<?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">OJFD</journal-id><journal-title-group><journal-title>Open Journal of Fluid Dynamics</journal-title></journal-title-group><issn pub-type="epub">2165-3852</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ojfd.2015.51005</article-id><article-id pub-id-type="publisher-id">OJFD-54333</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>
 
 
  Possibility of a Straightening Flow-Meter by Using Woven Screen
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>akahiro</surname><given-names>Tsuchiya</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Yota</surname><given-names>Koishi</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Mitsuo</surname><given-names>Iwamoto</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Hidemi</surname><given-names>Yamada</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Mechanical and Energy Systems Engineering, Oita University, Oita, Japan</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>yamada@oita-u.ac.jp(HY)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>12</day><month>02</month><year>2015</year></pub-date><volume>05</volume><issue>01</issue><fpage>34</fpage><lpage>38</lpage><history><date date-type="received"><day>2</day>	<month>February</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>23</month>	<year>February</year>	</date><date date-type="accepted"><day>28</day>	<month>February</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>
 
 
  In this paper, the possibility of the flow rate measurement for a circular pipe flow by using a wo-ven screen with the property of straightening un-uniform flows is discussed. The resistance coefficient and the flow rate coefficient are estimated from the pressure difference caused by the woven screen under the experiment ranges of the wire Reynolds number, Red = 2.2 &#215; 102-1.8 &#215; 103, and of the open area ratio, β = 0.28-0.65. As a result, the resistance coefficient decreases and the flow rate coefficient increases as the wire Reynolds number Red or the open area ratio β increases. In addition, both coefficients are not affected by the difference between uniform and turbulent pipe flows approaching the woven screen. Therefore, the possibility of a flow-meter having the property to straighten the un-uniform flow is expected.
 
</p></abstract><kwd-group><kwd>Flow Rate Measurement</kwd><kwd> Woven Screen</kwd><kwd> Flow-Straightening</kwd><kwd> Resistance Coefficient</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>It is a significant assignment to measure the flow rate exactly in engineering fields using pipe line flows. A flow- meter generally requires a long runway approaching it and/or a straightening device, such as perforated plates, honeycombs or woven screens upstream of it. As for a woven screen, often used to straighten un-uniform flows such as a prejudice flow and a turbulent flow in many engineering fields [<xref ref-type="bibr" rid="scirp.54333-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.54333-ref2">2</xref>] , there have been a lot of studies on resistance thus far [<xref ref-type="bibr" rid="scirp.54333-ref3">3</xref>] - [<xref ref-type="bibr" rid="scirp.54333-ref10">10</xref>] . In recent years, the requirements of downsizing the apparatus have appeared.</p><p>Therefore, an idea of measuring the flow rate by using a woven screen is proposed in this paper, because it is expected that it could play both the role of straightening the flow as well as measuring the flow rate. The possibility as a flow-meter having the ability to straighten an un-uniform flow from the measurements of the flow rate coefficient and resistance coefficient of a woven screen for two different pipe flow fields is discussed.</p></sec><sec id="s2"><title>2. Experimental Approach</title><p><xref ref-type="fig" rid="fig1">Figure 1</xref> shows a summary of this experiment and nomenclature. The experimental apparatus is composed of the entrance nozzle and a straight circular pipe with an inner diameter of D = 42 mm. On the inner wall of the pipe, there are many pressure measurement holes (diameter 0.5 mm) along the flow direction. The woven screen is set at the position L = 210 mm or 1080 mm downstream from the tip of the entrance nozzle. The woven screen is made of stainless steel wires of 1.0 mm diameter and has four open area ratios. The wire Reynolds number, Re<sub>d</sub>, is defined in Equation (1) based on the wire diameter, the velocity averaged in the pipe’s cross section and the kinematic viscosity of the air was varied from 2.2 &#215; 10<sup>2</sup> to 1.8 &#215; 10<sup>3</sup>.