<?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">WJET</journal-id><journal-title-group><journal-title>World Journal of Engineering and Technology</journal-title></journal-title-group><issn pub-type="epub">2331-4222</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/wjet.2016.42020</article-id><article-id pub-id-type="publisher-id">WJET-66338</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Chemistry&amp;Materials Science</subject><subject> Engineering</subject></subj-group></article-categories><title-group><article-title>
 
 
  Heat Transfer Efficiency of Turbulent Film Boiling on a Horizontal Elliptical Tube with External Flowing Liquid
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>ai-Ping</surname><given-names>Hu</given-names></name><xref ref-type="aff" rid="aff1"><sub>1</sub></xref></contrib></contrib-group><aff id="aff1"><label>1</label><addr-line>Department of Marine Engineering, National Taiwan Ocean University, Taiwan</addr-line></aff><author-notes><corresp id="cor1">* E-mail:</corresp></author-notes><pub-date pub-type="epub"><day>29</day><month>04</month><year>2016</year></pub-date><volume>04</volume><issue>02</issue><fpage>206</fpage><lpage>219</lpage><history><date date-type="received"><day>17</day>	<month>March</month>	<year>2016</year></date><date date-type="rev-recd"><day>accepted</day>	<month>8</month>	<year>May</year>	</date><date date-type="accepted"><day>11</day>	<month>May</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>
 
 
  Film boiling on a horizontal elliptical tube immersed in external flowing nitrogen liquid is investigated in the present paper. The isothermal wall temperature is high enough to induce turbulent film boiling, and then a continuous vapor film runs upward over the surface. The high velocity of the flowing saturated liquid at the boundary layer is determined by potential flow theory. In addition, the present paper addresses a new model to predict the vapor-liquid interfacial shear on an elliptical tube under forced convection turbulent film boiling. In the results, film thickness and Nusselt number can be obtained under different eccentricity and Froude number. And a comparison between the results of the present study and those reported in previous experimental studies is provided. The results show that there is a good agreement between the present paper and the experimental data.
 
</p></abstract><kwd-group><kwd>Eccentricity</kwd><kwd> Elliptical</kwd><kwd> Interfacial Shear</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The pioneering investigator, Bromley [<xref ref-type="bibr" rid="scirp.66338-ref1">1</xref>] , conducted the research of film boiling on a horizontal tube. After Bromley’s research, many related researches had been reported. In 1966, Nishikawa and Ito [<xref ref-type="bibr" rid="scirp.66338-ref2">2</xref>] analyzed two- phase boundary-layer treatment of free-convection film boiling. The theoretical study investigated on film boiling from an isothermal vertical plate and a horizontal cylinder without considering radiative effects. Jordan [<xref ref-type="bibr" rid="scirp.66338-ref3">3</xref>] investigated the laminar film boiling and transition boiling, and the also discussed the separated region. Sakurai et al. [<xref ref-type="bibr" rid="scirp.66338-ref4">4</xref>] presented the pool film boiling on a horizontal cylinder with theoretical solutions. The analytical heat transfer model was based on laminar boundary theory including radiation effects. Besides, Huang et al. [<xref ref-type="bibr" rid="scirp.66338-ref5">5</xref>] conducted the research on the forced convection film boiling. They investigated the flow film boiling across a horizontal cylinder with uniform heat flux. The numerical results agreed with experimental data where the wall temperature did not vary a lot around the heater at high heat fluxes.</p><p>Laminar film boiling had been widely discussed in published literature, and so has turbulent film boiling. For example, Sarma et al. [<xref ref-type="bibr" rid="scirp.66338-ref6">6</xref>] presented turbulent film boiling with consideration to thermal radiation for the vertical surface. In the research, the assumption of equal shear condition both at the wall and the vapor-liquid interface was reasonable. Later, Sarma et al. [<xref ref-type="bibr" rid="scirp.66338-ref7">7</xref>] presented some theoretical results about the turbulent film boiling on a horizontal isothermal circular cylinder. The analysis compared the theoretical results with previous experimental results, and found that their results were in a good agreement with the experimental data. Hu [<xref ref-type="bibr" rid="scirp.66338-ref8">8</xref>] presented the surface tension effects in boiling heat transfer of cryogenic LN<sub>2</sub> on an ellipsoid. However, the study just researched into a simple theoretical model for turbulent film boiling heat transfer on an ellipsoid under a quiescent liquid. Furthermore, Hu [<xref ref-type="bibr" rid="scirp.66338-ref9">9</xref>] investigated the influences of interfacial shear in turbulent film boiling on a horizontal tube with external flowing liquid.