# Effect of Natural Fillers on Mechanical Properties of GFRP Composites

Authors: Vikas Dhawan; Sehijpal Singh; Inderdeep Singh
Journal: Journal of Composites
 (2013)

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## Abstract

Fiber reinforced plastics (FRPs) have replaced conventional engineering materials in many areas, especially in the field of automobiles and household applications. With the increasing demand, various modifications are being incorporated in the conventional FRPs for specific applications in order to reduce costs and achieve the quality standards. The present research endeavor is an attempt to study the effect of natural fillers on the mechanical characteristics of FRPs. Rice husk, wheat husk, and coconut coir have been used as natural fillers in glass fiber reinforced plastics (GFRPs). In order to study the effect of matrix on the properties of GFRPs, polyester and epoxy resins have been used. It has been found that natural fillers provide better results in polyester-based composites. Amongst the natural fillers, in general, the composites with coconut coir have better mechanical properties as compared to the other fillers in glass/epoxy composites.


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## Body

## 1. Introduction

The widespread use of the fiber reinforced plastics (FRPs) over the last few years has led to the increased research interest in the area of FRPs. Though the synthetic fiber reinforced plastics possess excellent properties, their cost of processing is quiet high, mainly due to the material cost. On the other hand, the use of natural fibers leads to cost reduction and light weight composites, though the mechanical properties of natural fiber composites are much lower as compared to the synthetic fiber composites [1]. Hence, researchers all around the world have resorted to hybrid composites by combining natural fibers with synthetic fibers in a common matrix. Mohan et al. [2] found that longitudinal compressive strength of jute-glass hybrid composites increases with increase in glass content whereas transverse compressive strength is even lower than that of jute composites. In another research effort it was found that water absorption increased with jute-glass hybrid composites which lead to decrease in mechanical properties [3]. The mechanical properties such as tensile, flexural, interlaminar shear strength, impact strength, notch sensitivity, and water absorption of jute-glass reinforced composites were studied and it was found that the mechanical properties are lower than those of plain GFRP and more than the jute fiber reinforced composites [1, 4, 5]. Water absorption was found to increase with the increase in jute content. A self-healing hybrid polymer composite of jute and glass fiber was developed to eliminate delamination and to obtain lighter composites with lower maintenance costs [6]. Thermal conductivity and thermal diffusivity were found to increase with the increase in glass content in a hybrid pineapple leaf and glass fiber reinforced polyester composite [7]. In a study made on Cordenka fiber reinforced polypropylene composites with partial jute fibers, it was concluded that the stiffness and heat distortion temperatures increased with the increase in jute proportion while the tensile strength and impact strength decreased [8]. John and Venkata Naidu [9–11] studied the tensile, impact, flexural, and compressive properties of sisal fiber and glass fiber hybrid composites with polyester as matrix material. The properties were studied for different glass contents and were found to improve with increasing glass percentages. The variation of tensile and flexural properties of Sisal/Carbon fiber hybrid composites with different fiber weight ratios were studied and significant improvement in these mechanical properties was observed with NaOH treatment of sisal fibers. It was found in chemical resistance tests that hybrid composites were not resistant to carbon tetra chloride [12]. Thermal conductivity of unsaturated polyester-based sisal/glass fiber hybrid composites was found to be lower than that of glass fiber reinforced composites and more than that of sisal fiber reinforced composites. It was also found that adding chalk powder to the resin also increased thermal conductivity [13]. Tewari et al. [14] found that mixing bagasse fiber with glass fiber improves the modulus of elasticity and impact strength but decreases the ultimate strength and bending strength. Sorption behavior and environmental aging in tensile properties were studied for short bamboo fiber reinforced polypropylene and short bamboo-glass fiber reinforced polypropylene composites. Later hygrothermal aging and fatigue behavior under cyclic loading were also studied. Tensile strength and elastic modulus of the two composites reduced considerably after aging at 75°C for 3 months [15, 16]. Cicala et al. [17] proposed that a cost reduction of 20% and a weight reduction of 23% could be achieved by using natural fibers along with glass fibers for the purpose of design of pipes. Two types of hybrid composites were fabricated in rooflite resin, one by mixing palmyra and glass fiber and the other by sandwiching palmyra fiber between glass fiber mats. The glass fiber skin with palmyra fiber core showed better mechanical properties than the dispersed one [18]. Rice husk along with glass fibers and unsaturated polyester was found to produce composites with acceptable properties [19]. Ultraviolet radiation pretreated jute and glass fiber hybrid composites were found to exhibit better mechanical properties than untreated jute-glass hybrid composites [20]. Coir-glass hybrid polyester composites were found to be promising candidates for structural applications where high strength and stiffness are required [21]. The tensile behavior of coir-glass hybrid composites at different temperatures was studied with coir and glass fibers in equal proportions. The mechanical strength increased with the increase in temperature after 50°C but reduced considerably at higher temperatures (100°C), especially for high fiber volume fractions [22]. From the literature it is clear that mechanical properties of the composites made by hybridization of natural fibers with synthetic fibers are lower than those of composites made with synthetic fibers alone. In order to reduce the cost and weight of the composites, natural fibers are used along with synthetic fibers. In the present research endeavor, coconut coir, wheat husk, and rice husk have been used as fillers along with glass fibers to form GFR-Polyester-based and GFR-Epoxy-based composites. The effect of the addition of natural fillers along with the effect of using different resin material on the mechanical properties of the GFRPs has been studied.


