the present study to analyze the influence of uniform load and non-uniform load on the test results under 1 – 5 mm loading area. According to the 3D FE simulation, for 3 mm and 4 mm thickness cylinders, when the loading area was less than the cylinder thickness, the load applied was non-uniform, the stress appeared mainly at the loading area, and the maximum principal stress was concentrated at the interface between composite and resin cement, as well as the interface between zirconia and resin cement. The cantilever theory explains it well; when the load is not uniform, the bending moment of the unloaded unit is 0, the bending moment of the segment under load is 1/2qb². During the loading process, the cylinder will fracture when its mechanical strength cannot resist the increasing internal bending moment. This premature failure cannot reflect true bonding effect, which would lead to a larger variation for SBS values. When the load flat width is no less than the cylinder thickness, the loading force is uniform theoretically, and the bending moment of the cantilever beam can be calculated by the formula of 1/2ql², where q is the load and l is the length of the cantilever beam. However, the load beyond bearing area was on the free ends of cylinder, making the location of the maximum principal stress changed from the top of the interface between the cylinder and the cement layer to the top of the cylinder free-end. It increased the area of stress distribution, which makes the true SBS values unable to be measured because of the cohesive fracture within the resin composite. Stress distribution can be uniform only when the load area is equal to the cylinder thickness, in which case the maximum principal stress occurs at the bonding interface and more accurate results can be obtained. When the composite resin thickness is 1 or 2 mm, uniform load and non-uniform load show the same stress results, which may be related to the cylinder thickness; the thickness may not be enough to fully reflect the stress distribution results. However, this does not prevent us to draw a conclusion based on the above results that it is necessary to select an appropriate resin cylinder thickness and corresponding loading area in order to obtain more accurate data in SBS test.

Based on the cantilever beam structure shown in Fig. 7, loading area and cylinder thickness are not the only affecting factor. The cantilever beam of a SBS bonding specimen consisted of the resin cement layer and the loading bear material. It has been reported previously that an increase in resin cement thickness led to decreased flexural strength between the glass-based ceramics and resin.8 Another study found that a resin cement layer thickness of between 50 – 150 µm did not affect the SBS of dentine, while 200 µm cement layer thickness led to a decline in SBS.9 In order to pursue consistency and standardization of resin cement thickness and to provide a criterion for the loads applied for preparing SBS bonding specimen, we prepared SBS bonding specimens under different pressure that led to the different resin cement thickness. Moreover, in order to make our study close to clinical situation as much as possible, the well-accepted bonding strategy for luting zirconia-based ceramic restorations in clinic, alumina air abrasion followed by conditioning with MDP-containing products, was adopted in the in vitro SBS test.25

Fig. 7
Schematic diagram of a zirconia/resin cement/composite resin structure shear bond strength bonding specimen in a cantilever beam structure. When the load flat width is not less than the length of l, the loading force is uniform, and the bending moment (M) of the cantilever beam is 1/2ql², where q is the load and l is the length of the cantilever beam; when the loading force is not uniform, the load flat width is less than the length of l, the bending moment of the a segment (without load) is 0, and the bending moment of the b segment (the length under load) is 1/2qb².

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The load applied for cementing the zirconia end varies from 4 N,26 6 N,27 7.35 N,28, 29 9.8 N,30, 31, 32 to 20 N18 in previous studies. The present study revealed a negative correlation between loading conditions and the resin cement layer thickness, and it can be deducted that the cement thickness ranged within 60 – 20 µm accompanied by the load between 5 – 20 N. The thickness of the cement layer reported in previous literature were 50 µm,20 80 µm,22 100 µm,23, 24 and 180 µm24 values. Basing on 3D FE analysis, the models were designed according to the dimensions of the specimens used in the SBS tests. The 3D FE analysis results show that it is easier for thinner resin cement layer to concentrate the internal stress, since the principal stress increases as the thickness of the cement layer decreases. This result is consistent with a previous report,16 which indicates that a thinner resin cement layer would reach the threshold of “load to failure” faster than a thicker one. This result can also explain why the mixed failure modes began to appear in the 9.8 N load group but failed to be detected in the 1.96 and 4.90 N load groups. Although the SBS values presented no statistical difference among these three groups, the proportion of the mixed failure mode increased when the load reached 19.60 N.

