<?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">OALibJ</journal-id><journal-title-group><journal-title>Open Access Library Journal</journal-title></journal-title-group><issn pub-type="epub">2333-9705</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/oalib.1101345</article-id><article-id pub-id-type="publisher-id">OALibJ-68482</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Biomedical&amp;Life Sciences</subject><subject> Business&amp;Economics</subject><subject> Chemistry&amp;Materials Science</subject><subject> Computer Science&amp;Communications</subject><subject> Earth&amp;Environmental Sciences</subject><subject> Engineering</subject><subject> Medicine&amp;Healthcare</subject><subject> Physics&amp;Mathematics</subject><subject> Social Sciences&amp;Humanities</subject></subj-group></article-categories><title-group><article-title>
 
 
  Of a Fatigued Thick-Walled Cylindrical Pipe on the Brink of Yielding
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Nzerem</surname><given-names>Francis Egenti</given-names></name><xref ref-type="aff" rid="aff1"><sub>1</sub></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff1"><label>1</label><addr-line>Department of Mathematics and Statistic, University of Port Harcourt, Port Harcourt, Nigeria</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>frankjournals@yahoo.com</email></corresp></author-notes><pub-date pub-type="epub"><day>31</day><month>07</month><year>2015</year></pub-date><volume>02</volume><issue>07</issue><fpage>1</fpage><lpage>6</lpage><history><date date-type="received"><day>14</day>	<month>June</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>30</month>	<year>June</year>	</date><date date-type="accepted"><day>7</day>	<month>July</month>	<year>2015</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
   
   The response to stress delivered by a non-isochoric hollow cylinder is critical to its future life and integrity. The design of cylinders must emphasize durability; therefore, the knowledge of the yield stress of the constituent material is essential. The stress component of a pressurized compressible circular cylinder made of non-linearly elastic material was considered here and the yield stress was determined. 
  
 
</p></abstract><kwd-group><kwd>Compressible</kwd><kwd> Pressure</kwd><kwd> Deformation Tensor</kwd><kwd> Elasto-Plastic Material</kwd><kwd> Strain</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Numerous literatures have considered stress onaxisymmetrically pressurized cylinders. When internally pressurized hollow circular cylinder is being considered, it is customary to assume that the cylinder has to contend with radial, hoop (circumferential) and axial stresses. The magnitude of the response to stress is related to the material constitution of the cylinder. In recent times several works [<xref ref-type="bibr" rid="scirp.68482-ref1">1</xref>] - [<xref ref-type="bibr" rid="scirp.68482-ref3">3</xref>] have considered the elasto-plastic materials as being able to meet the exigencies of modern times. The recourse to the elasto-plastic approach may be borne out of the relative availability and cost effectiveness of the plastic component. This approach is, however, not a paradigm shift from completely elastic materials.</p><p>The works done by Blatz and Ko [<xref ref-type="bibr" rid="scirp.68482-ref4">4</xref>] , Chung et al. [<xref ref-type="bibr" rid="scirp.68482-ref5">5</xref>] , Hills and Ariggo [<xref ref-type="bibr" rid="scirp.68482-ref6">6</xref>] dealt on materials of nonlinear elasticity. The question of stress-induced fatigue is a sine qua non for the design of conduit pipes. Although static response to stress immanent in materials accounts for the life span and integrity of pipes, relative longevity resides in those made of materials of (non-)linear elasticity, all else being equal. The need to increase the life span of conduits dominates every argument. It is this need that gives rise to the autofrettage process being adopted in present times. The process applies a sufficiently high pressure to the cylinder before it is put in use. The withdrawal of the internally applied pressure induces a residual stress on the part of the cylinder thickness which has become plastic. This would in effect help the cylinder to cushion the effect of high pressures in event of use. This process means well for elasto-plastic cylinders. It is gaining currency, as can be seen in literatures [<xref ref-type="bibr" rid="scirp.68482-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.68482-ref7">7</xref>] [<xref ref-type="bibr" rid="scirp.68482-ref8">8</xref>] . In any case, repeated or prolonged stress is usually implicated in material fatigue. Fatigue is a grave engineering liability, together with its attendant economic implications. The aforesaid underscores the need to determine the measure of stress applicable to a cylindrical medium under consideration. This paper therefore presented a theoretical formulation of pressure limits of a thick-walled cylinder, made of a non-linearly elastic material. This was done in the following order: Section 2 proposed the model of an axially symmetric hollow cylinder, of Blatz-Ko material, subjected to plane strain. The Cauchy-Green deformation tensors were used in determining the components of stress on the cylinder. Section 3 formulated a boundary-value problem (b.v.p) in which pressure p accounted for the radial stress in the cylinder. The emerging equation, together with boundary conditions, was transformed with the aid of a suitable transformation equation (see Equation (21)). The transformation successfully linearized the boundary conditions and facilitated the solution to the b.v.p. In event of this, the components of stress, with pressure content, were determined. Section 4 furnished the yield criterion. It supplied the critical stresses with the aid of Tresca yield criterion. Previous literatures may have sought a compact expression for the yield stress on the material under consideration; perhaps this is the missing link.