</p><p>Even though there were many researches about laminar film boiling and turbulent film boiling, there was little publication about the turbulent film boiling on a horizontal elliptical tube which his high velocity liquid was flowing outside. Predicting interfacial shear in a turbulent film boiling system under high velocity liquid was not easy. However, the present paper successfully predicted the vapor-liquid interfacial shear by using Colburn analogy. The present study applied the interfacial shear into the forced balance equation, and then combined the forced balance equation with the energy equation and thermal energy balance equation. At last, both the film thickness and Nusselt number were obtained. Then, the present analysis also included eddy diffusivity, radiation effects and temperature ratio. Finally, a comparison between the results of the present study and those reported in previous experimental studies was provided. It was found that a good agreement exists between the two sets of results.</p></sec><sec id="s2"><title>2. Formulations</title><p>Consider a horizontal elliptical tube immersed in an up flowing LN2 of the high velocity <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x6.png" xlink:type="simple"/></inline-formula> at saturated temperature T<sub>s</sub>. The wall temperature <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x7.png" xlink:type="simple"/></inline-formula> is assumed high enough to induce turbulent film boiling on the surface of the elliptical tube, and then a continuous film of vapor runs upward over the surface. The physical model and the coordinate system adopted in the present study are shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>, where the coordinates is use two-dimen- sional orthogonal curvilinear coordinate system.</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Physical model and coordinate system</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1560296x8.png"/></fig><p>For thin film flow of turbulent film boiling under the forced convection, the viscosity component and the buoyancy effect are assumed more significant than the inertia force. Then the force balance equation for the vapor film can be expressed as:</p><disp-formula id="scirp.66338-formula534"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x9.png"  xlink:type="simple"/></disp-formula><p>It is assumed the thickness of vapor film is much thinner than the diameter of the tube (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x10.png" xlink:type="simple"/></inline-formula>). And it’s further assumed the turbulent conduction term across the vapor layer is more significant than the convective term, and hence the convective term can be neglected. The energy equation can be expressed as:</p><disp-formula id="scirp.66338-formula535"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x11.png"  xlink:type="simple"/></disp-formula><p>The boundary conditions of energy equation under isothermal condition are as follows:</p><disp-formula id="scirp.66338-formula536"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x12.png"  xlink:type="simple"/></disp-formula><p>For a pure substance, the thermal energy balance equation of the vapor film can be expressed as:</p><disp-formula id="scirp.66338-formula537"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x13.png"  xlink:type="simple"/></disp-formula><p>The differential arc length for ellipse can be expressed with the following equation:</p><disp-formula id="scirp.66338-formula538"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x14.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.66338-formula539"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x15.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.66338-formula540"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x16.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x17.png" xlink:type="simple"/></inline-formula> is an equivalent diameter based on the equal outside surface area, which is compared with circular tubes.</p><p>Substitute the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x18.png" xlink:type="simple"/></inline-formula> into thermal energy balance equation, and (Equation (4)) can be modified as follows:</p><disp-formula id="scirp.66338-formula541"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x19.png"  xlink:type="simple"/></disp-formula><p>In the turbulent region the semi-empirical equation which describes heat transfer in the flow parallel to a moderately curved surface may also be used to describe the heat transfer in the flow parallel to an elliptical surface. Jakob [<xref ref-type="bibr" rid="scirp.66338-ref10">10</xref>] proposed that this situation may be described for any fluid by the following expression:</p><disp-formula id="scirp.66338-formula542"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x20.png"  xlink:type="simple"/></disp-formula><p>where C is a constant in flow configuration, C = 0.034.</p><p>According to Colburn analogy, the friction factor can be written as the following equation:</p><disp-formula id="scirp.66338-formula543"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x21.png"  xlink:type="simple"/></disp-formula><p>The mean friction coefficient in the streamwise direction may then be calculated as:</p><disp-formula id="scirp.66338-formula544"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x22.png"  xlink:type="simple"/></disp-formula><p>Furthermore, the local friction can be obtained as:</p><disp-formula id="scirp.66338-formula545"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x23.png"  xlink:type="simple"/></disp-formula><p>The turbulent boundary layer exerts a friction force on the liquid-vapor boundary. The shear stress is estimated by considering the external flowing liquid across the surface of the tube when there is no vapor