<?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.2015.68076</article-id><article-id pub-id-type="publisher-id">MSA-58661</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>
 
 
  Nonlinear Bending of Piezoelectric Cylindrical Shell Reinforced with BNNTs under Electro-Thermo-Mechanical Loadings
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>inhua</surname><given-names>Yang</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>Pengjun</surname><given-names>Zhang</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>School of Civil Engineering and Architecture, Changsha University of Science &amp;amp; Technology, Changsha, China</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>yangjinhua01@tom.com(IY)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>04</day><month>08</month><year>2015</year></pub-date><volume>06</volume><issue>08</issue><fpage>743</fpage><lpage>752</lpage><history><date date-type="received"><day>1</day>	<month>July</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>2</month>	<year>August</year>	</date><date date-type="accepted"><day>7</day>	<month>August</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>
 
 
  Under combined electro-thermo-mechanical loadings, the nonlinear bending of piezoelectric cylindrical shell reinforced with boron nitride nanotubes (BNNTs) is investigated in this paper. By employing nonlinear strains based on Donnell shell theory and utilizing piezoelectric theory including thermal effects, the constitutive relations of the piezoelectric shell reinforced with BNNTs are established. Then the governing equations of the structure are derived through variational principle and resolved by applying the finite difference method. In numerical examples, the effects of geometric nonlinear, voltage, temperature, as well as volume fraction on the deflection and bending moment of axisymmetrical piezoelectric cylindrical shell reinforced with BNNTs are discussed in detail.
 
</p></abstract><kwd-group><kwd>Nonlinear Bending</kwd><kwd> Piezoelectric</kwd><kwd> Cylindrical Shell</kwd><kwd> BNNT</kwd><kwd> Electro-Thermo-Mechanical Loadings</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>BNNTs are similar to CNTs in structure and their extraordinary mechanical properties, but are different in that BNNTs possess higher temperature resistance to oxidation and stronger piezoelectric characteristics. Also, unlike CNTs, BNNTs have stable semiconducting behavior with a large band gaps regardless of radius and chirality of the structure. This property of BNNTs makes them promising candidate materials in a large variety of nanosized electronic and photonic devices. Therefore, BNNTs seem to be more suitable as reinforcement in composite structures due to their high resistance to oxidation at elevated temperatures [<xref ref-type="bibr" rid="scirp.58661-ref1">1</xref>] , outstanding mechanical properties [<xref ref-type="bibr" rid="scirp.58661-ref2">2</xref>] and high thermal conductivity [<xref ref-type="bibr" rid="scirp.58661-ref3">3</xref>] . With the development of science and technology, a new sort of smart nanocomposites, with piezoelectric material as matrix and BNNTs as the reinforcement, has attracted increasing interests in both research and engineering communities. It is noted that the investigations on this new smart nanocomposites are limited in number and most discuss the linear problem. Therefore, it is necessary to do more extensive researches on the nonlinear behavior for this structure.</p><p>At present, most researches are limited to discussing the behavior of piezoelectric structure without reinforce- ment of BNNTs. Yao et al. [<xref ref-type="bibr" rid="scirp.58661-ref4">4</xref>] presented static behaviors of piezoelectric cantilever actuator under large electric field. Shen [<xref ref-type="bibr" rid="scirp.58661-ref5">5</xref>] studied the nonlinear bending for a simply supported, shear deformable cross-ply laminated plate with piezoelectric actuators subjected to a transverse uniform or sinusoidal load combined with electrical loads and in thermal environments. Shegokar et al. [<xref ref-type="bibr" rid="scirp.58661-ref6">6</xref>] deals with the stochastic nonlinear bending response of functionally graded materials beam with surface bonded piezoelectric layers subjected to thermo-electro-mechanical loadings. Narita et al. [<xref ref-type="bibr" rid="scirp.58661-ref7">7</xref>] illustrated an analytical and experimental study of nonlinear bending response and domain wall motion in piezoelectric laminated actuators under electric fields. Beldica et al. [<xref ref-type="bibr" rid="scirp.58661-ref8">8</xref>] analyzed the bending of nonlinear viscoelastic beams with small or large deformations. Yan et al. [<xref ref-type="bibr" rid="scirp.58661-ref9">9</xref>] investigated the time- dependent behavior of a simply supported, angle-ply piezoelectric laminate in cylindrical bending with viscoelastic interfaces. Narita et al. [<xref ref-type="bibr" rid="scirp.58661-ref10">10</xref>] discussed the static electromechanical displacement and polarization switching properties of piezoelectric laminated actuators under three point bending. Using a variational formulation, Li et al. [<xref ref-type="bibr" rid="scirp.58661-ref11">11</xref>] developed a size-dependent functionally graded piezoelectric beam model. Based on the local Petrov- Galerkin approach, Sladek et al. [<xref ref-type="bibr" rid="scirp.58661-ref12">12</xref>] proposed a meshless method for plate bending analysis with functionally graded piezoelectric material properties. Employing Euler-Bernoulli beam theory and the physical neutral surface concept, Fu et al. [<xref ref-type="bibr" rid="scirp.58661-ref13">13</xref>] presented the thermo-piezoelectric buckling, nonlinear free vibration and dynamic stability for the piezoelectric functionally graded beams. None of the above mentioned works have considered the behavior of piezoelectric structure reinforced with BNNTs.