<?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">WJNSE</journal-id><journal-title-group><journal-title>World Journal of Nano Science and Engineering</journal-title></journal-title-group><issn pub-type="epub">2161-4954</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/wjnse.2015.54020</article-id><article-id pub-id-type="publisher-id">WJNSE-62174</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><subject> Engineering</subject><subject> Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Vibration of Gold Nano-Beam with Variable Young’s Modulus Due to Thermal Shock
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>man</surname><given-names>A. N. Al-Lehaibi</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>Hamdy</surname><given-names>M. Youssef</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Mathematics Department, College of Science and Arts-Sharoura, Najran University, Najran, KSA</addr-line></aff><aff id="aff2"><addr-line>Mechanics Department, Faculty of Engineering, Umm Al-Qura University, Makkah, KSA</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>dremanallehaibi@gmail.com(MANA)</email>;<email>youssefanne2005@gmail.com(HMY)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>13</day><month>11</month><year>2015</year></pub-date><volume>05</volume><issue>04</issue><fpage>194</fpage><lpage>203</lpage><history><date date-type="received"><day>16</day>	<month>November</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>21</month>	<year>December</year>	</date><date date-type="accepted"><day>24</day>	<month>December</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>
 
 
  In this paper, we will study the most important effects in the nano-scale resonator: the coupling effect of temperature and strain rate, and the non-Fourier effect in heat conduction. A solution for the generalized thermoelastic vibration of nano-resonator induced by thermal loading has been developed. The Young’s modulus is taken as a linear function of the reference temperature. The effects of the thermal loading and the reference temperature in all the studied fields have been studied and represented in graphs with some comparisons. The Young’s modulus makes significant effects on all the studied fields where the values of the temperature, the vibration of the deflection, stress, displacement, strain, stress-strain energy increase when the Young’s modulus has taken to be variable.
 
</p></abstract><kwd-group><kwd>Thermoelasticity</kwd><kwd> Euler-Bernoulli Equation</kwd><kwd> Goldnano-Beam</kwd><kwd> Young’s Modulus</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Diao et al. [<xref ref-type="bibr" rid="scirp.62174-ref1">1</xref>] were the first who discussed the effects of the free surfaces on the structure and the elastic properties of the gold nanowires by atomistic simulations. Although the atomistic simulation is a good method to calculate the elastic parameters of the nano-structured materials, it is only used to homogeneous nano-structured materials (e.g., nano-plates, nano-wires, nano-beams, … , etc.) with a finite number of atoms.</p><p>Recently, nano mechanical resonators have attracted considerable attention due to their many applications on technology. The analysis of various effects on the characteristics of resonators, such as the resonant frequencies and the quality factorsis crucial for designing high-performance components. Many authors have studied the vibration and the heat transfer process of nano-beams [<xref ref-type="bibr" rid="scirp.62174-ref2">2</xref>] - [<xref ref-type="bibr" rid="scirp.62174-ref8">8</xref>] . Kidawa [<xref ref-type="bibr" rid="scirp.62174-ref2">2</xref>] studied a problem of transverse vibrations of a beam induced by a mobile heat source. The analytical solution of the problem was obtained by using the Green’s functions method. While, Kidawa did not consider the thermoelastic coupling effect between the governing equations. Boley [<xref ref-type="bibr" rid="scirp.62174-ref3">3</xref>] studied the vibrations of a simply supported rectangular nano-beam affected by a thermal shock distributed along its span. Manolis and Beskos [<xref ref-type="bibr" rid="scirp.62174-ref4">4</xref>] discussed the thermally induced vibration of structures consisting of nano-beams, exposed to rapid surface heating. They have also studied the effects of the damping and the axial loads on the structural response. Al-Huniti et al. [<xref ref-type="bibr" rid="scirp.62174-ref5">5</xref>] investigated the thermally induced displacements and stresses of a rod using the Laplace transforms technique. Ai Kah Soh et al. studied the vibration of micro/nano-scale beam resonators induced by ultra-short-pulsed laser by considering the thermoelastic coupling term in [<xref ref-type="bibr" rid="scirp.62174-ref6">6</xref>] and [<xref ref-type="bibr" rid="scirp.62174-ref7">7</xref>] . The propagation characteristics of the longitudinal wave in nano-plates with small- scale effects are studied by Wang et al. [<xref ref-type="bibr" rid="scirp.62174-ref8">8</xref>] .</p></sec><sec id="s2"><title>2. Variable Young’s Modulus</title><p>The temperature dependence of the Young’s modulus for some materials was measured in the range of 293K and 973 K, using the impulse excitation method and compared with literature data reported. The data could be fitted with [<xref ref-type="bibr" rid="scirp.62174-ref9">9</xref>]</p><disp-formula id="scirp.62174-formula1084"><label>. (1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x6.png"  xlink:type="simple"/></disp-formula><p>The values of parameters E<sub>0</sub> and T<sub>0</sub> are related to the temperature and the parameter B to the harmonic character of the medium.</p><p>Farraro and Rex found that no departure from linearity was detected when they studied the dependency of the Young’s modulus on the temperature, and the get the linear relation [<xref ref-type="bibr" rid="scirp.62174-ref10">10</xref>]</p><disp-formula id="scirp.62174-formula1085"><label>. (2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x7.