<?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">OJCE</journal-id><journal-title-group><journal-title>Open Journal of Civil Engineering</journal-title></journal-title-group><issn pub-type="epub">2164-3164</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ojce.2016.61003</article-id><article-id pub-id-type="publisher-id">OJCE-64131</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject></subj-group></article-categories><title-group><article-title>
 
 
  Nonlinear FEA of Pile Group Subjected to Lateral Load
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>.</surname><given-names>A. Sawant</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>K.</surname><given-names>B. Ladhane</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Civil Engineering, Indian Institute of Technology Roorkee, Roorkee, India</addr-line></aff><pub-date pub-type="epub"><day>25</day><month>02</month><year>2016</year></pub-date><volume>06</volume><issue>01</issue><fpage>19</fpage><lpage>30</lpage><history><date date-type="received"><day>6</day>	<month>February</month>	<year>2016</year></date><date date-type="rev-recd"><day>accepted</day>	<month>26</month>	<year>February</year>	</date><date date-type="accepted"><day>29</day>	<month>February</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>
 
 
  A finite element method based program has been developed to perform the static nonlinear analysis of pile group with six different configurations subjected to lateral loads. The pile has been assumed to remain elastic all the time whereas the soil has been assumed to undergo plastic yielding following von Mises yield criterion. The formulation of elasto-plastic analysis following von Mises yield criterion has been explained. The effect of Drucker-Prager and Mohr Coulomb yield criteria on the response of pile group is also investigated. The whole analysis is based on incremental load application. The external load is applied in small increments and the stresses are initially computed assuming elastic constitutive relation. Significant effect of soil nonlinearity is observed at smaller pile spacing which reduces with increase in spacing.
 
</p></abstract><kwd-group><kwd>Pile</kwd><kwd> Lateral Load</kwd><kwd> Constitutive Matrix</kwd><kwd> Stress Invariants</kwd><kwd> Yield Criterion</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Nonlinear p-y analysis is the most widely used method for design of laterally loaded piles due to its simplicity; the successful application of a p-y method depends upon the availability of detailed information on a spatial distribution of soil properties which are key factors in the design of laterally loaded deep foundation. The subgrade reaction method models soils as Winkler springs and piles as beams; hence, pile geometry can be considered only indirectly. The finite element method provides a more precise tool that is capable of modelling soil continuity, soil nonlinearity, pile-soil interface behaviour, and 3-D boundary conditions. It is more rigorous in its analytical methodology than any other existing methods. Randolph [<xref ref-type="bibr" rid="scirp.64131-ref1">1</xref>] used linear strain triangles in the semi- analytical finite element formulation to avoid special integration techniques. From the results of parametric study, a simplified expression was developed for the response of single and group piles embedded in elastic soil. The nonlinear behaviour of pile group was studied using 3-D FEA with nonlinear elastic soil model [<xref ref-type="bibr" rid="scirp.64131-ref2">2</xref>] [<xref ref-type="bibr" rid="scirp.64131-ref3">3</xref>] . In order to include the interaction effects involving relative slip and separation, a thin layer of interface element was used. Najjar and Zaman [<xref ref-type="bibr" rid="scirp.64131-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.64131-ref5">5</xref>] studied the effects of loading sequence and soil nonlinearity on the deformation behaviour of a pile group using a nonlinear 3-D finite element technique. Ladhane and Sawant [<xref ref-type="bibr" rid="scirp.64131-ref6">6</xref>] presented dynamic analysis of pile group and examined the effect of different pile configurations on dynamic response.