</p><p>Recently, some researches about the static buckling of piezoelectric shell reinforced with BNNTs have emerged. Buckling of BNNTs in a PVDF elastic medium subjected to combined electro-thermo-mechanical loadings was investigated by Salehi-Khojin and Jalili [<xref ref-type="bibr" rid="scirp.58661-ref14">14</xref>] who showed that applying direct and reverse voltages to BNNT changed buckling loads for any axial and circumferential wave-numbers. Mosallaie Barzoki et al. [<xref ref-type="bibr" rid="scirp.58661-ref15">15</xref>] studied torsional linear buckling of a PVDF cylindrical shell reinforced by BNNTs with an elastic core under the same loading condition as [<xref ref-type="bibr" rid="scirp.58661-ref14">14</xref>] were investigated, indicating that buckling strength increased substantially as harder foam cores were employed. Using virtual displacement method based on nonlocal cylindrical piezoelasticity continuum shell theory, Arani et al. [<xref ref-type="bibr" rid="scirp.58661-ref16">16</xref>] discussed the axial buckling of double-walled Boron Nitride nanotubes embedded in an elastic medium under combined electro-thermo-mechanical loadings. Up to now, to the best of authors’ knowledge, the research on nonlinear bending of piezoelectric shell reinforced with BNNTs has not been reported in the open literature.</p><p>Motivated by the considerations, we aim to study the nonlinear bending of axisymmetrical piezoelectric shell reinforced with BNNTs under combined electro-thermo-mechanical loadings. Using the difference method in space, the whole problem is resolved by the iteration method. Numerical results in nonlinear deflection and bending moment of axisymmetrical piezoelectric cylindrical shell reinforced with BNNTs are presented for different values of voltage, temperature, volume fraction and so on.</p></sec><sec id="s2"><title>2. Basic Equations</title><p>Consider that a piezoelectric cylindrical shell reinforced with BNNTs has midsurface radius R, thickness h, length L and mass density <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x6.png" xlink:type="simple"/></inline-formula> (see <xref ref-type="fig" rid="fig1">Figure 1</xref>). The shell is referred to the coordinate system (x, y, z) in which x and y are the axial and circumferential directions of the shell and z is in the direction of the inward normal to the middle surface. The origin of the coordinate system is located at the end of the shell on the middle plane. The shell is subjected to transverse static load<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x7.png" xlink:type="simple"/></inline-formula>, applied voltage V and a uniform temperature rise<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x8.png" xlink:type="simple"/></inline-formula>.</p><sec id="s2_1"><title>2.1. Strain Displacement Relationships</title><p>Supposing that <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x9.png" xlink:type="simple"/></inline-formula> denote the axial, circumferential and radial displacement of an arbitrary point on the shell, and the corresponding displacement components of middle surface are <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x10.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x11.png" xlink:type="simple"/></inline-formula>, then the displacement components of piezoelectric cylindrical shell can be written as</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> (a) Geometry of piezoelectric cylindrical shell reinforced with BNNTs; (b) section of cylindrical shell</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-7701648x12.png"/></fig><disp-formula id="scirp.58661-formula631"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x13.png"  xlink:type="simple"/></disp-formula><p>where the inferior mark (,) denotes the partial derivative to variables coordinate.</p><p>Based on classical shell theory with von K&#225;rm&#225;n-Donnell type kinematic relations, the nonlinear strain-dis- placement relations can be expressed as</p><disp-formula id="scirp.58661-formula632"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x14.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x15.png" xlink:type="simple"/></inline-formula> are the strain components on the middle surface and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x16.png" xlink:type="simple"/></inline-formula> are the change values of curvatures on the middle surface, and</p><disp-formula id="scirp.58661-formula633"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x17.