<?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.2014.44028</article-id><article-id pub-id-type="publisher-id">OJFD-52164</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><subject> Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Weis-Fogh Mechanism Mathematic Model of Wave Power Generation Device
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>in</surname><given-names>Chen</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>Quan</surname><given-names>Kuang</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>Yang</surname><given-names>Li</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>Songbo</surname><given-names>Wang</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>Yunling</surname><given-names>Ye</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>Shesheng</surname><given-names>Zhang</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>Wuhan University of Technology, Wuhan, China</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>sheshengz@qq.com(SZ)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>17</day><month>11</month><year>2014</year></pub-date><volume>04</volume><issue>04</issue><fpage>373</fpage><lpage>378</lpage><history><date date-type="received"><day>4</day>	<month>October</month>	<year>2014</year></date><date date-type="rev-recd"><day>4</day>	<month>November</month>	<year>2014</year>	</date><date date-type="accepted"><day>4</day>	<month>December</month>	<year>2014</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>
 
 
  A Weis-Fogh mechanism wave power generation system is designed, its physical model and mathematical model are discussed, and the component expressions of fluid dynamic expression are derived. Adopting numerical integral algorithm, the work done by fluid force acting on wing is calculated.
 
</p></abstract><kwd-group><kwd>Wave</kwd><kwd> Weis-Fogh</kwd><kwd> Power Generation</kwd><kwd> Mathematical Model</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Saving energy and reducing contaminant emission are important researching projects for economics and human living environment. As we know, using wave energy to generate electricity can reduce oil and coal consumption, and decease dust and emissions of harmful substances emission. So it attracts scientists to carry out power generation of scientific research by using wave energy [<xref ref-type="bibr" rid="scirp.52164-ref1">1</xref>] . According to the statistics data, there is huge amount of wave energy stored in the ocean, which can be used to transfer to electricity energy [<xref ref-type="bibr" rid="scirp.52164-ref2">2</xref>] . There are many devices to absorb wave energy, such as floating rope round of absorbing wave energy device [<xref ref-type="bibr" rid="scirp.52164-ref3">3</xref>] , matrix of relative movement absorbing wave energy device [<xref ref-type="bibr" rid="scirp.52164-ref4">4</xref>] , buoy type absorption wave energy device [<xref ref-type="bibr" rid="scirp.52164-ref5">5</xref>] and floating type absorption wave energy device [<xref ref-type="bibr" rid="scirp.52164-ref6">6</xref>] , according to the fluctuation characteristics of waves. All of those devices didn’t use the theory of Weis-Fogh [<xref ref-type="bibr" rid="scirp.52164-ref7">7</xref>] . According to the fluid mechanics theory of Weis-Fogh mechanism [<xref ref-type="bibr" rid="scirp.52164-ref8">8</xref>] , Weis-Fogh mechanism is a simulation of the wasp flying V vibration device, which is different from conventional produce wing lift mechanism [<xref ref-type="bibr" rid="scirp.52164-ref9">9</xref>] . Rigid body test measures the lift coefficient as high as 7 - 8 when the wing opens [<xref ref-type="bibr" rid="scirp.52164-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.52164-ref11">11</xref>] . Thus, Weis-Fogh mechanism is possible to be used in the case of wave energy power generation. But it needs a lot of scientific research.</p><p>The paper will consider Weis-Fogh wave power generation device, calculating its fluid doing work acted on the wing.</p></sec><sec id="s2"><title>2. The Working Principle of the Generation Set</title><p>Weis-Fogh wave power energy generation device makes of two parts mainly: one is Weis-Fogh absorbing wave energy mechanism; another is the power generation mechanism. As <xref ref-type="fig" rid="fig1">Figure 1</xref> shows, Weis-Fogh absorbing wave energy mechanism is below water surface, others are power generation mechanism. Those two parts are connected with push-rods which make the power generation device and Weis-Fogh absorbing wave energy mechanism as an integral device. One endpoint of the push-rod is connected with wing AB, the other point is connected with power generation. In <xref ref-type="fig" rid="fig1">Figure 1</xref>, wave makes the wing AB moving up and down, and wing AB drives the push-rod moving up and down at same times. As this way, the power generation device transfers kinetic energy into electrical energy.