</p><p>The review of literature has revealed that behaviour of laterally loaded piles is significantly influenced by the material non-linearity. Behaviour of pile group is further influenced by the arrangements of piles in the group. A 3-D finite element program has been developed for the analysis of a pile groups in clay considering the above aspects. Soil and pile media have been discretised into 3-D isoparametric continuum elements. The pile elements have been assumed to remain in elastic state at all the time. On the other hand, the soil elements are assumed to undergo plastic yielding according to the von Mises yield criterion. This model has been selected because it is suitable for analyzing the behaviour of purely cohesive soils under undrained condition. To simulate the stress transfer between soil and pile under lateral load, interface elements have been introduced at the soil-pile interface. Normal and tangential stiffness of these elements are assumed in such a way that shearing at the soil pile interface is allowed but gapping will be restricted. The formulation and implementation of additional features required for incorporating nonlinear behaviour are presented in this paper.</p></sec><sec id="s2"><title>2. Constitutive Model</title><p>Mainly, there are two types of materials involved in present study i.e. reinforced concrete and soil. The pile material is treated as linear elastic, whereas, the soil is replaced by an idealised material which behaves elastically up to some state of stress at which yielding occurs and beyond yielding, the theory of plasticity is implemented to account for the constitutive law of the soil. The constitutive relationships arising from the theory of plasticity are incremental in nature due to the stress path dependence of the material behaviour. The essential features of the plasticity theory are [<xref ref-type="bibr" rid="scirp.64131-ref7">7</xref>] :</p><p>・ A yield function, separates the elastic and plastic states of stresses in the body under consideration.</p><p>・ A plastic potential function defining the direction of plastic straining when yielding occurs (flow rule).</p><p>・ A hardening/softening law describing the dependence of the yield function on the plastic strains.</p><p>In the present study, von-Mises, Drucker-Prager [<xref ref-type="bibr" rid="scirp.64131-ref8">8</xref>] and modified Mohr-Coulomb [<xref ref-type="bibr" rid="scirp.64131-ref9">9</xref>] models have been considered. Viladkar et al. [<xref ref-type="bibr" rid="scirp.64131-ref7">7</xref>] have converted these models into convenient forms to make the computational aspect simple and presented a generalized approach to elasto-plastic finite element analysis. The associative flow rule is assumed, in which the yield function and plastic potential function are expressed by same function. The Yield criterions used to identify the onset of the yielding in the soil are explained here. Most of them are defined in terms of stress invariants. Here J<sub>1</sub>, J<sub>2</sub>, J<sub>3</sub> are first, second and third stress invariant and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x6.png" xlink:type="simple"/></inline-formula> is second stress invariant of the deviatoric stress components.</p><sec id="s2_1"><title>2.1. von-Mises Yield Criterion</title><p><xref ref-type="fig" rid="fig1">Figure 1</xref> shows the Graphical representation of von Mises yield criteria in deviatoric plane. When plotted in principal stress space it appears as circular cylinder whose central axis coincides with space diagonal. von-Mises yield function is approximation to the Tresca yield function and expressed in terms of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x7.png" xlink:type="simple"/></inline-formula> and material constant K as,</p><disp-formula id="scirp.64131-formula964"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x8.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_2"><title>2.2. Drucker-Prager Yield Criterion</title><p>An approximation to the Mohr-Coulomb law was presented by Drucker and Prager as a modification of the von- Mises yield criterion. The influence of the hydrostatic stress component on yielding was introduced by inclusion of an additional term in the von-Mises expression as:</p><disp-formula id="scirp.64131-formula965"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x9.png"  xlink:type="simple"/></disp-formula><p>where, a and K are material constants, which may be related to Coulomb’s material constants c and j. <xref ref-type="fig" rid="fig1">Figure 1</xref> shows graphical representation of Drucker-Prager and Mohr-Coulumb yield criteria in deviatoric plane. In order</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Representation of yield criteria in deviatoric plane</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1880481x10.png"/></fig><p>to make the Drucker-Prager circle coincide with the inner (Equation (3a)) and outer (Equation (3b)) apices of the Mohr-Coulomb hexagon at any section, it can be shown that [<xref ref-type="bibr" rid="scirp.64131-ref7">7</xref>] :</p><disp-formula id="scirp.64131-formula966"><label>(3a)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x11.