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_2"><title>2.2. Constitutive Equations</title><p>The constitutive relationship of a piezoelectric structure under combined mechanical, thermal and electrical loadings can be expressed as follows [<xref ref-type="bibr" rid="scirp.58661-ref15">15</xref>] <sup> </sup></p><disp-formula id="scirp.58661-formula634"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x18.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.58661-formula635"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x19.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x20.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x21.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x22.png" xlink:type="simple"/></inline-formula> represent respectively, thermal expansion coefficient, temperature rise and electric field, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x23.png" xlink:type="simple"/></inline-formula> are elastic constants, piezoelectric constant, dielectric constants, respectively. The material constants of the structure can be calculated using “XY (or YX) rectangle model” [<xref ref-type="bibr" rid="scirp.58661-ref17">17</xref>] . The closed-form formula used in “X model” (or “Y model”) expressing the mechanical, the thermal and the electrical properties of the material are as follows [<xref ref-type="bibr" rid="scirp.58661-ref15">15</xref>] :</p><disp-formula id="scirp.58661-formula636"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x24.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.58661-formula637"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x25.png"  xlink:type="simple"/></disp-formula><p>Superscripts r and m refer to the reinforced and matrix components of the composite, respectively. <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x26.png" xlink:type="simple"/></inline-formula>is the vol% of the reinforced BNNTs in matrix.</p></sec><sec id="s2_3"><title>2.3. Governing Equations</title><p>For the piezoelectric cylindrical shell reinforced with BNNTs, the total potential energy <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x27.png" xlink:type="simple"/></inline-formula> can be written as</p><disp-formula id="scirp.58661-formula638"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x28.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x29.png" xlink:type="simple"/></inline-formula> represents the strain energy and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x30.png" xlink:type="simple"/></inline-formula> represents the work done by the transverse load.</p><p>The expression of the strain energy is</p><disp-formula id="scirp.58661-formula639"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x31.png"  xlink:type="simple"/></disp-formula><p>Considering Equations (4) and (5), as well as the zigzag structure for BNNTs employed here, and the longitudinal arrangement of strips in matrix, makes<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x32.png" xlink:type="simple"/></inline-formula>. Hence, Equation (9) becomes:</p><disp-formula id="scirp.58661-formula640"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x33.png"  xlink:type="simple"/></disp-formula><p>Letting V is the voltage applied on both ends of shell, then</p><disp-formula id="scirp.58661-formula641"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x34.png"  xlink:type="simple"/></disp-formula><p>The work done by the transverse load <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x35.png" xlink:type="simple"/></inline-formula> is</p><disp-formula id="scirp.58661-formula642"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x36.png"  xlink:type="simple"/></disp-formula><p>Applying the variational principle<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x37.png" xlink:type="simple"/></inline-formula>, the nonlinear governing equations of piezoelectric cylindrical shell reinforced with BNNTs can be derived as</p><disp-formula id="scirp.58661-formula643"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x38.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.58661-formula644"><label>, (14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x39.png"  xlink:type="simple"/></disp-formula><p>in which</p><disp-formula id="scirp.58661-formula645"><label>, (15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x41.png"  xlink:type="simple"/></disp-formula><p>In the above equations, the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x43.png" xlink:type="simple"/></inline-formula> are the tensile and bending rigidity and they can be defined as</p><disp-formula id="scirp.58661-formula646"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x44.png"  xlink:type="simple"/></disp-formula><p>Under the axisymmetrical circumstances, the circumferential displacement <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x45.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x45.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x46.png" xlink:type="simple"/></inline-formula> is only the function of coordinate<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x45.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x46.