<?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">EPE</journal-id><journal-title-group><journal-title>Energy and Power Engineering</journal-title></journal-title-group><issn pub-type="epub">1949-243X</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/epe.2015.74015</article-id><article-id pub-id-type="publisher-id">EPE-56000</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject></subj-group></article-categories><title-group><article-title>
 
 
  Experimental Determination of Local Resistance Coefficient of Sudden Expansion Tube
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>inpeng</surname><given-names>Li</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>Changjin</surname><given-names>Wang</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>Mingda</surname><given-names>Ha</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>Northeast Petroleum University at Qinhuangdao, Qinhuangdao, China</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>214351651@qq.com(IL)</email>;<email>214351651@qq.com(CW)</email>;<email>Email: 214351651@qq.com(MH)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>28</day><month>04</month><year>2015</year></pub-date><volume>07</volume><issue>04</issue><fpage>154</fpage><lpage>159</lpage><history><date date-type="received"><day>15</day>	<month>April</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>27</month>	<year>April</year>	</date><date date-type="accepted"><day>28</day>	<month>April</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>
 
 
  Theoretical derivation of local resistance coefficient of sudden expansion tube is presented. Several assumptions are analyzed in the theoretical derivation. That the head loss shall be neglected is affirmed. Experimental data proves that the pressure before and after sudden expansion section is basically the same. That the friction force on the side face of control body is neglected is denied and it is pointed out that such neglect is the main cause for error between theoretical calculation and actual measurement. Experimental device for measuring local resistance coefficient is designed in combination with theoretical derivation process. Optimal gradually varied flow section is selected after sudden expansion pipe in Bernoulli equation based on variation of piezometer tube head. It is pointed out in accordance with experimental data analysis that the value of local resistance coefficient of sudden expansion tube determined through experimental data is closer to the actual situation during pipeline design.
 
</p></abstract><kwd-group><kwd>Sudden Expansion Pipe</kwd><kwd> Frictional Head Loss</kwd><kwd> Loss Head Loss</kwd><kwd> Local Resistance Coefficient</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Valves, bends and metering devices are installed on pipelines for oil exploitation and transportation to control, adjust and meter the fluid. The flow, direction and even form will be changed when the fluid passes these local parts, which causes the local head loss. Only the calculation of local head loss of sudden expansion tube when fluid passes is studied in this paper. When the fluid flows into pipeline with bigger diameter, it does not expand suddenly but expand gradually after leaving the pipeline of smaller diameter and forms eddy between corner of pipe wall and main stream. The eddy is driven by the main stream to turn and there is energy consumption dur- ing the turning. Besides, the fluid impact and collision produced due to sudden change of pipeline section all lead to loss of mechanical energy.</p><p>The calculation of local head loss is the essence of calculation of local resistance coefficient. The local resistance coefficient of sudden expansion pipe is the only one that can be got by the pure theory, the others are experimentally determined. But the current calculation formula shows that local resistance coefficient is only related to the expansion ratio of pipe diameter and it doesn’t matter with dynamic viscosity, flow rate, et al. The conclusion is questionable. In this paper, the determination of local resistance coefficient of sudden expansion tube is discussed on the basis of the experimental phenomena and data. This can provide some help for actual engineering calculation.</p></sec><sec id="s2"><title>2. Theoretical Derivation of Local Resistance Coefficient of Sudden Expansion Pipe</title><p>In <xref ref-type="fig" rid="fig1">Figure 1</xref>, take the space enclosed by internal wall of pipe, starting end of whirlpool and terminal end of whirl- pool as control body, and apply Bernoulli equation between Section 1 and sections, obtaining</p><disp-formula id="scirp.56000-formula742"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x5.png"  xlink:type="simple"/></disp-formula><p>where, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x6.png" xlink:type="simple"/></inline-formula>is statical head, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x7.png" xlink:type="simple"/></inline-formula>is pressure head, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x8.png" xlink:type="simple"/></inline-formula>is velocity head, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x9.png" xlink:type="simple"/></inline-formula>is kinetic energy correction factor, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x10.png" xlink:type="simple"/></inline-formula> is water head loss of liquid of unit gravity from Section 1 and Section 2.