<?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">JAMP</journal-id><journal-title-group><journal-title>Journal of Applied Mathematics and Physics</journal-title></journal-title-group><issn pub-type="epub">2327-4352</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/jamp.2016.411204</article-id><article-id pub-id-type="publisher-id">JAMP-72120</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Nano-Contact Problem with Surface Effects on Triangle Distribution Loading
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Liyuan</surname><given-names>Wang</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>Wei</surname><given-names>Han</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>Shanlin</surname><given-names>Wang</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>Lihong</surname><given-names>Wang</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>Yinping</surname><given-names>Xin</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Regional Circular Economy key Laboratory of Gansu Higher Institutions; Department of Mathematics, Longqiao College of Lanzhou University of Finance and Economics, Lanzhou, China</addr-line></aff><pub-date pub-type="epub"><day>10</day><month>11</month><year>2016</year></pub-date><volume>04</volume><issue>11</issue><fpage>2047</fpage><lpage>2060</lpage><history><date date-type="received"><day>August</day>	<month>29,</month>	<year>2016</year></date><date date-type="rev-recd"><day>Accepted:</day>	<month>November</month>	<year>15,</year>	</date><date date-type="accepted"><day>November</day>	<month>18,</month>	<year>2016</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 work presents a theoretical study of contact problem. The Fourier integral transform method based on the surface elasticity theory is adopted to derive the fundamental solution for the contact problem with surface effects, in which both the surface tension and the surface elasticity are considered. As a special case, the deformation induced by a triangle distribution force is discussed in detail. The results are compared with those of the classical contact problem. At nano-scale, the contributions of the surface tension and the surface elasticity to the stress and displacement are not equal at the contact surface. The surface tension plays a major role to the normal stress, whereas the shear stress is mainly affected by the surface elasticity. In addition, the hardness of material depends strongly on the surface effects. This study is helpful to characterize and measure the mechanical properties of soft materials through nanoindentation.
 
</p></abstract><kwd-group><kwd>Surface Tension</kwd><kwd> Surface Elasticity</kwd><kwd> Nano-Contact Problem</kwd><kwd> Fourier Integral Transforms Method</kwd><kwd> Triangle Distribution Force</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Nowadays, nanometer material and technology have been widely used in industrial and engineering fields. Many new nano-materials have been developed by utilizing the fact that materials begin to exhibit unique mechanical properties at nano-scale, which significantly differ from those at larger scale.</p><p>Nano-indention tests have been widely used to measure such mechanical properties of materials. For micro-nano solids with large surface-to-bulk ratio the significance of surfaces is likely to be important. Form the viewpoint of continuum mechanics, this difference can be described by such concepts as surface effects [<xref ref-type="bibr" rid="scirp.72120-ref1">1</xref>] . This is especially true for nano-scale materials or structures. In such cases, the surface tension and the surface elasticity play a critical role and thus have been adding its appeal to many researchers. For example, Miller and Shenoy [<xref ref-type="bibr" rid="scirp.72120-ref2">2</xref>] probed the size-dependent elastic properties of nano-plates and beams. Hang et al. [<xref ref-type="bibr" rid="scirp.72120-ref3">3</xref>] explained the size dependent phenomenon by the strain gradient continuum theory. Dingreville et al. [<xref ref-type="bibr" rid="scirp.72120-ref4">4</xref>] investigated the surface free energy and its effect on elastic behavior of the nano-sized particles, wires, and films. Yang [<xref ref-type="bibr" rid="scirp.72120-ref5">5</xref>] studied the size-dependent effective modulus of spherical nano- cavities at dilute concentrations. Gao et al. [<xref ref-type="bibr" rid="scirp.72120-ref6">6</xref>] built a simple model to describe the influence of surface stress on the nanoscale adhesive contact. There are a lot of work regarding the surface/interface energy effects on the nanostructures and solids, and we can only include a small part of them here. For more recent developments in this field, the readers can refer to a review article by Wang et al. [<xref ref-type="bibr" rid="scirp.72120-ref7">7</xref>] .