<?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.2016.62010</article-id><article-id pub-id-type="publisher-id">OJFD-67734</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>
 
 
  Radiative Effect on Flow and Heat Transfer over a Vertically Oscillating Porous Flat Plate Embedded in Porous Medium with Oscillating Surface Temperature
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Monika</surname><given-names>Miglani</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>Net</surname><given-names>Ram Garg</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Mukesh</surname><given-names>Kumar Sharma</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Department of Mathematics, Maharshi Dayanand University, Rohtak, India</addr-line></aff><aff id="aff3"><addr-line>Department of Mathematics, Guru Jambheshwer University of Science &amp;amp; Technology, Hisar, India</addr-line></aff><aff id="aff1"><addr-line>Department of Mathematics, Haryana College of Technology &amp;amp; Management, Kaithal, India</addr-line></aff><pub-date pub-type="epub"><day>29</day><month>04</month><year>2016</year></pub-date><volume>06</volume><issue>02</issue><fpage>119</fpage><lpage>129</lpage><history><date date-type="received"><day>2</day>	<month>March</month>	<year>2016</year></date><date date-type="rev-recd"><day>accepted</day>	<month>24</month>	<year>June</year>	</date><date date-type="accepted"><day>27</day>	<month>June</month>	<year>2016</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  The effect of radiation on flow and heat transfer over a vertically oscillating porous flat plate embedded in porous medium with oscillating surface temperature is investigated. The analytic solutions of momentum and energy equations are obtained. The velocity and temperature profiles are computed. The frictional force at the plate due to viscosity of fluid is estimated in terms of non dimensional skin friction coefficient and heat convection at the plate is estimated in the form of Nusselt number. The effects of physical parameters Prandtl number Pr, Grashof number Gr, Suction parameter S and radiative parameter R on velocity and temperature profiles are analyzed through graphs. The effects of oscillation on the velocity and temperature profiles are shown through 3-D surface plot.
 
</p></abstract><kwd-group><kwd>Radiation</kwd><kwd> Suction</kwd><kwd> Heat Flux</kwd><kwd> Oscillating Porous Plate</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The radiative free convective flow has many important applications in countless industrial and environment processes e.g. heating and cooling chambers, fossil fuel combustion energy processes, evaporation from large open water reservoirs, astrophysical flows, solar power technology and space vehicle re-entry. The radiative heat transfer plays an important role in manufacturing industries for the design of reliable equipment. Nuclear power plants, gas turbines and various propulsion devices for aircraft, missiles and satellites are examples of such engineering applications.</p><p>Magneto hydrodynamic free convection flow past an infinite vertical plate oscillating in its own plane was first studied by Soundalgekar [<xref ref-type="bibr" rid="scirp.67734-ref1">1</xref>] in case of an isothermal plate. Mansour [<xref ref-type="bibr" rid="scirp.67734-ref2">2</xref>] has studied the interaction of free convection with thermal radiation of the oscillatory flow past a vertical plate. Soundalgekar and Takhar [<xref ref-type="bibr" rid="scirp.67734-ref3">3</xref>] have considered radiation effects on free convection flow past a semi-infinite vertical plate. Helmy [<xref ref-type="bibr" rid="scirp.67734-ref4">4</xref>] has investigated MHD unsteady free convective flow past a vertical porous plate. Hossain et al. [<xref ref-type="bibr" rid="scirp.67734-ref5">5</xref>] have analyzed the heat transfer response of MHD free convective flow along a vertical plate to surface temperature oscillations. Radiation and free convection flow past a moving plate was considered by Raptis and Perdikis [<xref ref-type="bibr" rid="scirp.67734-ref6">6</xref>] . Hossain et al. [<xref ref-type="bibr" rid="scirp.67734-ref7">7</xref>] have described the effect of radiation on free convection from a porous vertical plate. Kim [<xref ref-type="bibr" rid="scirp.67734-ref8">8</xref>] has founded an unsteady MHD convective heat transfer past a semi-infinite vertical porous moving plate with variable suction. Radiation effects on the free convection over a vertical flat plate embedded in porous medium with high porosity have been studied by Hossain and Pop [<xref ref-type="bibr" rid="scirp.67734-ref9">9</xref>] . El-Arabawy [<xref ref-type="bibr" rid="scirp.67734-ref10">10</xref>] studied the effect of suction/injection on a micro polar fluid past a continuously moving plate in the presence of radiation. The effects of thermal radiation on the flow past an oscillating plate with variable temperature have been studied by Pathak et al. [<xref ref-type="bibr" rid="scirp.67734-ref11">11</xref>] . Chandrakala and Raj [<xref ref-type="bibr" rid="scirp.67734-ref12">12</xref>] have studied the effects of thermal radiation on the flow past a semi infinite vertical isothermal plate with uniform heat flux in the presence of transversely applied magnetic field. Das [<xref ref-type="bibr" rid="scirp.67734-ref13">13</xref>] has analyzed the exact solution of MHD free convection flow and mass transfer near a moving vertical plate in the presence of thermal radiation. Chandrakala [<xref ref-type="bibr" rid="scirp.67734-ref14">14</xref>] have studied the radiation effects