</p><p>Since distance between the two sections is short, frictional head loss can be neglected, i.e. head loss only includes local head loss<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x11.png" xlink:type="simple"/></inline-formula>. Take<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x12.png" xlink:type="simple"/></inline-formula>, obtaining</p><disp-formula id="scirp.56000-formula743"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x13.png"  xlink:type="simple"/></disp-formula><p>Apply momentum equation on control body. Since it is difficult to determine the pressure at Section 1, it can only be assumed equal to pressure before the section. Therefore, total pressure on Section 1 is <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x14.png" xlink:type="simple"/></inline-formula><sub> </sub>and total pressure on Section 2 is<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x15.png" xlink:type="simple"/></inline-formula><sub>. </sub>Neglecting side friction of control body, the join force on liquid in the control body on flow direction is</p><disp-formula id="scirp.56000-formula744"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x16.png"  xlink:type="simple"/></disp-formula><p>Therefore the momentum equation is</p><disp-formula id="scirp.56000-formula745"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x17.png"  xlink:type="simple"/></disp-formula><p>Two sides both divided by<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x18.png" xlink:type="simple"/></inline-formula>, obtaining</p><disp-formula id="scirp.56000-formula746"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x19.png"  xlink:type="simple"/></disp-formula><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Scheme of local resistance of sudden expansion joint and control body selection</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-6201818x20.png"/></fig><p>Substitute it into formula (2), obtaining</p><disp-formula id="scirp.56000-formula747"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x21.png"  xlink:type="simple"/></disp-formula><p>Sort it and obtain</p><disp-formula id="scirp.56000-formula748"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x22.png"  xlink:type="simple"/></disp-formula><p>It can be obtained from continuity equation that <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x23.png" xlink:type="simple"/></inline-formula> or <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x24.png" xlink:type="simple"/></inline-formula></p><p>Formula (7) can be converted to</p><disp-formula id="scirp.56000-formula749"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x25.png"  xlink:type="simple"/></disp-formula><p>or</p><disp-formula id="scirp.56000-formula750"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x26.png"  xlink:type="simple"/></disp-formula><p>Further obtaining</p><disp-formula id="scirp.56000-formula751"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x27.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x28.png" xlink:type="simple"/></inline-formula>is the local resistance coefficient of sudden expansion pipe [<xref ref-type="bibr" rid="scirp.56000-ref1">1</xref>] . It is shown from the formula that local resistance coefficient is only related to the expansion ratio of pipe diameter.</p></sec><sec id="s3"><title>3. Discussion of Several Assumptions in Theoretical Derivation</title><p>In 2009, Zhao Haiyan et al. concluded through numerical simulation analysis that the backflow zone expands with the increase of expansion ratio, so does the eddy size. The existence of eddy necessarily consumes the energy of mainstream. The bigger the eddy size and strength, the more the energy consumption of the main- stream, and the bigger the energy loss through sudden expansion [<xref ref-type="bibr" rid="scirp.56000-ref2">2</xref>] . This conclusion conforms to the results of theoretical derivation above.</p><p>Zhao Haiyan et al. also pointed out that the backflow in the backflow zone becomes increasingly obvious with the increase of the Reynolds number, and backflow length continues to increase. The conclusion is consistent with the conclusion of Bedakes D., et al. [<xref ref-type="bibr" rid="scirp.56000-ref3">3</xref>] . In 2012, Zhou Zaidong et al. also concluded through numerical simulation analysis that the bigger Reynolds number leads to more violent eddy, larger effect zone, longer time to reach mainstream and bigger speed at the middle position of the pipeline, and the range affected by the maximum speed is even further from the pipe opening, which conforms to the actual situation [<xref ref-type="bibr" rid="scirp.56000-ref4">4</xref>] . This conclusion is not consistent with results of theoretical derivation above, which indicates that the local resistance loss is not only related to expansion ratio of the pipe diameter, but also to the kinestate of fluid.