<?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">MSA</journal-id><journal-title-group><journal-title>Materials Sciences and Applications</journal-title></journal-title-group><issn pub-type="epub">2153-117X</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/msa.2014.514109</article-id><article-id pub-id-type="publisher-id">MSA-52814</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>
 
 
  Microscopic Characterisation of &lt;i&gt;Pinus sylvestris&lt;/i&gt; Cell Structures under Compression Loading
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>zgi</surname><given-names>Günay</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Hamad</surname><given-names>Golmohammadi</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>Şükrü</surname><given-names>Tayfun Kaya</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>TCDD High Speed Train District Office, Alt?ndag, Ankara, Turkey </addr-line></aff><aff id="aff1"><addr-line>Mechanical Engineering Department, Gazi University, Ankara, Turkey</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>ezgigunay@gazi.edu.tr(ZG)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>03</day><month>12</month><year>2014</year></pub-date><volume>05</volume><issue>14</issue><fpage>1060</fpage><lpage>1073</lpage><history><date date-type="received"><day>11</day>	<month>September</month>	<year>2014</year></date><date date-type="rev-recd"><day>8</day>	<month>October</month>	<year>2014</year>	</date><date date-type="accepted"><day>24</day>	<month>November</month>	<year>2014</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 study is mainly focused on the 3D mechanical cell deformations of 20 &#215; 20 &#215; 60 mm sized softwood specimens under 35 - 40 MPa compression loading at room temperature of 20?C. The moisture content of the specimens was 6% - 7%. The data of microscopic images were measured and compared in terms of the permanently degenerated individual cell structures each in micro-scale . 3D cell deformations of tissues were observed with a magnification of (&#215;100) - (&#215;1500) and in the range of 3.0 - 5.0 kV voltage under the SEM microscope. The specimens were examined under magnification and photographed before and after the compression loading applied parallel to the grain angles to the wood samples. Specimens were painted with gold liquid (12 &#215; 12 &#215; 12 mm sized specimens) in obtaining the SEM images. Under the SEM, these specimens were photographed and lengths between the cell walls ranged between 15 to 40 micrometers. In this study, relative deformations of pinewood cells were determined statistically considering the percentage permanent deformation under the compression loading. It was performed by using knowledge of structural mechanics, considering the measurement of permanent deformation in honeycomb-pinewood structure material. 
 
</p></abstract><kwd-group><kwd>Biomechanics</kwd><kwd> Nano-Composites</kwd><kwd> Micromechanics</kwd><kwd> &lt;i&gt;Pinus  sylvestris&lt;/i&gt; L.</kwd><kwd> Compression Loading</kwd><kwd> Cell Deformation</kwd><kwd> SEM</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Reviewing the literature, a study on axial compression tests was performed on samples of Norway spruce wood with different orientations of the annual rings relative to the load direction performed to obtain the stress-strain measurement results. The results of this study showed us that permanent deformation in honeycomb-pinewood exhibited a nonlinear mechanical behavior [<xref ref-type="bibr" rid="scirp.52814-ref1">1</xref>] .</p><p>According to the results of another study, a micromechanical model was developed in which shear modulus was related to the density gradient of the annual ring. The purpose of this study was to understand the low transverse shear modulus in spruce. A hexagonal honeycomb model in the transverse spruce softwood plane was combined with finite element analysis, so that local shear strains were modeled. Testing procedures on a spruce sample were performed in terms of shear to determine the strain profile at the annual ring scale as a function of radial position [<xref ref-type="bibr" rid="scirp.52814-ref2">2</xref>] .</p><p>In another study, the proportion of bending and stretching deformation associated with different cases were investigated considering the important parameters including cell shape angle, relative density and cell wall modulus. A two-phase wood model is introduced based on a layered early wood and latewood material. In place of a one-phase model, a two-phase model was developed based on two different regions with constant densities of early wood and latewood. Each of the two regions was two honeycombs, and the free parameters of the two honeycombs (cell wall modulus and cell shape angle) were determined using a fitting procedure to global experimental data for wood. The resulting values for cell wall modulus and cell shape angle were then compared with previously reported data. The predicted cell shape angle was 12.5˚, which was in good agreement with experimental observations. The resulting average cell wall modulus is 20.5 GPa [<xref ref-type="bibr" rid="scirp.52814-ref3">3</xref>] .</p><p>A research made on the mechanical properties of a few common porous materials: carbon rods, ceramics, polymeric foams and bricks were performed by experimental and analytical methods. The characterization of pore structures was performed using a Mercury Porosimeter technique. Using this technique, detailed information was obtained on the density, porosity, surface area and pore size distribution. Scanning Electron Microscopy (SEM) with an image analyzer was employed to determine the porosity of foams. A large number of experiments were conducted with either bending or compression setup and their macro-mechanical properties such as Young’s modulus, hardness and strength were obtained [<xref ref-type="bibr" rid="scirp.52814-ref4">4</xref>] .