Received 7 December 2015; accepted 26 January 2016; published 29 January 2016
Research on improving the ballistic performance of ceramics (including multi-hit capability) is a dynamic subject, as is made necessary by the ever-increasing threat level of bullets. So far, processing, characterisation and ballistic performance evaluations have highlighted the key roles of static mechanical properties and microstructure  . However, while the roles of hardness, sonic velocity, strength and density during ballistic events are relatively well understood, the relevance of fracture toughness is still unclear and controversial. Overall however, it is assumed that toughening of ceramics is synonymous for improved ballistic performance which has led to the widespread effort to reinforce ceramics with the aim of improving their strength and fracture toughness, and consequently the multi-hit capability  -  . Specifically, the multi-hit capability is shown to be a function of crack resistance that significantly affects the fragmentation process during ballistic impact on ceramics  . Of particular interest in toughening efforts is a synergistic combination of toughening mechanisms including microstructure design and particle or fiber reinforcement.
Zirconia toughened alumina (ZTA) tiles with a size of 100 × 100 × 7 mm manufactured through a pressureless sintering process were obtained from NP Aerospace Inc. Specific details of the process and product are of a proprietary nature and are not disclosed here. Polished specimens were etched in air at 1300˚C for 30 minutes. The microstructure was characterized using scanning electron microscopy (SEM: Hitachi and Carl Zeiss) with secondary electron and backscattered detectors (BSD) and energy-dispersive X-ray spectroscopy (EDS). Phases were characterised using X-ray diffraction (XRD) analysis. The average grain size and grain size distributions were determined using the line intercept method, as presented by ASTM E112-10. The porosity was measured through the Image J software.
The hardness of the material was characterised using three indentation methods including Vickers, Knoop, and nano indentation  . Vickers and Knoop hardness tests were performed according to ASTM C1327-09 and ASTM 1326-13, respectively, using loads ranging from 0.5 to 50 kg and 0.5 to 10 kg, respectively. Nano indentation testing was run on ten cycles each for loads ranging from 0.1 to 2.5 kg, and the hardness was evaluated according to Equation 1.
where F is the applied load in kgf, and h is the total penetration depth under nanoindentation.
The fracture toughness was evaluated using cracks measured at Vickers hardness indent corners using the non-standardised indentation fracture toughness (IFT) method  . The average of a minimum of 10 measurable indents at each load was considered and Equation (2) by Lawn et al. was used  .
where H is the hardness; a is the half diagonal of the Vickers indent; c is the crack length measured from the centre of the indent to the tip of the crack and E is the modulus of elasticity calculated to be 330 GPa using the rule of mixture and literature elastic modulus values of alumina and zirconia and their respective concentrations in the investigate material. The Young’s Modulus was further corrected by considering porosity and the semi-empirical Equation (3)  as well as the Oliver-Pharr method using unloading nano indentation hardness test curves  .
where Eo is the elastic modulus of fully dense ZTA; p is the porosity; and b is a characteristic constant that is related to the particle stacking and pore shape and usually has values that range between 1 and 4.35.
In addition to the IFT method, Charpy impact and the drop tower tests were used to measure the toughness. Charpy testing was performed using unnotched specimens with size 50 × 7 × 7 mm on a TMI No 43-1 impact tester with a total energy range of 2 to 15 J and an impact speed of 3.46 m/sec. The drop tower tests were performed according to ASTM D562-10, on 50 × 50 × 7 mm sample using a total assembly drop weight of 5.02 kg and an Intron Dynatup tester 9200. The strength was characterised using ring-on-ring (RoR), and 4-point bend tests according to ASTM standards C 1410 and C 1161c-15, respectively. A fracture mode study was conducted using fractured specimens from RoR tests and cracks in Vickers indention specimens at high load. Ultrasonic tests, the Archimedes test and porosity tests were used to calculate the density using Equation (4)  .
where ρo is the pore-free density; ρ is the density to be determined; P is the porosity and ρo taken as 4.08.