film on the surface. The local shear stress is defined as:</p><disp-formula id="scirp.66338-formula546"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x24.png"  xlink:type="simple"/></disp-formula><p>According to potential flow theory, when the uniform liquid flow of velocity <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x25.png" xlink:type="simple"/></inline-formula> passing a tube, the liquid velocity at the edge of the boundary is as follows:</p><disp-formula id="scirp.66338-formula547"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x26.png"  xlink:type="simple"/></disp-formula><p>Combining Equations (12)-(14), the local shear stress can be expressed as:</p><disp-formula id="scirp.66338-formula548"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x27.png"  xlink:type="simple"/></disp-formula><p>Incorporating the interfacial vapor shear stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x28.png" xlink:type="simple"/></inline-formula> given by Equation (15) into the elemental forced balance equation enables Equation (1) to be rewritten in the following form:</p><disp-formula id="scirp.66338-formula549"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x29.png"  xlink:type="simple"/></disp-formula><p>The forced balance equation Equation (17) yields the following dimensionless equation:</p><disp-formula id="scirp.66338-formula550"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x30.png"  xlink:type="simple"/></disp-formula><p>It’s further assuming the pressure across the boundary layer is constant and the density variation across the boundary layer is given by the following equation:</p><disp-formula id="scirp.66338-formula551"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x31.png"  xlink:type="simple"/></disp-formula><p>The energy equation Equation (2) yields the following dimensionless energy equation:</p><disp-formula id="scirp.66338-formula552"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x32.png"  xlink:type="simple"/></disp-formula><p>The dimensionless boundary conditions of Equation (19) are:</p><disp-formula id="scirp.66338-formula553"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x33.png"  xlink:type="simple"/></disp-formula><p>where the absolute viscosity equation <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x34.png" xlink:type="simple"/></inline-formula> in dimensionless energy equation Equation (19) is expressed as the vapors of liquid nitrogen at the saturation temperature corresponding to a system pressure under 1 atm. i.e.</p><disp-formula id="scirp.66338-formula554"><label>(21)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x35.png"  xlink:type="simple"/></disp-formula><p>Besides, the thermal energy balance equation Equation (8) can be rewritten in dimensionless form as follows:</p><disp-formula id="scirp.66338-formula555"><label>(22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x36.png"  xlink:type="simple"/></disp-formula><p>where the absolute conductivity equation <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x37.png" xlink:type="simple"/></inline-formula> in thermal energy balance equation Equation (22) is expressed as the vapors of liquid nitrogen the saturation temperature corresponding to a system pressure under 1 atm.:</p><disp-formula id="scirp.66338-formula556"><label>(23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x38.png"  xlink:type="simple"/></disp-formula><p>Furthermore, the dimensionless thermal energy balance equation Equation (22) requires the velocity profile <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x39.png" xlink:type="simple"/></inline-formula> in the vapor film. And <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x39.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x40.png" xlink:type="simple"/></inline-formula> can be obtained by following equation:</p><disp-formula id="scirp.66338-formula557"><label>(24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x41.png"  xlink:type="simple"/></disp-formula><p>The boundary condition is:</p><disp-formula id="scirp.66338-formula558"><label>(25)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x42.png"  xlink:type="simple"/></disp-formula><p>The eddy diffusivity distribution presented by Kato et al. [<xref ref-type="bibr" rid="scirp.66338-ref11">11</xref>] is expressed as:</p><disp-formula id="scirp.66338-formula559"><label>(26)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x43.png"  xlink:type="simple"/></disp-formula><p>The heat transfer of turbulent film boiling can be given by the following equation:</p><disp-formula id="scirp.66338-formula560"><label>(27)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x44.png"  xlink:type="simple"/></disp-formula><p>Obviously, the local Nusselt number can be expressed as:</p><disp-formula id="scirp.66338-formula561"><label>(28)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x45.png"  xlink:type="simple"/></disp-formula><p>The mean Nusselt number for the entire surface of the tube can be written as:</p><disp-formula id="scirp.66338-formula562"><label>(29)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x46.png"  xlink:type="simple"/></disp-formula></sec><sec id="s3"><title>3. Numerical Method</title><p>The dimensionless governing Equations (17), (22)-(26) and (28), (29) subject to the relevant boundary conditions given can be used to estimate<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x47.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x47.