## 2. Experimental Details

### 2.1. Fabrication of Epoxy Laminates with Natural Fillers and Glass Fibers

Composite laminates of 4 mm thickness were prepared using boron-free EC-R glass mats, epoxy resin, and natural fillers. Rice husk, wheat husk, and coconut coir were used as filler materials. Composite laminates were prepared by conventional hand layup technique in chrome plated mild steel mold, 560 mm by 460 mm at room temperature. The mold is specially designed to produce 4 mm thick laminate sheets. All the composites have 6 layers of woven boron-free EC-R glass fiber mats of 610 GSM manufactured by Owens Corning Fiber Glass, USA. The EC-R glass had a young’s modulus of 80 GPa and density of 2.62 g/cm3. Epoxy resin LY556 (density 1.15–1.20 g/cm3 at 25°C) and hardener HY 951 (density 1 g/cm3 at 20°C) were used. The resin and hardener were mixed and stirred mechanically in a ratio of 10 : 1 by weight. In order to follow a standard comparative procedure, it was decided to fabricate laminates with a thickness of 4 mm. The natural fillers were used in a proportion of 5% of the weight of glass fibers. The decision to add only 5% natural fillers was taken after a pilot study. Initially, 10% natural fillers were added and a remarkable decrease in the mechanical properties was observed. The reduction in the properties may be attributed to the nonwetting of the fibers and fillers by the polymer matrix and agglomeration of the fillers. Moreover, the thickness constraint of 4 mm was also not achieved with the addition of 10% fillers. Here, it is worthwhile to mention that natural fibers before use were reduced to a size of one to four cm in length. Initially, the work side of the mold was coated with a thin layer of PVA (Poly Vinyl Alcohol) which acts as a release agent. After the PVA coating has dried, a light layer of the resin is made with the help of a brush and then the first layer of woven glass sheet is placed in the lower part of the mold. The glass sheet is thoroughly coated with the resin with the help of a brush and then one-fifth of the filler is evenly spread over the layer and the second glass layer is placed. Again, the resin is applied thoroughly so that the resin drips down the glass layer and coats the natural fibers also. This process is continued till the final layer of glass mat is coated with the resin. The top plate of the mold is then properly placed over the lower one to complete the assembly. Finally, the complete mold is placed in a press and a compression load of 15 tonnes is applied. The compression ensures that the entrapped air bubbles are completely removed and the excess resin flows out. The mold is left for 10 hours at room temperature to complete the curing process. The same technique was used to fabricate the other laminates. In all, four different types of specimens were fabricated. Three of the GFR-epoxy-based composites consisted of different natural biofillers, that is rice husk, wheat husk, and coconut coir, as fillers and the fourth laminate had glass fiber alone as a reinforcement.


### 2.2. Fabrication of Unsaturated Polyester Laminates with Natural Fillers and Glass Fibers

General purpose polyester resin (density 1.1 g/cm3) was used along with Methyl Ethyl Ketone Peroxide (MEKP) and Cobalt Octoate. First, the general purpose resin was mixed with Cobalt Octoate (with 6% Cobalt content) which acts as an accelerator. The accelerator accelerates the decomposition of organic peroxide initiators called catalysts and in turn increases the polymerization. Then just before the application of the resin to glass fiber, MEKP is added to the resin which acts as a catalyst and initiates the polymerization of polyester resins. MEKP also helps in cold setting of polyester-based composites. As the sheets were made in summers with normal temperature being around 40 degree plus in India, just 10 mL of Cobalt Octoate and 10 mL of MEKP were added to the resin. It has to be kept in mind that once MEKP has been added to the resin, the hand layup process has to be completed quickly; otherwise, the resin starts to gel and leads to wastage. The manufacturing of polyester-based glass fiber sheets with natural fillers is done in the same way as the epoxy-based sheets. The natural fibers are again used in the proportion of 5% by weight of the glass fiber weight and initially hand-layup process is used and then the complete mold assembly is subjected to compressive force of 15 tonnes in a press. The polyester-based laminates get ready for use within 3 hours. Similar to the epoxy-based FRP laminates; four polyester-based FRP sheets were prepared. One with woven glass fiber alone and other three laminates are with different natural fillers, that is, wheat husk, rice husk, and coconut coir.


