<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">JAMP</journal-id><journal-title-group><journal-title>Journal of Applied Mathematics and Physics</journal-title></journal-title-group><issn pub-type="epub">2327-4352</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/jamp.2015.38119</article-id><article-id pub-id-type="publisher-id">JAMP-59104</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>
 
 
  Unsteady Flows Characteristics in a Channel with Oblique Plates
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Yinxiao</surname><given-names>Zhan</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>Tae</surname><given-names>Seon Park</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>School of Mechanical Engineering, Kyungpook National University, Daegu, South Korea</addr-line></aff><pub-date pub-type="epub"><day>26</day><month>08</month><year>2015</year></pub-date><volume>03</volume><issue>08</issue><fpage>974</fpage><lpage>979</lpage><history><date date-type="received"><day>30</day>	<month>April</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>19</month>	<year>August</year>	</date><date date-type="accepted"><day>26</day>	<month>August</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>
 
 
   Unsteady flows in a channel with oblique plates have been numerically investigated. The oblique plates as disturbance promoters are installed at the upper wall. Unsteady characteristics are examined for Re = 350 and the plate angles of a = 60<sup>。</sup>- 120<sup>。</sup>. The flow fields represent three-dimensional features variously as the plate angle varies. From frequency analysis, it is noted that the disturbed flow by the oblique plates has peculiar unsteady modes. As the flow is more unstable, multiple frequencies are appeared. 
 
</p></abstract><kwd-group><kwd>Unsteady Flow</kwd><kwd> Frequency</kwd><kwd> Oblique Plate</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Many researchers have paid much attention to the unsteady flow of a channel having various obstacles such as fins, ribs, baffles or plates [<xref ref-type="bibr" rid="scirp.59104-ref1">1</xref>]-[<xref ref-type="bibr" rid="scirp.59104-ref10">10</xref>]. The highly unsteady flows have positive influences on the heat transfer enhancement, because it can provoke the flow mixing [<xref ref-type="bibr" rid="scirp.59104-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.59104-ref2">2</xref>]. In particular, the plate of those obstacles has the geometric advantages to control the flow unsteadiness depending on the variation of plate height, plate interval, and inclination angle. In general, the laminar flow in a channel becomes turbulent flows, as the Reynolds number increases. The turbulent flow is characterized by chaotic changes related to coherent vortices of many scales. So, the occurrence of many vortices can be connected directly to the turbulent flow or unsteady laminar flow. From this point of view, the disturbed flow by the plate is very interesting to study the unsteady evolution.</p><p>From the previous studies [<xref ref-type="bibr" rid="scirp.59104-ref3">3</xref>] [<xref ref-type="bibr" rid="scirp.59104-ref4">4</xref>] for a channel having the plates/baffles mounted normally in the streamwise direction on both channel walls, it was found that the flow instability is strongly correlated to the wall heat transfer. Zhan and Park [<xref ref-type="bibr" rid="scirp.59104-ref5">5</xref>] studied the effect of insulated oblique plates on oscillating flow in a channel. The result revealed the significant heat transfer enhancement by activating unsteady flow due to the oblique plate mounted on the channel wall. Yang et al. [<xref ref-type="bibr" rid="scirp.59104-ref6">6</xref>]-[<xref ref-type="bibr" rid="scirp.59104-ref8">8</xref>] identified that the velocity fluctuation is responsible for the heat transfer enhancement. They investigated the effects of baffle interval and Reynolds number on the flow instabilities. On the other hand, several researchers [<xref ref-type="bibr" rid="scirp.59104-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.59104-ref10">10</xref>] investigated the influences of baffle shape on the heat transfer in a duct flow. The results showed that the vortical flows caused by the angled baffles induce the increase in heat transfer rate. Accordingly, we can expect that the development of unsteady vertical flows is a primary factor to enhance the heat transfer in a channel or duct. However, when obstacles are introduced in a channel or duct, the detailed evolution of unsteady flows is scarcely reported in the literature.</p><p>In the present study, the unsteady flow for the channel having a wall with periodic plates is investigated. For a channel with various obstacles, as the Reynolds number increases, the two-dimensional steady flow becomes a time-periodic and chaotic flow. This can be explained by a bifurcation theory. An example is Hopf bifurcation where a steady state bifurcates into a time-periodic state. Compared with other obstacles, the plate has a geometrical advantage to realize various flow conditions using one configuration. The channel flow with plates can be diversely changed depending on the inclination of plates. So, this study attempts a parametric study to examine the effects of geometrical variation on the unsteady flow characteristics for the channel flow with plates. The plate interval is 2 H and the plate length is 0.4 H. The inclination angle of the plates are changed for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x3.png" xlink:type="simple"/></inline-formula>. The effects of the inclination angle on the critical Reynolds number for Hopf bifurcation and the spectral analysis are discussed. After that, as the two-dimensional unsteady flow develops further, the flow transits to three-dimensional structure. So, several simulations are performed to elucidate three-dimensional unsteady flow characteristics</p></sec><sec id="s2"><title>2. Numerical Methods and Flow Condition</title><sec id="s2_1"><title>2.1. Governing Equation</title><p>The flow is two-dimensional with constant properties. The x-axis is taken in the flow direction and the y-axis is perpendicular to the flow direction. The flow is assumed to be laminar and incompressible. Buoyancy induced effects are neglected. The governing equations for continuity, momentum and temperature are given by</p><disp-formula id="scirp.59104-formula69"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/59104x4.