<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">JAMP</journal-id><journal-title-group><journal-title>Journal of Applied Mathematics and Physics</journal-title></journal-title-group><issn pub-type="epub">2327-4352</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/jamp.2015.37092</article-id><article-id pub-id-type="publisher-id">JAMP-57628</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Perturbation Solutions for Annular Flow of Small Gap
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Xiaojian</surname><given-names>Cao</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>Yuefang</surname><given-names>Wang</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Engineering Mechanics, Dalian University of Technology, Dalian, China</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>cxjdlut@mail.dlut.edu.cn(XC)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>30</day><month>06</month><year>2015</year></pub-date><volume>03</volume><issue>07</issue><fpage>761</fpage><lpage>765</lpage><history><date date-type="received"><day>1</day>	<month>April</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>23</month>	<year>June</year>	</date><date date-type="accepted"><day>30</day>	<month>June</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 perturbation method is used to solve the control equations of a three-dimensional annular flow inside a small gap. The nonlinear equations are separated into zeroth-order and first-order perturbation equations. The velocity and pressure distributions are solved successively by different numerical methods with the zeroth-order and first-order equation. Agreement in results is found with the present method and software ANSYS-CFX, which illustrates the applicability of perturbation method in solving complicated flow field inside small gaps.  
     
 
</p></abstract><kwd-group><kwd>Perturbation</kwd><kwd> Annular Flow</kwd><kwd> Gap</kwd><kwd> Velocity</kwd><kwd> Pressure</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The annular flow inside small gaps between rotors and stators can be found in many fluid circumstances such as sliding bearings, radial dynamic pressure seals, submersible pumps and nuclear pumps. The study of dynamical effects related to gap fluid field has been one of the research hotspots of fluid mechanics. Fritz [<xref ref-type="bibr" rid="scirp.57628-ref1">1</xref>] investigated the dynamics model of an annular flow with large gap and simplified it to a two-dimensional incompressible fluid flow field. However, this model suffered from a disadvantage that it ignored the impact of the axial flow of the fluid. Hirs [<xref ref-type="bibr" rid="scirp.57628-ref2">2</xref>] proposed the theory of the turbulence overall flow which was applied to investigate the three- dimensional turbulent flow field of a seal ring by Childs [<xref ref-type="bibr" rid="scirp.57628-ref3">3</xref>]. Nelson [<xref ref-type="bibr" rid="scirp.57628-ref4">4</xref>] believed Moody wall friction coefficient equations [<xref ref-type="bibr" rid="scirp.57628-ref5">5</xref>] were more reasonable than Hirs wall friction coefficient equations in the study of the annular flow with gap. Antunes [<xref ref-type="bibr" rid="scirp.57628-ref6">6</xref>] studied the static and dynamic characteristics of an annular eccentric rotor with large gap based on the overall flow theory and Hirs wall friction coefficient equation. Moody wall friction coefficient equations are widely applied in the study of the dynamics of the seal ring subjected to the radial pressure. Sun [<xref ref-type="bibr" rid="scirp.57628-ref7">7</xref>] proposed the dynamic modeling of a 3D annular flow with large gap using the overall flow.</p><p>In this study, the perturbation method is used to solve three-dimensional control equations of an annular fluid flow inside a small gap that separates a rotating shaft and a fixed stator. The equations are expanded into zeroth- order and first-order perturbation equations of small eccentricity. The velocity and pressure distribution for the flow domain are solved successively with the zeroth-order and first-order equations by difference methods.</p></sec><sec id="s2"><title>2. Control Equations for Flow</title><p>Consider a small-sized control volume, CV, shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>, across a fluctuating gap thickness, with the whole boundary CS. The continuity equation and the momentum equation of three-dimensional annular flow of a small gap can be written as:</p><disp-formula id="scirp.57628-formula292"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x4.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.57628-formula293"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x5.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/57628x6.png" xlink:type="simple"/></inline-formula> is fluid volume mass, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/57628x7.png" xlink:type="simple"/></inline-formula>is the velocity of the fluid crossing CS, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/57628x8.png" xlink:type="simple"/></inline-formula>is the local unit vector normal to the boundary. <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/57628x9.png" xlink:type="simple"/></inline-formula>is the external and volume force acting on the fluid in CV.</p><p>The control equations can be expressed based on overall flow theory and Moody’s wall friction coefficient equations [<xref ref-type="bibr" rid="scirp.57628-ref5">5</xref>]:</p><disp-formula id="scirp.57628-formula294"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x10.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.57628-formula295"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x11.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.57628-formula296"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x12.png"  xlink:type="simple"/></disp-formula></sec><sec id="s3"><title>3. Perturbation Expression</title><p>For nonlinear ordinary and partial differential equations, perturbation methods can be used to quantify the change in solution with respect to unperturbed linear systems due to tiny disturbance to parameters. These methods have been used and developed in various fields with different backgrounds [<xref ref-type="bibr" rid="scirp.57628-ref8">8</xref>]-[<xref ref-type="bibr" rid="scirp.57628-ref10">10</xref>].</p><p>The eccentricity of the rotor shaft is defined as the small disturbance in this study. The thickness of the gap, the pressure and velocity of the annular flow are assumed to be:</p><disp-formula id="scirp.57628-formula297"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x13.