</p><disp-formula id="scirp.54333-formula2234"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-2320195x5.png"  xlink:type="simple"/></disp-formula><p><xref ref-type="table" rid="table1">Table 1</xref> shows the geometric parameters of woven screen models used in this study. M is number of the meshes, and β is the open area ratio defined as<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-2320195x6.png" xlink:type="simple"/></inline-formula>. <xref ref-type="fig" rid="fig2">Figure 2</xref> shows the velocity distribution in the pipe’s cross section measured at the positions of L = 1080 mm and 210 mm under the Reynolds number based on the circular pipe diameter, Re<sub>D</sub> = 8.3 &#215; 10<sup>3</sup> − 8.7 &#215; 10<sup>4</sup>, before the woven screens is set. The velocity in the pipe is obtained from the pressure difference between total pressure measured by a small handmade total pressure tube and static pressure taken from a pressure hole in the position nearest to the tip of the total pressure tube.</p><p>It is understood that the velocity distributions obtained at the pipe’s cross section in the case of L = 1080 mm are almost consistent with the 1/6-power law as shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>(a). Because the inner flow in the case of L = 1080 mm can be regarded as a developed turbulent pipe flow, thereafter it is called “the turbulent pipe flow”. On the other hand, the velocity distributions in the case of L = 210 mm are almost uniform, except in the vicinity of the pipe wall as shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>(b). Because the constant velocity region occupies about 70% in the pipe’s cross section, thereafter the inner flow is called “the uniform pipe flow”. For all pressure measurements, a Gottingen type manometer (minimum scale 0.05 mm) is used.</p></sec><sec id="s3"><title>3. Experimental Results and Discussions</title><sec id="s3_1"><title>3.1. Wall Pressure Distribution</title><p><xref ref-type="fig" rid="fig3">Figure 3</xref> shows a typical example of the x direction distribution of a wall pressure coefficient C<sub>p</sub> upstream and downstream of the woven screen. The wall pressure coefficient is defined as</p><disp-formula id="scirp.54333-formula2235"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-2320195x7.png"  xlink:type="simple"/></disp-formula><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Experimental apparatus and coordinate system</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-2320195x8.png"/></fig><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Geometric parameters of woven screen models</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >d [mm]</th><th align="center" valign="middle" >M</th><th align="center" valign="middle" >β</th><th align="center" valign="middle" >Symbol</th></tr></thead><tr><td align="center" valign="middle" >1.0</td><td align="center" valign="middle" >12</td><td align="center" valign="middle" >0.28</td><td align="center" valign="middle" >◆</td></tr><tr><td align="center" valign="middle" >1.0</td><td align="center" valign="middle" >8</td><td align="center" valign="middle" >0.47</td><td align="center" valign="middle" >■</td></tr><tr><td align="center" valign="middle" >1.0</td><td align="center" valign="middle" >6</td><td align="center" valign="middle" >0.58</td><td align="center" valign="middle" >▲</td></tr><tr><td align="center" valign="middle" >1.0</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.65</td><td align="center" valign="middle" >●</td></tr></tbody></table></table-wrap><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Velocity profiles in circular pipe flow. (a) Turbulent pipe flow; (b) Uniform pipe flow.</title></caption><fig id ="fig2_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-2320195x10.png"/></fig><fig id ="fig2_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-2320195x9.png"/></fig></fig-group><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Wall pressure distribution in circular pipe (β = 0.65, Turbulent pipe flow, Re<sub>d</sub> = 990)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-2320195x11.png"/></fig><p>where P is the wall pressure, P<sub>∞</sub> is the atmospheric pressure and ρ<sub>air</sub> is the density of the air. It is noted that the wall pressure varies linearly over the wide range of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-2320195x12.png" xlink:type="simple"/></inline-formula>, and that a difference in the wall pressure coefficient, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-2320195x13.png" xlink:type="simple"/></inline-formula>, occurs between the regions upstream and downstream of the woven screen.