</p><sec id="s2_1"><title>2.1. Weis-Fogh Wave Power Device</title><p>The wing AB’s movements of Weis-Fogh mechanism wave power device will be described as below paper. According to <xref ref-type="fig" rid="fig2">Figure 2</xref>, at the beginning, the wing attaches the low wall tightly. Acted by the wave force, the endpoint of wing B leaves the wall, the wing opens, around the A point rotation. Such movement is called as opening stage, see <xref ref-type="fig" rid="fig2">Figure 2</xref>(a). After the angle is opened to the<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x6.png" xlink:type="simple"/></inline-formula>, the point A leaved away from bottom wall, and all point of wing AB moves up in same speed until the point B meets the top wall. In this case, wing AB moves up without angle turning, see <xref ref-type="fig" rid="fig2">Figure 2</xref>(b). After point B attaches top wall, the wing makes close motion until the point A meets the top wall, such movements is called the closing stage, see <xref ref-type="fig" rid="fig2">Figure 2</xref>(c). As the same way, acted by wave force, the point A leaves the wall, the wing opens, around the B point rotation. Such movement is also called as opening stage. After the angle is opened to the<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x7.png" xlink:type="simple"/></inline-formula>, the point B leaved away from bottom wall, and all point of wing AB moves down in same speed until the point A meets the low wall. In this case, wing AB moves up without angle turning. After point A attaches low wall, the wing makes close motion until the point B meets the low wall, Such movements is also called the closing stage. In such way, the wing finishes one cycle movement.</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Weis-Fogh wave power generation device</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-2320167x8.png"/></fig><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> The movements of the Weis-Fogh wave power generation device.</title></caption><fig id ="fig2_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-2320167x9.png"/></fig></fig-group></sec><sec id="s2_2"><title>2.2. Power Generation Device</title><p>The power generation device is shown as <xref ref-type="fig" rid="fig1">Figure 1</xref>, it connected with Weis-Fogh absorbing wave energy mechanism by push-rod, and transports wave energy into electrical energy. There are two push-rods by which can control the wing rotation angle.</p></sec><sec id="s2_3"><title>2.3. Force Model</title><p>According to the Weis-Fogh wave energy device, the wing is acted by fluid force. During the opening stage, the endpoint of wing A doesn’t leave the wall, the fluid force acting on wing can be calculated by using the theory of Weis-Fogh mechanism. Between the opening stage and the closed stage, the fluid force acting on wing can be calculated by fluid-solid coupling method. At the opening stage and at the closing stage, the fluid is supposed as ideal.</p></sec><sec id="s2_4"><title>2.4. The Equations of Motion of the Wing</title><p>During the opening stage, the low wall supports wing at point A, the push-rod thrusts wing, and fluid force acts on the wing. As the influence of above forces, the wing rotates around the endpoint of wing A, the motion equation is:</p><disp-formula id="scirp.52164-formula567"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x10.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x11.png" xlink:type="simple"/></inline-formula> is the moment of inertia, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x12.png" xlink:type="simple"/></inline-formula>is the torque acted by fluid force on the wing, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x13.png" xlink:type="simple"/></inline-formula>is the torque which the push-rod acts on the wing. Let opening angle is <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x14.png" xlink:type="simple"/></inline-formula> and the velocity is <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x15.png" xlink:type="simple"/></inline-formula> when<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x16.png" xlink:type="simple"/></inline-formula>.</p><p>Above equation is also used to the closing stage.</p><p>Between the opening stage and the closing stage, the wing just moves up and down, the corresponding equation of motion is:</p><disp-formula id="scirp.52164-formula568"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x17.png"  xlink:type="simple"/></disp-formula><p>Here <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x18.png" xlink:type="simple"/></inline-formula> is mass of wing, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x19.png" xlink:type="simple"/></inline-formula>is the force of the fluid to the wing projected on the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x20.png" xlink:type="simple"/></inline-formula> direction, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x21.png" xlink:type="simple"/></inline-formula>is the push from push-rod. When<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x22.png" xlink:type="simple"/></inline-formula>, let <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x23.png" xlink:type="simple"/></inline-formula> equal to<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x24.png" xlink:type="simple"/></inline-formula>, velocity is<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x25.png" xlink:type="simple"/></inline-formula><sub>.</sub></p><p>This paper will consider the fluid power during opening stage and closing stage.</p></sec></sec><sec id="s3"><title>3. Fluid Power at Opening and Closing Stage</title><p>During this period, the wing’s thickness is considered very thin compared with its length. For using theory of Weis-Fogh mechanism, the wing can be supposed as a tablet. As <xref ref-type="fig" rid="fig3">Figure 3</xref>(a) shows, the fluid domain surrounded by boundary GEFA<sub>1</sub>BA<sub>2</sub>FG is mapped into up <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula> plane. The boundary point <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula> on physic plane mappings to the real axis point <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula> on mapping plane. Point <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x29.png" xlink:type="simple"/></inline-formula> mappings to point<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x30.png" xlink:type="simple"/></inline-formula>, point <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x31.png" xlink:type="simple"/></inline-formula> mappings to point<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x32.png" xlink:type="simple"/></inline-formula>, point <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x33.png" xlink:type="simple"/></inline-formula> mappings to point<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x34.png" xlink:type="simple"/></inline-formula>, point <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x35.png" xlink:type="simple"/></inline-formula><sub> </sub>mappings to point<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x36.png" xlink:type="simple"/></inline-formula>, point <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x37.png" xlink:type="simple"/></inline-formula> mappings to point<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x38.png" xlink:type="simple"/></inline-formula>.