</p><p>Another research evaluates in parallel wood fibers and plant fibers to highlight their similarities and differences regarding their use as reinforcement in composites [<xref ref-type="bibr" rid="scirp.52814-ref5">5</xref>] .</p><p>Fratzl, Burgert and Keckes studied on the molecular mechanisms and its responsibility for the deformation of wood, as well as the mechanical interaction of cell-wall components, such as cellulose, lignin and hemicelluloses, which were not well understood. In a recently published experiment, they have shown that wood foils and single cells of compression wood of spruce (Picea abies [L.] Karst.) could deform permanently under tensile load via a stick and slip mechanism at the molecular level occurring during shear of the matrix between cellulose micro fibrils [<xref ref-type="bibr" rid="scirp.52814-ref6">6</xref>] .</p><p>Wood foils and fibers of compression wood of spruce (Picea abies [L.] Karst.) were investigated in cyclic tensile tests in laboratory condition. Additionally, wood foils and fibers were strained in a tensile stage while simultaneously monitoring stress response and collecting X-ray diffraction pattern (XRD) by using a two-di- mensional detector. It was found that micro fibril angle decreased in the cell wall while stretching. The cyclic load tests indicated a recovery mechanism after irreversible deformation, which was interpreted as a stick-and- slip mechanism on the molecular level of the cell wall [<xref ref-type="bibr" rid="scirp.52814-ref7">7</xref>] .</p><p>The irreversible behavior of wood cell-walls has been investigated by means of a finite element-based computational multi scale approach. A finite strain three-scale model has been proposed where the overall response of the cell-wall composite was obtained by the computational homogenization of a Representative Volume Element (RVE) of cell-wall material, whose mechanical response prediction, in turn, was described by the computational homogenization of a cellulose core-RVE [<xref ref-type="bibr" rid="scirp.52814-ref8">8</xref>] .</p><p>The 3D micromechanical analytical-computational model of softwood, which takes into account the wood microstructures at four scale levels, from micro fibrils to annual rings, is developed [<xref ref-type="bibr" rid="scirp.52814-ref9">9</xref>] . They showed that comparison of the single phase models, the two-phase model gave much more accurate transverse anisotropic predictions. In another study, the microscopic investigation of the lumen shape and tracheid shape for compression wood together with the method uses the Fast Fourier Transform (FFT); a reduction of the two-dimensional image data to one-dimensional data was obtained [<xref ref-type="bibr" rid="scirp.52814-ref10">10</xref>] .</p><p>In this research, the Pinus Sylvestris L. (acronym: P. Sylvestris) pinewood specimen was examined in both macro mechanical and micromechanical aspects by using the scanning electron microscopy (SEM). In the macro mechanical review step, axial compression tests were performed on wood samples with parallel annual ring orientations relative to the load direction in obtaining the stress-strain measurement results. In the micromechanical review step, the change of shapes of the tracheid cell walls and sieve-plate structural parts were examined by comparing the SEM images obtained from unloaded and loaded specimens.</p></sec><sec id="s2"><title>2. Macromechanical Studies</title><p>Compression tests were conducted by Dartec tensile test machine (<xref ref-type="fig" rid="fig1">Figure 1</xref>(a)) in laboratory conditions [<xref ref-type="bibr" rid="scirp.52814-ref11">11</xref>] . Test specimens of pinewood in size 20 &#215; 20 &#215; 60 mm were prepared ((a &#215; a &#215; h) (<xref ref-type="fig" rid="fig1">Figure 1</xref>(b) &amp; <xref ref-type="fig" rid="fig1">Figure 1</xref>(c)). These specimens were prepared by cutting pieces from the tree trunk in such a way that the fiber directions of the specimens extending along with the parallel direction to the longer side of them (h = 60 mm, <xref ref-type="fig" rid="fig1">Figure 1</xref>(c)).</p><p>On the pinewood specimens the compression tests were applied and normal strain data was gathered with strain gages that affixed to two neighboring face of the specimens (<xref ref-type="fig" rid="fig1">Figure 1</xref>(d) &amp; <xref ref-type="fig" rid="fig1">Figure 1</xref>(e)).</p><p>Then the specimens were separated into two categories. The first category was the wood grain orientations situated parallel to the loading direction. The second category was the perpendicular situated wood grain orientations to the loading direction. Our study was performed considering the first category and the experimental results obtained from macro scale were used in understanding the micromechanical behavior of wood cells under compression.</p><p>The samples were placed in such a way that not to slip during the pressure application. Compression testing was started from scratch, enhanced with specific steps and the experiment was terminated when the stress reached to the available maximum stress levels. Maximum applicable stress levels and the corresponding developed strains measured by using strain gauges were presented in <xref ref-type="fig" rid="fig2">Figure 2</xref> and <xref ref-type="table" rid="table1">Table 1</xref>.</p><p>The ninth experiment among the performed eighteen experiments was chosen for studying under SEM and according to the results of microscopic investigation, two slope lines were plotted starting from the origin</p><fig-group id="fig1"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> (a) Testing machine DARTEC; (b)-(e) (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x13.png" xlink:type="simple"/></inline-formula>19.98 &#180; 20.30 &#180; 50.4 mm) sized pinewood (P. Sylvestris) specimen attached with two strain gauges; (f) Samples cut in 12 &#180; 12 &#180; 12 mm sized and painted with gold liquid for SEM examination.