</p><p>To study the mechanical behavior of nano-materials, the most celebrated continuum-based surface/interface model was first established by Gurtin, Murdoch and coworkers [<xref ref-type="bibr" rid="scirp.72120-ref8">8</xref>] [<xref ref-type="bibr" rid="scirp.72120-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.72120-ref10">10</xref>] , which known as the theory of surface elasticity. In the study of nano-scale problems, all material constants appearing in that constitutive model were commonly calibrated with data obtained from either experimental measurements [<xref ref-type="bibr" rid="scirp.72120-ref11">11</xref>] or atomistic simulations [<xref ref-type="bibr" rid="scirp.72120-ref2">2</xref>] [<xref ref-type="bibr" rid="scirp.72120-ref12">12</xref>] . Therefore, the surface effect has been widely adopted to investigate the mechanical phenomena at nano-scale. Cammarata et al. [<xref ref-type="bibr" rid="scirp.72120-ref13">13</xref>] considered the size-dependent deformation in thin film with surface effects. Gao et al. [<xref ref-type="bibr" rid="scirp.72120-ref14">14</xref>] developed a finite-element method to account for the effect of surface elasticity. Wang et al. [<xref ref-type="bibr" rid="scirp.72120-ref15">15</xref>] studied to a half-plane subjected to normal pressures with surface tension. Zhao and Rajapakse [<xref ref-type="bibr" rid="scirp.72120-ref16">16</xref>] proposed a continuum-based model to study the influence of surface stresses on mechanical responses of an elastic half-space compressed by an axisymmetric, rigid, frictionless nano-indentor. Long and Wang [<xref ref-type="bibr" rid="scirp.72120-ref17">17</xref>] studied the effect of the residual surface stress on the two dimensional Hertz contact problem, and later Long et al. [<xref ref-type="bibr" rid="scirp.72120-ref18">18</xref>] generalized their work to the three dimensional case. Wang [<xref ref-type="bibr" rid="scirp.72120-ref19">19</xref>] derived the general analytical solution of nano-contact problem with surface effects by using the complex variable function method. Gao et al. [<xref ref-type="bibr" rid="scirp.72120-ref20">20</xref>] [<xref ref-type="bibr" rid="scirp.72120-ref21">21</xref>] derived the influence of the surface stress on the JKR adhesive contact, which is investigated by employing the non-classical Boussinesq fundamental solutions. In this paper, Fourier integral transform method is used to solve the non-classical boundary value problems with surface effects.</p></sec><sec id="s2"><title>2. Problem Description</title><p>Now we consider a material occupying the upper half-plane<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x2.png" xlink:type="simple"/></inline-formula>, we refer to a Cartesian coordinate system (o-xyz), as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>, where the x axis is along the surface and the z axis perpendicular to the surface. It is assumed that the material is subjected to triangle distribution force <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x3.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x4.png" xlink:type="simple"/></inline-formula> over the region<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x5.png" xlink:type="simple"/></inline-formula>. While the normal and shear force form zero (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x6.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x7.png" xlink:type="simple"/></inline-formula>) uniformly increased to maximum <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x8.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x9.png" xlink:type="simple"/></inline-formula> at the point O. The plane-strain conditions are assumed to<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x10.png" xlink:type="simple"/></inline-formula>, and</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Schematic of contact problem under triangle distribution loads</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/7-1720687x11.png"/></fig><p>the contact is assumed to be frictionless.</p><p>The problem statement is to determine the triangle distribution force exerted by the elastic field (e.g., displacement and stresses) with the half-plane for the influence of surface effects.</p></sec><sec id="s3"><title>3. Basic Equations of Surface Elasticity and General Solutions</title><p>In surface elasticity theory, the equilibrium and constitutive equations in the bulk of material are the same as those in classical elastic theory, but the presence of surface stresses gives rise to a non-classical boundary condition.</p><sec id="s3_1"><title>3.1. Basic Equations</title><p>In the absence of body force, the equilibrium equations, constitutive law, and geometry relations in the bulk are as follows</p><disp-formula id="scirp.72120-formula383"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x12.png"  xlink:type="simple"/></disp-formula><p>where G and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x13.png" xlink:type="simple"/></inline-formula> are the shear modulus and Poisson’s ratio of the bulk material, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x14.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x15.png" xlink:type="simple"/></inline-formula> are the stress tensor and strain tensor in the bulk material, respectively.</p><p>The strain tensor is related to the displacement vector <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x16.png" xlink:type="simple"/></inline-formula> by</p><disp-formula id="scirp.72120-formula384"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x17.png"  xlink:type="simple"/></disp-formula><p>On the surface, the generalized Young-Laplace equation [<xref ref-type="bibr" rid="scirp.72120-ref22">22</xref>] , surface constitutive relation and strain-displacement relationship can be expressed as</p><disp-formula id="scirp.72120-formula385"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x18.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72120-formula386"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x19.