3. Results and Discussion
The ZrO2 particles are of various sizes and shapes and are homogeneously dispersed in the alumina matrix (Figure 1(b)). They were found most often at grain boundaries adopting the shape of the triple point junctions. The XRD analysis (Figure 2) confirmed the second phase particles to be zirconia  . The alumina matrix grain structure is bimodal with finer equiaxed grains around 1 μm in size and larger elongated grains with a grain size up to 10 μm and a grain aspect ratio of about 2.
While the use of zirconia as a second phase does prevent grain growth  , it is also known to potentially impede densification during processing, leading to poor sintering ability  , particularly during pressureless sintering  . This is reflected in the measured high porosity of 10.5% as shown in Figure 3(a), and corroborated by the image J analysis shown in Figure 3(b).
3.2. Mechanical Properties
A summary of the mechanical properties is presented in Table 1. The variation of material hardness with applied loads is shown in Figure 4 plotted using the data presented in Table 2. This figure illustrates how the tested material shows a Vickers hardness of 1700 HV at 1 kgf that drops to 1500 HV at higher test loads (2 kgf to 50 kgf). This is typical for the indentation size effect (ISE), which is primarily caused by incomplete and reversible deformations at low loads as shown in Figure 5(a) and Figure 5(b). Further potential causes of the in-
Figure 1. (a) EDS of the sample showing the two major phasesin ZTA. In the bar chart, (1) is alumina and (2) is zirconia; (b) SEM micrograph of the etched specimen used for the EDS analysis.
Table 1. Summary of mechanical properties.
Figure 2. X-ray diffraction spectra for ZTA showing the two major phases: ZrO2 and Al2O3.
Figure 3. (a) SEM of polished sample surface on X 1000 showing the high level of porosity; and (b) porosity contrast (dark) producedby the image J analysis of (a).
Figure 4. Hardness-load graph for the three indentation methods.
Figure 5. Low loads indents following (a) and (b) Vickers hardness; and (c) Knoop hardness testing.
Table 2. Hardness data.
dentation size effect include the indenter/specimen friction, the elastic/plastic deformation response of the material and the high porosity in ZTA  . The load independent value of 1509 HV was used as the characteristic hardness of this material.
Similar to the Vickers hardness, the Knoop hardness shows a strong load-hardness dependency, indicating an accentuated ISE phenomenon. The evaluated hardness value equals 1345 HK. The nanoindentation results fluctuate around 1800 HV below 5 N showing a certain level of repeatability under low loads  . At higher loads however, a strong load dependency can also be recognised. An average nanohardness value of 1387 HV with a coefficient of variance of 28.12% was calculated within the load range of up to 25 N. The theoretical Vickers hardness can be calculated using the rule of mixture and hardness values of fully dense Al2O3 and ZrO2and can be expected to range from 16 - 17 GPa whereas the actual hardness was measured to be 14.89 GPa. This implies a 7.5% drop with respect to the lower range of the theoretical value. The reason for this drop may be attributed to the average grain size of 5 μm, which is larger than what is commonly reported in literature  and the relatively high porosity level, which is in agreement with literature  . In summary, the wide distribution of hardness values can be attributed to the variations in porosity, grain structure and ZrO2 particle structure.
The hardness has so far been used as the primary selection criterion for armour ceramics  and is often directly compared to the hardness of the projectile to be defeated. Common projectile cores are made of hard steel and WC with hardness values ranging from 600 - 920 HV to 1250 - 1500 HV, respectively  . Therefore, it can be seen that ZTA is strongly adequate for defeating hard steel core projectiles, but barely meets the requirements for defeating WC core threats.
3.2.2. Fracture Toughness and Fracture Mode
Well-formed visible cracks started at loads of 10 kg. Presented in Figure 6(a) is an image of one of the cracks formed on the indent illustrating the measurement of the parameters c and a. The summary of the measured a, c and c/a values is presented in Table 3 and the plots of c, a, and c/a versus loads are presented in Figure 6(b). This study suggests that ZTA exhibits median type cracks with c/a ratios between 2.50 and 2.71, just above the value of 2.5 known to mark the transition from radial to median type cracking. Therefore, fracture toughness values calculated using the semi-empirical Equation (2) by Lawn et al. are in good agreement with toughness values measured using standard methods in this study and in literature  .
