# Effect of Fiber Content on Abrasive Wear Behavior of Date Palm Leaf Reinforced Polyvinyl Pyrrolidone Composite

Authors: Jyoti R. Mohanty; Sankar N. Das; Harish C. Das
Journal: ISRN Tribology
 (2014)

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## Abstract

The effect of fiber contents on wear behavior of date palm leaf reinforced polyvinyl pyrrolidone (PVP/DPL) composites has been experimentally investigated. The test samples with fillers in 10, 20, 30, and 40% based on weight of fibers were prepared using injection molding. The optimum fiber content (i.e., 26 wt%) for maximum mechanical strength of the composites was determined by regression analysis. The dry sliding wear tests were conducted for each composition at different sliding velocities (0.392, 0.471, and 0.549 m/s) and sliding distances (188, 254, and 376 m) by applying normal loads of 5, 10, 15, and 20 N using pin-on-disc wear testing machine. The specific wear rate, wear loss, and coefficient of friction were plotted against the normal load and sliding distance at all sliding velocities. The results reveal that incorporation of date palm leaf fibers leads to significant improvement in the wear resistance of composites up to optimum fiber content and then decreases as fiber content increases. Further, it is found that surface modification has significant effect on wear performance. Worn surfaces of some selected samples were studied by scanning electron microscopy to analyze the wear mechanism.


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## Body

## 1. Introduction

Growing environmental awareness has focused considerable interest in the development of nonconventional materials which are renewable, recyclable, biodegradable, sustainable, and ecofriendly. Recently, organic lingocellulosic fibers reinforced in either thermoplastic or thermosetting polymers have attracted wide attention of many researchers and scientists around the world due to their advantages over conventional synthetic fibers such as glass fibers and carbon fibers. The thermoplastic polymers, in particular, have been proved as good matrix materials for production of natural fiber-reinforced thermoplastic composites due to their excellent chemical resistance, high damping properties, low noise emission, good processability, high impact resistance, damage tolerance, and above all high cost-performance ratio [1–3]. But, high level of moisture absorption, poor wettability, and insufficient adhesion between untreated natural fibers and the polymer matrix lead to debonding. However, proper surface modifications of natural fibers with suitable chemicals can overcome these problems to a certain extent.Recently, characterization and properties of several natural fibers such as hemp, flax, jute, linen, kenaf, oil palm, and bamboo [4–12] have been explored in order to find their potential in numerous applications, for example, automobiles, furniture, packing, and construction. There are certain properties like viscoelastic and viscoplastic properties, time-dependent behavior due to creep and fatigue, tribological properties, and so forth, where less attention has been devoted by the material designers. With regards to the usage of natural fiber-reinforced polymer (NFRP) composite in tribological application, surprisingly few works [13–18] have been reported in the tribology literature. As far as tribological behavior of date palm leaf fiber-reinforced thermoplastic composite is concerned, almost no works have been done till date. However, some investigations [19–24] have been undertaken to study various properties on this other than tribological property. Therefore, the objective of the present investigation is to study the effect of fiber content on abrasive wear behavior of date palm leaf reinforced polyvinyl pyrrolidone (PVP/DPL) composites.