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x20.png" xlink:type="simple"/></inline-formula> denotes the normal to the surface, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x21.png" xlink:type="simple"/></inline-formula>the curvature tensor of the surface, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x22.png" xlink:type="simple"/></inline-formula>is the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x23.png" xlink:type="simple"/></inline-formula> surface stress tensor on the surface, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x24.png" xlink:type="simple"/></inline-formula>is the stress tensor in the elastic material, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x25.png" xlink:type="simple"/></inline-formula> is the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x26.png" xlink:type="simple"/></inline-formula> surface strain tensor which is equal to the tangential components of the strain tensor of the elastic material on the surface, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x27.png" xlink:type="simple"/></inline-formula>is the residual surface tension under unstrained conditions, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x28.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x29.png" xlink:type="simple"/></inline-formula> are surface Lam&#233; constants which can be determined by atom simulations or experiments [<xref ref-type="bibr" rid="scirp.72120-ref2">2</xref>] .</p></sec><sec id="s3_2"><title>3.2. General Solutions</title><p>Based on previous work by Wang [<xref ref-type="bibr" rid="scirp.72120-ref15">15</xref>] and Wang [<xref ref-type="bibr" rid="scirp.72120-ref23">23</xref>] , Fourier integral transformation method is adopted to solve the stress and displacement components by</p><disp-formula id="scirp.72120-formula387"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x30.png"  xlink:type="simple"/></disp-formula><p>where A and B are generally functions of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x31.png" xlink:type="simple"/></inline-formula> as yet to be determined by boundary conditions.</p></sec></sec><sec id="s4"><title>4. Elastic Solution under Normal Triangle Distribution Force</title><p>As a particular example, let us consider the effect of a normal triangle distribution force <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x32.png" xlink:type="simple"/></inline-formula> over the region<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x33.png" xlink:type="simple"/></inline-formula>, and the normal force form zero (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x34.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x35.png" xlink:type="simple"/></inline-formula>) uniformly increased to maximum <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x36.png" xlink:type="simple"/></inline-formula> (O), while remainder of the boundary <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x37.png" xlink:type="simple"/></inline-formula> being unstressed as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>.</p><p><img data-original="http://html.scirp.org/file/7-1720687x39.png" /><img data-original="http://html.scirp.org/file/7-1720687x38.png" /> (6)</p><p>Due to the surface tension mostly influences the normal stress [<xref ref-type="bibr" rid="scirp.72120-ref20">20</xref>] . Therefore, we keep only the first term in Equation (4). Then, the surface stresses are given by</p><disp-formula id="scirp.72120-formula388"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x40.png"  xlink:type="simple"/></disp-formula><p>On the surface, the boundary conditions (3) can be written by</p><disp-formula id="scirp.72120-formula389"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x41.png"  xlink:type="simple"/></disp-formula><p>Substituting Equation (8) into Equation (5), one obtains</p><disp-formula id="scirp.72120-formula390"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x42.png"  xlink:type="simple"/></disp-formula><p>Due to deformation the radius of curvature of the surface is given by</p><disp-formula id="scirp.72120-formula391"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x43.png"  xlink:type="simple"/></disp-formula><p>By substituting Equations (9) and (10) into the surface condition Equation (8), <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x44.png" xlink:type="simple"/></inline-formula>is determined by</p><disp-formula id="scirp.72120-formula392"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x45.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.72120-formula393"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x46.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72120-formula394"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x47.png"  xlink:type="simple"/></disp-formula><p>where s is a length parameter depending on the surface property and material elastic constants. It should be pointed out that this parameter indicates the thickness size of the zone where the surface effect is significant, and plays a critical role in the surface elasticity. For metals, s is estimated on the order of nanometers.</p><p>Therefore <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x48.png" xlink:type="simple"/></inline-formula> is given by</p><disp-formula id="scirp.72120-formula395"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x49.png"  xlink:type="simple"/></disp-formula><p>Substituting Equation (14) into Equation (5), the stresses component and displaces component are obtained as</p><disp-formula id="scirp.72120-formula396"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x50.png"  xlink:type="simple"/></disp-formula><p>It is seen, when<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x51.png" xlink:type="simple"/></inline-formula>, that is, the surface influence is ignored in Equation (15), the stresses of the half-plane are consistent with those in the classical elastic contact results which is the same result [<xref ref-type="bibr" rid="scirp.72120-ref23">23</xref>] , respectively.