<?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">AM</journal-id><journal-title-group><journal-title>Applied Mathematics</journal-title></journal-title-group><issn pub-type="epub">2152-7385</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/am.2014.513182</article-id><article-id pub-id-type="publisher-id">AM-47624</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>COMPUTER SCIENCE &amp; COMMUNICATIONS</subject><subject>ENGINEERING</subject><subject>PHYSICS &amp; MATHEMATICS</subject></subj-group></article-categories><title-group><article-title>Study of Stability Analysis for a Class of Fourth Order Boundary Value Problems</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>C.</surname><given-names>Bala Rama Krishna</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>P.</surname><given-names>S. Rama Chandra Rao</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Department of Mathematics, Kakatiya Institute of Technology &amp; Science, Warangal, India</addr-line></aff><aff id="aff1"><addr-line>Department of Mathematics, Chaitanya Degree College (Autonomous), Warangal, India</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>cbrk2004@gmail.com(CBRK)</email>;<email>patibanda20@yahoo.co.in(PSRCR)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>07</day><month>07</month><year>2014</year></pub-date><volume>05</volume><issue>13</issue><fpage>1887</fpage><lpage>1893</lpage><history><date date-type="received"><day>16</day>	<month>April</month>	<year>2014</year></date><date date-type="rev-recd"><day>28</day>	<month>May</month>	<year>2014</year>	</date><date date-type="accepted"><day>8</day>	<month>June</month>	<year>2014</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>Fourth order differential equations are considered to develop the class
of methods for the numerical solution of boundary value problems. In this
paper, we have discussed the regions of absolute stability of fourth order
boundary value problems. Methods proposed and derived in this paper are applied
to solve a fourth-order boundary value problem. Numerical results are given to
illustrate the efficiency of our methods and compared with exact solution.</p></abstract><kwd-group><kwd>Numerical Differentiation</kwd><kwd> Initial Value Problem</kwd><kwd> Boundary Value Problem</kwd><kwd> Absolute Stability</kwd><kwd> Multistep Methods</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The determination process for the numerical solution of initial value problems in ordinary differential equations can be classified into two categories-single step methods and multistep methods. Single step methods are those in which the approximation for the point <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\033794cb-3832-456c-b4c2-79bc0dd161d7.png" xlink:type="simple"/></inline-formula> involves information from only one of the previous points<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\fb71feab-bedc-487b-a283-ddd92d031866.png" xlink:type="simple"/></inline-formula>. Methods using the approximation at more than one previous points to determine the approximation at the next point are called multistep methods. Thus a k-step method requires information about the solution at k points <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\41adf206-696a-4a49-898a-014ab9ae19c3.png" xlink:type="simple"/></inline-formula> to compute the solution at the point<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\f4f5ac7c-85ae-4814-9015-b1586a375d44.png" xlink:type="simple"/></inline-formula>. Finite difference methods for boundary value problems are discussed in [<xref ref-type="bibr" rid="scirp.47624-ref1">1</xref>] . Linear multi step methods of second order differential equations are discussed in [<xref ref-type="bibr" rid="scirp.47624-ref2">2</xref>] . The methods based on numerical differentiation for first-order differential equations have been shown to be stiffly stable by Gear [<xref ref-type="bibr" rid="scirp.47624-ref3">3</xref>] . A detailed study of the single step and multistep methods has been carried out by Gear [<xref ref-type="bibr" rid="scirp.47624-ref3">3</xref>] , Gragg and Statter [<xref ref-type="bibr" rid="scirp.47624-ref4">4</xref>] and Henrici [<xref ref-type="bibr" rid="scirp.47624-ref5">5</xref>] . Gear [<xref ref-type="bibr" rid="scirp.47624-ref3">3</xref>] and Peter Henrici [<xref ref-type="bibr" rid="scirp.47624-ref5">5</xref>] have derived special multistep methods based on numerical integration and numerical differentiation for