## 2.1. Fabrication of Epoxy Laminates with Natural Fillers and Glass Fibers

Composite laminates of 4 mm thickness were prepared using boron-free EC-R glass mats, epoxy resin, and natural fillers. Rice husk, wheat husk, and coconut coir were used as filler materials. Composite laminates were prepared by conventional hand layup technique in chrome plated mild steel mold, 560 mm by 460 mm at room temperature. The mold is specially designed to produce 4 mm thick laminate sheets. All the composites have 6 layers of woven boron-free EC-R glass fiber mats of 610 GSM manufactured by Owens Corning Fiber Glass, USA. The EC-R glass had a young’s modulus of 80 GPa and density of 2.62 g/cm3. Epoxy resin LY556 (density 1.15–1.20 g/cm3 at 25°C) and hardener HY 951 (density 1 g/cm3 at 20°C) were used. The resin and hardener were mixed and stirred mechanically in a ratio of 10 : 1 by weight. In order to follow a standard comparative procedure, it was decided to fabricate laminates with a thickness of 4 mm. The natural fillers were used in a proportion of 5% of the weight of glass fibers. The decision to add only 5% natural fillers was taken after a pilot study. Initially, 10% natural fillers were added and a remarkable decrease in the mechanical properties was observed. The reduction in the properties may be attributed to the nonwetting of the fibers and fillers by the polymer matrix and agglomeration of the fillers. Moreover, the thickness constraint of 4 mm was also not achieved with the addition of 10% fillers. Here, it is worthwhile to mention that natural fibers before use were reduced to a size of one to four cm in length. Initially, the work side of the mold was coated with a thin layer of PVA (Poly Vinyl Alcohol) which acts as a release agent. After the PVA coating has dried, a light layer of the resin is made with the help of a brush and then the first layer of woven glass sheet is placed in the lower part of the mold. The glass sheet is thoroughly coated with the resin with the help of a brush and then one-fifth of the filler is evenly spread over the layer and the second glass layer is placed. Again, the resin is applied thoroughly so that the resin drips down the glass layer and coats the natural fibers also. This process is continued till the final layer of glass mat is coated with the resin. The top plate of the mold is then properly placed over the lower one to complete the assembly. Finally, the complete mold is placed in a press and a compression load of 15 tonnes is applied. The compression ensures that the entrapped air bubbles are completely removed and the excess resin flows out. The mold is left for 10 hours at room temperature to complete the curing process. The same technique was used to fabricate the other laminates. In all, four different types of specimens were fabricated. Three of the GFR-epoxy-based composites consisted of different natural biofillers, that is rice husk, wheat husk, and coconut coir, as fillers and the fourth laminate had glass fiber alone as a reinforcement.


## 2.2. Fabrication of Unsaturated Polyester Laminates with Natural Fillers and Glass Fibers

General purpose polyester resin (density 1.1 g/cm3) was used along with Methyl Ethyl Ketone Peroxide (MEKP) and Cobalt Octoate. First, the general purpose resin was mixed with Cobalt Octoate (with 6% Cobalt content) which acts as an accelerator. The accelerator accelerates the decomposition of organic peroxide initiators called catalysts and in turn increases the polymerization. Then just before the application of the resin to glass fiber, MEKP is added to the resin which acts as a catalyst and initiates the polymerization of polyester resins. MEKP also helps in cold setting of polyester-based composites. As the sheets were made in summers with normal temperature being around 40 degree plus in India, just 10 mL of Cobalt Octoate and 10 mL of MEKP were added to the resin. It has to be kept in mind that once MEKP has been added to the resin, the hand layup process has to be completed quickly; otherwise, the resin starts to gel and leads to wastage. The manufacturing of polyester-based glass fiber sheets with natural fillers is done in the same way as the epoxy-based sheets. The natural fibers are again used in the proportion of 5% by weight of the glass fiber weight and initially hand-layup process is used and then the complete mold assembly is subjected to compressive force of 15 tonnes in a press. The polyester-based laminates get ready for use within 3 hours. Similar to the epoxy-based FRP laminates; four polyester-based FRP sheets were prepared. One with woven glass fiber alone and other three laminates are with different natural fillers, that is, wheat husk, rice husk, and coconut coir.


## 3. Mechanical Characterization

### 3.1. Tensile Strength

The tensile test was performed in accordance with ASTM D3039. The test specimen size was 250 mm × 25 mm × 4 mm. The test was performed on a universal testing machine (UTM) of 10-tonne capacity. The flat specimens of required size were fixed between the grips of each head of the testing machine in a way that the direction of force applied to the specimen is coincident with the longitudinal axis of the specimen. The strain rate was so selected so as to produce the failure from 1 to 10 min:(1)TensileStrength=WBDW= Load in Kgs, B = Breadth in cm, and D = thickness in cm.