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x47.png" xlink:type="simple"/></inline-formula>. Hence, the second equation of Equation (12) is automatic balance and it can be omitted. Then by Equations (3), (14) and introducing the following dimensionless parameters,</p><disp-formula id="scirp.58661-formula647"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x48.png"  xlink:type="simple"/></disp-formula><p>the nonlinear governing equations of axisymmetrical piezoelectric shell reinforced with BNNTs under electro- thermo-mechanical loadings can be reduced as</p><disp-formula id="scirp.58661-formula648"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x49.png"  xlink:type="simple"/></disp-formula><p>where,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x50.png" xlink:type="simple"/></inline-formula>.</p><p>Supposing the both ends of the shell are clamped, then the dimensionless boundary conditions are respectively as follows:</p><disp-formula id="scirp.58661-formula649"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x51.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.58661-formula650"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x52.png"  xlink:type="simple"/></disp-formula></sec></sec><sec id="s3"><title>3. Solution Methodology</title><p>For seeking the solution of differential Equation (18) with boundary condition (19), the dimensionless displacement functions <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x53.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x54.png" xlink:type="simple"/></inline-formula> are dispersed in time-space domain to obtain their approximate solution.</p><p>Difference method is adopted in space domain. For the disposal of linear item, taking <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x55.png" xlink:type="simple"/></inline-formula> as example, we have</p><disp-formula id="scirp.58661-formula651"><label>(21)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x56.png"  xlink:type="simple"/></disp-formula><p>Referring to difference scheme, the difference expressions of the other linear items in governing equation can be easily achieved.</p><p>Then the nonlinear items of governing equations are linearized and can be written as follows [<xref ref-type="bibr" rid="scirp.58661-ref18">18</xref>] ,</p><disp-formula id="scirp.58661-formula652"><label>(22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x57.png"  xlink:type="simple"/></disp-formula><p>in which <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x58.png" xlink:type="simple"/></inline-formula> is the value of the former iterative. For the primary iteration, secondary extrapolation method is introduced to obtain the value of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x59.png" xlink:type="simple"/></inline-formula>, that is</p><disp-formula id="scirp.58661-formula653"><label>(23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x60.png"  xlink:type="simple"/></disp-formula><p>As for different iterations, the coefficients<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x61.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x61.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x62.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x61.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x62.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x63.png" xlink:type="simple"/></inline-formula> are decided as follows:</p><disp-formula id="scirp.58661-formula654"><label>(24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-7701648x64.png"  xlink:type="simple"/></disp-formula><p>After the equations and conditions are linearized and disposed by using the finite difference method, the nonlinear partial differential equations are transformed into linear algebraical equations expressed by difference schemes. These algebraic equations are solved by using the iteration method. For every step, the iterative lasts until the difference of the present value and the former is smaller than 0.01%, then continues the calculation of the next step.</p></sec><sec id="s4"><title>4. Numerical Results and Discussion</title><p>The nonlinear bending of piezoelectric shell reinforced with BNNTs under electro-thermo-mechanical loadings is investigated in the following calculations. The geometrical parameter of the shell is<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x65.png" xlink:type="simple"/></inline-formula>. The material used for matrix is PVDF and the reinforced material is BNNT. The material constants are listed in <xref ref-type="table" rid="table1">Table 1</xref>. In the following figures (Figures 2-5), the vertical ordinate <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x65.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x66.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x65.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x66.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x67.png" xlink:type="simple"/></inline-formula> are the dimensionless deflection and bending moment of each point on shell along x.