solving first-order differential equations. Jain [<xref ref-type="bibr" rid="scirp.47624-ref6">6</xref>] has considered high order stiffly stable methods. Further information can be had from [<xref ref-type="bibr" rid="scirp.47624-ref7">7</xref>] and [<xref ref-type="bibr" rid="scirp.47624-ref8">8</xref>] . Special multistep methods based on numerical differentiation for solving the initial value problem have been derived in Rama Chandra Rao [<xref ref-type="bibr" rid="scirp.47624-ref9">9</xref>] . The methods now to be discussed are based on replacing the function <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\61906985-bbfd-483e-bdc6-64af9546391e.png" xlink:type="simple"/></inline-formula> which is unknown, by an interpolating polynomial having the values <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\9eb23466-6e8e-4b8c-8ced-5e1e12761d57.png" xlink:type="simple"/></inline-formula> on a set of points x<sub>n</sub> where y<sub>n</sub> has already been computed. The methods discussed in this paper are essentially based on the idea that the solution is best approximated by polynomials. The motivation for the work carried out in this paper arises from the methods based on numerical differentiation for the first-order differential equations, special multistep methods based on numerical integration for the solution of the special second-order differential equations by Henrici [<xref ref-type="bibr" rid="scirp.47624-ref5">5</xref>] and Special multistep methods based on numerical differentiation for solving the initial value problem by Rama Chandra Rao [<xref ref-type="bibr" rid="scirp.47624-ref9">9</xref>] . In Henrici [<xref ref-type="bibr" rid="scirp.47624-ref5">5</xref>] methods based on Numerical Integration have been derived by integrating <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\1def8138-658c-4874-ad29-961213a02645.png" xlink:type="simple"/></inline-formula> twice and replacing the function <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\2319e7b3-ff47-4543-9856-ff9d4a5f6690.png" xlink:type="simple"/></inline-formula> by an interpolating polynomial. Special multistep methods have been derived by replacing <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\ba641a19-af60-4c44-98aa-781ed8ddf02f.png" xlink:type="simple"/></inline-formula> on the left hand side of<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\b466bc11-bfa9-46ab-b321-bdf4645accbc.png" xlink:type="simple"/></inline-formula> by an interpolating polynomial and differentiating it four times. We have investigated a class of implicit methods. It is found that the implicit methods have order<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\fbdb5bc0-4f33-4be6-b21d-fde2381ae2a2.png" xlink:type="simple"/></inline-formula>. Some local truncation errors are provided. The regions of absolute stability of the methods are derived. Numerical tests of the performance of the methods are established by solving differential equation and compared with the exact solution. The numerical results reported show the validity of our methods.</p></sec><sec id="s2"><title>2. General Linear Multistep Methods for Special Fourth-Order Differential Equations</title><p>The special fourth order differential equation</p><disp-formula id="scirp.47624-formula341"><label>(1)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\ab30a545-88c9-49e2-be2b-6d4c37bf8c0e.png"/></disp-formula><p>occurs frequently in many number of problems of science and engineering.</p><p>A general linear multistep method of step number k for the numerical solution of equation (1) is given by</p><disp-formula id="scirp.47624-formula342"><label>(2)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\f7decb62-b454-4357-bb3f-ca994119e561.png"/></disp-formula><p>where a<sub>j</sub>, b<sub>j</sub> are constants and “h” is the step length.