on flow past an impulsively started vertical oscillating plate with uniform heat flux. Ibrahim and Makinde [<xref ref-type="bibr" rid="scirp.67734-ref15">15</xref>] have studied the radiation effect on chemically reacting MHD boundary layer flow of heat and mass transfer through a porous vertical flat plate. Radiation effect on natural convection near a vertical plate embedded in porous medium with ramped wall temperature has been studied by Das et al. [<xref ref-type="bibr" rid="scirp.67734-ref16">16</xref>] . Chandrakala [<xref ref-type="bibr" rid="scirp.67734-ref17">17</xref>] studied the effects of thermal radiation on the flow past an infinite vertical oscillating plate with uniform heat flux. Janaand Manna [<xref ref-type="bibr" rid="scirp.67734-ref18">18</xref>] studied the effects of radiation on unsteady MHD free convective flow past an oscillating vertical porous plate embedded in a porous medium with oscillatory heat flux. Vidyasagar and Ramana [<xref ref-type="bibr" rid="scirp.67734-ref19">19</xref>] studied the radiation effect on MHD free convection flow of Kuvshinshiki fluid with mass transfer past a vertical porous plate through porous medium. Radiation effects on mass transfer flow through a highly porous medium with heat generation and chemical reaction has studied by Mohammed Ibrahim [<xref ref-type="bibr" rid="scirp.67734-ref20">20</xref>] .</p><p>The aim of the present study is to investigate the radiative effect on flow and heat transfer over a vertically oscillating porous flat plate with oscillating surface temperature.</p></sec><sec id="s2"><title>2. Formulation and Solution</title><sec id="s2_1"><title>2.1. Mathematical Model of Flow</title><p>To study free convective flow and heat transfer through a vertical porous flate plate in the influence of radiative heat flux is considered (<xref ref-type="fig" rid="fig1">Figure 1</xref>). The axis of x is taken along the vertical plate and the axis of y is normal to the plate.The plate is oscillating in its own plane with a frequency of oscillation <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x6.png" xlink:type="simple"/></inline-formula> and mean velocity<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x7.png" xlink:type="simple"/></inline-formula>. The temperature at the plate is also oscillating and the free stream temperature is constant<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x8.png" xlink:type="simple"/></inline-formula>. A constant suction velocity <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x9.png" xlink:type="simple"/></inline-formula> is applied at the oscillating porous plate. Since the plate is of semi infinite length therefore the</p><p>variation along x-axis will be negligible as compared to the variation along y-axis so <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x10.png" xlink:type="simple"/></inline-formula></p><p>In view of the physical description the governing equations are defined as follows:</p><p>The equation of continuity</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x11.png" xlink:type="simple"/></inline-formula>reduces into</p><disp-formula id="scirp.67734-formula1498"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x12.png"  xlink:type="simple"/></disp-formula><fig-group id="fig1"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Physical model of the problem.</title></caption><fig id ="fig1_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x13.png"/></fig></fig-group><p>&#222;v, is independent of y and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x14.png" xlink:type="simple"/></inline-formula> (constant) is suction normal to the plate.</p><p>The momentum equation for the prescribed geometry is given by</p><disp-formula id="scirp.67734-formula1499"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x15.png"  xlink:type="simple"/></disp-formula><p>Under usual Boussinesq’s approximation the Equation (2) becomes</p><disp-formula id="scirp.67734-formula1500"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x16.png"  xlink:type="simple"/></disp-formula><p>The energy equation is given by</p><disp-formula id="scirp.67734-formula1501"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x17.png"  xlink:type="simple"/></disp-formula><p>The associated boundary conditions are</p><disp-formula id="scirp.67734-formula1502"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x18.png"  xlink:type="simple"/></disp-formula><p>where u the flow velocity component in the x-direction, ν the kinematic viscosity, g the acceleration due to gravity, β the volumetric expansion coefficient, α the thermal diffusivity, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x19.png" xlink:type="simple"/></inline-formula>the thermal conductivity, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x20.png" xlink:type="simple"/></inline-formula>the radiative heat flux, T the fluid temperature, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x21.png" xlink:type="simple"/></inline-formula>the ambient temperature and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x22.png" xlink:type="simple"/></inline-formula> the amplitude of oscillation of the plate.</p><p>The Roseland approximation for radiative heat flux [Brewster, 1992] is given by</p><disp-formula id="scirp.67734-formula1503"><graphic  xlink:href="http://html.scirp.org/file/4-2320275x23.png"  xlink:type="simple"/></disp-formula><p>where σ is Stefan ? Boltzmann constant and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x24.png" xlink:type="simple"/></inline-formula> is the mean absorption coefficient.