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.64131-formula967"><label>(3b)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x12.png"  xlink:type="simple"/></disp-formula><p>However, since the values of c and j are determined by using conventional triaxial compression tests, these are different from those determined under a plane strain condition. Under this plane strain condition, the values of a and K can be expressed as:</p><disp-formula id="scirp.64131-formula968"><label>(3c)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x13.png"  xlink:type="simple"/></disp-formula><p>The two material parameters a and K for the Drucker-Prager model can be determined from the slope and intercept of the failure envelope plotted in the J<sub>1</sub>-(<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x14.png" xlink:type="simple"/></inline-formula>)<sup>1/2</sup> space.</p></sec><sec id="s2_3"><title>2.3. Mohr-Coulomb Yield Criterion</title><p>This criteria possess angular vertices at which the gradient with respect to the stresses, and hence the elasto- plastic constitutive law, is undefined at q = &#177;30˚ (<xref ref-type="fig" rid="fig1">Figure 1</xref>). A satisfactory method for dealing with these singularities is needed as they are often encountered in finite element computations. One technique for dealing with this problem has been discussed by Owen and Hinton [<xref ref-type="bibr" rid="scirp.64131-ref10">10</xref>] . In the vicinity of the vertices, their procedure uses the Drucker-Prager criterion to round-off the Mohr-Coulomb criterion. Another modified yield function suggested by Sloan and Brooker [<xref ref-type="bibr" rid="scirp.64131-ref9">9</xref>] is used to round-off these vertices. When used in conjunction with the parent yield function, the modified yield function results in a yield surface which is continuous and differentiable for all values of the stresses. The modified yield function is used in the vicinity of the vertices. The Mohr-Coulomb yield criterion is defined by following expression,</p><disp-formula id="scirp.64131-formula969"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x15.png"  xlink:type="simple"/></disp-formula><p>In which,</p><disp-formula id="scirp.64131-formula970"><label>(−30˚ ≤ θ ≤ 30˚)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x16.png"  xlink:type="simple"/></disp-formula><p>To avoid the singularities at the vertices of the Mohr-Coulomb surface, Sloan and Brooker [<xref ref-type="bibr" rid="scirp.64131-ref9">9</xref>] assume a different type of yield surface whenever q approaches &#177;30˚. In practice, the modified yield criterion is used whenever,</p><disp-formula id="scirp.64131-formula971"><graphic  xlink:href="http://html.scirp.org/file/3-1880481x17.png"  xlink:type="simple"/></disp-formula><p>where, q<sub>T</sub> is specified and represents the absolute value of the angle at which the transition occurs. To ensure that the Mohr-Coulomb yield surface is modelled with acceptable accuracy, q<sub>T</sub> should typically be in the range 25˚ to 29˚. At these transition points modified function is used which is expressed as,</p><disp-formula id="scirp.64131-formula972"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x18.png"  xlink:type="simple"/></disp-formula><p>where,</p><disp-formula id="scirp.64131-formula973"><graphic  xlink:href="http://html.scirp.org/file/3-1880481x19.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_4"><title>2.4. Elasto-Plastic Constitutive Matrix</title><p>Relation between incremental stresses, {Dσ} and incremental strains {De} in elasto-plastic state is given as,</p><disp-formula id="scirp.64131-formula974"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x20.png"  xlink:type="simple"/></disp-formula><p>where, [D]<sub>ep</sub> elasto-plastic constitutive matrix.</p><disp-formula id="scirp.64131-formula975"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x21.png"  xlink:type="simple"/></disp-formula><p>[D]<sub>ep</sub> represents the elasto-plastic constitutive matrix. Parameter A depends on type of plasticity (e.g. perfect plasticity, strain hardening/softening plasticity or work hardening/softening plasticity). For perfectly plastic material, A = 0 and k = constant.</p><p>In the present study, associated (yield and potential surface coincides) flow rule is considered which gives symmetric constitutive matrix and consequently symmetric global stiffness matrix. This helps in reducing memory requirement for storage as well as time of computation.