</p></sec><sec id="s2"><title>2. Deformation of the Cylinder</title><p>We consider a hollow cylinder whose reference configuration is</p><disp-formula id="scirp.68482-formula4"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x5.png"  xlink:type="simple"/></disp-formula><p>where a is the inner radius and b is the outer radius of the cylinder. Its deformed configuration is given by the mapping</p><disp-formula id="scirp.68482-formula5"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x6.png"  xlink:type="simple"/></disp-formula><p>For this axisymmetric plane strain, it suffices to assume that R(r) is twice continuously differentiable, and we write</p><disp-formula id="scirp.68482-formula6"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x7.png"  xlink:type="simple"/></disp-formula><p>The deformation gradient tensor F associated with (3) is</p><disp-formula id="scirp.68482-formula7"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x8.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/68482x9.png" xlink:type="simple"/></inline-formula>. The tensor F is required to satisfy the non-singularity condition by virtue of the local invertibility of χ. Moreover, we suppose detF &gt; 0. The assumption of the existence of strain at some point X &#206; R<sub>o</sub> ensues that</p><disp-formula id="scirp.68482-formula8"><label>, (5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x10.png"  xlink:type="simple"/></disp-formula><p>where I is the identity tensor, the superscripted T indicates the transpose of F. (Note that X are position vectors of points in R<sub>o</sub>). A class of materials under consideration is characterized by the strain energy density function W(I, J), whose related Blatz-Ko model is given by [<xref ref-type="bibr" rid="scirp.68482-ref5">5</xref>]</p><disp-formula id="scirp.68482-formula9"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x11.png"  xlink:type="simple"/></disp-formula><p>where μ is the initial shear modulus of the material. The function W is just one among the scalar functions of strain tensors used in determining stress components. In terms of the second Piola-Kirchhoff’s (PK-2) stress tensor S<sub>ij</sub>, we have</p><disp-formula id="scirp.68482-formula10"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x12.png"  xlink:type="simple"/></disp-formula><p>where S<sub>ij</sub> is the component of the PK-2 stress tensor, W is the strain energy function per unit undeformed volume, E<sub>ij</sub> is the component of the Lagrangean strain tensor and C<sub>ij</sub> is the Cauchy-Green deformation tensor.</p><p>The associated right Cauchy-Green deformation tensors is</p><disp-formula id="scirp.68482-formula11"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x13.png"  xlink:type="simple"/></disp-formula><p>With the invariants, I and J as</p><disp-formula id="scirp.68482-formula12"><graphic  xlink:href="http://html.scirp.org/file/68482x14.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68482-formula13"><label>. (9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x15.png"  xlink:type="simple"/></disp-formula><p>With the principal stretches</p><disp-formula id="scirp.68482-formula14"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x16.png"  xlink:type="simple"/></disp-formula><p>The stress tensor σ associated with this deformation is given by</p><disp-formula id="scirp.68482-formula15"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x17.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/68482x18.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/68482x19.png" xlink:type="simple"/></inline-formula>and I is the identity tensor.</p><p>From Equation (6) we get</p><disp-formula id="scirp.68482-formula16"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x20.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68482-formula17"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x21.png"  xlink:type="simple"/></disp-formula><p>Using equation (8), (12) and (13) in (11) we get the following stress component</p><disp-formula id="scirp.68482-formula18"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x22.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68482-formula19"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x23.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68482-formula20"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x24.png"  xlink:type="simple"/></disp-formula></sec><sec id="s3"><title>3. Boundary-Value Problem</title><p>When uniform pressure is applied at the boundaries, the circumferential component of displacement is zero, and the radial component will depend on the radial distance r only. The stress components will therefore depend on r only. If body force is absent, the equilibrium equation is given by</p><disp-formula id="scirp.68482-formula21"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x25.png"  xlink:type="simple"/></disp-formula><p>Using Equations (14) and (15) in Equation (17) we get the equation for R(r) as</p><disp-formula id="scirp.68482-formula22"><label>, (18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x26.png"  xlink:type="simple"/></disp-formula><p>with the constraints</p><disp-formula id="scirp.68482-formula23"><graphic  xlink:href="http://html.scirp.org/file/68482x27.