</p><p>Introducing the polynomials</p><disp-formula id="scirp.47624-formula343"><label>(3)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\6dbe9370-6d2d-4774-a6f0-3989bad99c06.png"/></disp-formula><p>Equation (2) can be written as</p><disp-formula id="scirp.47624-formula344"><label>(4)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\774d613c-7145-4d78-a7f9-f487c846f062.png"/></disp-formula><p>In Equation (4), “E” is the shift operator defined by <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\54b12cf1-9ca0-49dc-878c-73cfeee3f137.png" xlink:type="simple"/></inline-formula></p><p>Applying (4) to<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\2753b2ee-9bb8-4365-a4c8-6144c0d8d4c9.png" xlink:type="simple"/></inline-formula>, we get the characteristic equation</p><disp-formula id="scirp.47624-formula345"><label>(5)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\0105ea86-a553-4632-9aaa-be2c2910c388.png"/></disp-formula><p>The roots <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\95659db4-c249-43fa-818e-0d6401437ac3.png" xlink:type="simple"/></inline-formula> of the characteristic Equation (5) and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\be857272-4c98-4773-a4b1-7aa986a28786.png" xlink:type="simple"/></inline-formula> are in general, complex and the region of absolute stability is defined to be the region of the complex <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\ca7f2d3d-2cea-40ea-98c0-9cc21b2f1ba5.png" xlink:type="simple"/></inline-formula>-plane such that the roots of the characteristic Equation (5) lie within the unit circle whenever <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\e3f2ef0f-5222-45d9-bf13-ef25238b1e8d.png" xlink:type="simple"/></inline-formula> lies in the interior of the region. Denoting the region of absolute stability of R and its boundary by<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\430aeef8-ac93-46c7-a806-22c8fce13638.png" xlink:type="simple"/></inline-formula>, the locus of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\c4c96f53-2066-4609-b4d8-f02d0f48ac4c.png" xlink:type="simple"/></inline-formula> is given by</p><disp-formula id="scirp.47624-formula346"><label>(6)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\3b49337e-9c5f-46bb-a9d9-93df45de4b90.png"/></disp-formula></sec><sec id="s3"><title>3. Derivation of the Methods</title><p>Let <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\dc8d18b8-9a6e-4988-bf4f-eea74f7546d3.png" xlink:type="simple"/></inline-formula> be the backward difference interpolating polynomial of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\0268cb0c-879e-463c-8ced-80c140d68e1b.png" xlink:type="simple"/></inline-formula> at <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\75e952fb-16eb-453a-b7f4-49a07cad5316.png" xlink:type="simple"/></inline-formula> abscissas<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\456c4851-dadf-4a88-a4c4-c602831d74a4.png" xlink:type="simple"/></inline-formula><sub>.</sub> Then <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\4b2326f4-0507-4b50-ba80-87d119e8e0fe.png" xlink:type="simple"/></inline-formula> is given by</p><disp-formula id="scirp.47624-formula347"><label>(7)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\01050d71-8c4e-4e44-8408-d1dfd8ef9eea.png"/></disp-formula><p>Differentiating (7) four times with respect to x, we get</p><disp-formula id="scirp.47624-formula348"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\91d92286-1e2c-4140-8e02-2f6b68fa33f4.png"/></disp-formula><p>Replacing <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\a627d5ba-86b1-4439-92db-c88cbcca2812.png" xlink:type="simple"/></inline-formula> by <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\7b32661e-ec22-4d6f-be13-e3b5284def4e.png" xlink:type="simple"/></inline-formula> in Equation (1) and putting <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\515c5a6b-97d9-480c-af9d-2ce9cb2879d4.png" xlink:type="simple"/></inline-formula> i.e.<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\a2e30665-085c-478b-885b-b18f473120c6.png" xlink:type="simple"/></inline-formula>, we get,</p><disp-formula id="scirp.47624-formula349"><label>(8)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\15651ead-5f51-4a1a-bc48-8c5687a3c7ad.png"/></disp-formula><p>where</p><disp-formula id="scirp.47624-formula350"><label>(9)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\87bafa3e-9048-46f6-92fb-2b26de5c428e.png"/></disp-formula><p>Taking r = 0 in (8), a class of methods can be attained which are given by</p><disp-formula id="scirp.47624-formula351"><label>(10)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\1107c0bc-e6e8-4a30-971c-d468a3e21a2e.png"/></disp-formula><p>The coefficients <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\b07fbdc5-2b16-45b6-b829-92103d399d17.png" xlink:type="simple"/></inline-formula> are shown in <xref ref-type="table" rid="table1">Table 1</xref>.</p><p>Differences in (10) are expressed in terms of function values.