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x48.png" xlink:type="simple"/></inline-formula>and Nu for the vapor film by means of the following procedures by using C<sup>++</sup>:</p><p>1) Suitable dimensionless parameters, such as e, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x49.png" xlink:type="simple"/></inline-formula>, S, NR, Fr and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x49.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x50.png" xlink:type="simple"/></inline-formula> are specified.</p><p>2) The boundary conditions of velocity and temperature are as follows:</p><disp-formula id="scirp.66338-formula563"><label>(30)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1560296x51.png"  xlink:type="simple"/></disp-formula><p>3) Since the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x52.png" xlink:type="simple"/></inline-formula> at the bottom of the tube (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x52.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x53.png" xlink:type="simple"/></inline-formula>, i = 0) is zero, the dimensionless film thickness δ<sup>+</sup> is also zero (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x52.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x54.png" xlink:type="simple"/></inline-formula>). At the next node, i.e. i = i + 1, the value of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x52.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x54.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x55.png" xlink:type="simple"/></inline-formula> is given by<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x52.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x54.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x55.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x56.png" xlink:type="simple"/></inline-formula>, where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x52.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x54.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x55.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x56.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x57.png" xlink:type="simple"/></inline-formula>.</p><p>4) Guess an initial value of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x58.png" xlink:type="simple"/></inline-formula>; substitute Equations (21), (26) into Equation (19) and then get the value of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x59.png" xlink:type="simple"/></inline-formula>.</p><p>5) Substitute<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x60.png" xlink:type="simple"/></inline-formula>, Equations (23), (24) and (25) into Equation (22), and get the value of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x60.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x61.png" xlink:type="simple"/></inline-formula>. After calculating, the values of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x60.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x61.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x62.png" xlink:type="simple"/></inline-formula> can be gotten, and then substitute the values of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x60.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x61.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x62.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x63.png" xlink:type="simple"/></inline-formula> into Equation (17).</p><p>6) The criterion for the accuracy of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x64.png" xlink:type="simple"/></inline-formula> is assessed by Equation (17), and it can be expressed as the following unequal equation:</p><disp-formula id="scirp.66338-formula564"><graphic  xlink:href="http://html.scirp.org/file/9-1560296x65.png"  xlink:type="simple"/></disp-formula><p>If the calculation is a convergence, process the film thickness of next angular position. If the calculation is not a convergence, guess a new thickness and repeat processes (4)-(6).</p><p>7) The process above is repeated at the next node position, i.e.<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x66.png" xlink:type="simple"/></inline-formula>, and then subsequently at all nodes within the range<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x66.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x67.png" xlink:type="simple"/></inline-formula>.</p><p>8) The local Nusselt number and mean Nusselt number are then calculated.</p></sec><sec id="s4"><title>4. Results and Discussion</title><p><xref ref-type="fig" rid="fig2">Figure 2</xref>(a) plots the three-dimensional local velocity distributions in vapor film for Fr = 500. For each angular position <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x68.png" xlink:type="simple"/></inline-formula> on the entire tube surface, it is shown that with an increase in y<sup>+</sup>, u<sup>+</sup> will increase to a maximum value, and then it will slightly decrease. The results also show that the dimensionless velocity increases with an increasing angular position on the elliptical surface. <xref ref-type="fig" rid="fig2">Figure 2</xref>(b) shows the two-dimensional equi-velocities in vapor film for Fr = 500. The dimensionless velocity at the wall of the elliptical tube is zero because of the no- slip condition and it will increase along the y-direction. This can be apprehended that the velocity will become larger due to the shear stress of vapor-liquid interface under the condition of flowing liquid.