<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">OJCM</journal-id><journal-title-group><journal-title>Open Journal of Composite Materials</journal-title></journal-title-group><issn pub-type="epub">2164-5612</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ojcm.2015.54014</article-id><article-id pub-id-type="publisher-id">OJCM-60752</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Chemistry&amp;Materials Science</subject></subj-group></article-categories><title-group><article-title>
 
 
  Physico-Mechanical Properties of Luffa aegyptiaca Fiber Reinforced Polymer Matrix Composite
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>.</surname><given-names>I. Ichetaonye</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>I.</surname><given-names>C. Madufor</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>M.</surname><given-names>E. Yibowei</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>D.</surname><given-names>N. Ichetaonye</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Department of Polymer and Textile Engineering, Federal University of Technology, Owerri, Nigeria</addr-line></aff><aff id="aff1"><addr-line>Department of Polymer and Textile Technology, Yaba College of Technology, Yaba, Lagos, Nigeria</addr-line></aff><pub-date pub-type="epub"><day>16</day><month>09</month><year>2015</year></pub-date><volume>05</volume><issue>04</issue><fpage>110</fpage><lpage>117</lpage><history><date date-type="received"><day>27</day>	<month>May</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>23</month>	<year>October</year>	</date><date date-type="accepted"><day>29</day>	<month>October</month>	<year>2015</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  This paper presents the study of moisture content, hardness, bulk density, apparent porosity, tensile and flexural characteristics of composite properties of Luffa aegyptiaca fiber. Luffa aegyptiaca reinforced epoxy composites have been developed by hand lay-up method with Luffa fiber untreated and treated conditions for 12 Hrs and 24 Hrs in different filler loading as in 2:1 ratio (5%, 10%, 15%, 20% and 25%). The effects of filler loading on the moisture content, hardness, bulk density, apparent porosity, tensile and flexural properties were studied. In general, the treated Luffa fibre composite for 24 Hrs showed better improvement properties via addition of modified Luffa fibre as reinforcement. However, tensile and flexural properties improved continuously with increasing filler loading up to 20% but decreasing at 25% due to weak interfacial bonding for both untreated and treated composite. The favourable results were obtained at 20% for treated composite at 24 Hrs especially at tensile and flexural characteristics and are suitable for mechanical applications.
 
</p></abstract><kwd-group><kwd>Luffa aegyptiaca</kwd><kwd> Fiber</kwd><kwd> Flexural</kwd><kwd> Filler Loading</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Composite material can be referred to as a combination of two or more materials that results in better properties than the individual component used alone [<xref ref-type="bibr" rid="scirp.60752-ref1">1</xref>] or it can also be described as a structural material that consists of two or more constituents at a macroscopic level and constituents are not soluble in each other [<xref ref-type="bibr" rid="scirp.60752-ref2">2</xref>] . The two constituents are reinforcement and a matrix [<xref ref-type="bibr" rid="scirp.60752-ref3">3</xref>] . However, in modern materials engineering the term usually refers to a “MATRIX” material that is reinforced with fibers [<xref ref-type="bibr" rid="scirp.60752-ref4">4</xref>] . Most composites used today are at the leading edge of materials technology with performance and costs appropriate to ultra demanding applications such as spacecraft [<xref ref-type="bibr" rid="scirp.60752-ref5">5</xref>] .</p><p>All of the different fibers used in composites have different properties and so affect the properties of the composite in different ways. This also provides stiffness to the composites. Fillers find application in the polymer industry, almost exclusively to improve mechanical, thermal, electrical properties and dimensional stability [<xref ref-type="bibr" rid="scirp.60752-ref6">6</xref>] . Fillers increase the number of chains, which share the load of a broken polymer chain. Research activities in recent time were towards finding alternatives fillers to replace the inorganic one [<xref ref-type="bibr" rid="scirp.60752-ref7">7</xref>] . The uses of natural fibers (organic fillers) have the following advantages when compare to the inorganic fillers: low density, low-cost, non-abrasive, availability from natural resources, they are renewable natural resources, they are recyclable and biodegradable [<xref ref-type="bibr" rid="scirp.60752-ref8">8</xref>] . Natural fibre reinforced FRPs can solve both the performance and environment related issues.