</p><p>After simplification, the Equation (10) will turn out into the form</p><disp-formula id="scirp.47624-formula352"><label>(11)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\1b2b9e6b-b4ee-4335-b9c1-6b039e5ab659.png"/></disp-formula><p>The coefficients <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\e17829cc-71e6-428b-ab97-861dc6551322.png" xlink:type="simple"/></inline-formula> are shown in <xref ref-type="table" rid="table2">Table 2</xref>.</p><p>The local truncation error of the formula (11) is given by</p><disp-formula id="scirp.47624-formula353"><label>(12)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\be136af9-45ce-4f48-9a18-f5a31630f863.png"/></disp-formula><p><xref ref-type="table" rid="table1">Table 1</xref>. Coefficients of<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\d68f0934-90c5-4701-943b-340b1e187746.png" xlink:type="simple"/></inline-formula>;<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\a879604c-b476-4749-b5b6-3ff8b7648b6a.png" xlink:type="simple"/></inline-formula>.</p><table-wrap id="table1"  position="float"><object-id pub-id-type="pii">Table 1</object-id><label>Table 1. Coefficients of<img src="htmlimages\5-7402256x\d68f0934-90c5-4701-943b-340b1e187746.png" width="42.5" height="37.5" />;<img src="htmlimages\5-7402256x\a879604c-b476-4749-b5b6-3ff8b7648b6a.png" width="100" height="40" />.</label><caption><p>Table 1. Coefficients of<img src="htmlimages\5-7402256x\d68f0934-90c5-4701-943b-340b1e187746.png" width="42.5" height="37.5" />;<img src="htmlimages\5-7402256x\a879604c-b476-4749-b5b6-3ff8b7648b6a.png" width="100" height="40" />.</p></caption><table><thead><tr><th align="center" valign="middle" >M</th><th align="center" valign="middle" >0</th><th align="center" valign="middle" >1</th><th align="center" valign="middle" >2</th><th align="center" valign="middle" >3</th><th align="center" valign="middle" >4</th><th align="center" valign="middle" >5</th><th align="center" valign="middle" >6</th><th align="center" valign="middle" >7</th><th align="center" valign="middle" >8</th><th align="center" valign="middle" >9</th></tr></thead><tbody><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</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><p><xref ref-type="table" rid="table2">Table 2</xref>. Coefficients of<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\49811a5c-1ced-48a6-9391-17de7bf999c2.png" xlink:type="simple"/></inline-formula>;<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\81a40030-314b-4a87-903c-2c1037faa878.png" xlink:type="simple"/></inline-formula>,<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\619ac694-c12a-4cd6-8ad4-1eeee12cdf6c.png" xlink:type="simple"/></inline-formula>.</p><table-wrap id="table2"  position="float"><object-id pub-id-type="pii">Table 2</object-id><label>Table 2. Coefficients of<img src="htmlimages\5-7402256x\49811a5c-1ced-48a6-9391-17de7bf999c2.png" width="27.5" height="37.5" />;<img src="htmlimages\5-7402256x\81a40030-314b-4a87-903c-2c1037faa878.png" width="96.25" height="40" />,<img src="htmlimages\5-7402256x\619ac694-c12a-4cd6-8ad4-1eeee12cdf6c.png" width="96.25" height="40" />.</label><caption><p>Table 2. Coefficients of<img src="htmlimages\5-7402256x\49811a5c-1ced-48a6-9391-17de7bf999c2.png" width="27.5" height="37.5" />;<img src="htmlimages\5-7402256x\81a40030-314b-4a87-903c-2c1037faa878.png" width="96.25" height="40" />,<img src="htmlimages\5-7402256x\619ac694-c12a-4cd6-8ad4-1eeee12cdf6c.png" width="96.25" height="40" />.</p></caption><table><thead><tr><th align="center" valign="middle" >K</th><th align="center" valign="middle" >J</th><th align="center" valign="middle" ></th><th align="center" valign="middle" ></th><th align="center" valign="middle" ></th><th align="center" valign="middle" ></th><th align="center" valign="middle" ></th><th align="center" valign="middle" ></th><th align="center" valign="middle" ></th><th align="center" valign="middle" ></th><th align="center" valign="middle" ></th></tr></thead><tbody><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >3</td><td align="center" valign="middle" >4</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >6</td><td align="center" valign="middle" >7</td><td align="center" valign="middle" >8</td><td align="center" valign="middle" >9</td></tr><tr><td align="center" valign="middle" >4</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >−4</td><td align="center" valign="middle" >6</td><td align="center" valign="middle" >−4</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" >5</td><td align="center" valign="middle" >3</td><td align="center" valign="middle" >−14</td><td align="center" valign="middle" >26</td><td