## 2. Materials and Method

### 2.1. Raw Materials and Composite Fabrication

Polyvinyl pyrrolidone (PVP) was procured from Merck India, while date palm leaves were collected from Baleswar (Odisha), India, as forest waste. The chemicals such as sodium hydroxide, acrylic acid, and benzene of analytical grade were used without any further purification. All solutions were made in double distilled water.The raw date palm leaf fibers (1.5 cm long and 1 mm width) were washed with distilled water and dried at 70°C for 24 hrs to remove the moistures. The fibers were first pretreated with 5% NaOH solution for 1 h at 80°C and then given acrylic acid treatment as per the procedure described earlier [19] by the present authors. The alkaline pretreated fibers were swelled in a water/benzene solvent (45/5 cm3) for 15 min at 85°C and modified with 0.3 M acrylic acid. The composite specimens for different tests were fabricated by mixing various weight percentages (e.g., 0%, 10%, 20%, 30%, and 40%) of acrylic acid-treated DPL fibers with PVP matrix by injection molding.It is worthwhile to mention here that, as a usual practice, surface treatments are given to almost all natural fibers in order improve interfacial adhesion and surface wettability of polar hydrophilic fiber with nonpolar hydrophobic matrix before fabrication of NFRP composites. However, it has been reported that [25] fiber strength decreases for most of the chemically treated NFRP composites due to breakage of the bond structure and disintegration of the noncellulosic materials. But, acrylation [26] treatment leads to strong covalent bond formation and the strength is enhanced marginally. Further, it has also been proved by the present authors [19] that acrylic acid-treated DPL fibers give highest tensile strength in comparison to other chemical treatment methods. Hence, in the present work, acrylic acid treatment has been adopted for the preparation of PVP/DPL composites specimens.In order to study the surface property of DPL fibers, micrographs for both untreated and treated fibers were taken by scanning electron microscope (SEM) and presented in Figures1(a) and 1(b), respectively. It has been found from Figure 1(a) that a lot of foreign substances are trapped on the fiber surface before chemical treatment. However, after the treatment, the surface of date palm leaf fiber is rougher than that of untreated one and free from foreign substances (Figure 1(b)). It clearly indicates that acrylic acid treatment eliminates hemicelluloses and soluble lignin from the fiber surface thereby enhancing the fiber surface wettability between the PVP matrix and DPL fiber.SEM images showing the difference of untreated and treated DPL fiber.
(a)
Untreated date palm leaf fiber
(b)
Acrylic acid-treated date palm leaf fibers


### 2.2. Mechanical Properties

Tensile properties of the composite were measured on a servohydraulic static testing machine (INSTRON 3382) with load cell of 5 kN as per ASTM D 638 standard. Three identical samples were tested at each fiber loading (i.e., 0%, 10%, 20%, 30%, and 40%) at a cross head speed of 2 mm/min out of which average readings were taken. Flexural strengths were measured on the same machine at each fiber loading using 3-point bending method as per ASTM D 790 standard.Impact strengths of the composite samples were obtained on a pendulum type Izod Impact tester as per ASTM D 256. Microhardness measurement was made using Leitz Microhardness tester equipped with a monitor and a microprocessor-based controller, with a load of 0.245 N and a loading time of 20 seconds. About five readings were taken on each sample and the average value was taken.


### 2.3. Abrasive Wear Test

Wear and frictional tests were conducted under multipass two-body abrasion condition on a pin-on-disc (POD) type wear testing machine (Figure2) as per ASTM G99-95 standard. A load cell was adopted in proper position to measure frictional forces, while a digital friction indicator was integrated directly to the load cell to capture the frictional readings.Figure 2
Pin-on-disc type wear testing machine.Cylindrical (pin) type specimen of length 35 mm and diameter of 10 mm was slid against a rotating disc (EN 31 Steel disc) of 120 mm diameter, on which abrasive paper of 400 grade (grit size≈ 23 μm) was mounted using double-sided adhesive tape. The specimens under test were fixed to the sample holder. The track diameter was changed after each test selecting a fresh one for new specimen. For each test, new abrasive paper was used and the specimen was abraded for total sliding distance of 376 m. The different test parameters for dry sliding wear test have been presented in Table 1.Table 1
Test parameters for dry sliding wear test.
Fiber weightFraction (%)
Load(N)
Sliding speed(m/s)
Sliding distance(m)
0
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00
10
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00
20
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00
26
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00
30
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00
40
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00Frictional force at the sliding interface was measured at every 5 s using load cell mounted on the load lever that holds the specimen. The frictional coefficient was determined using (1). Each test was repeated for three times and the average of each measurement was taken. Consider
(1)μ=FfFn,
where Ff is the friction force (N), and Fn is the normal load (N).After measuring the initial weight of test specimen, it was subjected to run on the counter disc for a particular test condition. The worn specimens were cleaned by tissue paper soaked with acetone and then by dry air before measuring the weight. Weight of the specimens was measured by an electronic balance (Shimadzu, Japan, AUW. 220D) with 0.01 mg least count. The difference in the weight measured before and, after each test gives the weight loss of the composite specimen. The specific wear rate(Ws) was calculated by the following equation:
(2)Ws=ΔWρFnSdm3/Nm,
where Fn is the normal load (N), Sd the sliding distance (m), ΔW the weight loss (kg), and ρ the density of the composite (kg/m3).