The measured experimental KIC value of 4.90 MPam1/2 is in agreement with the study conducted by Ganesh et al.  where 0 - 20 vol% ZrO2 was used in the alumina matrix. This is well corroborated by the measured Charpy impact toughness of 0.34 J  . Comparing the measured toughness value to that of monolithic alumina with a toughness of about 2.69 MPam1/2  , ZTA shows an increase by 82.2%. Moreover, residual stresses might also be created during indentation, which can accelerate crack growth and lead to an under-estimation of the materials toughness  . However, the radial crack length factor c is observed to remain a consistent function of the applied load and material properties. In fact, the c3/2 versus indentation load plot shown in Figure 7(a) indicates a good linear dependence in agreement with previous work by Lee et al.  .
The mechanism of toughening by ZrO2 is predominantly governed by its particle size. In this study, three toughening mechanisms are found to account for the KIC increase. Firstly, the stress-induced tetragonal-to-mo- noclinic phase transformation where the size of ZrO2 particle is predominantly below 1 μm  , leading to a vo- lume increase by about 4%  . The volume increase has the tendency to close growing cracks, thereby impeding crack growth leading to an increase in KIC. Secondly, the grain size of the alumina (5 - 10 μm) with an aspect ratio of 2 contributes to crack deflection and crack bridging. In addition, mechanical loading was observed to cause local plastic deformation, pore collapse and densification which promotes local further energy absorption and retards the initiation of large fracture causing cracks.
Table 3. Measured crack size  .
Figure 6. (a) SEM images showing Vickers indents and radial cracks. The arrows illustrate the measurement of the crack size parameters a and c; and (b) a, c and c/a ratios as a function of indentation load.
The crack growth path and fracture mode are presented in the SEM images of Figure 8(a) and Figure 8(b). They reveal evidence of predominantly intergranular fracture. Previous studies have shown that the intergranular failure mode on low porosity material, as found in this study, has great potential for energy absorption during fracture  .
Figure 7. (a) Relationship between crack length c and indentation load; (b) SEM image of Vickers indent under 30 kg load showing pore collapse and densification during loading.
Figure 8. SEM images of the material showing predominantly an intergranular mode of failure: (a) etched specimen; (b) unpolished surface.
Presented on Table 4 are the results of the ring-on-ring (RoR) test, evaluated using Equation (5). The recorded average strength value is 184.4 MPa. Figure 9(b) shows image of the fractured RoR test samples. It is evident that the fracture originated in the maximum stress region within the loading ring, thereby confirming the test validity according to the standard. The fracture is typical for low crack density failure with exclusively primary crack patterns resulting into only 5 to 7 fragments (Figure 9(b) and Figure 9(c)). Microscopy revealed a primarily intergranular mode of failure as shown in Figure 8 above. The observed small number of fragments indicate high fracture toughness, high fraction of energy absorption by deformation, and low fraction of energy absorption by fracture surface formation. Moreover, the low fragment density is characteristic of a lower amount of elastic energy under load that would need to be released upon fracture.
where h and l are the thickness and length of the square plates, respectively; L is 0.5(l + l); the equivalent sample diameter (D) is calculated using Equation (6); Ds is the supporting ring diameter = 50 mm; DL is the loading ring diameter = 25 mm and ν is the Poisson ratios = 0.21. The modulus of elasticity is taken to be 330 MPa.
Table 5 shows the results of the four-point bend test. An average flexural strength of 292 MPa was calculated, which is 58.4% higher than the RoR strength determined from ring-on-ring tests. This difference is expected from earlier literature observations  and can be rationalised by the larger material test volume involved in RoR tests that statistically increases the likelihood of larger defects resulting in larger stress concentration and earlier fracture. Overall however, it must be noted that the RoR strength value might also be under-estimated due to sub-critical crack growth  . Therefore, the uniaxial 4 point bend strength of 292 MPa is adopted in this study as custom in literature with respect to the fracture strength of ceramics.