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x8.png" xlink:type="simple"/></inline-formula> is the Young’s modulus in the standard case and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x9.png" xlink:type="simple"/></inline-formula> is constant, and they measured it for pure Nickel, Platinum, and Molybdenum.</p><p>Now, we will consider the Young’s modulus depends on the temperature by the following function</p><disp-formula id="scirp.62174-formula1086"><label>, (3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x10.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x11.png" xlink:type="simple"/></inline-formula> is constant and</p><disp-formula id="scirp.62174-formula1087"><label>. (4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x12.png"  xlink:type="simple"/></disp-formula><p>In this paper, the non-Fourier effect on heat conduction, and the coupling effect between temperature and strain rate in the nano-scale beam will be studied when Young’s modulus is variable as a function of temperature. A general solution for the generalized thermoelastic vibration of gold nano-beam resonator induced by thermal shock will be developed. Laplace transforms and direct method will be used to get the lateral vibration, the temperature, the displacement, the stress-strain energy of the beam. The effects of Young’s modulus will be studied and represented graphically.</p></sec><sec id="s3"><title>3. Problem Formulation</title><p>Since nano-beams with rectangular cross-sections are easier to fabricate, such cross-sections are commonly adopted in the design of NEMS resonators. Consider small flexural deflections of a thin elastic beam of length</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x13.png" xlink:type="simple"/></inline-formula>, width <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x14.png" xlink:type="simple"/></inline-formula> and thickness<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x15.png" xlink:type="simple"/></inline-formula>, for which the x, y and z-axes are defined</p><p>along the longitudinal, width and thickness directions of the beam, respectively (<xref ref-type="fig" rid="fig1">Figure 1</xref>). In equilibrium, the beam is unstrained, unstressed, without damping mechanism, and the temperature is T<sub>0</sub> everywhere [<xref ref-type="bibr" rid="scirp.62174-ref6">6</xref>] .</p><p>In the present work, the Euler-Bernoulli equation is considered, and then, any plane cross-section, initially perpendicular to the axis of the beam remains plane and perpendicular to the neutral surface during bending. Thus, the displacements are given by [<xref ref-type="bibr" rid="scirp.62174-ref6">6</xref>] [<xref ref-type="bibr" rid="scirp.62174-ref7">7</xref>] :</p><disp-formula id="scirp.62174-formula1088"><label>. (5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x16.png"  xlink:type="simple"/></disp-formula><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Cross-sections in the design of NEMS resonators</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-4400213x17.png"/></fig><p>Thus, the differential equation of thermally induced lateral vibration of the beam may be expressed in the form [<xref ref-type="bibr" rid="scirp.62174-ref6">6</xref>] [<xref ref-type="bibr" rid="scirp.62174-ref7">7</xref>] [<xref ref-type="bibr" rid="scirp.62174-ref11">11</xref>] -[<xref ref-type="bibr" rid="scirp.62174-ref13">13</xref>] :</p><disp-formula id="scirp.62174-formula1089"><label>, (6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x18.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x19.png" xlink:type="simple"/></inline-formula> the density of the beam, E is Young’s modulus, I [= bh<sup>3</sup>/12] the inertial moment about x-axis, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x20.png" xlink:type="simple"/></inline-formula>the coefficient of linear thermal expansion, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x21.png" xlink:type="simple"/></inline-formula>the lateral deflection, x the distance along the length of the beam, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x22.png" xlink:type="simple"/></inline-formula>is the area of the cross section and t the time and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x23.png" xlink:type="simple"/></inline-formula> is the thermal moment as follows [<xref ref-type="bibr" rid="scirp.62174-ref6">6</xref>] [<xref ref-type="bibr" rid="scirp.62174-ref7">7</xref>] [<xref ref-type="bibr" rid="scirp.62174-ref11">11</xref>] -[<xref ref-type="bibr" rid="scirp.62174-ref13">13</xref>] :</p><disp-formula id="scirp.62174-formula1090"><label>, (7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x24.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x25.png" xlink:type="simple"/></inline-formula> is the dynamical temperature increment of the resonator, T(x, z, t) is the temperature distribution, and T<sub>0</sub> the room temperature.</p><p>According to Lord-Shulman model (L-S), the non-Fourier heat conduction equation has the following form [<xref ref-type="bibr" rid="scirp.62174-ref6">6</xref>] [<xref ref-type="bibr" rid="scirp.62174-ref7">7</xref>] [<xref ref-type="bibr" rid="scirp.62174-ref11">11</xref>] -[<xref ref-type="bibr" rid="scirp.62174-ref14">14</xref>] :</p><disp-formula id="scirp.62174-formula1091"><label>, (8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x26.png"  xlink:type="simple"/></disp-formula><p>Where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x27.png" xlink:type="simple"/></inline-formula> is the volumetric strain, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x28.png" xlink:type="simple"/></inline-formula>is the specific heat at constant volume, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x29.png" xlink:type="simple"/></inline-formula>the thermal relaxation time, K the thermal conductivity, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x30.