### 2.4. Examination of Worn Surfaces

Scanning electron microscope (SEM) model JEOL, JSM-840 was used to analyze the worn surfaces’ morphology. Before taking the SEM image, the specimen surfaces were coated with a thin layer of gold using an ion sputtering device (JEOL, JFC-1600).


## 2.1. Raw Materials and Composite Fabrication

Polyvinyl pyrrolidone (PVP) was procured from Merck India, while date palm leaves were collected from Baleswar (Odisha), India, as forest waste. The chemicals such as sodium hydroxide, acrylic acid, and benzene of analytical grade were used without any further purification. All solutions were made in double distilled water.The raw date palm leaf fibers (1.5 cm long and 1 mm width) were washed with distilled water and dried at 70°C for 24 hrs to remove the moistures. The fibers were first pretreated with 5% NaOH solution for 1 h at 80°C and then given acrylic acid treatment as per the procedure described earlier [19] by the present authors. The alkaline pretreated fibers were swelled in a water/benzene solvent (45/5 cm3) for 15 min at 85°C and modified with 0.3 M acrylic acid. The composite specimens for different tests were fabricated by mixing various weight percentages (e.g., 0%, 10%, 20%, 30%, and 40%) of acrylic acid-treated DPL fibers with PVP matrix by injection molding.It is worthwhile to mention here that, as a usual practice, surface treatments are given to almost all natural fibers in order improve interfacial adhesion and surface wettability of polar hydrophilic fiber with nonpolar hydrophobic matrix before fabrication of NFRP composites. However, it has been reported that [25] fiber strength decreases for most of the chemically treated NFRP composites due to breakage of the bond structure and disintegration of the noncellulosic materials. But, acrylation [26] treatment leads to strong covalent bond formation and the strength is enhanced marginally. Further, it has also been proved by the present authors [19] that acrylic acid-treated DPL fibers give highest tensile strength in comparison to other chemical treatment methods. Hence, in the present work, acrylic acid treatment has been adopted for the preparation of PVP/DPL composites specimens.In order to study the surface property of DPL fibers, micrographs for both untreated and treated fibers were taken by scanning electron microscope (SEM) and presented in Figures1(a) and 1(b), respectively. It has been found from Figure 1(a) that a lot of foreign substances are trapped on the fiber surface before chemical treatment. However, after the treatment, the surface of date palm leaf fiber is rougher than that of untreated one and free from foreign substances (Figure 1(b)). It clearly indicates that acrylic acid treatment eliminates hemicelluloses and soluble lignin from the fiber surface thereby enhancing the fiber surface wettability between the PVP matrix and DPL fiber.SEM images showing the difference of untreated and treated DPL fiber.
(a)
Untreated date palm leaf fiber
(b)
Acrylic acid-treated date palm leaf fibers


## 2.2. Mechanical Properties

Tensile properties of the composite were measured on a servohydraulic static testing machine (INSTRON 3382) with load cell of 5 kN as per ASTM D 638 standard. Three identical samples were tested at each fiber loading (i.e., 0%, 10%, 20%, 30%, and 40%) at a cross head speed of 2 mm/min out of which average readings were taken. Flexural strengths were measured on the same machine at each fiber loading using 3-point bending method as per ASTM D 790 standard.Impact strengths of the composite samples were obtained on a pendulum type Izod Impact tester as per ASTM D 256. Microhardness measurement was made using Leitz Microhardness tester equipped with a monitor and a microprocessor-based controller, with a load of 0.245 N and a loading time of 20 seconds. About five readings were taken on each sample and the average value was taken.