</title></caption><fig id ="fig1_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x7.png"/></fig><fig id ="fig1_2"><label> (c)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x8.png"/></fig><fig id ="fig1_3"><label>(d)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x9.png"/></fig><fig id ="fig1_4"><label> (e)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x10.png"/></fig><fig id ="fig1_5"><label> (f)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x11.png"/></fig><fig id ="fig1_6"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x12.png"/></fig></fig-group><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Compression test results of the (P. Sylvestris) pinewood specimen</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x14.png"/></fig><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Summary of compression test specimen properties and data of the original and modified slope lines</title></caption><table><tbody><thead><tr><th align="center" valign="middle"  colspan="3"  >Experimental Data</th></tr></thead><tr><td align="center" valign="middle" >Geometric Properties of Wood Specimen-Size</td><td align="center" valign="middle" >Measured Data Specifications</td><td align="center" valign="middle" >Magnitude</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x15.png" xlink:type="simple"/></inline-formula>: Undeformed length (mm): 50.40</td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x16.png" xlink:type="simple"/></inline-formula>: Original slope of stress-strain data obtained from gauge_1 (GPa)<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x17.png" xlink:type="simple"/></inline-formula>: Modified slope of stress-strain data obtained from gauge_1 (GPa)</td><td align="center" valign="middle" >5.08 4.83</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x18.png" xlink:type="simple"/></inline-formula>: Deformed length (mm): 50.31</td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x19.png" xlink:type="simple"/></inline-formula>: Original slope of stress-strain data obtained from gauge_2 (GPa)<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x20.png" xlink:type="simple"/></inline-formula>: Modified slope of stress-strain data obtained from gauge_1 (GPa)</td><td align="center" valign="middle" >7.01 6.66</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x21.png" xlink:type="simple"/></inline-formula>: Undeformed thickness_1 (mm): 19.98</td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x22.png" xlink:type="simple"/></inline-formula>: Orientation of stress-strain curve obtained from for gauge_1<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x23.png" xlink:type="simple"/></inline-formula>: Modified orientation of stress-strain curve obtained from for gauge_1</td><td align="center" valign="middle" >78.87˚ 74.92˚</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x24.png" xlink:type="simple"/></inline-formula>: Deformed thickness_1 (mm): 19.98</td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x25.png" xlink:type="simple"/></inline-formula>: Orientation of the curve stress-strain curve obtained from gauge_2<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x26.png" xlink:type="simple"/></inline-formula>: Modified orientation of stress-strain curve obtained from for gauge_1</td><td align="center" valign="middle" >81.877˚ 77.78˚</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x27.png" xlink:type="simple"/></inline-formula>: Undeformed thickness_2 (mm): 20.30</td><td align="center" valign="middle" >Applied maximum stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x28.png" xlink:type="simple"/></inline-formula> (MPa) and measured corresponding strain <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x29.png" xlink:type="simple"/></inline-formula> from gauge_1</td><td align="center" valign="middle" >−37.01 −7.48E−3</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x30.png" xlink:type="simple"/></inline-formula>: Deformed thickness_2 (mm): 20.31</td><td align="center" valign="middle" >Applied maximum stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x31.png" xlink:type="simple"/></inline-formula> (MPa) and measured corresponding strain <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x32.png" xlink:type="simple"/></inline-formula> from gauge_2</td><td align="center" valign="middle" >−40.79 −5.5E−3</td></tr><tr><td align="center" valign="middle" >Cross sectional area (mm<sup>2</sup>): 405.59</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x33.png" xlink:type="simple"/></inline-formula>: Initial volume (mm<sup>3</sup>): 20.44</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x34.png" xlink:type="simple"/></inline-formula>: Final volume (mm<sup>3</sup>): 20.41</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td></tr></tbody></table></table-wrap><p>through the two stress-strain curves. By the application of maximum stresses<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x35.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x36.png" xlink:type="simple"/></inline-formula> to the specimen, two different strain values were obtained on the two adjacent faces. <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x37.png" xlink:type="simple"/></inline-formula>value was obtained from strain gauge_1 and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x38.png" xlink:type="simple"/></inline-formula> was obtained from strain gauge_2 as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>.</p><p>The first stress strain curve represents the data obtained with the “G1-gauge_1” measurements. The second curve seen on the same graph represents the instantaneously measured data obtained with the “G2-gauge_2” (second gauge) which was located on the adjacent surface of the specimen. Slopes of the two stress-strain curves were determined as <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x39.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x40.png" xlink:type="simple"/></inline-formula> respectively. The approximate yield stress value of a specimen was determined by using the 5% offset principle on the related stress-strain diagram. These two offset new lines generates the other two modified slope angles as; <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x41.