</p></sec></sec><sec id="s3"><title>3. Elasto-Plastic Constitutive Matrix</title><p>Nayak and Zienkiewicz [<xref ref-type="bibr" rid="scirp.64131-ref11">11</xref>] have converted the yield criteria into convenient forms to make the computational aspect simple and presented a generalized approach to elasto-plastic finite element analysis. Further, Viladkar et al. [<xref ref-type="bibr" rid="scirp.64131-ref7">7</xref>] transform several yield criteria with isotropic hardening and associated flow characteristics into convenient forms and make them available for easy implementation into the finite element codes.</p><p>This formulation is due to Nayak and Zienkiewicz [<xref ref-type="bibr" rid="scirp.64131-ref11">11</xref>] and Viladkar et al. [<xref ref-type="bibr" rid="scirp.64131-ref7">7</xref>] and is achieved by expressing the yield function as,</p><disp-formula id="scirp.64131-formula976"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x22.png"  xlink:type="simple"/></disp-formula><p>where, q is an alternative to the third stress invariant and determined by,</p><disp-formula id="scirp.64131-formula977"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x23.png"  xlink:type="simple"/></disp-formula><p>Here J<sub>1</sub>, J<sub>2</sub>, J<sub>3</sub> are first, second and third stress invariant and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x24.png" xlink:type="simple"/></inline-formula> is second stress invariant of the deviatoric stress components.</p><p>The flow vector, a, is rewritten in terms of J<sub>1</sub>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x25.png" xlink:type="simple"/></inline-formula>and q in the following way using the chain rule:</p><disp-formula id="scirp.64131-formula978"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x26.png"  xlink:type="simple"/></disp-formula><p>Substituting <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x27.png" xlink:type="simple"/></inline-formula> from Equation (9), the flow vector can be expressed as:</p><disp-formula id="scirp.64131-formula979"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x28.png"  xlink:type="simple"/></disp-formula><p>where, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x29.png" xlink:type="simple"/></inline-formula></p><p>Calculation of C<sub>1</sub>, C<sub>2</sub> and C<sub>3</sub>:</p><p>Differentiating Equation (9) with respect to s,</p><disp-formula id="scirp.64131-formula980"><graphic  xlink:href="http://html.scirp.org/file/3-1880481x30.png"  xlink:type="simple"/></disp-formula><p>Substituting in Equation (18),</p><disp-formula id="scirp.64131-formula981"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x31.png"  xlink:type="simple"/></disp-formula><p>Simplifying radical in third term from above equation,</p><disp-formula id="scirp.64131-formula982"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x32.png"  xlink:type="simple"/></disp-formula><p>Substituting in Equation (12),</p><disp-formula id="scirp.64131-formula983"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x33.png"  xlink:type="simple"/></disp-formula><p>From Equations (11) and (14)</p><disp-formula id="scirp.64131-formula984"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x34.png"  xlink:type="simple"/></disp-formula><p>Calculation of a<sub>1</sub>, a<sub>2</sub> and a<sub>3</sub>:</p><p>Following are the stress invariants required to evaluate the constants a<sub>1</sub>, a<sub>2</sub> and a<sub>3</sub>.</p><p>The stress invariants are given as,</p><disp-formula id="scirp.64131-formula985"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x35.png"  xlink:type="simple"/></disp-formula><p>The second deviatoric stress invariants is given as,</p><disp-formula id="scirp.64131-formula986"><graphic  xlink:href="http://html.scirp.org/file/3-1880481x36.png"  xlink:type="simple"/></disp-formula><p>From Equations (11) and (16) and substituting<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x37.png" xlink:type="simple"/></inline-formula>,</p><disp-formula id="scirp.64131-formula987"><label>(17a)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x38.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.64131-formula988"><label>(17b)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x39.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.64131-formula989"><label>(17c)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x40.png"  xlink:type="simple"/></disp-formula><p>The constants C<sub>1</sub>, C<sub>2</sub> and C<sub>3</sub> can be evaluated from the expression of yield function using Equation (15).