### 3.2. Compressive Strength

The compressive strength of the test specimens was found using UCSB compressive fixture [23]. The size of the test specimens was 127 mm × 38.1 mm × 4 mm. A hole of 6.35 mm was then drilled in the center of the flat specimens. The test was performed on a universal testing machine of 10-tonne capacity. The test specimens were fixed in a UCSB fixture and the fixture was placed in between two flat circular plates on the UTM. The compressive load was applied in the axial direction so as to cause the failure of the specimen. 								(2)CompressiveStrength=WBDW = Load in Kgs, B = Breadth in cm, D = thickness in cm.


### 3.3. Cross Breaking Strength

The cross breaking test was conducted as per IS: 1998-1962. According to the IS standards, the test specimen needs to be 15 mm ± 0.5 mm in breadth and should have a length of 24 to 30 times the thickness of the laminate measured nearest to 0.03 mm. The test was conducted on the UTM. Two parallel V-shaped supports were used to fix the specimen in the machine. The distance between the supports was kept equal to sixteen times the measured thickness of the test specimen. A load was applied by the third V-block parallel to and between the supporting blocks across the width of the test specimen. The load was steadily increased at such a rate that the test specimen fractures in 15 to 45 seconds from the time of initial application of load:(3)CrossBreakingStrength=1.5WLBD2W = Load in kgs, L = Distance between supports in cm, B = Breadth in cm, and D = Thickness in cm.


### 3.4. Izod Impact Strength

Izod Impact Strength was found according to IS0 180 : 1993, on an Izod Impact Testing Machine (0–168 Joule capacity). A rectangular piece of length 63.5 ± 2 mm and width 12.7 ± 0.2 mm having thickness of the laminate (4 mm) was prepared as shown in Figure1. The specimen is having a V-notch at a point equidistant from the ends of the long side. The specifications of the specimen as per the standard are shown in Figure 1. The specimen was fixed in the vice of the testing machine so that the notched face of the specimen faces the striker and the root of the notch is in level with the horizontal face of the vice. When the pendulum is released with the help of an operating lever, the notched side of the specimen is struck by the striking edge of the pendulum. The energy absorbed in breaking the specimen was then recorded:
(4)IzodImpactStrength(KJ/m2)=EnergyabsorbedinjoulesWidthofnotchedface×Lengthbelowthenotch.Figure 1
Specimen for Izod Impact Strength.


### 3.5. Rockwell Hardness Test

Test specimens of size 25 mm by 25 mm were prepared according to ASTM D785-08. A steel ball indenter of 3.175 mm diameter was used to find the hardness on a Rockwell machine. The hardness was measured on Rockwell hardness K-scale with a major load of 150 kg and an average of five hardness tests was taken.


### 3.6. Specific Gravity Test

The specific gravity test was done in accordance with Indian Standard IS: 10192-1982. The specimen prepared for the test was a square of 40 ± 1 mm with thickness being that of the laminate (4 mm). The specimen was first weighed in air by suspending it with the help of a thread fixed to the hook of the balance, and the weightW1 was recorded. Then, the weight W2 was recorded by measuring the specimen in fresh distilled water. The specimen was allowed to attain the temperature of the water by immersing it in water for sufficient time. Care was also taken that no air bubbles stick to the specimen:
(5)Specificgravity=W1W1-W2.


### 3.7. Water Absorption Test

The water absorption test was conducted according to Indian Standard IS: 1998-1962. A square test specimen of38-0.0+0.5 mm was made. The weight of the specimen was first measured in air (W1), and then the specimen was immersed in distilled water for a period of 24 ± 1 hour. On removal from water, the specimen was wiped properly and was weighed within two minutes of its removal from water. This weight was recorded as W2:
(6)WaterAbsorption=W2-W1W1×100.


### 3.8. Volume Fraction of Glass Fibers

The volume fraction of glass fibers (glass content) was found according to ASTM D2584-08. The test specimens of 20 mm × 20 mm × 4 mm were prepared. Initially, a desiccated ceramic crucible was weighed (W1), and then it was weighed along with the specimen (W2). Then, the crucible with the specimen was placed in a muffle furnace at 590°C. After the carbonaceous material disappeared, the crucible was cooled to a room temperature and the crucible was weighed again with glass fibers left alone (W3):
(7)IgnitionLoss=W2-W3W2-W1×100GlassContent=100-IgnitionLoss.