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x42.png" xlink:type="simple"/></inline-formula> (<xref ref-type="table" rid="table1">Table 1</xref>). These straight lines were used to define the first physically failure point of the wood structure under compression. Beside these slope lines, another slope line was drawn by 95% reduction of the original slope line which were referred as the offset lines and the corresponding angle was <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x43.png" xlink:type="simple"/></inline-formula> as previously mentioned. These second slopes were defined as the modified slopes and their lines cut the stress-strain curves at the definite points which define the yielding values of the material <xref ref-type="fig" rid="fig2">Figure 2</xref>. As shown in <xref ref-type="fig" rid="fig2">Figure 2</xref> and <xref ref-type="table" rid="table2">Table 2</xref>, yield stress values were found as <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x44.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x45.png" xlink:type="simple"/></inline-formula>. The other critical stress values obtained from two strain gauges were <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x45.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x46.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x45.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x46.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x47.png" xlink:type="simple"/></inline-formula> respectively.</p></sec><sec id="s3"><title>3. Micromechanical Studies</title><p>The specimen chosen for investigation was divided into three equal (12 &#215; 12 &#215; 12 mm) cubic shape parts in order to visualize each of the six faces microscopically (<xref ref-type="fig" rid="fig1">Figure 1</xref>(f)). They were painted with gold liquid for SEM examination. The moisture content of the specimens was 6% - 7%. SEM microscopy was used in examination of cell structures of the uncompressed and the compressed wood samples. Selected sample images of the microscopic views were used for detail examination and for detection of the physical changes caused by the load compression to the cell walls and sieve-plates.</p><p>A living plant cell consists of two primary domains: the protoplast and the cell wall (<xref ref-type="fig" rid="fig4">Figure 4</xref>). The protoplast is the sum of the living contents that are bounded by the cell membrane (<xref ref-type="fig" rid="fig3">Figure 3</xref>(a)-(b), <xref ref-type="fig" rid="fig3">Figure 3</xref>(d)). The cell wall is a non-living, largely carbohydrate matrix extruded by the protoplast to the exterior of the cell membrane. The plant cell wall protects the protoplast from osmoticlysis and often provides mechanical support to the plant at large [<xref ref-type="bibr" rid="scirp.52814-ref12">12</xref>] -[<xref ref-type="bibr" rid="scirp.52814-ref15">15</xref>] (<xref ref-type="fig" rid="fig4">Figure 4</xref>).</p><p>Wood fiber is composed of layers of crystalline cellulose (fibrils) wrapped in a cylindrical shape with an open center, or “lumen” (<xref ref-type="fig" rid="fig3">Figure 3</xref>(b)). Wood fiber is broken down into five distinct layers and is referred to as layers ML, P, S1, S2, and S3. The fibrils in the “S2” layer form the major strength-producing portion of the wood fiber [<xref ref-type="bibr" rid="scirp.52814-ref16">16</xref>] -[<xref ref-type="bibr" rid="scirp.52814-ref18">18</xref>] (<xref ref-type="fig" rid="fig5">Figure 5</xref>).</p><p>In this research, deformation of the cell walls and sieve-plates were explained according to the applied compression loading. The measured cell wall and sieve-plate sizes were obtained from the SEM images (<xref ref-type="fig" rid="fig4">Figure 4</xref>, <xref ref-type="fig" rid="fig6">Figure 6</xref>), and all of the related data summarized in <xref ref-type="table" rid="table3">Table 3</xref>.</p></sec><sec id="s4"><title>4. Results and Discussions</title><p>The results of our study could be assessed separately according to the macro mechanical and micromechanical</p><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Properties of the stress-strain curves of the specimen under compression loading</title></caption><table><tbody><thead><tr><th align="center" valign="middle"  rowspan="2"  ></th><th align="center" valign="middle"  colspan="8"  >Compression Loading Parallel to the Grains</th></tr></thead><tr><td align="center" valign="middle"  colspan="6"  >The Slope Lines Cross the Stress-Strain Curve at Definite Points</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" ></td><td align="center" valign="middle"  colspan="2"  >(1)</td><td align="center" valign="middle"  colspan="2"  >(2)</td><td align="center" valign="middle"  colspan="2"  >(3)</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x48.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x49.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x50.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x51.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x52.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x53.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x54.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x55.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x56.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x57.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x58.