</p>Nonlinear Solution Algorithm<p>The total load is applied in the ten equal increments and the stiffness matrix, [K] is kept constant for all the load increments in <xref ref-type="fig" rid="fig2">Figure 2</xref>. Following is the algorithm used for nonlinear analysis:</p><p>1) Apply incremental load <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x41.png" xlink:type="simple"/></inline-formula> and solve for incremental displacement, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x42.png" xlink:type="simple"/></inline-formula></p><disp-formula id="scirp.64131-formula990"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x43.png"  xlink:type="simple"/></disp-formula><p>2) Update the total displacements u<sub>i</sub> for i<sup>th</sup> increment by adding incremental displacement <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x44.png" xlink:type="simple"/></inline-formula> in</p><disp-formula id="scirp.64131-formula991"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x45.png"  xlink:type="simple"/></disp-formula><p>3) Set m<sub>e</sub> = 0, where m<sub>e</sub> indicates number of yielded elements.</p><p>4) For each element, set m<sub>p</sub> = 0 (number of yielded points within the given element), obtain the element incremental displacement vector <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x46.png" xlink:type="simple"/></inline-formula><sup> </sup>from global incremental displacement vector,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x46.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x47.png" xlink:type="simple"/></inline-formula>.</p><p>5) For each Gauss point, compute the incremental stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x48.png" xlink:type="simple"/></inline-formula> and total stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x48.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x49.png" xlink:type="simple"/></inline-formula> for i<sup>th</sup> increment from following relations,</p><disp-formula id="scirp.64131-formula992"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x50.png"  xlink:type="simple"/></disp-formula><p>Check for yield, if the point have not yielded then go to next Gauss point, else, set m<sub>p</sub> = m<sub>p</sub> + 1, and calculate extra stress over yield stress, {Δσ}<sub>ext </sub></p><disp-formula id="scirp.64131-formula993"><label>(21)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x51.png"  xlink:type="simple"/></disp-formula><p>Set total stress at yield level</p><disp-formula id="scirp.64131-formula994"><label>(22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x52.png"  xlink:type="simple"/></disp-formula><p>Update the additional force vector to be applied in next iteration</p><disp-formula id="scirp.64131-formula995"><label>(23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x53.png"  xlink:type="simple"/></disp-formula><p>Complete loop over the Gauss points of the element</p><p>6) If m<sub>p</sub> &gt; 0, then assemble load vector <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x54.png" xlink:type="simple"/></inline-formula> and set m<sub>e</sub> = m<sub>e</sub> + 1.</p><p>7) Repeat Step 4) to 6) for all the elements.</p><p>8) If m<sub>e</sub> = 0, then not a single element have yielded, go to next load level.</p><p>9) If m<sub>e</sub> &gt; 0, then check for convergence using following displacement criteria,</p><disp-formula id="scirp.64131-formula996"><label>(24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-1880481x55.png"  xlink:type="simple"/></disp-formula><p>where, e<sub>d</sub> = displacement norm, q<sub>i</sub> = total displacement at the i<sup>th</sup> iteration and u<sub>i</sub><sub>−</sub><sub>1</sub> = total displacement at the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x56.png" xlink:type="simple"/></inline-formula> iteration.</p><p>If the convergence criterion is satisfied, then apply next load increment. If a convergence criterion is not satisfied then repeat the procedure from step 1) to step 9), till the displacements are converged.</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Nonlinear algorithm for elasto-plastic analysis</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1880481x57.png"/></fig></sec><sec id="s4"><title>4. Validation</title><p>For validation, the field data reported by Gabr et al. [<xref ref-type="bibr" rid="scirp.64131-ref12">12</xref>] and Ismael and Klym [<xref ref-type="bibr" rid="scirp.64131-ref13">13</xref>] are used. A detailed geotechnical investigation of the soil at Canons Park site (England) was carried out as reported by Gabr et al. [<xref ref-type="bibr" rid="scirp.64131-ref12">12</xref>] . The soil profile consisted of stiff slightly gravelly fissured London clay to the depth of 4 m. The test pile, 0.17 m in diameter, was bored cast in place with an embedment length of 4.5 m. Cohesion of the soil linearly increased with depth at the rate of 10 kPa/m, with a value of 45 kPa at ground level. The EI value of the pile was 1500 KNm<sup>2</sup>. Soil was assumed to follow von-Mises yield criterion. Measured versus predicted lateral-pile response is presented in <xref ref-type="fig" rid="fig3">Figure 3</xref> along with 3-D FEM prediction by Dewaikar et al. [<xref ref-type="bibr" rid="scirp.64131-ref14">14</xref>] . A reasonably good agreement is observed at lower load levels. But the difference at higher load level suggests to adopt different yield criterion. von-Mises yield criterion is independent of hydrostatic stress which resulted discrepancy at higher load level. So in the present study, Drucker-Prager and Mohr-Coulomb yield criterion are employed.