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/57628x14.png" xlink:type="simple"/></inline-formula> is the small parameter, being small eccentricity of the shaft centroid in this study.</p><p>Equations (3) through (5) are separated in terms of order of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/57628x15.png" xlink:type="simple"/></inline-formula>, giving zeroth-order and first-order perturbation equations. The zeroth-order perturbation equations are as follows:</p><disp-formula id="scirp.57628-formula298"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x16.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.57628-formula299"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x17.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.57628-formula300"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x18.png"  xlink:type="simple"/></disp-formula><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Geometry of the annular flow of gap</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/57628x19.png"/></fig><p>The first-order perturbation equations are:</p><disp-formula id="scirp.57628-formula301"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x20.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.57628-formula302"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x21.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.57628-formula303"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x22.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.57628-formula304"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/57628x23.png"  xlink:type="simple"/></disp-formula><p>The difference method is used to discretize the zeroth-order perturbation equations. The nonlinear partial differential equations are transformed into algebraic equations. The zeroth-order solution is substituted into the first-order perturbation equations to obtain the solution of the first order. The results of Equations (3) through (5) are the addition of zeroth-order perturbation solutions to Equations (7) through (9) and the first-order perturbation solutions to Equations (10) through (12).</p></sec><sec id="s4"><title>4. Results of the Flow Field</title><p>Numerical simulations using software ANSYS-CFX [<xref ref-type="bibr" rid="scirp.57628-ref11">11</xref>] are carried out to verify the perturbation solution obtained from the present method. An example is illustrated with boundary conditions of a 5 m/s velocity at inlet and a zero pressure at outlet. The results of pressure and circumferential velocity obtained through the perturbation equations are compared with those obtained through ANSYS-CFX, as illustrated in <xref ref-type="fig" rid="fig2">Figure 2</xref> and <xref ref-type="fig" rid="fig3">Figure 3</xref>.</p><p>The results displayed in <xref ref-type="fig" rid="fig2">Figure 2</xref>(a) are the solution to the zeroth-order perturbation equations. It is noticed that the pressure distribution is axially symmetric. The closer of a position to the inlet is, the greater its pressure will be, which is qualitatively consistent with the results through ANSYS-CFX shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>(b). Similarly, the circumferential velocity obtained through the zeroth-order perturbation equations in <xref ref-type="fig" rid="fig3">Figure 3</xref> shows the same trend with those calculated by ANSYS-CFX. The profile of velocity is also centrosymmetric, and the farther to the inlet is, the greater the circumferential velocity will be. The solutions to the first-order perturbation,</p><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Comparison of pressure distribution. (a) Perturbation solution; (b) ANSYS-CFX.</title></caption><fig id ="fig2_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/57628x24.png"/></fig><fig id ="fig2_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/57628x25.png"/></fig></fig-group><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Comparison of circumferential velocity distribution. (a) Perturbation method; (b) ANSYS-CFX.</title></caption><fig id ="fig3_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/57628x26.png"/></fig><fig id ="fig3_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/57628x27.png"/></fig></fig-group><p>equations also agree well with the results through ANSYS-CFX qualitatively which will not be discussed any further.</p></sec><sec id="s5"><title>5. Conclusion</title><p>The solution to a three-dimensional annular flow inside a small gap between rotor and stator is obtained using zeroth-order and first-order perturbed control equations. The perturbed solutions are compared with the numerical results through ANSYS-CFX and they are found to agree qualitatively. Consequently, it is applicable to solve three-dimensional nonlinear control equations of the small-gap annular fluid when the eccentricity of axis is small enough compared with the average clearance between the rotor and the stator.</p></sec><sec id="s6"><title>Acknowledgements</title><p>This paper is sponsored by the National Basic Research Program of China (Grant 2015CB057300), the Key Specific Projects of Liaoning Scientific Innovation (201303002), Liaoning Provincial Science and Technology Programs(2014010499-301), Program of Cultivated Key Project of Dalian University of Technology, and the Free Exploration Project of State Key Laboratory of Structural Analysis for Industrial Equipment (S14204).</p></sec><sec id="s7"><title>Cite this paper</title><p>Xiaojian Cao,Yuefang Wang, (2015) Perturbation Solutions for Annular Flow of Small Gap. Journal of Applied Mathematics and Physics,03,761-765. doi: 10.4236/jamp.2015.37092</p></sec><sec id="s8"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.57628-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Fritz, R.J. (1970) The Effects of an Annular Fluid on the Vibrations of a Long Rotor, Part 1-Theory. Journal of Basic Enginneering, 1970, 923-929. http://dx.doi.org/10.1115/1.3425165</mixed-citation></ref><ref id="scirp.57628-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Hirs, G.G. (1973) A Bulk-Flow Theory for Turbulence in Lubrication Film. ASME Journal of Lubrication Technology, 95, 137-146. http://dx.doi.org/10.1115/1.3451752</mixed-citation></ref><ref id="scirp.57628-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Childs, D.W. (1983) Dynamic Analysis of Turbulent Annular Seals Base on Hirs’ Lubrication Equation. 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