</p><disp-formula id="scirp.72120-formula397"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x52.png"  xlink:type="simple"/></disp-formula><p>where</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x53.png" xlink:type="simple"/></inline-formula>.</p><p>On the contact surface (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x54.png" xlink:type="simple"/></inline-formula>), the normal stress is given by</p><disp-formula id="scirp.72120-formula398"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x55.png"  xlink:type="simple"/></disp-formula><p>According to the Saint-Venant’s Principle, we assume that the normal displacement is w specified to be zero at a distance <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x56.png" xlink:type="simple"/></inline-formula> on the contact surface, that is,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x56.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x57.png" xlink:type="simple"/></inline-formula> , the displacement on the surface is derived as</p><disp-formula id="scirp.72120-formula399"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x58.png"  xlink:type="simple"/></disp-formula><p>Assuming that the origin has no displacement in the x direction, that is, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x59.png" xlink:type="simple"/></inline-formula>one obtains</p><disp-formula id="scirp.72120-formula400"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x60.png"  xlink:type="simple"/></disp-formula><p>As show in <xref ref-type="fig" rid="fig2">Figure 2</xref>, the results indicated that the normal stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x61.png" xlink:type="simple"/></inline-formula> is a smooth distribution when the surface tension is considered by at the loading boundary (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x61.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x62.png" xlink:type="simple"/></inline-formula>), However, it is just the reverse with classical results that is the surface tension is ignored (s/a = 0). In addition, the actual normal stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x61.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x62.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x63.png" xlink:type="simple"/></inline-formula> is smaller than the classical value in the loading zone and is larger outside of the zone.</p><p>Due to the different surface tension value, the horizontal displacement is displayed in <xref ref-type="fig" rid="fig3">Figure 3</xref>, where we set<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x64.png" xlink:type="simple"/></inline-formula>, and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x64.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x65.png" xlink:type="simple"/></inline-formula>. It is seen that the horizontal displacement is continuous everywhere on the deformed surface. However, the classical elasticity theory predicted unreasonably that the horizontal displacement is discontinuously at the load boundary<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x64.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x65.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x66.png" xlink:type="simple"/></inline-formula>, as seen from the curve of s/a = 0. The indent depth is plotted in <xref ref-type="fig" rid="fig4">Figure 4</xref> with<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x64.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x65.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x66.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x67.png" xlink:type="simple"/></inline-formula>, which also shows that the slope of the deformed surface is continuous everywhere. It is also found the indent depth decreases with the increase of surface tension.</p></sec><sec id="s5"><title>5. Elastic Solution under Tangential Triangle Distribution Force</title><p>Now, let us consider the effect of a tangential triangle distribution force <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x68.png" xlink:type="simple"/></inline-formula> over the region<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x69.png" xlink:type="simple"/></inline-formula>, while the shears force form zero (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x69.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x70.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x69.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x70.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x71.png" xlink:type="simple"/></inline-formula>) uniformly increased to maximum <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x69.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x70.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x71.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x72.png" xlink:type="simple"/></inline-formula> at the point O, while remainder of the boundary <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x69.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x70.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x71.