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x59.png" xlink:type="simple"/></inline-formula> Modified Slope</td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x60.png" xlink:type="simple"/></inline-formula> Stress-Strain Curve</td></tr><tr><td align="center" valign="middle" >Gauge-1</td><td align="center" valign="middle" >−4.08</td><td align="center" valign="middle" >−</td><td align="center" valign="middle" >−</td><td align="center" valign="middle" >−</td><td align="center" valign="middle" >−</td><td align="center" valign="middle" >−</td><td align="center" valign="middle" >−24.82</td><td align="center" valign="middle" >−37.007</td></tr><tr><td align="center" valign="middle" >Gauge−2</td><td align="center" valign="middle" >−35.00</td><td align="center" valign="middle" >−4.70</td><td align="center" valign="middle" >−</td><td align="center" valign="middle" >−</td><td align="center" valign="middle" >−</td><td align="center" valign="middle" >−</td><td align="center" valign="middle" >−24.82</td><td align="center" valign="middle" >−40.787</td></tr></tbody></table></table-wrap><table-wrap-group id="3"><label><xref ref-type="table" rid="table3">Table 3</xref></label><caption><title> The measured dimensional values of the pinewood specimen</title></caption><table-wrap id="3_1"><table><tbody><thead><tr><th align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x61.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle"  colspan="2"  >Loaded specimen (&#181;m)</th><th align="center" valign="middle"  colspan="2"  >Unloaded specimen (&#181;m)</th></tr></thead><tr><td align="center" valign="middle"  rowspan="2"  >1</td><td align="center" valign="middle" >sp-w</td><td align="center" valign="middle" >4.00</td><td align="center" valign="middle" >sp-w</td><td align="center" valign="middle" >5.63 5.64</td></tr><tr><td align="center" valign="middle" >sp-h</td><td align="center" valign="middle" >3.21</td><td align="center" valign="middle" >sp-h</td><td align="center" valign="middle" >2.43 2.61</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >2</td><td align="center" valign="middle" >sp-w</td><td align="center" valign="middle" >3.56</td><td align="center" valign="middle" >sp-w</td><td align="center" valign="middle" >6.92 8.04</td></tr><tr><td align="center" valign="middle" >sp-h</td><td align="center" valign="middle" >2.54</td><td align="center" valign="middle" >sp-h</td><td align="center" valign="middle" >3.85 3.47</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >3</td><td align="center" valign="middle" >sp-w</td><td align="center" valign="middle" >4.91</td><td align="center" valign="middle" >sp-w</td><td align="center" valign="middle" >5.43 5.64 6.92</td></tr><tr><td align="center" valign="middle" >sp-h</td><td align="center" valign="middle" >3.60</td><td align="center" valign="middle" >sp-h</td><td align="center" valign="middle" >2.43 3.47 3.85</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x62.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle"  colspan="2"  >Loaded specimen dimension (&#181;m)</td><td align="center" valign="middle"  colspan="2"  >Unloaded specimen dimension (&#181;m)</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >1</td><td align="center" valign="middle" >cw</td><td align="center" valign="middle" >39.9</td><td align="center" valign="middle" >cw</td><td align="center" valign="middle" >15.6</td></tr><tr><td align="center" valign="middle" >ch</td><td align="center" valign="middle" >14.7</td><td align="center" valign="middle" >ch</td><td align="center" valign="middle" >13.7</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >2</td><td align="center" valign="middle" >cw</td><td align="center" valign="middle" >42.7 33.6</td><td align="center" valign="middle" >cw</td><td align="center" valign="middle" >20.2</td></tr><tr><td align="center" valign="middle" >ch</td><td align="center" valign="middle" >51.0 30.8</td><td align="center" valign="middle" >ch</td><td align="center" valign="middle" >9.34</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >3</td><td align="center" valign="middle" >cw</td><td align="center" valign="middle" >23.7 32.8 33.3</td><td align="center" valign="middle" >cw</td><td align="center" valign="middle" >18.6</td></tr><tr><td align="center" valign="middle" >ch</td><td align="center" valign="middle" >38.2 47.9 47.6 47.9</td><td align="center" valign="middle" >ch</td><td align="center" valign="middle" >19.2</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >4</td><td align="center" valign="middle" >cw</td><td align="center" valign="middle" >24.0 27.7 26.0</td><td align="center" valign="middle" >cw</td><td align="center" valign="middle" >38.5 37.2 36.9 38.1</td></tr><tr><td align="center" valign="middle" >ch</td><td align="center" valign="middle" >44.2 28.5 11.5</td><td align="center" valign="middle" >ch</td><td align="center" valign="middle" >36.5 37.2 36.3 40.0</td></tr></tbody></table></table-wrap><table-wrap id="3_2"><table><tbody><thead><tr><th align="center" valign="middle"  rowspan="2"  >5</th><th align="center" valign="middle" >cw</th><th align="center" valign="middle" >21.7 20.3 21.6 22.1 25.4 23.5</th><th align="center" valign="middle" >cw</th><th align="center" valign="middle" >50.0 45.0 25.0 25.0 25.0</th></tr></thead><tr><td align="center" valign="middle" >ch</td><td align="center" valign="middle" >12.2 13.4 12.1 11.0 13.1 15.1</td><td align="center" valign="middle" >ch</td><td align="center" valign="middle" >50.0 45.0 62.0 70.0 50.0</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x63.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle"  colspan="2"  >Loaded specimen dimension (&#181;m)</td><td align="center" valign="middle"  colspan="2"  >Unloaded specimen dimension (&#181;m)</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >1</td><td align="center" valign="middle" >cwt</td><td align="center" valign="middle" >9.7</td><td align="center" valign="middle" >cwt</td><td align="center" valign="middle" >5.0</td></tr><tr><td align="center" valign="middle" >cht</td><td align="center" valign="middle" >7.9</td><td align="center" valign="middle" >cht</td><td align="center" valign="middle" >5.0</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >2</td><td align="center" valign="middle" >cwt</td><td align="center" valign="middle" >5.9</td><td align="center" valign="middle" >cwt</td><td align="center" valign="middle" >7.0</td></tr><tr><td align="center" valign="middle" >cwt</td><td align="center" valign="middle" >5.9</td><td