## 2.3. Abrasive Wear Test

Wear and frictional tests were conducted under multipass two-body abrasion condition on a pin-on-disc (POD) type wear testing machine (Figure2) as per ASTM G99-95 standard. A load cell was adopted in proper position to measure frictional forces, while a digital friction indicator was integrated directly to the load cell to capture the frictional readings.Figure 2
Pin-on-disc type wear testing machine.Cylindrical (pin) type specimen of length 35 mm and diameter of 10 mm was slid against a rotating disc (EN 31 Steel disc) of 120 mm diameter, on which abrasive paper of 400 grade (grit size≈ 23 μm) was mounted using double-sided adhesive tape. The specimens under test were fixed to the sample holder. The track diameter was changed after each test selecting a fresh one for new specimen. For each test, new abrasive paper was used and the specimen was abraded for total sliding distance of 376 m. The different test parameters for dry sliding wear test have been presented in Table 1.Table 1
Test parameters for dry sliding wear test.
Fiber weightFraction (%)
Load(N)
Sliding speed(m/s)
Sliding distance(m)
0
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00
10
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00
20
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00
26
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00
30
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00
40
5
0.392
188.55
10
0.471
254.32
15
0.549
314.20
20
376.00Frictional force at the sliding interface was measured at every 5 s using load cell mounted on the load lever that holds the specimen. The frictional coefficient was determined using (1). Each test was repeated for three times and the average of each measurement was taken. Consider
(1)μ=FfFn,
where Ff is the friction force (N), and Fn is the normal load (N).After measuring the initial weight of test specimen, it was subjected to run on the counter disc for a particular test condition. The worn specimens were cleaned by tissue paper soaked with acetone and then by dry air before measuring the weight. Weight of the specimens was measured by an electronic balance (Shimadzu, Japan, AUW. 220D) with 0.01 mg least count. The difference in the weight measured before and, after each test gives the weight loss of the composite specimen. The specific wear rate(Ws) was calculated by the following equation:
(2)Ws=ΔWρFnSdm3/Nm,
where Fn is the normal load (N), Sd the sliding distance (m), ΔW the weight loss (kg), and ρ the density of the composite (kg/m3).


## 2.4. Examination of Worn Surfaces

Scanning electron microscope (SEM) model JEOL, JSM-840 was used to analyze the worn surfaces’ morphology. Before taking the SEM image, the specimen surfaces were coated with a thin layer of gold using an ion sputtering device (JEOL, JFC-1600).