</p></sec><sec id="s3_2"><title>3.2. Resistance Coefficient</title><p><xref ref-type="fig" rid="fig4">Figure 4</xref>(a) shows the relationship between the resistance coefficient K and the wire Reynolds number Re<sub>d</sub>. The resistance coefficient K is defined as</p><disp-formula id="scirp.54333-formula2236"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-2320195x14.png"  xlink:type="simple"/></disp-formula><p>The resistance coefficient K decreases as the wire Reynolds number Re<sub>d</sub> and the open area ratio β increase. Although the resistance coefficients K for each β is obtained under two different pipe flow approaching the woven screen, the turbulent flow and the uniform flow, they agree very well. Then, it is noted that the resistance coefficient is not affected by the difference of flow approaching the woven screen. This may be because two approaching-flows become similar to each other by the damming effect which occurs in front of the woven screen. Therefore, it is expected that the woven screen has a property which could straighten the turbulent pipe flow as well as the uniform pipe flow. The black-lines in <xref ref-type="fig" rid="fig4">Figure 4</xref>(a) exhibit the approximation of the obtained resistance coefficient K and are given by the following Equation (4), depending on the wire Reynolds number Re<sub>d</sub> and the open area ratio β. They approximate the resistance coefficient K very well.</p><disp-formula id="scirp.54333-formula2237"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-2320195x15.png"  xlink:type="simple"/></disp-formula></sec><sec id="s3_3"><title>3.3. Flow Rate Coefficient</title><p><xref ref-type="fig" rid="fig4">Figure 4</xref>(b) shows the variation of the flow rate coefficient α for the wire Reynolds number Re<sub>d</sub> and the open area ratio β. The flow rate coefficient α is derived from general formulas, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-2320195x16.png" xlink:type="simple"/></inline-formula>, where A<sub>o</sub> is the open area of the woven screen. The flow rate coefficient α increases as the wire Reynolds number Re<sub>d</sub> and the open area ratio β increases. In addition, it was noticed that the flow rate coefficient α obtained in two different pipe flows, the turbulent pipe flow and the uniform pipe flow, are close to each other. On the other hand, the flow rate coefficient α can be calculated from the wall pressure difference based on the following Equation (5), where A is the pipe cross-sectional area.</p><disp-formula id="scirp.54333-formula2238"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/5-2320195x17.png"  xlink:type="simple"/></disp-formula><p>The black-lines in <xref ref-type="fig" rid="fig4">Figure 4</xref>(b) are converted from the black-lines in <xref ref-type="fig" rid="fig4">Figure 4</xref>(a), and agree with the experimental results of the flow rate coefficient α.</p></sec><sec id="s3_4"><title>3.4. Reconfirmation from Direct Pressure Drop</title><p>Generally, in the case of the flow rate measurement using the pressure difference, the pressure difference <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-2320195x18.png" xlink:type="simple"/></inline-formula> is decided as the wall pressure drop between the front and the back of a device’s position. Therefore, the measurement of the pressure drop in the case of the transient pipe flow was attempted in the vicinity of the woven screen as shown in <xref ref-type="fig" rid="fig5">Figure 5</xref>. Because the pressure drop coefficient <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-2320195x19.png" xlink:type="simple"/></inline-formula> measured between two positions nearest to the woven screen, x = −1.05 D and 0.10 D, is fairly larger than the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-2320195x19.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-2320195x20.png" xlink:type="simple"/></inline-formula> obtained from the pressure difference of the two pressure distribution lines as shown in <xref ref-type="fig" rid="fig3">Figure 3</xref>, the property as flow-meter is expected to be good when taking the pressure drop in the downstream position nearer to the woven screen.