</p><p><xref ref-type="fig" rid="fig3">Figure 3</xref>(a) shows the velocity distribution of the vapor film on the entire elliptical tube. <xref ref-type="fig" rid="fig3">Figure 3</xref>(b) presents the two-dimensional isothermal lines in the vapor film. For the boundary conditions prescribed in the proposed model, the dimensionless temperature on the tube surface and on the vapor-liquid interface are unity and zero respectively. Furthermore, the assumption of the stagnation flow is imposed at the bottom of the tube. As a result, the temperature variation along the vapor film thickness at <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x69.png" xlink:type="simple"/></inline-formula> is linear. In addition, the interfacial shear with high velocity liquid, and the effects of turbulence are considered in this work. As the angular position increases, the effects of eddy diffusivity get stronger and the non-linear temperature profile of the vapor film appears.</p><p><xref ref-type="fig" rid="fig4">Figure 4</xref> displays the variation of the dimensionless vapor film thickness on the elliptical tube along<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x70.png" xlink:type="simple"/></inline-formula>. Specifically, the film thickness increases continuously from a minimum value at the bottom of the tube <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x70.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x71.png" xlink:type="simple"/></inline-formula> and reaches its maximum value at the top of the tube<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x70.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x71.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x72.png" xlink:type="simple"/></inline-formula>. Besides, according to potential theory, the increase in the eccentricity value will lead to a decrease in the liquid velocity. And the decrease in the liquid velocity will lead to the decrease in heat transfer efficiency and evaporative rate. The former phenomenon will bring about the decrease in the film thickness. Besides, the figure also states the influence of Fr on the film thickness. The film thickness will increase when Fr values increase. An increase in Fr will bring out an increase in the interfacial shear stress and then leads to an increase in the evaporative rate. Consequently, the increase of evaporative rate may cause an increase of the vapor film thickness.</p><p><xref ref-type="fig" rid="fig5">Figure 5</xref> presents the effects of eccentricity on mean Nusselt number under five different Froude numbers. According to the potential flow theory, the larger the eccentricity parameter is, the smaller the liquid velocity and interfacial shear are. Consequently, both the vapor velocity and the mean Nusselt number will decrease. Besides, under the condition of the forced convective film boiling, increasing Fr will result in an increase of the mean Nusselt numbers.</p><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> (a) Local velocity distribution in vapor film. (b) Constant dimensionless velocity lines in vapor film (Fr = 500, e = 0.6, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x75.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x75.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x76.png" xlink:type="simple"/></inline-formula>, S = 0.38, T<sub>r</sub> = 1.4, NR = 0.5).</title></caption><fig id ="fig2_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1560296x73.png"/></fig><fig id ="fig2_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1560296x74.png"/></fig></fig-group><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> (a) Local temperature distribution in vapor film. (b) Constant dimensionless temperature lines in vapor film (Fr = 500, e = 0.6, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x79.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x79.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x80.png" xlink:type="simple"/></inline-formula>, S = 0.38, T<sub>r</sub> = 1.4, NR = 0.5).</title></caption><fig id ="fig3_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1560296x77.png"/></fig><fig id ="fig3_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1560296x78.png"/></fig></fig-group><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Dimensionless film thickness on tube surface</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1560296x81.png"/></fig><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Effects of the eccentricity parameter on mean Nusselt number</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1560296x82.png"/></fig><p><xref ref-type="fig" rid="fig6">Figure 6</xref> presents the relationship between the mean Nusselt number and the Froude numbers for five values of Grashof number. The figure shows the results of the forced convection film boiling. A higher Froude number will bring an increase in the mean Nusselt. Besides, the Grashof number Gr is also one of the dominant factors, and therefore increasing the Grashof number will bring out an increase in the mean Nusselt.</p><p>To validate the present model, a comparison is made between this work and previous studies for different</p><p>cases. For this reason, a modified Rayleigh number is introduced as <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x83.png" xlink:type="simple"/></inline-formula> which can be further nondimensionalized in the form of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x83.