</p><p>The effects of geometric nonlinear on the bending of piezoelectric shell reinforced with BNNTs are presented in <xref ref-type="fig" rid="fig2">Figure 2</xref>(a) and <xref ref-type="fig" rid="fig2">Figure 2</xref>(b). The volume fraction<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x68.png" xlink:type="simple"/></inline-formula>, the voltage <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x69.png" xlink:type="simple"/></inline-formula> and the temperature rise<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x69.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x70.png" xlink:type="simple"/></inline-formula>.</p><p>From the two figures, it can be noticed that the dimensionless deflection and bending moment of the shell in linear case is greater than that in nonlinear case, and this phenomenon becomes more evident when the transverse load Q increases. As we know, the linearity case is based on the limited deformation consumption, and the higher order item in the geometric relations is neglected while it is in consideration for the nonlinear case. So in some sense it can be concluded that the linear lowly predicts the stiffness of the structure. In order to reflect the property of the piezoelectric shell reinforced with BNNTs accurately, the consideration of the nonlinear effect is very necessary.</p><p><xref ref-type="fig" rid="fig3">Figure 3</xref> shows the effect of positive and negative voltage on the nonlinear bending of piezoelectric shell reinforced with BNNTs. The volume fraction<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x71.png" xlink:type="simple"/></inline-formula>, the temperature rise <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x71.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x72.png" xlink:type="simple"/></inline-formula> and the mechanical load is taken as<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x71.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x72.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x73.png" xlink:type="simple"/></inline-formula>. From the figure, it is observed that applying negative voltage to BNNT decreases the deflection and bending moment. This is due to the fact that applying negative voltage creates polarization in the BNNT in the longitudinal direction, and leads to its contraction. This makes the structure of BNNT more compact and strong, and correspondingly increases the structure’s stiffness. Therefore, the deflection and bending moment of the structure decrease. <xref ref-type="fig" rid="fig3">Figure 3</xref> also depicts the results of deflection and bending moment when applying positive voltage. As expected, the deflection and bending moment increase compared to normal situation, and the results can be explained using the similar concept as mentioned above.</p><p>The effects of temperature on the nonlinear bending of the shell are presented in <xref ref-type="fig" rid="fig4">Figure 4</xref>. The volume fraction<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x74.png" xlink:type="simple"/></inline-formula>, the voltage <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x75.png" xlink:type="simple"/></inline-formula> and the mechanical load is taken as <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x75.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x76.png" xlink:type="simple"/></inline-formula> in the figure. As can be seen, the deflection as well as the bending moment increases when the temperature increases.</p><p>The effect of volume fraction on the nonlinear bending of piezoelectric shell reinforced with BNNTs is discussed in <xref ref-type="fig" rid="fig5">Figure 5</xref>. The voltage is<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x77.png" xlink:type="simple"/></inline-formula>, the temperature rise is <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x77.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x78.png" xlink:type="simple"/></inline-formula> and the mechanical load is <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x77.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x78.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x79.png" xlink:type="simple"/></inline-formula></p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Mechanical, electrical and thermal properties of PVDF and BNNT</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >PVDF</th><th align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x80.png" xlink:type="simple"/></inline-formula></th></tr></thead><tr><td align="center" valign="middle" >BNNT</td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x81.png" xlink:type="simple"/></inline-formula></td></tr></tbody></table></table-wrap><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Effect of geometric nonlinear on bending of piezoelectric shell reinforced with BNNTs; (a) Deflection of each point along x; (b) Bending moment of each point along x.</title></caption><fig id ="fig2_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-7701648x82.png"/></fig><fig id ="fig2_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-7701648x83.png"/></fig></fig-group><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Effect of voltage on nonlinear bending of piezoelectric shell reinforced with BNNTs; (a) Deflection of each point along x; (b) Bending moment of each point along x.