</p></sec></sec><sec id="s4"><title>4. Conclusion</title><p>The resistance coefficient K and the flow rate coefficient α of the woven screen placed in the circular pipe were experimentally investigated. As a result, although the flow rate coefficient α varies depending on the wire Reynolds number Re<sub>d</sub> and the open area ratio β increases, both coefficients is not affected by the difference between</p><fig-group id="fig4"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Influence of Reynolds number and open area ratio. (a) Resistance coefficient; (b) Flow rate coefficient.</title></caption><fig id ="fig4_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-2320195x22.png"/></fig><fig id ="fig4_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-2320195x21.png"/></fig></fig-group><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Wall pressure distribution in circular pipe (β = 0.65, Transient pipe flow, Re<sub>d</sub> = 880)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-2320195x23.png"/></fig><p>a uniform and a turbulent pipe flows approaching the woven screen. Therefore, the possibility of a flow-meter having the ability of straightening an un-uniform flow can be expected. Furthermore, considering the pressure measurement points, the numbers of woven screens and/or combination with perforated plates and honeycombs, its ability as a straightening flow-meter will rise.</p></sec></body><back><ref-list><title>References</title><ref id="scirp.54333-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Makita, H. (2002) Turbulence Wind Tunnel (Wind Tunnel Experiments). Journal of Japan Society of Fluid Mechanics, 21, 409-418. (In Japanese) http://dx.doi.org/10.11426/nagare1982.21.409</mixed-citation></ref><ref id="scirp.54333-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Masaki, D., Futamura, H. and Nishizawa, T. (2010) Design of JAXA TechClean Fan Stage (Base Configuration). JAXA (Japan Aerospace Exploration Agency) Research and Development Report, 10, 1-16. (In Japanese)</mixed-citation></ref><ref id="scirp.54333-ref3"><label>3</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Wieghardt</surname><given-names> K.E.G. </given-names></name>,<etal>et al</etal>. (<year>1953</year>)<article-title>On the Resistance of Screens</article-title><source> The Aeronautical Quarterly</source><volume> 4</volume>,<fpage> 186</fpage>-<lpage>192</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.54333-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">Armour, J.C. and Cannon, J. (1968) Fluid Flow through Woven Screens. AIChE Journal, 14, 415-420.</mixed-citation></ref><ref id="scirp.54333-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">Sodré, J.R. and Parise, J.A.R. (1997) Friction Factor Determination for Flow through Finite Wire-Mesh Woven-Screen Matrices. Journal of Fluids Engineering, 119, 847-851.</mixed-citation></ref><ref id="scirp.54333-ref6"><label>6</label><mixed-citation publication-type="other" xlink:type="simple">Hamaguchi, K., Magara, Y. and Yamashita, I. (2004) Effects of Stacking Method on Pressure Loss and Heat Transfer Characteristics in Stacked Wire Gauze. The Japan Society of Mechanical Engineers, 70, 187-194. (In Japanese)</mixed-citation></ref><ref id="scirp.54333-ref7"><label>7</label><mixed-citation publication-type="other" xlink:type="simple">Shiozaki, T., Maruyama, S., Mohri, T. and Hosumi, Y. (2005) Fluid Flow Characteristics through a Wire Mesh at Low Reynolds Number for High Temperature Air Combustion Furnace. The Japan Society of Mechanical Engineers, 71, 163-166. (In Japanese)</mixed-citation></ref><ref id="scirp.54333-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">Wu, W.T., Liu, J.F. and Hsieh, W.H. (2005) Measurement and Correlation of Hydraulic Resistance of Flow through Woven Metal Screens. International Journal of Heat and Mass Transfer, 48, 3008-3017. http://dx.doi.org/10.1016/j.ijheatmasstransfer.2005.01.038</mixed-citation></ref><ref id="scirp.54333-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">Kolodziej, A., Lojewska, J., Jaroszyński, M., Gancarczyk, A. and Jodnowski, P. (2012) Heat Transfer and Flow Resistance for Stacked Wire Gauzes: Experiments and Modelling. International Journal of Heat and Fluid Flow, 33, 101-108. http://dx.doi.org/10.1016/j.ijheatfluidflow.2011.11.006</mixed-citation></ref><ref id="scirp.54333-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">Fischer, A. and Gerstmann, J. (2013) Flow Resistance of Metallic Screens in Liquid, Gaseous and Cryogenic Flow. 5th European Conference for Aero-Space Science, München, 1-5 July 2013, 1-12.</mixed-citation></ref></ref-list></back></article>