## 3.1. Tensile Strength

The tensile test was performed in accordance with ASTM D3039. The test specimen size was 250 mm × 25 mm × 4 mm. The test was performed on a universal testing machine (UTM) of 10-tonne capacity. The flat specimens of required size were fixed between the grips of each head of the testing machine in a way that the direction of force applied to the specimen is coincident with the longitudinal axis of the specimen. The strain rate was so selected so as to produce the failure from 1 to 10 min:(1)TensileStrength=WBDW= Load in Kgs, B = Breadth in cm, and D = thickness in cm.


## 3.2. Compressive Strength

The compressive strength of the test specimens was found using UCSB compressive fixture [23]. The size of the test specimens was 127 mm × 38.1 mm × 4 mm. A hole of 6.35 mm was then drilled in the center of the flat specimens. The test was performed on a universal testing machine of 10-tonne capacity. The test specimens were fixed in a UCSB fixture and the fixture was placed in between two flat circular plates on the UTM. The compressive load was applied in the axial direction so as to cause the failure of the specimen. 								(2)CompressiveStrength=WBDW = Load in Kgs, B = Breadth in cm, D = thickness in cm.


## 3.3. Cross Breaking Strength

The cross breaking test was conducted as per IS: 1998-1962. According to the IS standards, the test specimen needs to be 15 mm ± 0.5 mm in breadth and should have a length of 24 to 30 times the thickness of the laminate measured nearest to 0.03 mm. The test was conducted on the UTM. Two parallel V-shaped supports were used to fix the specimen in the machine. The distance between the supports was kept equal to sixteen times the measured thickness of the test specimen. A load was applied by the third V-block parallel to and between the supporting blocks across the width of the test specimen. The load was steadily increased at such a rate that the test specimen fractures in 15 to 45 seconds from the time of initial application of load:(3)CrossBreakingStrength=1.5WLBD2W = Load in kgs, L = Distance between supports in cm, B = Breadth in cm, and D = Thickness in cm.


## 3.4. Izod Impact Strength

Izod Impact Strength was found according to IS0 180 : 1993, on an Izod Impact Testing Machine (0–168 Joule capacity). A rectangular piece of length 63.5 ± 2 mm and width 12.7 ± 0.2 mm having thickness of the laminate (4 mm) was prepared as shown in Figure1. The specimen is having a V-notch at a point equidistant from the ends of the long side. The specifications of the specimen as per the standard are shown in Figure 1. The specimen was fixed in the vice of the testing machine so that the notched face of the specimen faces the striker and the root of the notch is in level with the horizontal face of the vice. When the pendulum is released with the help of an operating lever, the notched side of the specimen is struck by the striking edge of the pendulum. The energy absorbed in breaking the specimen was then recorded:
(4)IzodImpactStrength(KJ/m2)=EnergyabsorbedinjoulesWidthofnotchedface×Lengthbelowthenotch.Figure 1
Specimen for Izod Impact Strength.


## 3.5. Rockwell Hardness Test

Test specimens of size 25 mm by 25 mm were prepared according to ASTM D785-08. A steel ball indenter of 3.175 mm diameter was used to find the hardness on a Rockwell machine. The hardness was measured on Rockwell hardness K-scale with a major load of 150 kg and an average of five hardness tests was taken.


## 3.6. Specific Gravity Test

The specific gravity test was done in accordance with Indian Standard IS: 10192-1982. The specimen prepared for the test was a square of 40 ± 1 mm with thickness being that of the laminate (4 mm). The specimen was first weighed in air by suspending it with the help of a thread fixed to the hook of the balance, and the weightW1 was recorded. Then, the weight W2 was recorded by measuring the specimen in fresh distilled water. The specimen was allowed to attain the temperature of the water by immersing it in water for sufficient time. Care was also taken that no air bubbles stick to the specimen:
(5)Specificgravity=W1W1-W2.


## 3.7. Water Absorption Test

The water absorption test was conducted according to Indian Standard IS: 1998-1962. A square test specimen of38-0.0+0.5 mm was made. The weight of the specimen was first measured in air (W1), and then the specimen was immersed in distilled water for a period of 24 ± 1 hour. On removal from water, the specimen was wiped properly and was weighed within two minutes of its removal from water. This weight was recorded as W2:
(6)WaterAbsorption=W2-W1W1×100.


## 3.8. Volume Fraction of Glass Fibers

The volume fraction of glass fibers (glass content) was found according to ASTM D2584-08. The test specimens of 20 mm × 20 mm × 4 mm were prepared. Initially, a desiccated ceramic crucible was weighed (W1), and then it was weighed along with the specimen (W2). Then, the crucible with the specimen was placed in a muffle furnace at 590°C. After the carbonaceous material disappeared, the crucible was cooled to a room temperature and the crucible was weighed again with glass fibers left alone (W3):
(7)IgnitionLoss=W2-W3W2-W1×100GlassContent=100-IgnitionLoss.