</p><p>Taking the Taylor series expansion of T<sup>4</sup> and neglecting terms with higher powers, we have</p><disp-formula id="scirp.67734-formula1504"><graphic  xlink:href="http://html.scirp.org/file/4-2320275x25.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_2"><title>2.2. Mathematical Formulation</title><p>Introducing following dimensionless quantities</p><disp-formula id="scirp.67734-formula1505"><graphic  xlink:href="http://html.scirp.org/file/4-2320275x26.png"  xlink:type="simple"/></disp-formula><p>Equations (3), (4) and the associated boundary conditions (5) reduces into</p><disp-formula id="scirp.67734-formula1506"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x27.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.67734-formula1507"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x28.png"  xlink:type="simple"/></disp-formula><p>where, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x29.png" xlink:type="simple"/></inline-formula>is suction parameter, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x30.png" xlink:type="simple"/></inline-formula>the Grashof number, M the magnetic parameter, Da the Darcy number, R the radiative parameter, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x31.png" xlink:type="simple"/></inline-formula>the Prandtl number, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x32.png" xlink:type="simple"/></inline-formula></p><p>The corresponding boundary conditions are</p><disp-formula id="scirp.67734-formula1508"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x33.png"  xlink:type="simple"/></disp-formula><p>There is no loss of generality in omitting the asterisk from (6) to (8).</p></sec><sec id="s2_3"><title>2.3. Numerical Solution</title><p>To solve the coupled nonlinear partial differential Equation (6) and (7) along with the boundary conditions (8), the solution for u and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x34.png" xlink:type="simple"/></inline-formula> (after dropping *) the following form will be suitable</p><disp-formula id="scirp.67734-formula1509"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x35.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.67734-formula1510"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x36.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x37.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x38.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x38.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x39.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x38.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x39.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x40.png" xlink:type="simple"/></inline-formula> are unknown to be determined.</p><p>Invoking the Equations (9) and (10) in the Equations (6) and (7) and equating harmonic and non harmonic terms, the set of ordinary differential equations are given as</p><disp-formula id="scirp.67734-formula1511"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x41.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.67734-formula1512"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x42.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.67734-formula1513"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x43.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.67734-formula1514"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x44.png"  xlink:type="simple"/></disp-formula><p>where, primes denote derivative with respect to y</p><p>The corresponding boundary conditions are</p><disp-formula id="scirp.67734-formula1515"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x45.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.67734-formula1516"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x46.png"  xlink:type="simple"/></disp-formula><p>The Equations (13) and (14) are ordinary differential equations with prescribed boundary conditions as given in (15) and (16), therefore their solutions are straight forward are given by</p><disp-formula id="scirp.67734-formula1517"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x47.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.67734-formula1518"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x48.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x49.png" xlink:type="simple"/></inline-formula></p><p>Now using expression of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x50.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x50.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x51.png" xlink:type="simple"/></inline-formula> in the Equations (11) and (12) we get second order ordinary differential equations in <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x50.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x51.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x52.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x50.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x51.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x52.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x53.png" xlink:type="simple"/></inline-formula> given by</p><disp-formula id="scirp.67734-formula1519"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x54.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.67734-formula1520"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x55.png"  xlink:type="simple"/></disp-formula><p>In view of the boundary conditions associated with <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x56.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x56.