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x31.png" xlink:type="simple"/></inline-formula> is Poisson’s ratio. Where there is no heat flow across the upper and lower surfaces of the beam, so that <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x32.png" xlink:type="simple"/></inline-formula> at <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x33.png" xlink:type="simple"/></inline-formula> For a very thin nano-beam</p><p>and assuming the temperature varies in terms of a <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x34.png" xlink:type="simple"/></inline-formula> function along the thickness direction [<xref ref-type="bibr" rid="scirp.62174-ref6">6</xref>] [<xref ref-type="bibr" rid="scirp.62174-ref7">7</xref>] [<xref ref-type="bibr" rid="scirp.62174-ref11">11</xref>] -[<xref ref-type="bibr" rid="scirp.62174-ref13">13</xref>] , where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x35.png" xlink:type="simple"/></inline-formula>, gives</p><disp-formula id="scirp.62174-formula1092"><label>. (9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x36.png"  xlink:type="simple"/></disp-formula><p>Hence, Equation (6) gives</p><disp-formula id="scirp.62174-formula1093"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x37.png"  xlink:type="simple"/></disp-formula><p>Moreover, Equation (8) gives</p><disp-formula id="scirp.62174-formula1094"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x38.png"  xlink:type="simple"/></disp-formula><p>After doing the integrations, Equation (10) takes the form</p><disp-formula id="scirp.62174-formula1095"><label>. (12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x39.png"  xlink:type="simple"/></disp-formula><p>In Equation (11), we multiply the both sides by z and integrating with respect to z from <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x40.png" xlink:type="simple"/></inline-formula> to<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x41.png" xlink:type="simple"/></inline-formula>, and then</p><p>we obtain</p><disp-formula id="scirp.62174-formula1096"><label>, (13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x42.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x43.png" xlink:type="simple"/></inline-formula>.</p><p>For simplicity, we will use the following dimensionless variables [<xref ref-type="bibr" rid="scirp.62174-ref15">15</xref>] :</p><disp-formula id="scirp.62174-formula1097"><label>. (14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x44.png"  xlink:type="simple"/></disp-formula><p>Then, we have</p><disp-formula id="scirp.62174-formula1098"><label>, (15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x45.png"  xlink:type="simple"/></disp-formula><p>and</p><disp-formula id="scirp.62174-formula1099"><label>, (16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x46.png"  xlink:type="simple"/></disp-formula><p>where</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x47.png" xlink:type="simple"/></inline-formula> ,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x47.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x48.png" xlink:type="simple"/></inline-formula> ,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x47.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x48.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x49.png" xlink:type="simple"/></inline-formula> ,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x47.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x48.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x49.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x50.png" xlink:type="simple"/></inline-formula>.</p><p>For convenience, we dropped the prime.</p></sec><sec id="s4"><title>4. Formulation the Problem in the Laplace Transform Domain</title><p>Applying the Laplace transform for Equations (14) and (15), this is defined by the following formula</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x51.png" xlink:type="simple"/></inline-formula>.</p><p>Hence, we obtain the following system</p><disp-formula id="scirp.62174-formula1100"><label>, (17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x52.png"  xlink:type="simple"/></disp-formula><p>and</p><disp-formula id="scirp.62174-formula1101"><label>. (18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x53.png"  xlink:type="simple"/></disp-formula><p>We will consider the function <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x54.png" xlink:type="simple"/></inline-formula> as follows:</p><disp-formula id="scirp.62174-formula1102"><label>, (19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x55.png"  xlink:type="simple"/></disp-formula><p>Then, we have</p><disp-formula id="scirp.62174-formula1103"><label>, (20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x56.png"  xlink:type="simple"/></disp-formula><p>and</p><disp-formula id="scirp.62174-formula1104"><label>, (21)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x57.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x58.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x59.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x59.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x60.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x59.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x60.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x61.png" xlink:type="simple"/></inline-formula>,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x59.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x60.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x61.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x62.png" xlink:type="simple"/></inline-formula>.</p><p>Consider the first end of the beam x = 0 is clamped and loaded thermally, which gives [<xref ref-type="bibr" rid="scirp.62174-ref6">6</xref>] [<xref ref-type="bibr" rid="scirp.62174-ref7">7</xref>] :</p><disp-formula id="scirp.62174-formula1105"><label>, (22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x63.png"  xlink:type="simple"/></disp-formula><p>and</p><disp-formula id="scirp.62174-formula1106"><label>, (23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x64.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x65.png" xlink:type="simple"/></inline-formula> is constant.