## 4. Results and Discussion

In all, eight different types of GFRP laminates were fabricated. Four of the GFRPs were epoxy resin based and other four were general purpose polyester (orthophthalic resin commonly known as G. P resin) based. In general, with the same resin, one specimen was reinforced with glass fiber alone and three other were reinforced with different natural fillers that is wheat husk, Rice husk, and coconut coir. Various characterization tests were conducted and their results are depicted in Table1 and are discussed in the following sections.Table 1
Summary of experimental findings.
Property
FRP
Glass fiber reinforced epoxy
Glass fiber reinforced polyester
No filler
Wheat husk filler
Coconut coir filler
Rice filler
No filler
Wheat husk filler
Coconut coir filler
Rice filler
Tensile strength (N/mm2)
398.73
353.05
372
307.65
352.5
283
315
324.9
Compressive strength (N/mm2)
351.3
222.24
289
280.43
212.9
173.69
224.14
199.47
Cross breaking strength (N/mm2)
896.07
698.03
827.45
733.33
614
522
702
548
Impact strength (N/mm2)
263.84
206.47
214.84
234.37
234.37
245.53
278.93
256.69
Hardness   (K-scale)
56.1
30.33
42.83
40.33
41
33.25
35.9
41.375
Specific gravity
1.6727
1.6152
1.6629
1.6166
2.082
1.6723
1.707
1.7272
Water absorption
0.0343
0.6541
0.205
0.2316
0.47395
1.824
0.7522
0.685
Glass content
52.14
54.77
52.83
55.55
52.39
54.02
51.41
53.19


### 4.1. Tensile Strength

In general, it has been found that the tensile strength of epoxy-based GFRPs is more than polyester-based composites. The tensile strength values of the eight different composites under consideration are shown in Figure2. Though the tensile strength of composites developed with epoxy and polyester decreases when the natural fillers are added, the tensile strength of epoxy-based composites with coconut coir and wheat husk as fillers is greater than the plain glass reinforced polyester composites. On the contrary, the composites developed with rice husk fillers in polyester show more strength than the composites developed in epoxy with rice husk as fillers. The reason may be attributed to the better bonding of rice husk with polyester rather than with epoxy. The epoxy-based composites with coconut coir as fillers show comparable strength with plain GFRP composites, and on the other hand, polyester-based composites with rice husk fillers show good tensile strength in comparison to other polyester-based composites with fillers. The tensile strength of the epoxy-based composites decreased by a maximum of 22.8% (with rice husk fillers) and that of polyester-based composites decreased by 19.71% (with wheat husk fillers).Figure 2
Tensile strength of composites with/without filler.


### 4.2. Compressive Strength

The compressive strength was found using UCSB fixture on Universal Testing Machine. The compressive strength of epoxy-based composites is more than that of  polyester-based composites as shown in Figure3. The compressive strength of all the composites with and without fillers with epoxy as matrix is more than glass fiber reinforced polyester laminates. This shows that epoxy should be used as matrix for better compressive strength. Amongst the GFR-Polyester composites, the specimens with coconut coir as filler show better compressive strength than the plain GFR-Polyester specimens. In general, the composites with wheat husk as fillers have the minimum compressive strength. The compressive strength of epoxy-based and polyester-based composites decreased by a maximum of 36.7% and 18.41% on the addition of wheat husk fillers.Figure 3
Compressive strength of composites with/without filler.


### 4.3. Cross Breaking Strength

The three-point bending test conducted on UTM shows that among the GFR-Polyester composites, the composites with coconut coir fillers show better strength than the plain GFR-polyester composites. Even in GFR-Epoxy composites, the specimens with coconut coir fillers show comparable strength to the plain GFR-Epoxy specimens. As shown in Figure4, the cross breaking strength of GFR-Epoxy composites is better than GFR-Polyester composites. The cross breaking strength of composites with wheat husk fillers is lower in both GFR-Epoxy and GFR-Polyester composites. The cross breaking strength of epoxy-based composites decreased by 22.1% on the addition of wheat husk fillers whereas that of polyester-based composites increased by 14.33% on the addition of coconut coir fillers.Figure 4
Results of three-point bending test.


### 4.4. Impact Strength

Figure5 clearly shows that the izod impact strength of polyester-based composites with coconut coir as fillers was found to be the best among all the composites fabricated. Different patterns were observed in epoxy- and polyester-based composites. In epoxy-based composites, plain GFRP specimens showed more impact strength followed by those with rice fillers, coconut coir fillers and the least impact strength was with wheat husk fillers, whereas in polyester-based composites, the highest impact strength was shown by specimens with coconut coir as fillers followed by those with rice husk fillers, wheat husk fillers, and the minimum impact strength was depicted by plain GFR-Polyester composites. On the whole it is observed that the impact strength improves in polyester-based composites on the addition of natural fillers. The impact strength of polyester-based composites increased by a maximum of 19.01% on the addition of coconut coir as fillers, but it reduced by 21.6% on the addition of wheat husk fillers in epoxy-based composites.Figure 5
Izod Impact Strength of composites with/without filler.