</p><p>Luffa is a plant from the cucumber family grown for its multipurpose fruit (<xref ref-type="fig" rid="fig1">Figure 1</xref>) in many tropical countries. It is an annual climbing or trailing herbaceous species that can be 15 m long. The Luffa genus encompasses seven (7) species among which Luffa aegyptiaca and Luffa acutangula are primarily grown for its fibre production. The young fruits and leaves can be cooked as vegetable (fruits can be used in India to make curry) or eaten fresh or dried [<xref ref-type="bibr" rid="scirp.60752-ref9">9</xref>] . More so, when the fruit matures it becomes fibrous (<xref ref-type="fig" rid="fig2">Figure 2</xref>); the fiber is used as sponge for washing and scrubbing utensils as well as the human body. But due to the presence of hydroxyl groups from cellulose and lignin, natural fiber exhibits highly hydrophilic properties [<xref ref-type="bibr" rid="scirp.60752-ref10">10</xref>] . This makes fiber-ma- trix adhesion very difficult because most structural polymers are hydrophobic in nature which results in an unexpected failure of the composite material in service [<xref ref-type="bibr" rid="scirp.60752-ref11">11</xref>] . Therefore, in order to maximize natural fiber reinforced composite performance, fiber surface modification as well as a chemical additive to polymer matrix is required to improve the performance [<xref ref-type="bibr" rid="scirp.60752-ref12">12</xref>] . Thus, the present investigation seeks to characterize the physic-me- chanical and morphological properties of sponge gourd (Luffa aegyptiaca) reinforced epoxy composite.</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Luffa aegyptiaca</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x6.png"/></fig><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Dried Luffa aegyptiaca</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x7.png"/></fig></sec><sec id="s2"><title>2. Experiment</title><sec id="s2_1"><title>2.1. Materials</title><p>1) Luffa aegyptiaca (fibrous);</p><p>2) Epoxy (LY 556) and Hardener (HY 951);</p><p>3) Sodium Hydroxide;</p><p>4) Distilled Water;</p><p>5) 88 Universal Mold Release Wax;</p><p>6) Acetic Acid.</p></sec><sec id="s2_2"><title>2.2. Equipment</title><p>The equipment used was:</p><p>1) Digital weighing balance (Pocket Scale, Black AWS-100 g);</p><p>2) Steel mould (Fabricated 3-piece mould with detachable top and base for dumb-bell and sheet shape);</p><p>3) 1.0mm sieve, (YS-C-638);</p><p>4) Beaker and measuring cylinder (200 and 100 mils respectively);</p></sec><sec id="s2_3"><title>2.3. Material Preparation</title><p>Raw Luffa aegyptiaca fiber was cut opened lengthwise, the dried seeds shaken out and the dried fibrous sun- dried for six (6) hours. It was later cut into smaller sizes, grounded and then sieved with 1.0 mm sieve to obtain fine fiber particles (<xref ref-type="fig" rid="fig3">Figure 3</xref>). Composite samples were fabricated with 5%, 10%, 15%, 20% and 25% fillers in the ratio of 2:1 as in volume fraction using dumb-bell mould of 120 mm &#215; 30 mm &#215; 3 mm and rectangular sheet mould of 187 mm &#215; 125 mm &#215; 3 mm by hand laying method and finally left to air-cure for 24 Hrs (<xref ref-type="fig" rid="fig4">Figure 4</xref>). Thereafter, the laminates are taken carefully without any damage. Specimens are cut for testing as per ASTM standards.</p><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Grinded Luffa fibers of particle size 1.0 .mm</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x8.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Preparation of composite testing</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x9.png"/></fig></sec><sec id="s2_4"><title>2.4. Fiber Chemical Treatment</title><p>The fibers were immersed in NaOH solution with a concentration of 20% for 12 and 24 hours respectively at room temperature. After treatment, the fibers were washed with 2% acetic acid and again washed under running water then finally allowed to dry at room temperature for 2 days.</p></sec></sec><sec id="s3"><title>3. Characterization of Composite Materials</title><sec id="s3_1"><title>3.1. Determination of Moisture Content</title><p>A representative sample of the test fibers was weighed (M<sub>2</sub>), dried at 110˚C for 1 hour and then weighed (M<sub>1</sub>) again. The difference in mass was divided by the initial mass, and then multiplied by 100:</p><p>Mathematically, this was calculated using Equation (1).