</p><p>By using Laplace transform, the conditions will take the forms</p><disp-formula id="scirp.62174-formula1107"><label>, (24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x66.png"  xlink:type="simple"/></disp-formula><p>and</p><disp-formula id="scirp.62174-formula1108"><label>. (25)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x67.png"  xlink:type="simple"/></disp-formula><p>Consider the other end of the beam <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x68.png" xlink:type="simple"/></inline-formula> is clamped and remains at zero increments of temperature as follows:</p><disp-formula id="scirp.62174-formula1109"><label>. (26)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x69.png"  xlink:type="simple"/></disp-formula><p>After using Laplace transform, we have</p><disp-formula id="scirp.62174-formula1110"><label>. (27)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x70.png"  xlink:type="simple"/></disp-formula><p>After some simplifications by using MAPLE programme, we get the final solutions in the Laplace transform domain as follows:</p><p>The lateral deflection</p><disp-formula id="scirp.62174-formula1111"><label>(28)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x71.png"  xlink:type="simple"/></disp-formula><p>The temperature</p><disp-formula id="scirp.62174-formula1112"><label>(29)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x72.png"  xlink:type="simple"/></disp-formula><p>The displacement</p><disp-formula id="scirp.62174-formula1113"><label>(30)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x73.png"  xlink:type="simple"/></disp-formula><p>The Strain</p><disp-formula id="scirp.62174-formula1114"><label>(31)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x74.png"  xlink:type="simple"/></disp-formula><p>where</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x75.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x75.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x76.png" xlink:type="simple"/></inline-formula> are the roots of the equation</p><disp-formula id="scirp.62174-formula1115"><label>, (32)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x77.png"  xlink:type="simple"/></disp-formula><p>and</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x78.png" xlink:type="simple"/></inline-formula> , <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x78.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x79.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x78.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x79.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x80.png" xlink:type="simple"/></inline-formula>.</p></sec><sec id="s5"><title>5. The Stress-Strain Energy</title><p>The stress on the x-axis, according to Hooke’s law is:</p><disp-formula id="scirp.62174-formula1116"><label>. (33)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x81.png"  xlink:type="simple"/></disp-formula><p>By using the non-dimensional variables in (13), we obtain the stress in the form</p><disp-formula id="scirp.62174-formula1117"><label>. (34)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x82.png"  xlink:type="simple"/></disp-formula><p>By using Laplace transform, the above equation takes the form:</p><disp-formula id="scirp.62174-formula1118"><label>. (35)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x83.png"  xlink:type="simple"/></disp-formula><p>The stress-strain energy, which is generated by the beam, is given by</p><disp-formula id="scirp.62174-formula1119"><label>, (36)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x84.png"  xlink:type="simple"/></disp-formula><p>We can re-write Equation (36) to be in the form</p><disp-formula id="scirp.62174-formula1120"><label>, (37)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x85.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x86.png" xlink:type="simple"/></inline-formula>is the inversion of Laplace transform.</p><p>To complete the solution in the Laplace transform domain, we have to determine the type of heating which we have used to load the boundary of the medium thermally.</p><p>We have applied harmonic thermal loading as follows [<xref ref-type="bibr" rid="scirp.62174-ref16">16</xref>] :</p><disp-formula id="scirp.62174-formula1121"><label>, (38)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x87.png"  xlink:type="simple"/></disp-formula><p>after using Laplace transform, we obtain</p><disp-formula id="scirp.62174-formula1122"><label>, (39)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x88.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x89.png" xlink:type="simple"/></inline-formula>is the angular frequency of thermal vibration.</p></sec><sec id="s6"><title>6. Numerical Inversion of the Laplace Transform</title><p>To determine the solutions in the time domain, the Riemann-sum approximation method is used to obtain the numerical results. In this method, any function in Laplace domain can be inverted to the time domain as</p><disp-formula id="scirp.62174-formula1123"><label>(40)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-4400213x90.png"  xlink:type="simple"/></disp-formula><p>where Re is the real part and i is imaginary number unit. For faster convergence, numerous numerical experiments have shown that the value of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x91.png" xlink:type="simple"/></inline-formula> satisfies the relation <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x91.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x92.png" xlink:type="simple"/></inline-formula> Tzou [<xref ref-type="bibr" rid="scirp.62174-ref17">17</xref>] .</p></sec><sec id="s7"><title>7. Numerical Results and Discussion</title><p>Now, we will consider a numerical example for which computational results are given. For this purpose, Gold (Au) is taken as the thermoelastic material for which we take the following values of the different physical constants [<xref ref-type="bibr" rid="scirp.62174-ref18">18</xref>] :</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x93.