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x72.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x73.png" xlink:type="simple"/></inline-formula> being unstressed as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>.</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> The distribution of contact normal stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x75.png" xlink:type="simple"/></inline-formula> under normal triangle distribution load</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/7-1720687x74.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> The distribution of surface displacement u under normal triangle distribution load</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/7-1720687x76.png"/></fig><p>At this moment, the boundary conditions (3) on the contact surface (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x77.png" xlink:type="simple"/></inline-formula>) are simplified to</p><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> The distribution of surface indentation w under normal triangle distribution load</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/7-1720687x78.png"/></fig><disp-formula id="scirp.72120-formula401"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x79.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x80.png" xlink:type="simple"/></inline-formula> is the tangential triangle distribution force applied on the materials surface, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x80.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x81.png" xlink:type="simple"/></inline-formula> is a surface constant.</p><p><img data-original="http://html.scirp.org/file/7-1720687x83.png" /><img data-original="http://html.scirp.org/file/7-1720687x82.png" /> (21)</p><p>Substituting Equation (21) into Equation (20), one can be obtained</p><disp-formula id="scirp.72120-formula402"><label>(22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x84.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.72120-formula403"><label>(23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x85.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72120-formula404"><label>(24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x86.png"  xlink:type="simple"/></disp-formula><p>where b is a length parameter depending on the material surface property. It should be pointed out that this parameter plays a critical role in the surface elasticity.</p><p>Substituting Equation (24) into the surface condition Equations (12) and (13), the solution of stresses and displaces under pure shear load were obtained</p><disp-formula id="scirp.72120-formula405"><label>(25)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x87.png"  xlink:type="simple"/></disp-formula><p>Substituting Equation (24) into Equations (22), one obtains</p><disp-formula id="scirp.72120-formula406"><label>(26)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x88.png"  xlink:type="simple"/></disp-formula><p>Therefore <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x89.png" xlink:type="simple"/></inline-formula> is given by</p><disp-formula id="scirp.72120-formula407"><label>(27)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x90.png"  xlink:type="simple"/></disp-formula><p>Substituting Equation (27) into Equations (25), the stresses component and displaces component are obtained as</p><disp-formula id="scirp.72120-formula408"><label>(28)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x91.png"  xlink:type="simple"/></disp-formula><p>It is seen, when<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x92.png" xlink:type="simple"/></inline-formula>, that is, the surface influence is ignored in Equation (28), the stresses and displacements of the half-plane are consistent with those in the classical elastic results [<xref ref-type="bibr" rid="scirp.72120-ref24">24</xref>] , respectively.</p><disp-formula id="scirp.72120-formula409"><label>(29)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x93.png"  xlink:type="simple"/></disp-formula><p>On the contact surface<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x94.png" xlink:type="simple"/></inline-formula>, the stresses is given by</p><disp-formula id="scirp.72120-formula410"><label>(30)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x95.png"  xlink:type="simple"/></disp-formula><p>Based on the previous assumption, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x96.png" xlink:type="simple"/></inline-formula>, the displacement on the surface component is derived as</p><disp-formula id="scirp.72120-formula411"><label>(31)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/7-1720687x97.png"  xlink:type="simple"/></disp-formula><p>It is instructive to examine the influence of the surface elasticity on the stresses and displacements of the contact surface and compare them with those in classical contact problem. <xref ref-type="fig" rid="fig5">Figure 5</xref> and <xref ref-type="fig" rid="fig6">Figure 6</xref> show the distribution of the stresses <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x98.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x98.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x99.png" xlink:type="simple"/></inline-formula> on the contact surface, where the solution of b/a = 0 is consistent with the classical elastic result.</p><p>It can be seen from <xref ref-type="fig" rid="fig7">Figure 7</xref> that the normal stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x100.png" xlink:type="simple"/></inline-formula> transits continuously across the loading boundary<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x100.