The thickness of the resin cement layer was maximum under the load of 0.49 N, while the 19.6 N load resulted in the highest dispersion, which in turn resulted in the thinnest resin cement layer. Obviously, the thinner the cement thickness is, the better the marginal fitness for restoration.22 However, it should be noted that constant load applied on restorations by fingers cannot reach 20 N when bonded to the abutments in clinic because it will make fingers pain. Such a higher load should be achieved by bite force.33, 34 Another result was found in the 3D FE analysis of models with different cement thickness. The distribution areas resulted from 50 N and 300 N showed similar values of the maximum principal and the maximum principal stress was located at the interface between the resin composite and the resin cement, which decreased quickly in the resin cement and slowly in the resin composite. The principal stress was larger and more widely distributed in the resin composite cylinder than in the cement layer. This result suggested that we should focus on whether composite resin itself affects stress distribution since it is the indispensable part of bonding specimen.

A previous study found that von Mises stresses for composites with lower elastic moduli spread over a large area, while composite materials with high elastic moduli accumulated stresses at the bonded interface.15 The present study gave a similar result that for the three kinds of composites, the values of the maximum principal increased as composite elastic modulus decreased under 50 N or 300 N load. Chiba et al.15 showed through 3D FE analysis that the cervical surface shear stress of the resin core decreased as its elastic modulus increased.

There were also several studies adopting glass-based ceramic or zirconia as the load bearing end to build the sandwich structured SBS bonding specimen for evaluating the bond strength of zirconia.35 Obviously, the elastic modulus of either glass-based ceramic or zirconia is much higher than that of composite resins. Based on the present results, it can be inferred that the SBS values of bonding specimens containing glass-based ceramic or zirconia as the load bearing end would be lower. The present SBS results are in correspondence with the 3D FE analysis. The lowest bond strength was found in the group with the highest elastic modulus resin composite Filtek Z100. Although bond strength showed no significant difference between group of Filtek Z350 and Filtek Z250, this may be due not enough precision of SBS test to detect the small difference in these two elastic modulus values.

The present 3D FE analysis also suggested that the maximum principal stress occurs at the bonding interface. This result can explain the residual resin or cement composition in the mixed failure bonded specimens. The control group without the use of primer presented mainly adhesive failures while groups conditioned with primers showed mainly mixed failure modes. This result was due to MDP contained in the primers, which chemically bond with zirconia, improve the bond strength and change the failure modes. However, the chemical bond formation between MDP and zirconia cannot be reflected in the models of finite element simulation. Nevertheless, only a small number of adhesive failures appeared in the specimens conditioned with primers in Filtek Z250 and Filtek Z350 groups, which can be explained by 3D FE analysis that showed the quick decrease of the maximum principal stress in the resin cement and the slow decrease in the resin composite. Most bending moment concentrated on composites resulted in mixed failures. The stress existed at the resin cement layer that made the resin cement layer separated, which was more typical in the control group without chemical bonding, showing an adhesive failure mode.

Although SBS test is the most commonly used method for evaluation of resin bond strength of zirconia, it is still a challenge to ensure its objectivity and repeatability because of its absence of standardization. In the present study, SBS bonding specimen with a structure of zirconia/resin cement/composite resin was considered as a cantilever beam, which revealed that the load flat width, the resin cement thickness, and different composite resins mechanical properties influenced the SBS values. During SBS test, the thickness of the composite resin should be consistent with the width load flat to obtain the appropriate stress distribution. When thickness of resin-composite cylinder was 1 mm or 2 mm, the change of the loading flat width ranging from 1 mm to 5 mm had no effect on the stress distribution. When the composite resin thickness was 3 mm and 4 mm, an equal load flat width was recommended. When preparing SBS specimens, a higher load is recommended during cementation of resin composite cylinder to zirconia to obtain a thicker resin cement layer, and 20 N load would be preferred. Besides, choosing resin composite with lower elastic modulus would create higher SBS value than the one with higher elastic modulus.