## 3. Results and Discussions

As reported in the review work conducted by Shalwan and Yousif [18] regarding the effect of volume (or weight) fraction of fiber on tensile strength of NFRP composites, it is found that the strength increases proportionately with the increase in volume fraction and after reaching a specific value, it further deteriorates. In the present case, also almost the same trend is observed when the measured tensile strength data of synthesized PVP/DPL composites are plotted against different weight percentages of acrylic acid-treated DPL fibers (Figure 3).Figure 3
Tensile strengths of PVP/DPL biocomposite at different wt% of fiber loadings.In order to get the optimum weight percentage theoretically, the tensile strength data are fitted with weight percentages of fibers by regression analysis. As depicted in Figure3, the data fit well by 2nd degree polynomial with regression coefficient (R2-value) of 0.998 which gives the optimum strength (i.e., 20.21 ± 1.56 MPa) at 26 wt% of fiber loading. Compared to neat PVP, 59% increase in tensile strength has been observed for PVP/DPL composites at optimum fiber loading.After obtaining the optimum weight percentage of DPL fiber (i.e., 26%) in PVP matrix for maximum tensile strength, composite specimens were fabricated on this fiber loading also to find out the other mechanical properties such as flexural strength, impact strength, and hardness. The above properties of the composite were measured at all fiber loadings (i.e., 0%, 10%, 20%, 26%, 30%, and 40%) as per the procedure given in the previous section and presented in Table2. From the results, it is evident that, similar to tensile strength, flexural strength, and impact strength first increase with fiber loading, and reaching maximum values at optimum fiber loading, then decrease. However, microhardness of the composites increases with fiber loading due to the incorporation of hard brittle fibers in soft matrix.Table 2
Mechanical properties of PVP/DPL composites at different fiber loadings.
wt% of DPL fiber
Tensile strength(MPa)
Flexural strength(MPa)
Impact strength(kJ/m2)
Hardness(Hv)
Specific wear rate×10-11 (m3/Nm)
0
12.67
±
0.63
19.21
±
1.01
0.98
±
0.01
64.0
0.919
10
15.17
±
0.94
22.55
±
0.97
1.17
±
0.03
66.5
0.825
20
19.82
±
1.24
31.59
±
2.01
1.29
±
0.06
68.0
0.716
26
20.21
±
1.56
31.71
±
1.56
1.32
±
0.12
71.4
0.525
30
18.19
±
0.98
28.89
±
1.13
1.30
±
0.11
72.0
0.589
40
17.01
±
1.02
21.11
±
0.98
1.10
±
0.04
74.5
0.653In order to study the tribological behavior of PVP/DPL composite, the specimens were fabricated at different fiber loadings for abrasive wear test by injection molding as described in the previous section. The variations of specific wear rates with load and fiber content of PVP/DPL composite at sliding velocities of 0.392, 0.471, and 0.549 m/s have been presented in Figures4 and 5, respectively. Figure 4 shows the dependence of specific wear rate on applied load for 376 m sliding distance. It is found that specific wear rate increases as applied load increases at different sliding speeds (0.392–0.549 m/s) for both neat PVP (i.e., 0 wt%) and its composites. Similar results were also reported earlier [27, 28] in case of natural fiber-reinforced polymer composites. The reason for increasing specific wear rate with applied load is that, as the fiber content increases, the matrix transfers and distributes the applied load onto the fibers which in turn increases the wear resistance of the composite. However, it occurs up to a particular fiber loading (i.e., 26 wt%) as is evident from the figure. When the fiber content increases beyond the optimum value, DPL fibers get agglomerated as a result the interaction between DPL fibers and PVP matrix is reduced. This causes debonding of fibers from the matrix.  Hence, at higher fiber loading, the interfacial adhesion between the fiber and matrix is not sufficient enough to resist sliding force resulting in higher wear rate. Further, it is observed that, at lower speed (i.e., 0.392 m/s), the specific wear rate is somehow less in comparison to higher speeds (i.e., 0.471 and 0.549 m/s) for all weight percentages of DPL fibers (Figures 4(b) and 4(c)). Comparing the specific wear rate of PVP/DPL composite at different fiber loadings (Figure 5), it is observed that, as fiber content increases wear rate decreases, after reaching a minimum value at 26 wt% of DPL fiber, then it further increases. Shalwan and Yousif [18] have pointed out that there is no remarkable correlation between the mechanical and tribological performance of major polymeric composites. But, in the present work, it is found that both the mechanical and tribological properties of PVP/DPL composite show optimum value at 26 wt% of fiber loading.Effect of specific wear rate on variations of load of PVP/DPL composite at (a) 0.392 m/s, (b) 0.471 m/s, and (c) 0.549 m/s.
(a)
(b)
(c)Figure 5
Comparison of specific wear rate with fiber loading.The effect of friction coefficients on variations of applied load at all sliding speeds have been presented in Figure6. From the figure, it is observed that friction coefficient decreases as applied load increases for neat PVP and its composites for all sliding speeds. This is because, at low load, increased value of friction coefficient is due to mechanical interlocking of asperities at the interface. As the applied load increases, temperature at the contact surface between specimen and counterface also increases which causes heating of the contact surface. Thus, the friction coefficient decreases due to the micromelting and mechanical deterioration caused by friction heat at higher loads. Similar results have been obtained for sugarcane reinforced polyester composite by EI-Tayeb [15]. Therefore, from the above results, it can be concluded that addition of date palm leaf fiber in the composite reduces the friction coefficients which is a good sign of PVP/DPL composite for tribological applications.Effect of friction coefficient on variations of load of PVP/DPL composite at 0.392 m/s, (b) 0.471 m/s, and (c) 0.549 m/s.
(a)
(b)