</p><p>Comparison with pile load test data reported by Ismael and Klym [<xref ref-type="bibr" rid="scirp.64131-ref13">13</xref>] at Ontario is presented in <xref ref-type="fig" rid="fig4">Figure 4</xref>. A concrete pile with diameter 60 in (1.52 m) was embedded in over-consolidated clay with cohesion 2000 lb/ft<sup>2</sup> (96.0 kPa). Total pile length was 39 ft (12.0 m) with one foot (0.30 m) length above ground-line. The flexural rigidity EI of pile was 93 &#215; 10<sup>10</sup> lb-in<sup>2</sup> (2.675 &#215; 10<sup>6</sup> kN∙m<sup>2</sup>). Comparison between measured and predicted pile response shows a good agreement at higher load levels.</p><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Validation with experimental results [<xref ref-type="bibr" rid="scirp.64131-ref12">12</xref>] </title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1880481x58.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Validation with experimental results [<xref ref-type="bibr" rid="scirp.64131-ref13">13</xref>] </title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1880481x59.png"/></fig></sec><sec id="s5"><title>5. Parametric Study</title><p>A parametric study is carried out to examine the effect of pile spacing and pile group configuration on static nonlinear response of pile groups (pile diameter D = 1.0 m, L/D ratio = 20). Six different pile group configurations (<xref ref-type="fig" rid="fig5">Figure 5</xref>) are considered as 2 &#215; 2, 3 &#215; 3, 3PP, 3PS, 2PP, 2PS (PP―piles in parallel arrangement, PS―piles in series arrangement). The pile is assumed linear elastic throughout the analysis and soil is modeled using von Mises yield criteria. The lateral force H = 2000 kN is applied at top. The values of the various parameters assumed for pile and soil in this study are summarized in <xref ref-type="table" rid="table1">Table 1</xref>.</p><sec id="s5_1"><title>5.1. Effect of Yield Criteria</title><p>An attempt has been made to study, the response of 2 &#215; 2 pile group configuration using different yield criteria. In the present study three yield criteria have been used viz. von Mises (vM), Drucker-Prager and Mohr-Coulomb yield criteria. All the three forms of Drucker-Prager yield criteria have been included i.e. Drucker-Prager yield surface passing through inner (DP-I) and outer (DP-2) apices of Mohr-Coulomb yield surface and with plain strain condition (DP-3). Two forms of Mohr-Coulomb yield criteria based on the modifications suggested to overcome singularity by Owen and Hinton [<xref ref-type="bibr" rid="scirp.64131-ref10">10</xref>] and Sloan and Brooker [<xref ref-type="bibr" rid="scirp.64131-ref9">9</xref>] . These are represented by MC-1 and MC-2, respectively.</p><p><xref ref-type="fig" rid="fig6">Figure 6</xref> shows the variation of displacements with load using different yield criteria for 2 &#215; 2 pile group configuration for L/D = 20, s/D = 2, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-1880481x60.png" xlink:type="simple"/></inline-formula>= 20,000 kPa and pile diameter 1.0 m. It is observed that MC-1 and MC-2 yield criteria predicted almost same displacements at all load levels except marginal variation at higher load level and the response is almost linear. After comparing the response due to three forms of Drucker-Prager yield criteria, it is seen that DP-2 predicted higher response and DP-3 predicted lowest response. This can be attributed to the higher size of DP-2 will offer less yielding of soil for the given state of stress. At intermediate</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Pile and soil properties for parametric study</title></caption><table><tbody><thead><tr><th align="center" valign="middle"  colspan="5"  >Soil properties</th></tr></thead><tr><td align="center" valign="middle" >Modulus of elasticity, Es</td><td align="center" valign="middle" >20,000 kPa</td><td align="center" valign="middle"  colspan="2"  >Density, γ<sub>s</sub></td><td align="center" valign="middle" >18 kN/m<sup>3</sup></td></tr><tr><td align="center" valign="middle" >Poisson’s ratio, ms</td><td align="center" valign="middle" >0.4</td><td align="center" valign="middle"  colspan="2"  >Yield stress, σ<sub>y</sub></td><td