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.59104-formula70"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/59104x5.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x6.png" xlink:type="simple"/></inline-formula>, are the velocity components, pressure, temperature, viscosity and Prandtl number, respectively. Quantities such as <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x7.png" xlink:type="simple"/></inline-formula> are set as air properties at room temperature. <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x8.png" xlink:type="simple"/></inline-formula>represent the stream wise mean pressure gradient, which needs to be calculated dynamically in order to maintain a constant mass flow rate and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x9.png" xlink:type="simple"/></inline-formula> is the kronecker delta.</p></sec><sec id="s2_2"><title>2.2. Numerical Methods and Boundary Condition</title><p>The spatial discretization is performed with the fourth-order compact scheme. The viscous term and the other terms are evaluated by the fourth-order central difference. A nonstaggered grid arrangement is adopted and the momentum interpolation techniqueis employed to avoid pressure-velocity decoupling. The PISO algorithm is employed for pressure-velocity coupling [<xref ref-type="bibr" rid="scirp.59104-ref11">11</xref>]. The momentum and energy equations are solved with second- order upwind scheme. Zhan and Park [<xref ref-type="bibr" rid="scirp.59104-ref5">5</xref>] adopted the same computational method. Periodic boundary condition with constant mass flow rates is specified at the inlet and outlet of the channel. No-slip and constant wall temperature conditions are specified on the upper and lower walls of the channel. Oblique plate is insulated.</p><p><xref ref-type="fig" rid="fig1">Figure 1</xref> shows the flow geometry and the coordinate system. It is consisted of two walls channel of height H with insulated a thin oblique plate (t = 0.02 H) on the upper wall. No-slip and constant wall temperature</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Flow configuration</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/59104x10.png"/></fig><p>conditions are specified on the upper and lower walls of the channel. The lengths of the oblique plates d is 0.4 H. Periodicity lengths <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x11.png" xlink:type="simple"/></inline-formula> is fixed at<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x12.png" xlink:type="simple"/></inline-formula>. For these cases, the inclination angle of the plates limited in α = 60˚ - 120˚ is defined as<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x13.png" xlink:type="simple"/></inline-formula>. Oblique plate is insulated. Because the flow is maintained at Re = 350, the steady flow can be bifurcated by the variation of tilt angles.</p></sec></sec><sec id="s3"><title>3. Result and Discussion</title><p>In order to examine the three-dimensional heat transfer for channel with oblique plates, two-dimensional simulations is performed to analyze basic transition process from the steady state to unstable state. For all selected tilt angle, the relationship between the flow frequency and the tilt angle is studied.</p><sec id="s3_1"><title>3.1. Two-Dimensional Flows</title><p>The presence of periodic oblique plates in a channel wall makes the flow unstable. When the flow evolves from a steady state to time-dependent self-sustained periodic flows, the critical Reynolds number (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x14.png" xlink:type="simple"/></inline-formula>) can be defined. As the tilt angle changes, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x15.png" xlink:type="simple"/></inline-formula>is significantly changed. Because the different <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x16.png" xlink:type="simple"/></inline-formula> gives different unsteady flows.</p><p><xref ref-type="fig" rid="fig2">Figure 2</xref> demonstrates the time history of the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x17.png" xlink:type="simple"/></inline-formula>-velocity at <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x18.png" xlink:type="simple"/></inline-formula> for Re = 350. As can be seen that for the predicted flows are unsteady for all tilt angles, and oscillation amplitude is increased and then decreased as the tilt angle increases. The highest of flow oscillation amplitude is also observed for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x19.png" xlink:type="simple"/></inline-formula>, and it is obviously larger for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x19.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x20.png" xlink:type="simple"/></inline-formula> than that for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x19.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x21.png" xlink:type="simple"/></inline-formula>.</p><p>In order to determine the unsteady flow characteristics, i.e., main fundamental frequencies and harmonics. As the tilt angle increases, Fourier power spectra of u-velocity and u-and v-phase portrait for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x22.png" xlink:type="simple"/></inline-formula>, at Re = 350 during 10 T are showed in <xref ref-type="fig" rid="fig3">Figure 3</xref>. One can see that flow have different frequency characteristic for each tilt angle. When<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x23.png" xlink:type="simple"/></inline-formula>, flow bifurcate into time-dependent periodic flow characterized by one fundamental frequency<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x24.png" xlink:type="simple"/></inline-formula>. The phase space trajectory approaches a limit cycle. When<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x25.png" xlink:type="simple"/></inline-formula>, flow with one frequency <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x26.png" xlink:type="simple"/></inline-formula> and harmonics<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x27.png" xlink:type="simple"/></inline-formula>, its trajectory of u and v velocity is limit cycle also. As increasing tilt angle to 80˚, a secondary instability occurs and a new characteristic fundamental frequency <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x28.png" xlink:type="simple"/></inline-formula> and their linear combinations (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x29.png" xlink:type="simple"/></inline-formula>) appears, which represents the flow evolved into a quasi periodic flow regime [<xref ref-type="bibr" rid="scirp.59104-ref12">12</xref>]. Here <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x30.