align="center" valign="middle" >−24</td><td align="center" valign="middle" >11</td><td align="center" valign="middle" >−2</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><tr><td align="center" valign="middle" >6</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></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><tr><td align="center" valign="middle" >7</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></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><tr><td align="center" valign="middle" >8</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></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><tr><td align="center" valign="middle" >9</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></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><p>It follows that the k-step method (14) has the order<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\e0b35169-430a-4cad-a1bf-e8cce51c597a.png" xlink:type="simple"/></inline-formula>, which is absolutely stable for <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\54ce65bd-1623-4908-9392-86688f1931eb.png" xlink:type="simple"/></inline-formula></p><p>For the method (13), we have</p><disp-formula id="scirp.47624-formula354"><label>. (13)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\353b2266-7eb1-4648-8c0a-0dc8459e08a8.png"/></disp-formula><p>The regions of absolute stability of the method for k = 4, 5, 6, 7, 8 and 9 are shown in <xref ref-type="fig" rid="fig1">Figure 1</xref> and <xref ref-type="fig" rid="fig2">Figure 2</xref> (Taking real part on x-axis and imaginary part on y-axis). The region of absolute stability is the region lying outside the boundary.</p><fig id="fig1"><label>Figure 1</label><caption><p> The region of absolute stability of the method (13) for k = 4, 5 and 6</p></caption><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\351a6845-b668-44cd-8809-08a33e2eb5e2.png"/></fig><fig id="fig2"><label>Figure 2</label><caption><p> The region of absolute stability of the method (13) for k = 7, 8 and 9</p></caption><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\bd19cc72-c89e-455e-9c8e-3ce7c8bbf640.png"/></fig></sec><sec id="s4"><title>4. Numerical Example</title><p>In this section, we have applied ND methods to solve the differential equation</p><disp-formula id="scirp.47624-formula355"><label>(14)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\fbe1ba39-2715-4cbf-8a10-7fb23406e06c.png"/></disp-formula><p>in the interval <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\213f870a-e7a9-414f-b8bf-ced24d4ce570.png" xlink:type="simple"/></inline-formula> with h = 0.01 and h = 0.02 and the results are shown in <xref ref-type="table" rid="table3">Table 3</xref> and <xref ref-type="table" rid="table4">Table 4</xref>.</p><p>The fourth order numerical differentiation method derived in this paper for k = 6 is</p><disp-formula id="scirp.47624-formula356"><label>(15)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\5-7402256x\16c439fc-5b23-408e-9340-1a5326207bc5.png"/></disp-formula></sec><sec id="s5"><title>5. Discussion and Conclusion</title><p>The methods based on numerical integration are found to be closed regions of absolute stability; the methods</p><table-wrap id="table3"  position="float"><object-id pub-id-type="pii">Table 3</object-id><label>Table 3</label><caption><p>. Solution by fifth order ND with h = 0.01</p></caption><table><thead><tr><th align="center" valign="middle" >X</th><th align="center" valign="middle" >Exact Solution</th><th align="center" valign="middle" >Numerical Solution by fifth order ND</th><th align="center" valign="middle" >Absolute Error</th></tr></thead><tbody><tr><td align="center" valign="middle" >0.10</td><td align="center" valign="middle" >9.500016525794E−02</td><td align="center" valign="middle" >9.500016525794E−02</td><td align="center" valign="middle" >7.813194535800E−15</td></tr><tr><td align="center" valign="middle" >0.20</td><td align="center" valign="middle" >1.800052419090E−01</td><td align="center" valign="middle" >1.800052419090E−01</td><td align="center" valign="middle" >5.329070518201E−15</td></tr><tr><td align="center" valign="middle" >0.30</td><td align="center" valign="middle" >2.550394442682E−01</td><td align="center" valign="middle" >2.550394442681E−01</td><td align="center" valign="middle" >5.662137425588E−15</td></tr><tr><td align="center" valign="middle" >0.40</td><td align="center" valign="middle" >3.201646548346E−01</td><td align="center" valign="middle" >3.201646548346E−01</td><td