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x84.png" xlink:type="simple"/></inline-formula>. <xref ref-type="fig" rid="fig7">Figure 7</xref> depicts the ef-</p><p>fects of Ra on the mean Nusselt numbers on an elliptical tube under e = 0 with special case of a tube subject to turbulent film boiling. It shows that the mean Nusselt number of the present study has a good agreement with previous experimental data [<xref ref-type="bibr" rid="scirp.66338-ref12">12</xref>] under the condition of quiescent liquid (i.e. Fr = 0 or<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x85.png" xlink:type="simple"/></inline-formula>). Besides, Nu<sub>m</sub> increases with Ra at fixed radiation parameter. The increase in the radiation parameter, conceivably, will bring out an increase in the mean Nusselt number at a given Ra.</p><p><xref ref-type="fig" rid="fig8">Figure 8</xref> shows the correlation of Rayleigh number and mean Nusselt number under five different Froude number. According the figure, the increase the Rayleigh number will bring out the increase the mean Nusselt number. Besides, the larger the Froude number will also increase the mean Nusselt number.</p></sec><sec id="s5"><title>5. Conclusions</title><p>The following conclusions can be drawn from the results of the present theoretical study:</p><p>1) With the help of Colburn analogy, the present research successfully predicts the shear stress of the vapor- liquid interface in a film boiling system under liquid of high velocity on an elliptical tube.</p><p>2) The increase in the eccentricity parameter of the elliptical tube will lead to a decrease in the mean Nusselt number. Besides, turbulent film boiling under the external flowing liquid with high velocity, the increase in both the Froude number and Grashof number will bring out an increase in the mean Nusselt number.</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Effects of the Froude number on mean Nusselt number</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1560296x86.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Comparison of the present results with previous data</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1560296x87.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Effects of the Ra on mean Nusselt number</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1560296x88.png"/></fig><p>3) The present paper includes interfacial shear, radiation effects, temperature ratio, eddy diffusivity and thermal properties of temperature dependent. It can predict the forced convection turbulent film boiling more exactly. Besides, under the condition of free convection film boiling, it shows a good agreement between the present result and the previous experimental studies.</p></sec><sec id="s6"><title>Acknowledgements</title><p>The authors gratefully acknowledge the support provided to this projects by the Ministry of Science and Technology of Taiwan under Contract Number MOST 104-2221-E-019-052.</p></sec><sec id="s7"><title>Cite this paper</title><p>Hai-Ping Hu, (2016) Heat Transfer Efficiency of Turbulent Film Boiling on a Horizontal Elliptical Tube with External Flowing Liquid. World Journal of Engineering and Technology,04,206-219. doi: 10.4236/wjet.2016.42020</p></sec><sec id="s8"><title>Nomenclature</title><p>a, b semimajor, semiminior axis of ellipse</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x89.png" xlink:type="simple"/></inline-formula> specific heat capacity, (J/kg∙K)</p><p>D<sub>e</sub> equivalent circular diameter of elliptical tube (m)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x90.png" xlink:type="simple"/></inline-formula> shear Reynolds, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x90.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x91.png" xlink:type="simple"/></inline-formula></p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x92.png" xlink:type="simple"/></inline-formula> wall shear parameter, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x92.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x93.png" xlink:type="simple"/></inline-formula></p><p>e eccentricity of ellipse, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x94.png" xlink:type="simple"/></inline-formula></p><p>Fr Froude number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x95.png" xlink:type="simple"/></inline-formula></p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x96.png" xlink:type="simple"/></inline-formula> modified Grashof number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x96.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x97.png" xlink:type="simple"/></inline-formula></p><p>g acceleration due to gravity (m/s<sup>2</sup>)<sup> </sup></p><p>h heat transfer coefficient, W/(m<sup>2</sup>∙K)</p><p>h<sub>fg</sub> latent heat (J/kg)</p><p>k thermal conductivity (W/m∙K)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x98.png" xlink:type="simple"/></inline-formula> dimensionless thermal conductivity, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x98.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x99.png" xlink:type="simple"/></inline-formula></p><p><img data-original="http://html.scirp.org/file/9-1560296x100.png" /> <img data-original="http://html.scirp.org/file/9-1560296x101.png" /></p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x102.png" xlink:type="simple"/></inline-formula> local Nusselt number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x102.