</p><p>To this end, several assumptions in above theoretical derivation are discussed in this paper.</p><sec id="s3_1"><title>3.1. Neglect of Frictional Head Loss</title><p>It is impossible to calculate accurately yet how long the eddy is which is formed after the flow passes the sudden expansion pipe. Currently, it is generally considered that the backflow length should be five to eight times of diameter of sudden expansion pipe. Normally the eddy length can be basically neglected when compared with length of transportation pipeline, so the frictional head loss can be neglected too. Meanwhile, when the energy loss of whole transportation pipeline system is calculated, the frictional head loss and local head loss of sudden expansion section are necessarily calculated. There would be repetition of calculation if frictional head loss [<xref ref-type="bibr" rid="scirp.56000-ref5">5</xref>] [<xref ref-type="bibr" rid="scirp.56000-ref6">6</xref>] is calculated here.</p></sec><sec id="s3_2"><title>3.2. Pressure of Two Sections of the Control Body</title><p>The theoretical derivation shows that it is rather difficult to determine the pressure at Section 1, so it is only possible to assume that the value is equal to the pressure at the front end of the section. Therefore, pressure at the front end of this section and Section 1 are measured in this experiment, see <xref ref-type="table" rid="table1">Table 1</xref>. The experiment shows that the pressure at Section 1 is not stable and there is certain fluctuation. Mean value of fluctuation is obtained approximately for measurements. The experimental data proves that this assumption has certain accuracy.</p></sec><sec id="s3_3"><title>3.3. Friction on the Side Face of Control Body</title><p>When momentum equation is applied to the control body, the friction force on the side face of the control body is neglected so as to conclude that the local friction coefficient is only related to the expansion ratio of pipe diameter. Literature [<xref ref-type="bibr" rid="scirp.56000-ref5">5</xref>] points out that the reason why the eddy area is able to keep moving is that energy supply is obtained through momentum exchange from the mainstream. This part of energy consumption finally becomes heat after friction with the eddy and wall inside the eddy and this loss is called eddy loss. Since the eddy loss is the most important loss in the local head loss of sudden expansion tube, the neglect of friction force between eddy and wall will lead to substantial error.</p></sec></sec><sec id="s4"><title>4. Design of Experimental Solution</title><p>The experimental device, as shown in <xref ref-type="fig" rid="fig2">Figure 2</xref> is placed horizontally on the experimental table. The inlet pipeline on the left is connected with the pipeline of constant head water tank and the tail of outlet pipeline on the right is controlled by the throttle valve. The flow is controlled by the outlet valve. The experiment pipeline is transparent organic glass pipe with inner diameter of inlet pipe being 16 mm, pipe diameter of expansion pipe being 20 mm and room temperature being 15 Celsius degrees.</p><p>Positions of piezometer tubes: the first piezometer tube is set at the limit position before sudden expansion, and the second one at the limit position at the entry of sudden expansion. The pressure measurements of these two piezometer tubes are used to check the assumption in the theoretical derivation that the pressure of two sections of control body is approximately the same. The eddy length at entry of sudden expansion tube is generally considered to be five to eight times of the diameter of sudden expansion tube, so the third to the sixth piezometer tubes are set at areas of 100 mm, 120 mm, 140 mm, 160 mm after sudden expansion to analyze the variation of energy loss.</p><p>Measurement of piezometer tube head: transparent organic glass pipe with 6 mm of inner diameter and 100 mm of height is fixed on the lifting pressure test plate with the minimum scale of mm.</p><p>Flow measuring: volumetric method is applied to measure the flow. Graduate cylinder and cup are used to measure the volume and electronic stopwatch is used for timing.</p></sec><sec id="s5"><title>5. Analysis of Experimental Results</title><p>There is always head loss which is monotonic decreasing along the flow due to viscosity of the fluid; the head of piezometer tube reflects the potential energy of the flow, so the head line of piezometer tube may rise, drop or stay unchanged. As for sudden expansion tube, the increase of overflow section leads to the decrease of mean flow of the section and the decrease of flow head. With the decrease of the energy loss and flow head of the sudden expansion tube flow, the total head line decreases while the head line of piezometer tube increases when close to the sudden expansion tube [<xref ref-type="bibr" rid="scirp.56000-ref7">7</xref>] . The head line of frictional head loss decreases in the flow direction. Therefore, one optimum pressure is selected from the third to the sixth piezometer tubes, which is the pressure at the starting position of the pipe section where the frictional resistance plays the dominant role after the eddy is finished, i.e. the pressure at the starting position of the section where the streamline completely recovers to the gradually varied flow.