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x101.png" xlink:type="simple"/></inline-formula>, which is increasing monotonically with respect to x in the loading region (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x100.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x101.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x102.png" xlink:type="simple"/></inline-formula>), and the inverse is observed outside the loading region (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x100.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x101.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x102.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x103.png" xlink:type="simple"/></inline-formula>). It means that the analytical expressions can give approximate results in the region that is far from the loading boundary. It is also found <xref ref-type="fig" rid="fig5">Figure 5</xref> that shear stress changes smoothly across the loading boundary<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x100.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x101.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x102.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x103.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x104.png" xlink:type="simple"/></inline-formula>, which is different from a</p><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> The distribution of the shear stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x106.png" xlink:type="simple"/></inline-formula> under tangential triangle distribution load</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/7-1720687x105.png"/></fig><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> The distribution of surface displacement u under tangential triangle distribution load</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/7-1720687x107.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> The distribution of the normal stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x109.png" xlink:type="simple"/></inline-formula> under tangential triangle distribution load</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/7-1720687x108.png"/></fig><p>singularity predicted by classical elasticity.</p><p>Due to the different surface elasticity value, the horizontal displacement is displayed in <xref ref-type="fig" rid="fig6">Figure 6</xref>, where we set<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x110.png" xlink:type="simple"/></inline-formula>, and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x110.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x111.png" xlink:type="simple"/></inline-formula>. It is seen that the slope of</p><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> The distribution of surface indentation w under tangential triangle distribution load</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/7-1720687x112.png"/></fig><p>the deformed surface for a &gt; 0 is continuous everywhere. It is also found the horizontal displacement decreases with the increase of surface elasticity. The indent depth is plotted in <xref ref-type="fig" rid="fig8">Figure 8</xref> with<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/7-1720687x113.png" xlink:type="simple"/></inline-formula>, which also shows that the normal displacement is continuous everywhere on the deformed surface. In addition, the indent depth decreases continuously with the increase of surface elasticity.</p></sec><sec id="s6"><title>6. Conclusion</title><p>In this paper, we consider the two-dimensional contact problem in the light of surface elasticity theory. Fourier integral transform method is adopted solving general analytical solution. For two particular loading cases of triangle distribution forces, the results are analyzed in detail and compared with the classical linear elastic solutions. A series of theoretical and numerical results show that the influences of the surface tension and the surface elasticity on the stresses and displacements are not always equal. It is found that the surface elasticity theory illuminates some interesting characteristics of contact problems at nano-scale, which are distinctly different from the classical solutions of elasticity without surface effects. Therefore, the influence of surface effects should be considered for nano-contact problems.</p></sec><sec id="s7"><title>Cite this paper</title><p>Wang, L.Y., Han, W., Wang, S.L., Wang, L.H. and Xin, Y.P. (2016) Nano-Contact Problem with Surface Effects on Triangle Distribution Loading. Journal of Applied Mathematics and Physics, 4, 2047-2060. http://dx.doi.org/10.4236/jamp.2016.411204</p></sec></body><back><ref-list><title>References</title><ref id="scirp.72120-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Cammarata, R.C. (1994) Surface and Interface Stress Effects in Thin Films. Progress in Surface Science, 46, 1-38. http://dx.doi.org/10.1016/0079-6816(94)90005-1</mixed-citation></ref><ref id="scirp.72120-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Miller, R.E. and Shenoy, V.B. (2000) Size-Dependent Elastic Properties of Nanosized Structural Elements. Nanotechnology, 11, 139-147. http://dx.doi.org/10.1088/0957-4484/11/3/301</mixed-citation></ref><ref id="scirp.72120-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Huang, Y., Zhang, F. and Hwang, K.C. 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