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x103.png" xlink:type="simple"/></inline-formula></p><p>Nu<sub>m</sub> mean Nusselt number</p><p>NR radiation parameter, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x104.png" xlink:type="simple"/></inline-formula></p><p>Pr Prandtl number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x105.png" xlink:type="simple"/></inline-formula></p><p>Ra modified Rayleigh number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x106.png" xlink:type="simple"/></inline-formula></p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x107.png" xlink:type="simple"/></inline-formula> Reynolds number of vapor, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x107.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x108.png" xlink:type="simple"/></inline-formula></p><p><img data-original="http://html.scirp.org/file/9-1560296x109.png" /> <img data-original="http://html.scirp.org/file/9-1560296x110.png" /></p><p>S heat capacity parameter, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x111.png" xlink:type="simple"/></inline-formula></p><p>St Stanton number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x112.png" xlink:type="simple"/></inline-formula></p><p>T temperature (K)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x113.png" xlink:type="simple"/></inline-formula> temperature ratio, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x113.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x114.png" xlink:type="simple"/></inline-formula></p><p>T<sup>+</sup> dimensionless temperature, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x115.png" xlink:type="simple"/></inline-formula></p><p>u vapor velocity in x-direction (m/s)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x116.png" xlink:type="simple"/></inline-formula> shear velocity, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x116.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x117.png" xlink:type="simple"/></inline-formula></p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x118.png" xlink:type="simple"/></inline-formula> dimensionless velocity, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x118.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x119.png" xlink:type="simple"/></inline-formula></p><p>v velocity normal to the direction of flow (m/s)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x120.png" xlink:type="simple"/></inline-formula> acceleration due to graviton force (m/s<sup>2</sup>)</p><p>x peripheral coordinate (m)</p><p>y coordinate measured distance normal to tube surface (m)</p><p>y<sup>+</sup> dimensionless distance, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x121.png" xlink:type="simple"/></inline-formula></p></sec><sec id="s9"><title>Greek Symbols</title><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x122.png" xlink:type="simple"/></inline-formula> vapor film thickness (m)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x123.png" xlink:type="simple"/></inline-formula> dimensionless film thickness, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x123.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x124.png" xlink:type="simple"/></inline-formula></p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x125.png" xlink:type="simple"/></inline-formula> absolute viscosity (kg/m∙s)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x126.png" xlink:type="simple"/></inline-formula> dimensionless absolute viscosity, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x126.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x127.png" xlink:type="simple"/></inline-formula></p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x128.png" xlink:type="simple"/></inline-formula> kinematic viscosity (m<sup>2</sup>/s)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x129.png" xlink:type="simple"/></inline-formula> density (kg/m<sup>3</sup>)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x130.png" xlink:type="simple"/></inline-formula> shear stress (N/m<sup>2</sup>)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x131.png" xlink:type="simple"/></inline-formula> angle measured from bottom of tube</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x132.png" xlink:type="simple"/></inline-formula> angle between the tangent to tube surface and the normal to direction of gravity</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x133.png" xlink:type="simple"/></inline-formula> interfacial shear parameter, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x133.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x134.png" xlink:type="simple"/></inline-formula></p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x135.png" xlink:type="simple"/></inline-formula> eddy diffusivity for momentum</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x136.png" xlink:type="simple"/></inline-formula> emissivity</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x137.png" xlink:type="simple"/></inline-formula> Stefan-boltzmann constant, W/m<sup>2</sup>∙K<sup>4</sup></p></sec><sec id="s10"><title>Subscripts</title><p>l liquid</p><p>s vapor at saturation temperature</p><p>v vapor</p><p>w tube wall</p><p>x x-direction</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1560296x138.png" xlink:type="simple"/></inline-formula> vapor-liquid interface</p></sec></body><back><ref-list><title>References</title><ref id="scirp.66338-ref1"><label>1</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Bromley</surname><given-names> L.A. </given-names></name>,<etal>et al</etal>. 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