</p><p>The Bernoulli equation is used for calculation of local head loss of sudden expansion tube based on the actual measurement (Refer to <xref ref-type="table" rid="table2">Table 2</xref> for the results).</p><p>As shown in above table, the head loss value calculated from theoretical equation is negligible compared with actually measured head loss value. The head loss value calculated from theoretical equation is less than 1 mm in most cases, that is to say, when the value based on the calculation results is reflected in the experiment, the pressure of piezometer tube is basically unchanged with the change of flow. However, it is obviously inconsis-</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> The pressure measurement before sudden expansion and Section 1</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Flow rate (mL/s)</th><th align="center" valign="middle" >Pressure measuring height before sudden expansion (mm)</th><th align="center" valign="middle" >Pressure measuring height at Section 1 (mm)</th><th align="center" valign="middle" >Flow rate (mL/s)</th><th align="center" valign="middle" >Pressure measuring height before sudden expansion (mm)</th><th align="center" valign="middle" >Pressure measuring height at Section 1 (mm)</th></tr></thead><tr><td align="center" valign="middle" >24.916</td><td align="center" valign="middle" >74.37</td><td align="center" valign="middle" >74.66</td><td align="center" valign="middle" >53.607</td><td align="center" valign="middle" >52.68</td><td align="center" valign="middle" >52.68</td></tr><tr><td align="center" valign="middle" >41.300</td><td align="center" valign="middle" >72.60</td><td align="center" valign="middle" >72.72</td><td align="center" valign="middle" >28.093</td><td align="center" valign="middle" >55.20</td><td align="center" valign="middle" >55.30</td></tr><tr><td align="center" valign="middle" >58.851</td><td align="center" valign="middle" >70.31</td><td align="center" valign="middle" >70.45</td><td align="center" valign="middle" >95.181</td><td align="center" valign="middle" >45.65</td><td align="center" valign="middle" >45.65</td></tr><tr><td align="center" valign="middle" >13.433</td><td align="center" valign="middle" >56.52</td><td align="center" valign="middle" >56.67</td><td align="center" valign="middle" >117.561</td><td align="center" valign="middle" >30.23</td><td align="center" valign="middle" >30.25</td></tr><tr><td align="center" valign="middle" >40.292</td><td align="center" valign="middle" >54.23</td><td align="center" valign="middle" >54.23</td><td align="center" valign="middle" >102.531</td><td align="center" valign="middle" >22.45</td><td align="center" valign="middle" >22.70</td></tr></tbody></table></table-wrap><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> The calculation of local head loss and resistance coefficient of sudden expansion</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Flow rate (mL/s)</th><th align="center" valign="middle" >Velocity of sudden expansion pipe (m/s)</th><th align="center" valign="middle" >Pressure measuring height before sudden expansion (mm)</th><th align="center" valign="middle" >Optimal pressure measuring height after sudden expansion (mm)</th><th align="center" valign="middle" >Actually measured value of local head loss (m)</th><th align="center" valign="middle" >Theoretically calculate value of local head loss (m)</th><th align="center" valign="middle" >Local resistance coefficient</th></tr></thead><tr><td align="center" valign="middle" >24.916</td><td align="center" valign="middle" >0.080</td><td align="center" valign="middle" >74.37</td><td align="center" valign="middle" >74.46</td><td align="center" valign="middle" >0.00037</td><td align="center" valign="middle" >0.00010</td><td align="center" valign="middle" >1.15</td></tr><tr><td align="center" valign="middle" >41.300</td><td align="center" valign="middle" >0.132</td><td align="center" valign="middle" >72.60</td><td align="center" valign="middle" >72.64</td><td align="center" valign="middle" >0.00123</td><td align="center" valign="middle" >0.00028</td><td align="center" valign="middle" >1.38</td></tr><tr><td align="center" valign="middle" >58.851</td><td align="center" valign="middle" >0.188</td><td align="center" valign="middle" >70.31</td><td align="center" valign="middle" >70.46</td><td align="center" valign="middle" >0.00242</td><td align="center" valign="middle" >0.00057</td><td align="center" valign="middle" >1.34</td></tr><tr><td align="center" valign="middle" >13.433</td><td align="center" valign="middle" >0.043</td><td align="center" valign="middle" >56.52</td><td align="center" valign="middle" >56.48</td><td align="center" valign="middle" >0.00017</td><td align="center" valign="middle" >0.00003</td><td align="center" valign="middle" >1.85</td></tr><tr><td align="center" valign="middle" >40.292</td><td