</title></caption><fig id ="fig3_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-7701648x84.png"/></fig></fig-group><fig-group id="fig4"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Effect of temperature on nonlinear bending of piezoelectric shell reinforced with BNNT; (a) Deflection of each point along x; (b) Bending moment of each point along x.</title></caption><fig id ="fig4_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-7701648x85.png"/></fig></fig-group><fig-group id="fig5"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Effect of volume fraction on nonlinear bending of piezoelectric shell reinforced with BNNT. (a) Deflection of each point along x; (b) Bending moment of each point along x.</title></caption><fig id ="fig5_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-7701648x86.png"/></fig></fig-group><p>in this figure. It can be noticed that the deflection and the bending moment decrease when the volume fraction of BNNT in matrix <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x87.png" xlink:type="simple"/></inline-formula> increases. That is due to the fact that the increase of volume fraction would increase the stiffness of the structure, and thus the deflection decreases.</p></sec><sec id="s5"><title>5. Conclusions</title><p>In present study, the governing equations of nonlinear bending are presented for piezoelectric cylindrical shell reinforced with BNNTs under combined electro-thermo-mechanical loadings. Results indicate that some parameters, including geometric nonlinear, voltage, temperature, volume fraction and so on, have significant influence on the deflection and bending moment of the shell. The following conclusions may be drawn from the present work:</p><p>1) The deflection and bending moment of the shell in linear case is greater than that in nonlinear case, and the nonlinear effect enhances when the transverse load <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-7701648x88.png" xlink:type="simple"/></inline-formula> increases.</p><p>2) Applying positive and negative voltage to BNNT leads to increase and decrease of the deflection and bending moment.</p><p>3) The deflection as well as the bending moment increases with the increase of temperature, and decreases when the volume fraction of BNNT in matrix increases.</p></sec><sec id="s6"><title>Acknowledgements</title><p>The work described in this paper was supported by National Natural Science Foundation of China (No: 11102028, 11202038, 11172051) and Research Foundation of Education Bureau of Hunan Province, China (No: 11B005).</p></sec><sec id="s7"><title>Cite this paper</title><p>JinhuaYang,PengjunZhang, (2015) Nonlinear Bending of Piezoelectric Cylindrical Shell Reinforced with BNNTs under Electro-Thermo-Mechanical Loadings. Materials Sciences and Applications,06,743-752. doi: 10.4236/msa.2015.68076</p></sec><sec id="s8"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.58661-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Chen, Y., Zou, J., Campbell, S.J. and Le Caer, G. (2004) Boron Nitride Nanotubes: Pronounced Resistance to Oxidation. Applied Physics Letters, 84, 2430-2432. http://dx.doi.org/10.1063/1.1667278</mixed-citation></ref><ref id="scirp.58661-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Suryavanshi, A.P., Yu, M.F., Wen, J.G., Tang, C.C. and Bando, Y. (2004) Elastic Modulus and Resonance Behavior of Boron Nitride Nanotubes. Applied Physics Letters, 84, 2527-2529. http://dx.doi.org/10.1063/1.1691189</mixed-citation></ref><ref id="scirp.58661-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Terrones, M., Romo-Herrera, J.M., Cruz-Silva, E., López-Urías, F., Mu&amp;ntilde;oz-Sandoval, E., Velázquez-Salazar, J.J., Terrones, H., Bando, Y. and Golberg, D. (2007) Pure and Doped Boron Nitride Nanotubes. Materials Today, 10, 30-38.  
http://dx.doi.org/10.1016/S1369-7021(07)70077-9</mixed-citation></ref><ref id="scirp.58661-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">Yao, L.Q., Zhang, J.G., Lu, L. and Lai, M.O. (2004) Nonlinear Static Characteristics of Piezoelectric Bending Actuators under Strong Applied Electric Field. Sensors and Actuators A: Physical, 115, 168-175.  
http://dx.doi.org/10.1016/j.sna.2004.04.037</mixed-citation></ref><ref id="scirp.58661-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">Shen, H.-S. (2004) Nonlinear Bending Analysis of Unsymmetric Cross-Ply Laminated Plates with Piezoelectric Actuators in Thermal Environments. Composite Structures, 63, 167-177. http://dx.doi.org/10.1016/S0263-8223(03)00145-4</mixed-citation></ref><ref id="scirp.58661-ref6"><label>6</label><mixed-citation publication-type="other" xlink:type="simple">Shegokar, N.L. and Lal, A. (2013) Stochastic Nonlinear Bending Response of Piezoelectric Functionally Graded Beam Subjected to Thermoelectromechanical Loadings with Random Material Properties. Composite Structures, 100, 17-33.  
http://dx.doi.org/10.1016/j.compstruct.2012.12.032</mixed-citation></ref><ref id="scirp.58661-ref7"><label>7</label><mixed-citation publication-type="other" xlink:type="simple">Narita, F., Shindo, Y. and Mikami, M. (2005) Analytical and Experimental Study of Nonlinear Bending Response and Domain Wall Motion in Piezoelectric Laminated Actuators under Electric Fields. Acta Materialia, 53, 4523-4529.  