(c)Weight loss as a function of load at different sliding speeds has been presented in Figure7. As is evident from the figure, weight loss of the composites increases with the increase in applied load. This is due to the deeper grooving and more material removal from the sample with increasing load. The PVP matrix shows the highest weight loss because abrasive particles penetrate deeper into the softer matrix forming a series of tracks. Addition of fibers into the matrix increases fiber-matrix adhesion which reduces the material removal. It continues up to 26 wt% of fiber loading, which is the optimum value of DPL fiber in PVP matrix for the composite that provides the higher wear resistance. This may be due to the proper combination of various dominating factors such as tensile properties, hardness, toughness, and above all the fiber-matrix adhesion. In case of higher fiber contents above the optimum value, internal slippage of chain molecules increases which lowers the wear resistance and hence there is an increase in weight loss in comparison to 26 wt% PVP/DPL composites.Effect of weight loss on variations of load of PVP/DPL composite at (a) 0.392 m/s, (b) 0.471 m/s, and (c) 0.549 m/s.
(a)
(b)
(c)The variation of specific wear rate and weight loss with sliding distance of PVP/DPL composites have been presented in Figures8 and 9, respectively. From Figures 8(a)–8(c) it is observed that specific wear rate is decreasing proportionately with the function of sliding distances and sliding velocities. At the initial stage of sliding distance, the range of specific wear rate is high. However, it reaches an almost steady state at a distance of about 250 m. This is attributed to the multipass abrasion condition in which the severity of the abrasives decreases with repeated passes causing minimum wear for maximum test duration. In other words, there is less removal of material at longer sliding distances.Effect of specific wear rate on variations of sliding distance (at 10 N) of PVP/DPL composite at (a) 0.392 m/s, (b) 0.471 m/s, and (c) 0.549 m/s.
(a)
(b)
(c)Effect of weight loss on variations of sliding distance (at 10 N) of PVP/DPL composite at (a) 0.392 m/s, (b) 0.471 m/s, and (c) 0.549 m/s.
(a)
(b)
(c)Examining the weight loss of PVP/DPL composite (Figure9), it is found that weight loss increases with increasing of sliding distance due to progressive material removal with sliding velocities. This is because of the fact that the temperature of contact region during abrasion increases with the increase of sliding distance, which deteriorates the bonding and thereby causing material removal. Further, it is found that date palm leaf fiber-reinforced PVP composite having 26 wt% exhibits minimum weight loss at all sliding speeds.Figure10 illustrates typical effects of the surface modification of DPL fiber on the abrasive wear of the composite at 10 N load and 0.549 m/s sliding speed. It is clear that acrylic acid modification of DPL fibers significantly improves the abrasive wear property of the composites showing minimum weight loss at 26 wt% of DPL fiber. Further, it is found that there is an 11% decrease in weight loss of surface-modified PVP/DPL composite in comparison to unmodified one at optimum fiber loading which clearly indicates the effect of surface modification on wear property.Figure 10
Comparison of weight loss with fiber loading.The morphology of worn surfaces of PVP/DPL composites is analyzed based on SEM features (Figures11(a)–11(c)) for selected samples (at optimum fiber loading) tested under a load of 10 N and sliding distance of 376 m at all the three sliding velocities.SEM micrographs of worn surfaces (at 10 N) of 26 wt% PVP/DPL composite (a) 0.392 m/s, (b) 0.471 m/s, and (c) 0.549 m/s.
(a)
(b)
(c)From the figure, it is observed that the worn surface of samples tested at low speed (Figure11(a)) is somehow smoother than those tested at higher speeds (Figures 11(a) and 11(b)), with no sign of fiber fracture, major cracks, and pits. The mechanism of wear at low velocities is characterized by microcracking, detachment of fiber, signs of debris formation (Figure 11(a)), and matrix breakage (Figure 11(b)). At higher velocity, the damage caused to the sample is severe in the form of major cracks, fiber fracture, matrix breakage (Figures 11(b) and 11(c)), and formation of pits (Figure 11(c)) causing greater wear of the material. In addition to that debonding is also observed at medium and high speeds (Figures 11(b) and 11(c)). Further, almost rough surfaces are noticed due to the high material removal process which assisted to increase the wear rate at longer sliding velocities.


## 4. Conclusions

The effect of fiber content on friction and wear properties of PVP/DPL composites has been investigated. From the results, it is observed that incorporation of date palm leaf fillers significantly improves the wear properties of PVP/DPL composites up to a certain fiber content (i.e., 26 wt%). After that the wear properties decrease similar to mechanical properties. Specific wear rate and weight loss of the composites increase with the increase in the normal load and sliding distances at all sliding velocities. Further, it is found that the coefficient of friction of the composites decreases as applied load increases at all sliding velocities. Lowest coefficient of friction in 26 wt% filled PVP/DPL composites indicates their higher wear resistance. Further, it is found that surface modification has significant effect on wear performance and it increases the wear resistance of PVP/DPL composites. From the morphology of worn surfaces, it is observed that the wear mechanism of PVP/DPL composites at low sliding velocity is dominated by fiber fracture, matrix breakage, and microcracking, whereas, at high velocities, major cracks, debonding, and formation of pits are the predominant wear mechanisms. Finally, it can be concluded that there is a correlation between the mechanical and tribological properties of PVP/DPL composites showing optimum values at 26 wt% of fiber loading.



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*Source: 453924-2014-01-22.xml*