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x57.png" xlink:type="simple"/></inline-formula>, the solution of the Equations (19) and (20) are known and given by</p><disp-formula id="scirp.67734-formula1521"><label>(21)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x58.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.67734-formula1522"><label>(22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x59.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x60.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x60.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x61.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x60.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x61.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x62.png" xlink:type="simple"/></inline-formula> are constant quantities.</p><p>Now substituting expression of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x63.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x63.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x64.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x63.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x64.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x65.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x63.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x64.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x65.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x66.png" xlink:type="simple"/></inline-formula> in the Equations (9) and (10)</p><disp-formula id="scirp.67734-formula1523"><label>(23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x67.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.67734-formula1524"><label>(24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x68.png"  xlink:type="simple"/></disp-formula></sec></sec><sec id="s3"><title>3. Skin Friction</title><p>The skin-friction at the plate, which in the non-dimensional form is given by</p><disp-formula id="scirp.67734-formula1525"><label>(25)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x69.png"  xlink:type="simple"/></disp-formula><p>and computed values are given in <xref ref-type="table" rid="table1">Table 1</xref>.</p></sec><sec id="s4"><title>4. Nusselt Number</title><p>The non dimensional coefficient of heat transfer defined by Nusselt number is obtained and given by</p><disp-formula id="scirp.67734-formula1526"><label>(26)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/4-2320275x70.png"  xlink:type="simple"/></disp-formula><p>and computed values are given in <xref ref-type="table" rid="table2">Table 2</xref>.</p></sec><sec id="s5"><title>5. Results and Discussion</title><p>The velocity profiles for different parameter like Suction parameter, Grashof number, magnetic parameter, Darcy number, Prandtl number and radiation parameter are shown by Figures 2-7. Temperature profiles are also shown by Figures 8-10. In <xref ref-type="fig" rid="fig2">Figure 2</xref>, the positive values of S correspond to cooling of the plate decreases in the vicinity of the permeable plate while increases in region close to non permeable wall. In <xref ref-type="fig" rid="fig3">Figure 3</xref>, the positive values of Gr correspond to cooling of the plate increases in the vicinity of the permeable plate while decreases in region close to non permeable wall. In <xref ref-type="fig" rid="fig4">Figure 4</xref> when magnetic parameter M is increased, keeping other parameters constant the velocity increases. In <xref ref-type="fig" rid="fig5">Figure 5</xref> when Darcy number Da is increased, keeping other parameters constant the velocity decreases. In <xref ref-type="fig" rid="fig6">Figure 6</xref> and <xref ref-type="fig" rid="fig7">Figure 7</xref> when Prandtl number Pr and radiation parameter</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Non dimensional coefficient of Skin Friction-C<sub>f</sub></title></caption><table><tbody><thead><tr><th align="center" valign="middle" >S</th><th align="center" valign="middle" >Gr</th><th align="center" valign="middle" >M</th><th align="center" valign="middle" >Da</th><th align="center" valign="middle" >Pr</th><th align="center" valign="middle" >R</th><th align="center" valign="middle" >C<sub>f</sub></th></tr></thead><tr><td align="center" valign="middle" >0.0</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >15.9195</td></tr><tr><td align="center" valign="middle" >0.2</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >16.2228</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >16.6869</td></tr><tr><td align="center" valign="middle" >−0.2</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >15.6222</td></tr><tr><td align="center" valign="middle" >−0.5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >15.1854</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >3.9841</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >10</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >37.8582</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >−2</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >−12.9529</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >−5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >−25.6557</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >−10</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >−46.8270</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >3</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >11.2156</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >8</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >26.3903</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.01</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >35.8229</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >13.7920</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >8.7570</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >0.71</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >11.0189</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >4</td><td