align="center" valign="middle" >0.129</td><td align="center" valign="middle" >54.23</td><td align="center" valign="middle" >54.06</td><td align="center" valign="middle" >0.00138</td><td align="center" valign="middle" >0.00027</td><td align="center" valign="middle" >1.63</td></tr><tr><td align="center" valign="middle" >53.607</td><td align="center" valign="middle" >0.171</td><td align="center" valign="middle" >52.68</td><td align="center" valign="middle" >52.57</td><td align="center" valign="middle" >0.00224</td><td align="center" valign="middle" >0.00047</td><td align="center" valign="middle" >1.50</td></tr><tr><td align="center" valign="middle" >28.093</td><td align="center" valign="middle" >0.090</td><td align="center" valign="middle" >55.20</td><td align="center" valign="middle" >55.17</td><td align="center" valign="middle" >0.00062</td><td align="center" valign="middle" >0.00013</td><td align="center" valign="middle" >1.50</td></tr><tr><td align="center" valign="middle" >95.181</td><td align="center" valign="middle" >0.304</td><td align="center" valign="middle" >45.65</td><td align="center" valign="middle" >45.93</td><td align="center" valign="middle" >0.00645</td><td align="center" valign="middle" >0.00149</td><td align="center" valign="middle" >1.37</td></tr><tr><td align="center" valign="middle" >117.561</td><td align="center" valign="middle" >0.376</td><td align="center" valign="middle" >30.23</td><td align="center" valign="middle" >30.93</td><td align="center" valign="middle" >0.00956</td><td align="center" valign="middle" >0.00228</td><td align="center" valign="middle" >1.33</td></tr><tr><td align="center" valign="middle" >102.531</td><td align="center" valign="middle" >0.328</td><td align="center" valign="middle" >22.45</td><td align="center" valign="middle" >23.17</td><td align="center" valign="middle" >0.00709</td><td align="center" valign="middle" >0.00173</td><td align="center" valign="middle" >1.29</td></tr></tbody></table></table-wrap><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Experimental device for determination of local resistance coefficient of sudden expansion tube</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/6-6201818x29.png"/></fig><p>tent with the actual experiment. It is because when the momentum equation is applied, the friction force on the side face of control body is neglected.</p><p>Since there are many types of local resistance, and most of them are in turbulent status, it is must to conduct experiment to get the accurate results. The local resistance coefficient of sudden expansion tube is also deter- mined by this experiment. The formula is as follows:</p><disp-formula id="scirp.56000-formula752"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x30.png"  xlink:type="simple"/></disp-formula><p>where, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x31.png" xlink:type="simple"/></inline-formula>is calculated by formula (2).</p><p>The calculation of local resistance coefficient of sudden expansion tube is shown in <xref ref-type="table" rid="table2">Table 2</xref>.</p><p>The mean value of experimental determination of local resistance coefficient of sudden expansion tube calculated from the table above is 1.43, which is quite larger than theoretical value of 0.32. Therefore, the friction force on the side face of control body cannot be neglected when momentum equation is applied.</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/6-6201818x32.png" xlink:type="simple"/></inline-formula>can be obtained from formula (11)</p><disp-formula id="scirp.56000-formula753"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/6-6201818x33.png"  xlink:type="simple"/></disp-formula><p>The average value of the error between the local head loss calculated in accordance with local resistance coefficient determined by experiment under different flow rates and the actual measurement is only 1.33%. Obviously, the error is in the allowable range of engineering design.</p></sec><sec id="s6"><title>6. Conclusion</title><p>The local resistance coefficient derived from theory is only related to the expansion ratio of the pipe diameter, and is always a constant no matter how the flow changes. The experimental data proves that the head loss calculated from theoretical formula has large difference from the actual measurement, which is mainly because of the neglect of friction force of side face during theoretical derivation. The laboratory determination formula for local resistance coefficient is given in this paper, and the error between the local head loss calculated in accordance with local resistance coefficient determined by experiment and the actual measurement is only 1.33%. Therefore, the value of local resistance coefficient of sudden expansion determined only by actually measured section size and the experimental data meets the design requirements during pipeline design.</p></sec></body><back><ref-list><title>References</title><ref id="scirp.56000-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Yang, S.R., Wang, Z.M., He, G.Y., et al. (2006) Engineering Fluid Mechanics. 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