align="center" valign="middle" >3.719247132494E−15</td></tr><tr><td align="center" valign="middle" >0.50</td><td align="center" valign="middle" >3.754975976986E−01</td><td align="center" valign="middle" >3.754975976986E−01</td><td align="center" valign="middle" >3.774758283726E−15</td></tr><tr><td align="center" valign="middle" >0.60</td><td align="center" valign="middle" >4.212257271813E−01</td><td align="center" valign="middle" >4.212257271813E−01</td><td align="center" valign="middle" >2.775557561563E−15</td></tr><tr><td align="center" valign="middle" >0.70</td><td align="center" valign="middle" >4.576217499812E−01</td><td align="center" valign="middle" >4.576217499812E−01</td><td align="center" valign="middle" >2.720046410332E−15</td></tr><tr><td align="center" valign="middle" >0.80</td><td align="center" valign="middle" >4.850567100313E−01</td><td align="center" valign="middle" >4.850567100313E−01</td><td align="center" valign="middle" >8.881784197001E−16</td></tr><tr><td align="center" valign="middle" >0.90</td><td align="center" valign="middle" >5.040115785530E−01</td><td align="center" valign="middle" >5.040115785530E−01</td><td align="center" valign="middle" >1.221245327088E−15</td></tr><tr><td align="center" valign="middle" >1.00</td><td align="center" valign="middle" >5.150873072263E−01</td><td align="center" valign="middle" >5.150873072263E−01</td><td align="center" valign="middle" >2.997602166488E−15</td></tr><tr><td align="center" valign="middle" >1.10</td><td align="center" valign="middle" >5.190133197868E−01</td><td align="center" valign="middle" >5.190133197868E−01</td><td align="center" valign="middle" >1.887379141863E−15</td></tr><tr><td align="center" valign="middle" >1.20</td><td align="center" valign="middle" >5.166544364783E−01</td><td align="center" valign="middle" >5.166544364783E−01</td><td align="center" valign="middle" >4.662936703426E−15</td></tr><tr><td align="center" valign="middle" >1.30</td><td align="center" valign="middle" >5.090162464214E−01</td><td align="center" valign="middle" >5.090162464214E−01</td><td align="center" valign="middle" >5.440092820663E−15</td></tr><tr><td align="center" valign="middle" >1.40</td><td align="center" valign="middle" >4.972489648573E−01</td><td align="center" valign="middle" >4.972489648573E−01</td><td align="center" valign="middle" >5.440092820663E−15</td></tr><tr><td align="center" valign="middle" >1.50</td><td align="center" valign="middle" >4.826498351587E−01</td><td align="center" valign="middle" >4.826498351587E−01</td><td align="center" valign="middle" >8.826273045770E−15</td></tr><tr><td align="center" valign="middle" >1.60</td><td align="center" valign="middle" >4.666641592316E−01</td><td align="center" valign="middle" >4.666641592316E−01</td><td align="center" valign="middle" >9.992007221626E−15</td></tr><tr><td align="center" valign="middle" >1.70</td><td align="center" valign="middle" >4.508850642096E−01</td><td align="center" valign="middle" >4.508850642096E−01</td><td align="center" valign="middle" >1.304512053935E−14</td></tr><tr><td align="center" valign="middle" >1.80</td><td align="center" valign="middle" >4.370521379547E−01</td><td align="center" valign="middle" >4.370521379547E−01</td><td align="center" valign="middle" >1.637578961322E−14</td></tr><tr><td align="center" valign="middle" >1.90</td><td align="center" valign="middle" >4.270490905788E−01</td><td align="center" valign="middle" >4.270490905789E−01</td><td align="center" valign="middle" >1.471045507628E−14</td></tr><tr><td align="center" valign="middle" >2.00</td><td align="center" valign="middle" >4.229006237963E−01</td><td align="center" valign="middle" >4.229006237963E−01</td><td align="center" valign="middle" >1.737499033538E−14</td></tr></tbody></table></table-wrap><table-wrap id="table4"  position="float"><object-id pub-id-type="pii">Table 4</object-id><label>Table 4</label><caption><p>. Solution by fifth order ND with h = 0.02</p></caption><table><thead><tr><th align="center" valign="middle" >X</th><th align="center" valign="middle" >Exact Solution</th><th align="center" valign="middle" >Numerical Solution by fifth order ND</th><th align="center" valign="middle" >Absolute Error</th></tr></thead><tbody><tr><td align="center" valign="middle" >0.10</td><td align="center" valign="middle" >9.500016525794E−02</td><td align="center" valign="middle" >9.500016525718E−02</td><td align="center" valign="middle" >7.650130529058E−13</td></tr><tr><td align="center" valign="middle" >0.20</td><td