align="center" valign="middle" >100 kPa</td></tr><tr><td align="center" valign="middle" >Pile properties</td><td align="center" valign="middle"  colspan="4"  ></td></tr><tr><td align="center" valign="middle" >Modulus of Elasticity, Ep</td><td align="center" valign="middle"  colspan="2"  >25 GPa</td><td align="center" valign="middle" >Poisson's ratio, m<sub>p </sub></td><td align="center" valign="middle" >0.2</td></tr><tr><td align="center" valign="middle" >Density, γp</td><td align="center" valign="middle"  colspan="2"  >25 kN/m<sup>3</sup></td><td align="center" valign="middle" >s/D ratio</td><td align="center" valign="middle" >3, 4, 5, 7</td></tr><tr><td align="center" valign="middle" >Pile cap thickness, tp</td><td align="center" valign="middle"  colspan="2"  >0.5 m</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" >Interface element</td><td align="center" valign="middle"  colspan="4"  ></td></tr><tr><td align="center" valign="middle" >Normal stiffness, Kn</td><td align="center" valign="middle"  colspan="2"  >1.0 &#215; 10<sup>6</sup> kN/m<sup>3</sup></td><td align="center" valign="middle" >Tangential stiffness, K<sub>s</sub></td><td align="center" valign="middle" >1000 kN/m<sup>3</sup></td></tr><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td></tr></tbody></table></table-wrap><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Arrangements of pile in different pile group configurations</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1880481x61.png"/></fig><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Variation in load-displacement response with yield criteria</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1880481x62.png"/></fig><p>load levels between about 800 kN to 1800 kN, vM yield criteria predicted higher response as compared to DP-1 and DP-3. This may be due to the fact that the effect of confining pressure is included in the Drucker-Prager yield criteria.</p></sec><sec id="s5_2"><title>5.2. Effect of Pile Group Configuration</title><p><xref ref-type="fig" rid="fig7">Figure 7</xref> shows the variation of displacement with load for different configurations of pile groups with L/D = 20, D = 1.0 m and E<sub>s</sub> = 20,000 kPa, s/D = 2 and 7. Pile top displacements for maximum load are summarized in <xref ref-type="table" rid="table2">Table 2</xref> for comparison. In case of pile in series and parallel configurations, series configurations are having higher displacements as compared to parallel configuration. This may be attributed to more passive resistance available in parallel arrangement. Among all the configurations 2PS group has highest displacement at all the load levels and 3 &#215; 3 pile group has lowest displacements. It is obvious that the stiffness offered by pile cap is higher in series arrangement as compare to parallel arrangement, due to which in case of linear response the series arrangements are undergoing smaller displacements at small to medium L/D ratio. At pile spacing 2D, maximum displacement is observed to be 118.18 mm for pile group 2PS and 94.16 mm for pile group 2PP. It shows that 2PS configuration predicted 25.5% higher displacements as compared to 2PP configuration. Similar trend is observed in 3PS and 3PP configurations. At pile spacing 7D there is no considerable difference in the observed displacements for 2PS and 2PP configuration. Similar observations are made for the 3PS and 3PP configuration. At higher spacing overlapping of stress zone will be minimum and nearly full passive resistance is available. So soil will offer nearly equal resistance in series and parallel arrangement.</p><p>In the square configuration 2 &#215; 2 pile group predicted higher displacements at all the load levels as compared to 3 &#215; 3 pile group. Nonlinear maximum displacement is observed to be 11.57 mm in 3 &#215; 3 configuration for pile spacing 2D. It is 25.6% higher than the linear displacement whereas nonlinear maximum displacement is 40.13 mm in 2 &#215; 2 pile group configuration, which is 166.8% higher than the linear displacement. Combined structural stiffness of pile and pile cap in square arrangement is considerably higher than those groups in series or parallel arrangement. Owing to this, they will have smaller displacements for the same load level. Obviously, 3 &#215; 3 pile group is much stiffer than 2 &#215; 2 pile group.</p><p>To compare the effect of pile group configuration on a common basis, load-displacement relationships are normalized as explained previously. Load-displacement relationships in normalized form are presented in <xref ref-type="fig" rid="fig8">Figure 8</xref> (s/D = 2). It is observed that relationship is linear up to normalized load level of 0.1 (except 3 &#215; 3 pile group). Effect of nonlinearity is increasing with number of piles in pile group. But for same number of piles, parallel configurations are stiffer than series configurations due to availability of more passive resistance.