</p><disp-formula id="scirp.60752-formula1282"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1810164x10.png"  xlink:type="simple"/></disp-formula><p>where M.C = Moisture content;</p><p>M<sub>1</sub> = Weight of the sample after drying;</p><p>M<sub>2</sub> = Weight of the sample before drying.</p></sec><sec id="s3_2"><title>3.2. Determination of Hardness Test</title><p>Micro-hardness measurement was done using a Leitz Hardnes (OS-2H) tester. This tester had a diamond indenter, in the form of a right pyramid with a square base and an angle 136˚ between opposite faces under a load of 3 N in accordance with ASTM E384.</p></sec><sec id="s3_3"><title>3.3. Determination of Bulk Density</title><p>The dried samples were weighed accurately on a weighing balance as (W<sub>d</sub>) after which the test pieces were soaked in a beaker of water of 1000 ml for about seven (7) hours of soaking, the specimens were weighed wet and the wet weight recorded as (W<sub>w</sub>). Each specimen was later suspended in the beaker of water with the aid of a thread and the suspended weight of each specimen was recorded as (W<sub>s</sub>).</p><p>The bulk density was calculated using Equation (2).</p><disp-formula id="scirp.60752-formula1283"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1810164x11.png"  xlink:type="simple"/></disp-formula><p>where B<sub>d</sub> = Bulk Density;</p><p>W<sub>d</sub> = Dried Weight;</p><p>ρ<sub>w</sub> = Density of Water (1 g/cm<sup>3</sup>);</p><p>W<sub>w</sub> = Wet Weight;</p><p>W<sub>s</sub> = Suspended Weight.</p></sec><sec id="s3_4"><title>3.4. Determination of Apparent Porosity</title><p>The specimens were weighed dried (D), immersed in water for seven (7) hours to soak and weighed thereafter as (W). Finally, the specimen was weighed when suspended in water. This was recorded as (S). The apparent porosity (P) was then calculated using Equation (3).</p><disp-formula id="scirp.60752-formula1284"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1810164x12.png"  xlink:type="simple"/></disp-formula></sec><sec id="s3_5"><title>3.5. Determination of Tensile Strength</title><p>The tensile strength test was conducted on a computerized universal testing machine (<xref ref-type="fig" rid="fig5">Figure 5</xref>). The test was conducted in accordance with ASTM D 3039 method. The sample of 120 mm length was clamped into the two jaws of the machine. Each end of the jaws covered 30 mm of the sample. Reading of the tensile strength test in-</p><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> UTS machine sample loaded for tensile</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x13.png"/></fig><p>strument for Newton force and extension were initially set at zero. Tensile stress was applied until the failure of the sample was obtained. Four (4) specimens of each sample have been used for the measurement of the above mechanical properties at ambient laboratory environment and average results are reported.</p></sec><sec id="s3_6"><title>3.6. Determination of Flexural Strength Test</title><p>Flexural Strength of samples was also tested on the computerized universal testing machine (<xref ref-type="fig" rid="fig6">Figure 6</xref>). The three-point bend flexural test was conducted in accordance with ASTM D 790 method. The σbh flexural strength, namely the maximum stress at break, was calculated using the formula.</p><disp-formula id="scirp.60752-formula1285"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1810164x14.png"  xlink:type="simple"/></disp-formula><p>where σbh = Flexural strength;</p><p>F = Breaking force (Newton);</p><p>L = Support distance (mm);</p><p>b = Width of Specimen (mm);</p><p>h = Thickness of Specimen (mm).</p></sec></sec><sec id="s4"><title>4. Results and Discussion</title><sec id="s4_1"><title>4.1. Moisture Content</title><p>The <xref ref-type="fig" rid="fig7">Figure 7</xref> revealed that the percentage moisture content rate for untreated fiber which is 10.36% was the highest among the treated one due the fact that natural fibers exhibits highly hydrophilic properties with the presence of cellulose and lignin compared to the treated.</p></sec><sec id="s4_2"><title>4.2. Hardness Test</title><p>From the graph of micro?hardness against filler loading in <xref ref-type="fig" rid="fig8">Figure 8</xref>, the hardness rate increases as the percentage filler loading increase. Exhibiting a maximum hardness rate at 25% filler loading for all polymer composite except for that of control sample with 44.3 Hv. Still at 25% filler loading, the treated polymer composite for 24 Hrs has the highest hardness rate of 100.2 Hv compared to other polymer samples due to the increase in percentage filler content which results in the highest micro-hardness.