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x93.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x94.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x93.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x94.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x95.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x93.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x94.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x95.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x96.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x93.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x94.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x95.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x96.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x97.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x93.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x94.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x95.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x96.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x97.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x98.png" xlink:type="simple"/></inline-formula>,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x93.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x94.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x95.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x96.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x97.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x98.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x99.png" xlink:type="simple"/></inline-formula>.</p><p>The aspect ratios of the beam are fixed as <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x100.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x100.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x101.png" xlink:type="simple"/></inline-formula> when h is varied, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x100.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x101.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x102.png" xlink:type="simple"/></inline-formula>and b change accordingly with h.</p><p>For the nano-scale beam, we will take the range of the beam length <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x103.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x103.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x104.png" xlink:type="simple"/></inline-formula>. The original time t will be considered in the picoseconds <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x103.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x104.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x105.png" xlink:type="simple"/></inline-formula> and the relaxation time <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x103.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x104.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x105.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x106.png" xlink:type="simple"/></inline-formula> in the range<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x103.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x104.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x105.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x106.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x107.png" xlink:type="simple"/></inline-formula>.</p><p>The figures (<xref ref-type="fig" rid="fig2">Figure 2</xref>-7) were prepared by using the non-dimensional variables which are defined in (9) for beam length<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x108.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x108.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x110.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x108.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x110.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x109.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x108.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x110.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x109.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-4400213x111.png" xlink:type="simple"/></inline-formula>.</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> The temperature distribution with different cases of Young’s modulus</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-4400213x112.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> The lateral vibration distribution with different cases of Young’s modulus</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-4400213x113.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> The stress distribution with different cases of Young’s modulus</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-4400213x114.png"/></fig><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> The displacement distribution with different cases of Young’s modulus</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-4400213x115.png"/></fig><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> The strain distribution with different cases of Young’s modulus</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-4400213x116.png"/></fig></sec><sec id="s8"><title>8. Conclusion</title><p>The Young’s modulus has significant effects on all the studied fields. The values of the temperature, the vibra-</p><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> The stress-strainenergy distribution with different cases of Young’s modulus</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-4400213x117.png"/></fig><p>tion of the deflection, stress, displacement, strain, stress-strain energy increase when the Young’s modulus is variable. The peak points of all the distributions increase when the Young’s modulus is variable with large differences in the case of Young’s modulus is constant.</p></sec><sec id="s9"><title>Cite this paper</title><p>Eman A. N.Al-Lehaibi,Hamdy M.Youssef, (2015) Vibration of Gold Nano-Beam with Variable Young’s Modulus Due to Thermal Shock. 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