align="center" valign="middle" >cwt</td><td align="center" valign="middle" >7.0</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >3</td><td align="center" valign="middle" >cwt</td><td align="center" valign="middle" >6.15</td><td align="center" valign="middle" >cwt</td><td align="center" valign="middle" >6.0</td></tr><tr><td align="center" valign="middle" >cht</td><td align="center" valign="middle" >10.11</td><td align="center" valign="middle" >cht</td><td align="center" valign="middle" >6.0</td></tr></tbody></table></table-wrap></table-wrap-group><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Microscopic transverse section views of P. Sylvestris. (a) Microscopic images (&#215;1000) of sieve-plates; (b) Microscopic images (&#215;500) of crystalline cellulose (fibrils) wrapped in a cylindrical shape with an open center; (c) The fibril angle Eta <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x68.png" xlink:type="simple"/></inline-formula> is measured as 22˚ on the uncompressed specimen (microscopic image &#215;16); (d) Microscopic images (&#215;750) of cells.</title></caption><fig id ="fig3_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x64.png"/></fig><fig id ="fig3_2"><label>(c)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x65.png"/></fig><fig id ="fig3_3"><label> (d)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x66.png"/></fig><fig id ="fig3_4"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x67.png"/></fig></fig-group><p>aspects. The obtained results were explained as below:</p><p>1) In terms of macroscopic scale; under the maximum stress application of 37 MPa, two different compression strains of −7.5E−3 and −5.5E−3 were obtained (<xref ref-type="fig" rid="fig2">Figure 2</xref>). These two different strain values were measured</p><fig-group id="fig4"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> The general honeycomb views of P. Sylvestris that is composed of tubular fibers shown in transverse section bounded together by a lignin “glue” material: Microscopic views of the P. Sylvestris cells (a) before (&#215;750) and (b) after (&#215;1500) compression test. (a) 5 kV voltage and &#215;750 magnification; (b) 5 kV voltage and &#215;1500 magnification.</title></caption><fig id ="fig4_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x69.png"/></fig><fig id ="fig4_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x70.png"/></fig></fig-group><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> A typical tracheid cell wall [<xref ref-type="bibr" rid="scirp.52814-ref16">16</xref>] </title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x71.png"/></fig><p>(a) (b)</p><p><xref ref-type="fig" rid="fig6">Figure 6</xref>. Images of P. Sylvestris under SEM. (a) Unloaded cell and sieve-plate structures; (b) Loaded cell and sieve-plate structures.</p><p>through two adjacent surfaces of the specimen. The difference between these two strains was calculated as 2.0E−3. This deformation difference can be explained by the different fiber arrangement (fibril angles) located on the two adjacent sides of the specimen. So, the fiber angles or the micro fibril angles in the S2 layer were larger than the S1 layer so that the compression strength and modulus elasticity of this layer was found to be less [<xref ref-type="bibr" rid="scirp.52814-ref19">19</xref>] (<xref ref-type="fig" rid="fig3">Figure 3</xref>(c)). According to these results, the implication is that mechanical compression loading gives two different slope lines instantaneously measured for the modulus of elasticity in compression.</p><p>2) SEM view examinations showed a non-symmetrical arrangement of cells and sieve plates; therefore wood material should be evaluated in anisotropic biocomposite category (<xref ref-type="fig" rid="fig3">Figure 3</xref>(c)).</p><p>3) The obtained volumetric change (dilatation) (<xref ref-type="table" rid="table1">Table 1</xref>) of the compressed specimen was as follows:</p><disp-formula id="scirp.52814-formula34"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/10-7701492x96.png"  xlink:type="simple"/></disp-formula><p>4) Implementation of compression loading to the specimen causes considerable amounts of reduction in width and height of the wood cell in micro scale.</p><p>5) During testing; the maximum compression stress values obtained from two strain gauges ranged between −37 and −42 MPa. In the light of these findings, the results can be evaluated as follows: The contraction rates in the width and height of the cell wall were 14.0% and 27.26% respectively. Secondly; as well as 31.13% average height reduction, a 15.95% average width reduction was detected in the sieve-plate (<xref ref-type="fig" rid="fig7">Figure 7</xref>, <xref ref-type="fig" rid="fig8">Figure 8</xref>).</p><p>6) Compression loading causes significant changes in the height and width dimensions of the cell walls (<xref ref-type="fig" rid="fig9">Figure 9</xref>, <xref ref-type="fig" rid="fig1">Figure 1</xref>0). The cell height and width strain values were calculated in terms of average values as follows:</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Over view of test results for the sieve-plates</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x97.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Over view of test results for the cells</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x98.png"/></fig><fig-group id="fig8"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Comparison of P. Sylvestris cell dimensions under compression: (a) Unloaded cell height/width dimensions; (b) loaded cell height/width dimensions.</title></caption><fig id ="fig8_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x100.png"/></fig><fig id ="fig8_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x99.png"/></fig></fig-group><fig-group id="fig9"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>0</label><caption><title> Comparison of P. Sylvestris cell dimensions under compression: (a) Width changes considering loaded/unloaded cases; (b) Height changes considering loaded/unloaded cases.