align="center" valign="middle" >1.800052419090E−01</td><td align="center" valign="middle" >1.800052419082E−01</td><td align="center" valign="middle" >7.430722703816E−13</td></tr><tr><td align="center" valign="middle" >0.30</td><td align="center" valign="middle" >2.550394442682E−01</td><td align="center" valign="middle" >2.550394442675E−01</td><td align="center" valign="middle" >6.964984144986E−13</td></tr><tr><td align="center" valign="middle" >0.40</td><td align="center" valign="middle" >3.201646548346E−01</td><td align="center" valign="middle" >3.201646548340E−01</td><td align="center" valign="middle" >6.305511668359E−13</td></tr><tr><td align="center" valign="middle" >0.50</td><td align="center" valign="middle" >3.754975976986E−01</td><td align="center" valign="middle" >3.754975976981E−01</td><td align="center" valign="middle" >5.463962615693E−13</td></tr><tr><td align="center" valign="middle" >0.60</td><td align="center" valign="middle" >4.212257271813E−01</td><td align="center" valign="middle" >4.212257271809E−01</td><td align="center" valign="middle" >4.425348976156E−13</td></tr><tr><td align="center" valign="middle" >0.70</td><td align="center" valign="middle" >4.576217499812E−01</td><td align="center" valign="middle" >4.576217499809E−01</td><td align="center" valign="middle" >3.217981436876E−13</td></tr><tr><td align="center" valign="middle" >0.80</td><td align="center" valign="middle" >4.850567100313E−01</td><td align="center" valign="middle" >4.850567100311E−01</td><td align="center" valign="middle" >1.886824030350E−13</td></tr><tr><td align="center" valign="middle" >0.90</td><td align="center" valign="middle" >5.040115785530E−01</td><td align="center" valign="middle" >5.040115785529E−01</td><td align="center" valign="middle" >4.274358644807E−14</td></tr><tr><td align="center" valign="middle" >1.00</td><td align="center" valign="middle" >5.150873072263E−01</td><td align="center" valign="middle" >5.150873072265E−01</td><td align="center" valign="middle" >1.179056852152E−13</td></tr><tr><td align="center" valign="middle" >1.10</td><td align="center" valign="middle" >5.190133197868E−01</td><td align="center" valign="middle" >5.190133197871E−01</td><td align="center" valign="middle" >2.902122986370E−13</td></tr><tr><td align="center" valign="middle" >1.20</td><td align="center" valign="middle" >5.166544364783E−01</td><td align="center" valign="middle" >5.166544364787E−01</td><td align="center" valign="middle" >4.607425552194E−13</td></tr><tr><td align="center" valign="middle" >1.30</td><td align="center" valign="middle" >5.090162464214E−01</td><td align="center" valign="middle" >5.090162464221E−01</td><td align="center" valign="middle" >6.451505996097E−13</td></tr><tr><td align="center" valign="middle" >1.40</td><td align="center" valign="middle" >4.972489648573E−01</td><td align="center" valign="middle" >4.972489648581E−01</td><td align="center" valign="middle" >8.351652702743E−13</td></tr><tr><td align="center" valign="middle" >1.50</td><td align="center" valign="middle" >4.826498351587E−01</td><td align="center" valign="middle" >4.826498351598E−01</td><td align="center" valign="middle" >1.023958695612E−12</td></tr><tr><td align="center" valign="middle" >1.60</td><td align="center" valign="middle" >4.666641592316E−01</td><td align="center" valign="middle" >4.666641592328E−01</td><td align="center" valign="middle" >1.214361944335E−12</td></tr><tr><td align="center" valign="middle" >1.70</td><td align="center" valign="middle" >4.508850642096E−01</td><td align="center" valign="middle" >4.508850642110E−01</td><td align="center" valign="middle" >1.404265592697E−12</td></tr><tr><td align="center" valign="middle" >1.80</td><td align="center" valign="middle" >4.370521379547E−01</td><td align="center" valign="middle" >4.370521379563E−01</td><td align="center" valign="middle" >1.590561016229E−12</td></tr><tr><td align="center" valign="middle" >1.90</td><td align="center" valign="middle" >4.270490905788E−01</td><td align="center" valign="middle" >4.270490905806E−01</td><td align="center" valign="middle" >1.771249813487E−12</td></tr><tr><td align="center" valign="middle" >2.00</td><td align="center" valign="middle" >4.229006237963E−01</td><td align="center" valign="middle" >4.229006237983E−01</td><td align="center" valign="middle" >1.950384298510E−12</td></tr></tbody></table></table-wrap><p>based on numerical differentiation are found to be absolutely stable outside some closed boundaries. 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