http://dx.doi.org/10.1016/j.actamat.2005.05.044</mixed-citation></ref><ref id="scirp.58661-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">Beldica, C.E. and Hilton, H.H. (2001) Nonlinear Viscoelastic Beam Bending with Piezoelectric Control-Analytical and Computational Simulations. Composite Structures, 51, 195-203. http://dx.doi.org/10.1016/S0263-8223(00)00139-2</mixed-citation></ref><ref id="scirp.58661-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">Yan, W., Wang, J. and Chen, W.Q. (2014) Cylindrical Bending Responses of Angle-Ply Piezoelectric Laminates with Viscoelastic Interfaces. Applied Mathematical Modelling, 38, 6018-6030. http://dx.doi.org/10.1016/j.apm.2014.05.025</mixed-citation></ref><ref id="scirp.58661-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">Narita, F., Shindo, Y. and Hayashi, K. (2005) Bending and Polarization Switching of Piezoelectric Laminated Actuators under Electromechanical Loading. Computers &amp; Structures, 83, 1164-1170.  
http://dx.doi.org/10.1016/j.compstruc.2004.08.025</mixed-citation></ref><ref id="scirp.58661-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">Li, Y.S., Feng, W.J. and Cai, Z.Y. (2014) Bending and Free Vibration of Functionally Graded Piezoelectric Beam Based on Modified Strain Gradient Theory. Composite Structures, 115, 41-50.  
http://dx.doi.org/10.1016/j.compstruct.2014.04.005</mixed-citation></ref><ref id="scirp.58661-ref12"><label>12</label><mixed-citation publication-type="other" xlink:type="simple">Sladek, J., Sladek, V., Stanak, P., Zhang, C.Z. and Wünsche, M. (2013) Analysis of the Bending of Circular Piezoelectric Plates with Functionally Graded Material Properties by a MLPG Method. Engineering Structures, 47, 81-89.  
http://dx.doi.org/10.1016/j.engstruct.2012.02.034</mixed-citation></ref><ref id="scirp.58661-ref13"><label>13</label><mixed-citation publication-type="other" xlink:type="simple">Fu, Y.M., Wang, J.Z. and Mao, Y.Q. (2012) Nonlinear Analysis of Buckling, Free Vibration and Dynamic Stability for the Piezoelectric Functionally Graded Beams in Thermal Environment. Applied Mathematical Modelling, 36, 4324-4340. http://dx.doi.org/10.1016/j.apm.2011.11.059</mixed-citation></ref><ref id="scirp.58661-ref14"><label>14</label><mixed-citation publication-type="other" xlink:type="simple">Salehi-Khojin, A. and Jalili, N. (2008) Buckling of Boron Nitride Nanotube Reinforced Piezoelectric Polymeric Composites Subject to Combined Electro-Thermo-Mechanical Loadings. Composites Science and Technology, 68, 1489-1501. http://dx.doi.org/10.1016/j.compscitech.2007.10.024</mixed-citation></ref><ref id="scirp.58661-ref15"><label>15</label><mixed-citation publication-type="other" xlink:type="simple">Mosallaie Barzoki, A.A., Arani, A.G., Kolahchi, R. and Mozdianfard, M.R. (2012) Electro-Thermo-Mechanical Torsional Buckling of a Piezoelectric Polymeric Cylindrical Shell Reinforced by DWBNNTs with an Elastic Core. Applied Mathematical Modelling, 36, 2983-2995. http://dx.doi.org/10.1016/j.apm.2011.09.093</mixed-citation></ref><ref id="scirp.58661-ref16"><label>16</label><mixed-citation publication-type="other" xlink:type="simple">Arani, A.G., Amir, S., Shajari, A.R. and Mozdianfard, M.R. (2012) Electro-Thermo-Mechanical Buckling of DWBNNTs Embedded in Bundle of CNTs Using Nonlocal Piezoelasticity Cylindrical Shell Theory. Composites Part B: Engineering, 43, 195-203. http://dx.doi.org/10.1016/j.compositesb.2011.10.012</mixed-citation></ref><ref id="scirp.58661-ref17"><label>17</label><mixed-citation publication-type="other" xlink:type="simple">Tan, P. and Tong, L.Y. (2001) Micro-Electromechanics Models for Piezoelectric-Fiber-Reinforced Composite Materials. Composites Science and Technology, 61, 759-769. http://dx.doi.org/10.1016/S0266-3538(01)00014-8</mixed-citation></ref><ref id="scirp.58661-ref18"><label>18</label><mixed-citation publication-type="other" xlink:type="simple">Fu, Y.M. (1997) Nonlinear Dynamic Analysis of Structures. Jinan University Press, Guangzhou.</mixed-citation></ref></ref-list></back></article>