### 4.5. Hardness

The hardness of plain GFR-Epoxy composites was found to be maximum with a value of HRK 56.1. The hardness of GFR-Epoxy composites reduced with the addition of fillers. The hardness of GFR-Polyester with rice fillers was more than simple GFR-Polyester composites. The hardness of composites with wheat husk as fillers was found to be the lowest with both epoxy and polyester as resin as shown in Figure6. The hardness of epoxy-based composites decreased by 45.9% on the addition of wheat husk fillers and that of polyester-based composites increased by 0.91% on the addition of rice fillers.Figure 6
Hardness of composites with/without filler.


### 4.6. Specific Gravity

The specific gravity of GFR-Polyester-based composites is more than GFR-Epoxy-based composites. As is clear from Figure7, the specific gravity of GFR-Epoxy composites is nearly the same whereas amongst the GFR-Polyester composites the specific gravity of plain GFR composites is found to be marginally more than those with fillers. The specific gravity of epoxy-based and polyester-based reduced by a maximum of 3.39% and 19.67%, respectively, on the addition of wheat husk fillers.Figure 7
Specific gravity of composites with/without fillers.


### 4.7. Water Absorption

Water absorption in case of GFR-Polyester composites was found to be much greater than the GFR-Epoxy composites. Water absorption, even in GFR-Epoxy composites with fillers, is less than the plain GFR-Polyester specimen. The test results of water absorption test are shown in Figure8.Figure 8
Results of Water Absorption Test.The water uptake may affect the mechanical behavior of the developed composites. It has already been established by the authors that the water uptake affects the tensile behavior of the polymer matrix composites [24, 25]. The researchers worldwide have tried to correlate the amount of water-up with the mechanical behavior of composite materials [25, 26].


### 4.8. Volume Fraction of Glass Fibers

The glass content for all the specimens is found to lie in the range of 51.4%–55.55%. The variation is due to the variation in weight of glass fiber mats used.


## 4.1. Tensile Strength

In general, it has been found that the tensile strength of epoxy-based GFRPs is more than polyester-based composites. The tensile strength values of the eight different composites under consideration are shown in Figure2. Though the tensile strength of composites developed with epoxy and polyester decreases when the natural fillers are added, the tensile strength of epoxy-based composites with coconut coir and wheat husk as fillers is greater than the plain glass reinforced polyester composites. On the contrary, the composites developed with rice husk fillers in polyester show more strength than the composites developed in epoxy with rice husk as fillers. The reason may be attributed to the better bonding of rice husk with polyester rather than with epoxy. The epoxy-based composites with coconut coir as fillers show comparable strength with plain GFRP composites, and on the other hand, polyester-based composites with rice husk fillers show good tensile strength in comparison to other polyester-based composites with fillers. The tensile strength of the epoxy-based composites decreased by a maximum of 22.8% (with rice husk fillers) and that of polyester-based composites decreased by 19.71% (with wheat husk fillers).Figure 2
Tensile strength of composites with/without filler.


## 4.2. Compressive Strength

The compressive strength was found using UCSB fixture on Universal Testing Machine. The compressive strength of epoxy-based composites is more than that of  polyester-based composites as shown in Figure3. The compressive strength of all the composites with and without fillers with epoxy as matrix is more than glass fiber reinforced polyester laminates. This shows that epoxy should be used as matrix for better compressive strength. Amongst the GFR-Polyester composites, the specimens with coconut coir as filler show better compressive strength than the plain GFR-Polyester specimens. In general, the composites with wheat husk as fillers have the minimum compressive strength. The compressive strength of epoxy-based and polyester-based composites decreased by a maximum of 36.7% and 18.41% on the addition of wheat husk fillers.Figure 3
Compressive strength of composites with/without filler.


## 4.3. Cross Breaking Strength

The three-point bending test conducted on UTM shows that among the GFR-Polyester composites, the composites with coconut coir fillers show better strength than the plain GFR-polyester composites. Even in GFR-Epoxy composites, the specimens with coconut coir fillers show comparable strength to the plain GFR-Epoxy specimens. As shown in Figure4, the cross breaking strength of GFR-Epoxy composites is better than GFR-Polyester composites. The cross breaking strength of composites with wheat husk fillers is lower in both GFR-Epoxy and GFR-Polyester composites. The cross breaking strength of epoxy-based composites decreased by 22.1% on the addition of wheat husk fillers whereas that of polyester-based composites increased by 14.33% on the addition of coconut coir fillers.Figure 4
Results of three-point bending test.