</p></sec><sec id="s4_3"><title>4.3. Bulk Density</title><p><xref ref-type="fig" rid="fig9">Figure 9</xref> revealed that the bulk density increased as the filler loading increased except for untreated composite</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> UTS machine Sample loaded for Flexural testing</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x15.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Moisture content variation of Luffa fiber composite</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x16.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Hardness of Luffa fiber composite against filler loading</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x17.png"/></fig><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Bulk density of Luffa fiber composite against filler loading</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x18.png"/></fig><p>which decreased. However, a maximum percentage rate of 2.07 g/cm<sup>3</sup> and 2.47 g/cm<sup>3</sup> for treated composites for 12 Hrs and 24 Hrs respectively at 25% filler loading was also exhibited. While that of untreated composite has 1.31 g/cm<sup>3</sup> at 5% filler loading lower than even the control sample which has 1.35 g/cm<sup>3</sup>. The bulk density measures the change in weight of the composite with respect to the total volume of material where the total volume is the sum of both closed and open pores. Thus, as the filler loading increases, this leads to the closure of internal pores.</p></sec><sec id="s4_4"><title>4.4. Apparent Porosity</title><p>In <xref ref-type="fig" rid="fig1">Figure 1</xref>0, the apparent porosity equally decreases as the filler loading increases except for untreated composite which increases. The favourable percentage rate of apparent porosity exhibited by Luffa fiber composite are that of treated composite (12 Hrs and 24 Hrs) having 0.94% and 0.72% respectively at 25% filler loading higher than the control sample with 0.44%. While that of untreated composite for the same filler loading at 25% had 1.67% due to micro-cracks and non-uniform interfacial interaction of fiber-matrix.</p></sec><sec id="s4_5"><title>4.5. Strength Properties</title><p>Fiber content and fiber strength are influencing parameters for the strength related properties of the composite [<xref ref-type="bibr" rid="scirp.60752-ref13">13</xref>] . <xref ref-type="fig" rid="fig1">Figure 1</xref>1 and <xref ref-type="fig" rid="fig1">Figure 1</xref>2 showed differently the strength variation with different percentage filler loading in tensile and flexural strength respectively. Thus, both figures indicate a gradual increase in both tensile and flexural strength up to 20% fiber content with 15% and 20% exhibiting the highest strength for treated polymer composite improved by the Luffa fiber than that of the control. However, at 25% filler loading there was a decrease in strength in both tensile and flexural strength for treated and untreated polymer composite due to maximum strength had been attained and further addition of fiber content weakened/disrupted the fiber-matrix bond. Similar observations were reported by Imoisili et al. 2012 [<xref ref-type="bibr" rid="scirp.60752-ref14">14</xref>] . They experimented on coconut shell ash on the tensile properties of epoxy composite.</p><fig id="fig10"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>0</label><caption><title> Apparent porosity of Luffa fiber composite against filler loading</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x19.png"/></fig><fig id="fig11"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>1</label><caption><title> Ultimate tensile strength of Luffa fiber composite against filler loading</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x20.png"/></fig><fig id="fig12"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>2</label><caption><title> Flexural strength of Luffa fiber composite against filler loading</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1810164x21.png"/></fig></sec></sec><sec id="s5"><title>5. Conclusion</title><p>The physico-mechanical properties of Luffa aegyptiaca fiber composite were investigated. In general, the treated composite for 24 Hrs showed an improvement by adding modified Luffa fiber as reinforcement. The results of moisture content of the Luffa fiber was reported and it revealed that the untreated fiber showed a higher content of moisture compared to the treated fibers due to the presence of hydroxyl group from cellulose and lignin fiber. However, tensile and flexural properties improved continuously with increasing filler loading up to 20% but decrease at 25% due to weak interfacial bonding for both untreated and treated composite with 20% having the favourable tensile and flexural strength.