</p><p>By conformal mapping of complex function theory, the physical to the mapping transformation formula for plane area is [<xref ref-type="bibr" rid="scirp.52164-ref7">7</xref>] :</p><disp-formula id="scirp.52164-formula569"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x39.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x40.png" xlink:type="simple"/></inline-formula> is the transform constant, function <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x41.png" xlink:type="simple"/></inline-formula> is expressed as:</p><disp-formula id="scirp.52164-formula570"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x42.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x43.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x44.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x45.png" xlink:type="simple"/></inline-formula>are constant and related to these expressions below:</p><disp-formula id="scirp.52164-formula571"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x46.png"  xlink:type="simple"/></disp-formula><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> (a) The coorespondings between physic plane and mapping plane; (b) Force direction.</title></caption><fig id ="fig3_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-2320167x47.png"/></fig><fig id ="fig3_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-2320167x48.png"/></fig></fig-group><p>Here <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x49.png" xlink:type="simple"/></inline-formula> is the length of wing, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x49.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x50.png" xlink:type="simple"/></inline-formula>is grid spacing. The steps of calculation is: getting the constant <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x49.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x50.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x51.png" xlink:type="simple"/></inline-formula> firstly, then solve the constant<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x49.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x50.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x51.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x52.png" xlink:type="simple"/></inline-formula>, finally calculating the constant<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x49.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x50.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x51.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x52.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x53.png" xlink:type="simple"/></inline-formula>.</p><p>The complex potential is:</p><disp-formula id="scirp.52164-formula572"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x54.png"  xlink:type="simple"/></disp-formula><p>Here <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x55.png" xlink:type="simple"/></inline-formula> is rotating angular velocity, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x55.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x56.png" xlink:type="simple"/></inline-formula>is the flow speed. According Bernoulli equation, we have:</p><disp-formula id="scirp.52164-formula573"><graphic  xlink:href="http://html.scirp.org/file/3-2320167x57.png"  xlink:type="simple"/></disp-formula><p>Integral the pressure along the wing surface, we get the force acting on the wing:</p><disp-formula id="scirp.52164-formula574"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x58.png"  xlink:type="simple"/></disp-formula><p>where:</p><disp-formula id="scirp.52164-formula575"><graphic  xlink:href="http://html.scirp.org/file/3-2320167x59.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.52164-formula576"><graphic  xlink:href="http://html.scirp.org/file/3-2320167x60.png"  xlink:type="simple"/></disp-formula><p>Here<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x61.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x61.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x62.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x61.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x62.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x63.png" xlink:type="simple"/></inline-formula>are frontal appeal, leading from the wing tips to the root, shown as <xref ref-type="fig" rid="fig3">Figure 3</xref>(b).</p><p>The force mapping on <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x64.png" xlink:type="simple"/></inline-formula> axis calls push.</p><disp-formula id="scirp.52164-formula577"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x65.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.52164-formula578"><graphic  xlink:href="http://html.scirp.org/file/3-2320167x66.png"  xlink:type="simple"/></disp-formula><p>The force mapping on <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x67.png" xlink:type="simple"/></inline-formula> axis calls lift</p><disp-formula id="scirp.52164-formula579"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x68.