</p><fig-group id="fig7"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Load-displacement comparison for different pile group configurations.</title></caption><fig id ="fig7_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1880481x63.png"/></fig><fig id ="fig7_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1880481x64.png"/></fig></fig-group><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Linear and nonlinear response for different pile group configurations</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Spacing</th><th align="center" valign="middle" >Analysis</th><th align="center" valign="middle" >2 &#215; 2</th><th align="center" valign="middle" >3 &#215; 3</th><th align="center" valign="middle" >3PP</th><th align="center" valign="middle" >3PS</th><th align="center" valign="middle" >2PP</th><th align="center" valign="middle" >2PS</th></tr></thead><tr><td align="center" valign="middle"  rowspan="2"  >2D</td><td align="center" valign="middle" >Linear</td><td align="center" valign="middle" >15.04</td><td align="center" valign="middle" >9.21</td><td align="center" valign="middle" >17.14</td><td align="center" valign="middle" >16.20</td><td align="center" valign="middle" >22.559</td><td align="center" valign="middle" >21.81</td></tr><tr><td align="center" valign="middle" >Nonlinear</td><td align="center" valign="middle" >40.13</td><td align="center" valign="middle" >11.57</td><td align="center" valign="middle" >46.49</td><td align="center" valign="middle" >59.79</td><td align="center" valign="middle" >94.16</td><td align="center" valign="middle" >118.18</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >7D</td><td align="center" valign="middle" >Linear</td><td align="center" valign="middle" >8.21</td><td align="center" valign="middle" >4.17</td><td align="center" valign="middle" >11.60</td><td align="center" valign="middle" >10.89</td><td align="center" valign="middle" >17.013</td><td align="center" valign="middle" >15.58</td></tr><tr><td align="center" valign="middle" >Nonlinear</td><td align="center" valign="middle" >10.40</td><td align="center" valign="middle" >4.31</td><td align="center" valign="middle" >18.00</td><td align="center" valign="middle" >18.95</td><td align="center" valign="middle" >43.53</td><td align="center" valign="middle" >43.81</td></tr></tbody></table></table-wrap><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Normalized load-displacement response for different pile group configurations</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-1880481x65.png"/></fig></sec></sec><sec id="s6"><title>6. Concluding Remarks</title><p>A finite element program has been developed to perform the static nonlinear analysis of pile group with six different configurations subjected to lateral loads. A brief description of the numerical algorithm and its features has been presented. The pile has been assumed to remain elastic all the time whereas the soil has been assumed to undergo plastic yielding following von Mises yield criterion. The formulation of elasto-plastic analysis following von Mises yield criterion has been explained. The effect of Drucker-Prager and Mohr Coulomb yield criteria on the response of pile group is also investigated. The whole analysis is based on incremental load application. The external load is applied in small increments and the stresses are initially computed assuming elastic constitutive relation. These stresses in the soil elements are then checked against the corresponding yield criteria and are adjusted to satisfy the required conditions. The excess stresses are applied back again in the form of residual forces in the next iteration. This procedure is continued until a satisfactory convergence is arrived at. Significant effect of soil nonlinearity is observed at smaller pile spacing which reduces with increase in spacing. Combined structural stiffness of pile and pile cap in square arrangement is considerably higher than that of those groups in series or parallel arrangement.</p></sec><sec id="s7"><title>Cite this paper</title><p>V. A.Sawant,K. B.Ladhane, (2016) Nonlinear FEA of Pile Group Subjected to Lateral Load. Open Journal of Civil Engineering,06,19-30. doi: 10.4236/ojce.2016.61003</p></sec></body><back><ref-list><title>References</title><ref id="scirp.64131-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Randolph, M.F. (1981) The Response of Flexible Piles to Lateral Loading. Géotechnique, 31, 247-259. 
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