## 4.4. Impact Strength

Figure5 clearly shows that the izod impact strength of polyester-based composites with coconut coir as fillers was found to be the best among all the composites fabricated. Different patterns were observed in epoxy- and polyester-based composites. In epoxy-based composites, plain GFRP specimens showed more impact strength followed by those with rice fillers, coconut coir fillers and the least impact strength was with wheat husk fillers, whereas in polyester-based composites, the highest impact strength was shown by specimens with coconut coir as fillers followed by those with rice husk fillers, wheat husk fillers, and the minimum impact strength was depicted by plain GFR-Polyester composites. On the whole it is observed that the impact strength improves in polyester-based composites on the addition of natural fillers. The impact strength of polyester-based composites increased by a maximum of 19.01% on the addition of coconut coir as fillers, but it reduced by 21.6% on the addition of wheat husk fillers in epoxy-based composites.Figure 5
Izod Impact Strength of composites with/without filler.


## 4.5. Hardness

The hardness of plain GFR-Epoxy composites was found to be maximum with a value of HRK 56.1. The hardness of GFR-Epoxy composites reduced with the addition of fillers. The hardness of GFR-Polyester with rice fillers was more than simple GFR-Polyester composites. The hardness of composites with wheat husk as fillers was found to be the lowest with both epoxy and polyester as resin as shown in Figure6. The hardness of epoxy-based composites decreased by 45.9% on the addition of wheat husk fillers and that of polyester-based composites increased by 0.91% on the addition of rice fillers.Figure 6
Hardness of composites with/without filler.


## 4.6. Specific Gravity

The specific gravity of GFR-Polyester-based composites is more than GFR-Epoxy-based composites. As is clear from Figure7, the specific gravity of GFR-Epoxy composites is nearly the same whereas amongst the GFR-Polyester composites the specific gravity of plain GFR composites is found to be marginally more than those with fillers. The specific gravity of epoxy-based and polyester-based reduced by a maximum of 3.39% and 19.67%, respectively, on the addition of wheat husk fillers.Figure 7
Specific gravity of composites with/without fillers.


## 4.7. Water Absorption

Water absorption in case of GFR-Polyester composites was found to be much greater than the GFR-Epoxy composites. Water absorption, even in GFR-Epoxy composites with fillers, is less than the plain GFR-Polyester specimen. The test results of water absorption test are shown in Figure8.Figure 8
Results of Water Absorption Test.The water uptake may affect the mechanical behavior of the developed composites. It has already been established by the authors that the water uptake affects the tensile behavior of the polymer matrix composites [24, 25]. The researchers worldwide have tried to correlate the amount of water-up with the mechanical behavior of composite materials [25, 26].


## 4.8. Volume Fraction of Glass Fibers

The glass content for all the specimens is found to lie in the range of 51.4%–55.55%. The variation is due to the variation in weight of glass fiber mats used.


## 5. Conclusions

In the present research endeavor, various characterization tests were conducted over GFR-Polyester- and GFR-Epoxy-based composites. In general, the addition of fillers leads to cost and weight reduction of the regular glass fiber reinforced composites. The effect of the addition of natural fillers has been studied and the following conclusions can be drawn.(1)
The tensile strength of epoxy-based composites is better than that of polyester-based. The tensile strength of GFR-Epoxy composites with coconut coir as fillers is comparable to that of plain GFR-Epoxy composite and in case of polyester composites GFR-polyester with rice husk filler is comparable to that of plain GFR-Polyester laminate.(2)
The compressive strength of GFR-Epoxy-based composites is better than that of  GFR-Polyester-based composites. The compressive strength of GFR-Polyester specimens with coconut coir as fillers results in better compressive strength than plain GFR-Polyester composites.(3)
The impact strength of polyester-based filler composites is better than that of epoxy-based composites. The impact strength of GFR-Polyester composites with coconut coir fillers is even more than the GFR-Epoxy composites with no fillers.(4)
The cross breaking strength of GFR-Epoxy composites is better than that of GFR-Polyester composites. Addition of coconut coir shows good results in both epoxy and polyester composites.(5)
The hardness of epoxy-based composites is more with respect to polyester-based composites.(6)
The specific gravity of polyester-based composites is more than epoxy-based composites. The addition of fillers leads to reduction of specific gravity in all types of composites investigated in the present research endeavor.(7)
Water absorption is more in polyester-based composites.(8)
Overall, coconut coir fillers should be used instead of wheat husk and rice husk in general to improve the properties of the developed glass fiber reinforced composite laminates.



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*Source: 792620-2013-07-08.xml*