</p></sec><sec id="s6"><title>Cite this paper</title><p>S. I.Ichetaonye,I. C.Madufor,M. E.Yibowei,D. N.Ichetaonye, (2015) Physico-Mechanical Properties of Luffa aegyptiaca Fiber Reinforced Polymer Matrix Composite. Open Journal of Composite Materials,05,110-117. doi: 10.4236/ojcm.2015.54014</p></sec><sec id="s7"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.60752-ref1"><label>1</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Campbell</surname><given-names> F.C. </given-names></name>,<etal>et al</etal>. (<year>2010</year>)<article-title>Introduction to Composite Material</article-title><source> Structural Composite Materials</source><volume> 1</volume>,<fpage> 1</fpage>-<lpage>29</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.60752-ref2"><label>2</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Jan</surname><given-names> G. </given-names></name>,<etal>et al</etal>. (<year>1990</year>)<article-title>Composite Material Research Laboratory</article-title><source> Advanced Material Science</source><volume> 1</volume>,<fpage> 61</fpage>-<lpage>82</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.60752-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Medraj, M. (2001) Composite Material. MECH. 321 Lecture, Mechanical Engineering Department, Concordia University, Montreal, 1-19.</mixed-citation></ref><ref id="scirp.60752-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">Chawla, K.K. (1998) Composite Materials: Science and Engineering. Springer-Verlag, New York, 380-404.http://dx.doi.org/10.1007/978-1-4757-2966-5</mixed-citation></ref><ref id="scirp.60752-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">David, R. (2000) Introduction to Composite Materials. Massachusetts Institute of Technology, Cambridge, 4, 2, 1-7.</mixed-citation></ref><ref id="scirp.60752-ref6"><label>6</label><mixed-citation publication-type="book" xlink:type="simple">Ebert, L.J. and Wright, P.K. (1999) Mechanical Aspects of the Interface. In: Metcalfe, A.G., Ed., Interfaces in Polymer Matrix Composites, Academic Press, New York, 285.</mixed-citation></ref><ref id="scirp.60752-ref7"><label>7</label><mixed-citation publication-type="other" xlink:type="simple">Gordon, J.E. (2012) The New Science of strong Materials. Penguin Books Limited.</mixed-citation></ref><ref id="scirp.60752-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">Clyne, T.W. and Withers, P.J. (1993) An Introduction to Composites. Cambridge University Press, Cambridge, 43-64.http://dx.doi.org/10.1017/CBO9780511623080</mixed-citation></ref><ref id="scirp.60752-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">Jyoti, P.D. and Mishra, S.C. (2012) Processing and Properties of Natural Fiber-Reinforced Polymer Composite. Journal of Materials, 10, Article ID: 297213.</mixed-citation></ref><ref id="scirp.60752-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">Myrtha, K., Holia, O. and Anung, S. (2007) Physical and Mechanical Properties of Natural Fibers Filled Polypropylene Composites and Its Recycle. Journal of Biological Sciences, 7, 393-396.</mixed-citation></ref><ref id="scirp.60752-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">Mallick, P.K. (2007) Fiber Reinforced Composites. CRC Press, London and New York, 1-15.http://dx.doi.org/10.1201/9781420005981</mixed-citation></ref><ref id="scirp.60752-ref12"><label>12</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Dieter</surname><given-names> H.M. </given-names></name>,<etal>et al</etal>. (<year>2004</year>)<article-title>Improving the Impact Strength of Natural Fiber Reinforced Composites by Specifically Designed Materials and Process Parameters</article-title><source> Irish Naturalist Journal</source><volume> 24</volume>,<fpage> 31 </fpage>-<lpage>38</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.60752-ref13"><label>13</label><mixed-citation publication-type="other" xlink:type="simple">Panneerdhass, P., Gnanavelbabu, A. and Rajkumar, K. (2014) Mechanical Properties of Luffa Fiber and Ground Nut Reinforced Epoxy Polymer Hybred Composites. Procedia Engineering, 97, 2042-2051.</mixed-citation></ref><ref id="scirp.60752-ref14"><label>14</label><mixed-citation publication-type="other" xlink:type="simple">Imoisili, P.E., Ibegbulam, C.M. and Adejugbe, T.I. (2012) Effect of Concentration of Coconut Shell Ash on the Tensile Properties of Epoxy Composites. The Pacific Journal of Science and Technology, 13, 463-468.</mixed-citation></ref></ref-list></back></article>