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.52164-formula580"><graphic  xlink:href="http://html.scirp.org/file/3-2320167x69.png"  xlink:type="simple"/></disp-formula><p>correspondingly, the moment is</p><disp-formula id="scirp.52164-formula581"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x70.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.52164-formula582"><graphic  xlink:href="http://html.scirp.org/file/3-2320167x71.png"  xlink:type="simple"/></disp-formula><p>Integration of the moment along the angle is the work of the wing</p><disp-formula id="scirp.52164-formula583"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-2320167x72.png"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. The Calculation of Fluid Power</title><p>According the above equations, the code is written to calculate the fluid power. <xref ref-type="fig" rid="fig4">Figure 4</xref>(a) shows that the components of force acting on wing varied with the angles when the grid spacing and the wing chord length ratio is 0.5. The curves’ widths vary large with the component of the subscript. When the dimensionless angle <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x73.png" xlink:type="simple"/></inline-formula> approaches to 0.5, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x73.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x74.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x73.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x75.png" xlink:type="simple"/></inline-formula> tend to infinity, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x73.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x75.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x76.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x73.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x75.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x76.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x77.png" xlink:type="simple"/></inline-formula> tend to 0, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x73.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x75.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x76.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x77.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x78.png" xlink:type="simple"/></inline-formula>tend to constants.</p><p>When the grid spacing and the wing chord length ratio is 0.5, <xref ref-type="fig" rid="fig4">Figure 4</xref>(b) shows the component’s moment varied with the angles. The curves’ widths vary large with the component of the subscript. The horizontal axis is dimensionless angle<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x79.png" xlink:type="simple"/></inline-formula>. When the dimensionless angle <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x79.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x80.png" xlink:type="simple"/></inline-formula> approaches to 0.5, the moment <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x79.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x80.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x81.png" xlink:type="simple"/></inline-formula> tends to infinity, and the moment <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x79.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x80.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x81.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x82.png" xlink:type="simple"/></inline-formula><sub> </sub>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x79.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x80.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x81.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x82.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x83.png" xlink:type="simple"/></inline-formula> tend to constants.</p></sec><sec id="s5"><title>5. Conclusion</title><p>The fluid force acting on the wing is the most important for Weis-Fogh wave power generation device. It is</p><fig-group id="fig4"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> (a) Component varied with the angle; (b) The component moments varied with the angle.</title></caption><fig id ="fig4_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-2320167x85.png"/></fig><fig id ="fig4_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-2320167x84.png"/></fig></fig-group><p>always calculated before device designed. According to the Weis-Fogh mechanism theory and conformal transformation theory, the fluid dynamics model of double push-rod cascade wave power generation device is built, and at opening stage and close stage, the expression formula of work done by fluid force acting on wing is derived by using integral method. Such formula is dependent with coming velocity <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-2320167x86.png" xlink:type="simple"/></inline-formula> and wing turning velocity, and can be calculated and saved in the disk. It can increase the speed of calculating fluid force and work.</p></sec><sec id="s6"><title>Acknowledgements</title><p>The paper is financially supported by China National Science &amp; Technology Innovation Fund (No. 20141049705002).</p></sec><sec id="s7"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.52164-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Kang, Q., Xiao, X., Lie, Z.X. and Huang, L.P. (2013) Control Strategy Optimization of Direct Drive Power Output Type Generation System. Automation of Electric Power Systems, 3, 24-29.</mixed-citation></ref><ref id="scirp.52164-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Jiao, Y.F. and Liu, Y.L. (2010) The Current Status and Prospect of Wave Power Generation. 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