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x31.png" xlink:type="simple"/></inline-formula> are integers. As we conjectured, the tilt angles of the plate completely control the flow field. The flow with large-amplitude oscillations is more unstable and is more easily to bifurcate into chaotic regime.</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Time history of the U velocity at<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x33.png" xlink:type="simple"/></inline-formula>, for Re = 350</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/59104x32.png"/></fig><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Fourier power spectra and phase portraits of u-and v-velocity at Re = 350.</title></caption><fig id ="fig3_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/59104x34.png"/></fig><fig id ="fig3_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/59104x35.png"/></fig></fig-group></sec><sec id="s3_2"><title>3.2. Characteristics of Three-Dimensional Flows</title><p>According to the above analysis, the change of the tilt angle brings significant change in flow characteristic. In order to detect the 3D flow, the two-dimensional flow field is expanded in the spanwise direction. <xref ref-type="fig" rid="fig4">Figure 4</xref> shows the time evolution of u-velocity for all tilt angles at two different points. Both of two points are taken at</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x36.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x37.png" xlink:type="simple"/></inline-formula>, and in span wise direction, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x38.png" xlink:type="simple"/></inline-formula>respectively. For all tilt angles, two-di-</p><p>mensional T-S wave grows with time and becomes unstable to three-dimensional perturbation. The two curves are identical before the appearance of the 3D disturbance, due to the secondary instability which induces the three-dimensional flow is not prevailing compared with the basic flow. After the different initial time, however, the secondary instability becomes big enough to distort the basic flow, the two curves deviate both in magnitude and in phase. 3D perturbation is infinitesimal for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x39.png" xlink:type="simple"/></inline-formula>. For different tilt angle, initial time that the base mean flow is distorted leading to 3D flow is different. When<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x39.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x40.png" xlink:type="simple"/></inline-formula>, the initial time is shortest. That may be influence the heat transfer in 3D. <xref ref-type="fig" rid="fig5">Figure 5</xref> shows instantaneous streamlines of upper wall for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x39.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x41.png" xlink:type="simple"/></inline-formula>, for Re = 350, t = 4457.862. The parallel streamlines are obtained for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x39.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x42.png" xlink:type="simple"/></inline-formula>. This confirm that the mean flow have not distorted yet. For the other tilt angle, the flow field is clearly bifurcated to three dimensional. And one can notice that the flow is more distorted near the oblique plates. Corresponding to the frequency characteristic (<xref ref-type="fig" rid="fig3">Figure 3</xref>), as the tilt angle increases, vortex is expanded to spanwise direction, inducing the appearance of the multiple frequencies.</p></sec></sec><sec id="s4"><title>4. Conclusions</title><p>Unsteady flow and heat transfer in a channel with oblique plates have been numerically investigated. The inclination angle of the plates is changed in a range of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x43.png" xlink:type="simple"/></inline-formula>. Flow characteristics are investigated for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x44.png" xlink:type="simple"/></inline-formula>.</p><p>As the tilt angle changes, the flows evolve from steady state to periodic state with one primary frequency and then to quasi periodic with two primary frequencies and their linear combinations (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x45.png" xlink:type="simple"/></inline-formula>). In particularly, two-dimensional flow with multiple frequencies can be easily three-dimensional. For the range of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x45.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x46.png" xlink:type="simple"/></inline-formula>,</p><fig-group id="fig4"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Three-dimensional geometry and time histories of u at two spanwise location: Re = 350.</title></caption><fig id ="fig4_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/59104x47.png"/></fig><fig id ="fig4_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/59104x48.png"/></fig></fig-group><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Instantaneous streamlines for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/59104x50.png" xlink:type="simple"/></inline-formula>, Re = 350 (y = 0.95 H)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/59104x49.png"/></fig><p>the transition from the periodic state to chaotic state is obtained quickly. For the geometric condition having multiple frequencies, the flow becomes chaotic not turbulent, because coherent vortices are not produced.</p></sec><sec id="s5"><title>Cite this paper</title><p>Yinxiao Zhan,Tae Seon Park, (2015) Unsteady Flows Characteristics in a Channel with Oblique Plates. Journal of Applied Mathematics and Physics,03,974-979. doi: 10.4236/jamp.2015.38119</p></sec></body><back><ref-list><title>References</title><ref id="scirp.59104-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Rowley, G.J. and Patankar, S.V. (1983) Analysis of Laminar Flow and Heat Transfer in Tubes with Internal Circumferential Fins. Int. J. Heat Mass Transfer, 27, 553-560. http://dx.doi.org/10.1016/0017-9310(84)90028-0</mixed-citation></ref><ref id="scirp.59104-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Mackley, M.R. and Stonestreet, P. 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