The measured four-point bend strength of ZTA is 16.6% lower compared to the uniaxial strength value of 350 MPa reported in literature  . This difference can be rationalised by the fact that the fracture strength of ceramic materials is primarily governed by flaws. Therefore, the Griffith mechanics theory of fracture given by Equation (7)  was applied. In this equation, the key independent factor is the critical size of flaws, which is
Figure 9. Fracture resistance and behaviour of ZTA: (a) 50 kg load Vickers indent; (b) photograph of RoR failed specimen; (c) photograph of failed drop tower test with 60 mm drop height.
Table 4. Test data, material parameters and strength of the material through ring-on-ring test.
Table 5. Four-point bend test result.
P is the load at fracture; L is the span; and b and d are specimen rectangular cross-section dimensions 4 mm and 3 mm, respectively.
referred to as failure-causing crack (FC).
where σa is the applied stress; KIC is the fracture toughness; a is the half crack length; and Y is the pore shape factor.
Solving Equation (7) for a, a critical flaw size of 173 µm was determined suggesting that multiple pores may coalesce to cause the final fracture of the material. Overall however, the observed relatively high porosity of 10.5% seems to be compensated by the presence of zirconia particles at grain boundaries  resulting in substantial toughening by crack deviation that leads to higher energy absorption during fracture. Therefore, the strength value of 292 MPa may be viewed as appropriate for the ballistic performance of ZTA considering its resistance to cracking in both RoR and drop weight tests. The adequacy of the ZTA strength for ballistic performance despite its high porosity is also stated in the literature  . Moreover, ZTA samples showed the ability to sustain loads as high as 50 kg, as shown in Figure 9(a), and exhibited a strong deformation resistance as confirmed during the Vickers indentation tests, all of which are indications for potentially good ballistic performance.
3.2.4. Drop Weight Test
Table 6 summarizes the results of the drop tower test. From this table, the transition from non-fractured to fractured samples can be found to have occurred at a drop height of 40 mm to 50 mm. However, other important parameters such as impact energy, impact velocity and total energy do not follow this pattern, especially in the 60 mm height test. This may be due to the influence of frictions in the machine and/or to residual stresses during specimen preparation. While a drop height of 50 mm causes a crack to form at the front surface (designated as the strike surface), the cracks do not propagate through the entire thickness to the back surface. However, at a drop height of 60 mm, the test plates break completely into four fragments, as shown in Figure 9(c). This relatively small number of fragments is an indication of considerable energy absorption capability confirming the adequacy of the strength and fracture toughness of ZTA.
A contrast image from the ultrasonic test is presented in Figure 10  . It shall be noted that the apparent density gradients may instead reflect thickness variations within the test plates leading to variations in sound path length and sound travel duration  . The relationship between the effective density (ρ) and the porosity (P) is given by Equation (4).
The theoretical density ρ0 is estimated using the rule of mixture and the theoretical densities of ZrO2 and Al2O3, which are 6.1 and 3.98 g/cm3, respectively. Considering the respective volume percentages of 85.4% and 12.9% of alumina and zirconia as measured using SEM/EDS, the theoretical density ρ0 of ZTA is calculated to be 4.15 g/cm3  . Density measurements using the Archimedes and porosity methods produced density values
Figure 10. Ultrasonic tests on the ceramic test plates. The centre of the plate is at the lower right corner of the images: (a) effective plate thickness; (b) sound velocity  .
Table 6. Drop weight test result.
Where S stands for the strike patterned face; B stands for the back surface and the drop weight for each test was 5.0292 kg.
of 3.78 g/cm3 and 3.75 g/cm3, respectively, in agreement with the work of Zhang and Li  . Comparing these measured values to the estimated theoretical density of 4.15 g/cm3 translates into a 8.9% drop to a relative density of 91.1%. The high level of porosity in ZTA is a result of the grains mismatch between the initial constituents ZrO2 and Al2O3, which persists at the interface, even after sintering  .