</title></caption><fig id ="fig9_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x101.png"/></fig><fig id ="fig9_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x102.png"/></fig></fig-group><disp-formula id="scirp.52814-formula35"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/10-7701492x103.png"  xlink:type="simple"/></disp-formula><p>7) The sieve-plate height and width strain values were calculated in terms of average values as follows;</p><disp-formula id="scirp.52814-formula36"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/10-7701492x104.png"  xlink:type="simple"/></disp-formula><p>8) The cell wall average thickness values that obtained by measuring the width and height of the cells after loading were; <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x105.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x105.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x106.png" xlink:type="simple"/></inline-formula> (<xref ref-type="table" rid="table3">Table 3</xref>, <xref ref-type="fig" rid="fig6">Figure 6</xref>(b)). The average wall thickness values of the wood cells before load application were approximately equal to <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x105.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x106.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x107.png" xlink:type="simple"/></inline-formula> (<xref ref-type="table" rid="table3">Table 3</xref>, <xref ref-type="fig" rid="fig3">Figure 3</xref>(d)). To explain this phenomenon, a figure is provided in which the failed cell wall surfaces can be observed (<xref ref-type="fig" rid="fig6">Figure 6</xref>(b)).</p><p>9) The measured average values of the width and height of the cell walls after loading were <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x108.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x108.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x109.png" xlink:type="simple"/></inline-formula> (<xref ref-type="table" rid="table3">Table 3</xref>). The measured average values of the width and height of the cell walls before loading were approximately equal to <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x108.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x109.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x110.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x108.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x109.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x110.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x111.png" xlink:type="simple"/></inline-formula> (<xref ref-type="table" rid="table3">Table 3</xref>). To explain this phenomenon, a figure is provided that the cell wall deformation can be seen easily (<xref ref-type="fig" rid="fig6">Figure 6</xref>(b10)).</p></sec><sec id="s5"><title>5. Conclusions</title><p>This study mainly focused on the 3D-mechanical cell deformations of 20 &#215; 20 &#215; 60 mm sized P. Sylvestris wood specimens under 35 - 40 MPa compression loading at room temperature of 20˚C. The moisture content of the specimens was 6% - 7%. In this research, wood specimens before and after the loading were visualized and photographed under the (Scanning Electron Microscope) SEM. The data of microscopic images were measured and compared in terms of the permanently degenerated individual cell structures each in micro-scale <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/10-7701492x112.png" xlink:type="simple"/></inline-formula> (<xref ref-type="fig" rid="fig1">Figure 1</xref>1, <xref ref-type="fig" rid="fig1">Figure 1</xref>2). It was concluded that a considerable amount of deformation occurred both in cell and sieve-plate dimensions of the wood specimen under compression loading. Beside this conclusion, it was detected that both cell and sieve-plate dimensions showed negative average straining values under mechanical compression loading.</p><p>The average percentage difference between height and width dimension measurements of cells for loaded and unloaded cases were as follows: 1) for loaded case: 57.475%; 2) for unloaded case: 26.592% (<xref ref-type="fig" rid="fig1">Figure 1</xref>3).</p><p>The average percentage difference measured between height and width dimensions of sieve-plates for loaded and unloaded cases were: 1) for loaded case: 33.718%; 2) for unloaded case: 32.938% (<xref ref-type="fig" rid="fig1">Figure 1</xref>4). As a conclusion of our study we can claim that, the largest deformation between the wood-cell and sieve-plates took place within the cell sections of the wood microstructure.</p><fig id="fig10"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>1</label><caption><title> Dimensional comparison of loaded and unloaded cells</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x113.png"/></fig><fig id="fig11"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>2</label><caption><title> Dimensional comparison of loaded and unloaded sieve-plates and cells</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x114.png"/></fig><fig id="fig12"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>3</label><caption><title> The average percentage change of the cells in terms of height and width values for loaded and unloaded cases. (Average changes; loaded: 57.475%, unloaded: 26.592%)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x115.png"/></fig><fig id="fig13"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>4</label><caption><title> The average percentage change of the sieve-plate in terms of height and width values for loaded and unloaded cases. (Average changes; loaded: 33.718%, unloaded: 32.938%)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/10-7701492x116.png"/></fig></sec><sec id="s6"><title>Acknowledgements</title><p>Compression tests were performed in the Mechanics Laboratory, Mechanical Engineering Department Gazi University. SEM microscopic images were obtained in the SEM-Laboratory of Biology Department, Science Faculty, Gazi University. We also owe thanks to Professor S. Candan, N. &#214;zyurt, D. Amutkan for providing the SEM laboratory. The macromechanical aspect of our study was supported by Gazi University Scientific Research Projects Department with Grant Ref No: 6/2006-07.