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68482-formula24"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x28.png"  xlink:type="simple"/></disp-formula><p>The Equations (19) may be rewritten, using (14) and (15), as</p><disp-formula id="scirp.68482-formula25"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x29.png"  xlink:type="simple"/></disp-formula><p>We apply the transformation similar to Ejike and Erumaka [<xref ref-type="bibr" rid="scirp.68482-ref9">9</xref>] , (also see [<xref ref-type="bibr" rid="scirp.68482-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.68482-ref11">11</xref>] )</p><disp-formula id="scirp.68482-formula26"><label>(21)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x30.png"  xlink:type="simple"/></disp-formula><p>Equation (18) becomes</p><disp-formula id="scirp.68482-formula27"><label>(22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x31.png"  xlink:type="simple"/></disp-formula><p>and the line arized boundary conditions (20) are</p><disp-formula id="scirp.68482-formula28"><label>(23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x32.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68482-formula29"><label>(24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x33.png"  xlink:type="simple"/></disp-formula><p>The series solution approach of the form</p><disp-formula id="scirp.68482-formula30"><label>(25)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x34.png"  xlink:type="simple"/></disp-formula><p>was employed rigorously by Nzerem [<xref ref-type="bibr" rid="scirp.68482-ref11">11</xref>] which yielded</p><disp-formula id="scirp.68482-formula31"><label>(26)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x35.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.68482-formula32"><label>(27)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x36.png"  xlink:type="simple"/></disp-formula><p>The resulting stress components are</p><disp-formula id="scirp.68482-formula33"><label>(28)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x37.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68482-formula34"><label>(29)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x38.png"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. Yield Criterion</title><p>Yielding becomes imminent when the maximum shear stress in the material equals the maximum shear stress. Thus, Tresca yield criterion [<xref ref-type="bibr" rid="scirp.68482-ref12">12</xref>] specifies that</p><disp-formula id="scirp.68482-formula35"><label>(30)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x39.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.68482-formula36"><label>, (31)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x40.png"  xlink:type="simple"/></disp-formula><p>σ<sub>max</sub> and σ<sub>min</sub> are the maximum and minimum principal stresses respectively. From the foregoing we get</p><disp-formula id="scirp.68482-formula37"><label>. (32)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x41.png"  xlink:type="simple"/></disp-formula><p>Thus, we get</p><disp-formula id="scirp.68482-formula38"><label>(33)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x42.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/68482x43.png" xlink:type="simple"/></inline-formula>. The outer surface pressure limit can be obtained through</p><disp-formula id="scirp.68482-formula39"><label>(34)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/68482x44.png"  xlink:type="simple"/></disp-formula><p>Equations (33) and (34) contain pressure (see Equation (27)); therefore, the non-dimensionalized inner and outer surface pressure limit can be obtained by solving for p.</p></sec><sec id="s5"><title>5. Conclusion</title><p>The need to ascertain the fatigue point of a thick-walled cylinder under stress is crucial in estimating the life span of the cylinder. The stress component must be known before determining the yield stress. In this work, the stress component was determined. The cylinder under consideration was made of compressible non-linearly elastic (Blatz-Ko) material. The yield stress was determined with the aid of Tresca criterion.</p></sec><sec id="s6"><title>Acknowledgements</title><p>The author is grateful to the reviewers of this paper for their useful comments.</p></sec><sec id="s7"><title>Cite this paper</title><p>Nzerem Francis Egenti, (2015) Of a Fatigued Thick-Walled Cylindrical Pipe on the Brink of Yielding. Open Access Library Journal,02,1-6. doi: 10.4236/oalib.1101345</p></sec></body><back><ref-list><title>References</title><ref id="scirp.68482-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Ayob, A.B., Tamin, M.N. and Elbasheer, M.K. (2009) Pressure Limits of Thick-Walled Cylinders. Proceedings of the International Multi-Conference of Engineers and Computer Scientists 2009, Vol. II IMECS, 18-20 March 2009.</mixed-citation></ref><ref id="scirp.68482-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Wang, Z. (1995) Elastic-Plastic Fracture Analysis of a Thick-Walled Cylinder. International Journal of Pressure Vessels and Piping, 63, 165-168. http://dx.doi.org/10.1016/0308-0161(94)00048-N</mixed-citation></ref><ref id="scirp.68482-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Chaaban, A. and Barake, N. (1993) Elasto-Plastic Analysis of High Pressure Vessels with Radial Cross Bores. 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