3.2.6. Young’s Modulus
The strong correlation between porosity and Young’s modulus allows the use of semi-empirical Equation (3)  to calculate the Young’s Modulus. This equation is adopted from the work of Deng et al.  and was used to simulate the compactness of ZTA by solving for the parameter b determined to be equal to 2. This value is an indication that the pores are not spherical or compact, as confirmed in Figure 11 that shows pores with complex shapes along grain boundaries and grain triple points. Using Equation (3) and a porosity value of 10.5%, the modulus of elasticity was estimated at 272 GPa. For this calculation, the pore free modulus of elasticity is taken to be 360, as determined using the rule of mixture. An alternative method used to estimate the modulus of elasticity is the instrumented indentation hardness test. Under this test, the modulus is determined using the slope of the load versus indentation depth below 3 N in the elastic region, as established by the Oliver-Pharr method   . The results are summarized in Table 7, giving an average value of 306 GPa.
3.3. General Discussion on the Impact of Toughening and Other Properties to Ballistic Performance
A thorough review of toughening mechanisms in carbon nanotube reinforced ceramic matrix composites is provided by the work of Samal and Bal  . In this study, it was reported that zirconia particles strengthen alumina
Figure 11. SEM of etched samples showing the grain structure.
Table 7. Young’s modulus data.
by both grain pining and refinement during fabrication as well as fracture resistance during failure  . The level of toughening was found to depend on volume fraction, size and distribution of zirconia particles within the alumina matrix. Toughening mechanisms in ZTA include tetragonal-to-monoclinic phase transformation in the ZrO2 particles, crack deflection and bridging, as well as energy absorption by plastic deformation, pore collapse and densification. This explains the coarse fragmentation illustrated in Figure 9. Overall, mechanical properties measured in this study on ZTA are within specification ranges for 7.62 × 51 AP level IV, 4068 J threats  , which is encouraging for future ballistic performance. It shall be noted that in addition to improved fracture toughness and strength, microstructure and other armour related mechanical properties also significantly influence ceramics fragmentation during ballistic events  .
Although pores are generally recognised as detrimental to the strength of ceramics, it has been proven that uniformly distributed small-size pores can indeed provide good ballistic performance  . In fact, thanks to energy absorption by local pore collapse and densification, pores can retard the initiation of relatively large fracture causing cracks making them potentially beneficial to the residual strength of ceramics  , which is recognised as an important factor for enhanced ballistic performance and multi-hit capability  . Other properties that are known to enhance the armour ceramics performance include the hardness, Young’s modulus, sonic velocity and grain size.
Furthermore, the improvement of multi-hit capability of ceramics as a function of increased fracture toughness has been studied through depth of penetration tests. In a comparative study  , Savio et al. found the fracture strength of ZTA and alumina to be 274 and 272 MPa, respectively, while their hardness under 0.2 kg indentation load was 1790 and 1780 HV, respectively. The study concluded that ZTA outperformed alumina because of its greater fracture toughness, as modest as the difference may seem. Also, a numerical study showed that the ballistic resistance of ZTA was better than that of AD 95 alumina due to increased KICin ZTA that also exhibited hardness and strength values of 1796 HV and 292 MPa, respectively  .
In this work, the properties of ZTA have been investigated. It was demonstrated that: 1) a synergistic combination of toughening mechanisms including phase transformation in ZrO2 particles, crack deflection and bridging, plastic deformation, local pore collapse and densification, is crucial in achieving a substantial increase in fracture toughness; 2) A reduction in flaws in terms of defect volume fraction, size and distribution is also key for preserving efficient toughening; 3) The relatively high fracture toughness of ZTA compared to common monolithic ceramics such as alumina makes it a promising material for ballistic body protection. This high fracture toughness combined with other optimised armour related properties, such as hardness, strength and Young’s modulus, can be key for improving the fragmentation behaviour and the multi-hit capability in ceramic armours.
The authors would like to thank the Defence R & D Canada (DRDC Valcartier), Quebec, Canada for providing the material and creating an enabling working environment, as well as the National Research Council Canada, NRC Aerospace, Ottawa, Canada for allowing the use of their facilities for the experimental work.
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