</p></sec><sec id="s7"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.52814-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Miksic, A., Myntti, M., Koivisto, J., Salminen, L. and Alava, M. (2013) Effect of Fatigue and Annual Rings’ Orientation on Mechanical Properties of Wood under Cross-Grain Uniaxial Compression. Wood Science and Technology, 47, 1117-1133. http://dx.doi.org/10.1007/s00226-013-0561-8</mixed-citation></ref><ref id="scirp.52814-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Hassel, B.I., Mod&amp;eacute;n, C.S. and Berglund, L.A. (2009) Functional Gradient Effects Explain the Low Transverse Shear Modulus in Spruce Full Field Strain Data and a Micromechanics Model. Composites Science and Technology, 69, 2491-2496. http://dx.doi.org/10.1016/j.compscitech.2009.06.025</mixed-citation></ref><ref id="scirp.52814-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Mod&amp;eacute;n, C.S. and Berglund, L.A. (2008) A Two-Phase Annual Ring Model of Transverse Anisotropy in Softwoods. Composites Science and Technology, 68, 3020-3026. http://dx.doi.org/10.1016/j.compscitech.2008.06.022</mixed-citation></ref><ref id="scirp.52814-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">Lu, G., Lu, G.Q. and Xiao, Z.M. (1999) Mechanical Properties of Porous Materials. Journal of Porous Materials, 6, 359-368. http://dx.doi.org/10.1023/A:1009669730778</mixed-citation></ref><ref id="scirp.52814-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">Madsen, B. and Gamstedt, E.K. (2013) Wood versus Plant Fibers: Similarities and Differences in Composite Applications. Advances in Materials Science and Engineering, 2013, Article ID: 564346.</mixed-citation></ref><ref id="scirp.52814-ref6"><label>6</label><mixed-citation publication-type="other" xlink:type="simple">Fratzl, P., Burgert, I. and Keckes, J. (2004) Mechanical Model for the Deformation of the Wood Cell Wall. Zeitschrift fur Metallkunde Metallurgy &amp; Metallurgical Engineering, 95, 579-584.</mixed-citation></ref><ref id="scirp.52814-ref7"><label>7</label><mixed-citation publication-type="book" xlink:type="simple">Burgert, I., Keckes, J. and Fratzl, P. (2006) Mechanics of the Wood Cell Wall. In: Stokke, D.D. and Groom, L.H., Eds., Characterization of the Cellulosic Cell Wall, Wiley, Grand Lake, 30-37.</mixed-citation></ref><ref id="scirp.52814-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">Flores, E.S., Souza Neto, E.A. and Pearce, S.C. (2011) A Large Strain Computational Multi-Scale Model for the Dissipative Behaviour of Wood Cell-Wall. Computational Materials Science, 50, 1202-1211. 
http://dx.doi.org/10.1016/j.commatsci.2010.11.023</mixed-citation></ref><ref id="scirp.52814-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">Qing, H. and Mishnaevsky Jr., L. (2010) 3D Multiscale Micromechanical Model of Wood: From Annual Rings to Microfibrils. International Journal of Solids and Structures, 47, 1253-1267.  
http://dx.doi.org/10.1016/j.ijsolstr.2010.01.014</mixed-citation></ref><ref id="scirp.52814-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">Mo&amp;euml;ll, M.K. and Minoru Fujita, M. (2004) Fourier Transform Methods in Image Analysis of Compression Wood at the Cellular Level. IAWA Journal, 25, 311-324. http://dx.doi.org/10.1163/22941932-90000368</mixed-citation></ref><ref id="scirp.52814-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">Kaya, S.T. (2007) Determination of the Failure Curve of Transversely Isotropic Fiber Composite Pinewood (Pinus Sylvestris) by the Help of Experimental Studies. M.Sc. Thesis, Gazi University, Institute of Science and Technology, Turkey.</mixed-citation></ref><ref id="scirp.52814-ref12"><label>12</label><mixed-citation publication-type="other" xlink:type="simple">Wiedenhoeft, A. (2014) Structure and Function of Wood: Wood Handbook. Chapter 3, Forest Products Library.  
http://www.fpl.fs.fed.us/documnts/fplgtr/fplgtr190/chapter_03.pdf.htm</mixed-citation></ref><ref id="scirp.52814-ref13"><label>13</label><mixed-citation publication-type="other" xlink:type="simple">Esau, K. (1977) Anatomy of the Seed Plants. 2nd Edition, John Wiley &amp; Sons Ltd, New York.</mixed-citation></ref><ref id="scirp.52814-ref14"><label>14</label><mixed-citation publication-type="other" xlink:type="simple">Raven, P., Evert, R. and Eichhorn, S. (1999) Biology of Plants. 6th Edition, W.H. Freeman &amp; Company, New York.</mixed-citation></ref><ref id="scirp.52814-ref15"><label>15</label><mixed-citation publication-type="other" xlink:type="simple">Dickison, W. (2000) Integrative Plant Anatomy. Academic Press, New York.</mixed-citation></ref><ref id="scirp.52814-ref16"><label>16</label><mixed-citation publication-type="other" xlink:type="simple">C&amp;ocirc;t&amp;eacute;, W.A. (1967) Wood Ultrastructure. University of Washington Press, Seattle.</mixed-citation></ref><ref id="scirp.52814-ref17"><label>17</label><mixed-citation publication-type="other" xlink:type="simple">Josza, L.A. and Middleton, G.R. (1994) Wood Quality Attributes and Their Practical Implications. Forintek Canada Corp., 2655 East Mall, Vancouver BC Canada V6T 1W5.</mixed-citation></ref><ref id="scirp.52814-ref18"><label>18</label><mixed-citation publication-type="other" xlink:type="simple">Logan, J.D. (2014) Sensitivity to Fundamental Wood Properties in the Metriguard Model 7200 HCLT and the CLT.  
http://www.metriguard.com/fiber.htm</mixed-citation></ref><ref id="scirp.52814-ref19"><label>19</label><mixed-citation publication-type="other" xlink:type="simple">Gardiner, B., Barnett, J., Saranpaa, P. and Gril, J. (2014) The Biology of Reaction Wood. (eBook) Springer, London. http://www.springer.com/life+sciences/forestry/book/978-3-642-10813-6</mixed-citation></ref></ref-list></back></article>