align="center" valign="middle" >28.0977</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >6</td><td align="center" valign="middle" >39.5676</td></tr></tbody></table></table-wrap><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Non dimensional coefficient of Heat Transfer- Nu</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >S</th><th align="center" valign="middle" >Pr</th><th align="center" valign="middle" >R</th><th align="center" valign="middle" >Nu</th></tr></thead><tr><td align="center" valign="middle" >0.0</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >0.0004</td></tr><tr><td align="center" valign="middle" >0.2</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >0.0757</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >0.2058</td></tr><tr><td align="center" valign="middle" >−0.2</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >−0.0657</td></tr><tr><td align="center" valign="middle" >−0.5</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >−0.1479</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >0.2174</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >0.71</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >0.2110</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >4</td><td align="center" valign="middle" >0.2028</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >6</td><td align="center" valign="middle" >0.2018</td></tr></tbody></table></table-wrap><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Variation in velocity with suction parameter at Gr = 5, M = 5, Da = 0.1, Pr = 1, R = 2,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x72.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x71.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Variation in velocity with Grashof number at S = 0.5, M = 5, Da = 0.1, Pr = 1, R = 2,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x74.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x73.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Variation in velocity with magnetic parameter at S = 0.5, Gr = 5, Da = 0.1, Pr = 1, R = 2,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x76.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x75.png"/></fig><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Variation in velocity with Darcy number at S = 0.5, Gr = 5, M = 5, Pr = 1, R = 2,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x78.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x77.png"/></fig><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Variation in velocity with Prandtl number at S = 0.5, Gr = 5, M = 5, Da = 0.1, R = 2,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x80.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x79.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Variation in velocity with radiation parameter at S = 0.5, Gr = 5, M = 5, Da = 0.1, Pr = 1,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x82.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x81.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Variation in temperature with suction parameter at Pr = 1, R = 2,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x84.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x83.png"/></fig><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Variation in temperature with Prandtl number Pr at S = 0.5, R = 2,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x86.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x85.png"/></fig><fig id="fig10"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>0</label><caption><title> Variation in temperature with radiation parameter at S = 0.5, Pr = 1,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x88.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x87.png"/></fig><p>R is increased, velocity increases in the vicinity of the permeable plate while decreases in region close to non permeable wall. In <xref ref-type="fig" rid="fig8">Figure 8</xref>, the positive values of S correspond to cooling of the plate increases temperature decreases and the negative values of S correspond to heating of the plate decreases temperature increases. <xref ref-type="fig" rid="fig9">Figure 9</xref> and <xref ref-type="fig" rid="fig1">Figure 1</xref>0 represent that temperature decreases when Prandtl number and radiation parameter R increases. The variation in fluid velocity and temperature in the porous medium through the one period of oscillation is demonstrated by <xref ref-type="fig" rid="fig1">Figure 1</xref>1 &amp; <xref ref-type="fig" rid="fig1">Figure 1</xref>2. The fluid velocity and temperature oscillates up to a certain distance from the plate while this oscillation diminishes at large distance from the plate.</p><p><xref ref-type="table" rid="table1">Table 1</xref> represents the values of skin friction. The positive values of S correspond to cooling of the plate increases skin friction increases and the negative values of S correspond to heating of the plate decreases skin friction decreases. The positive values of Gr correspond to cooling of the plate increases skin friction increases and the negative values of Gr correspond to heating of the plate decreases skin friction decreases. When M is increased the skin friction increases and when Da is increased skin friction decreased. When Pr and R is increased the skin friction increases.</p><p>The values of Nusselt number is given in <xref ref-type="table" rid="table2">Table 2</xref>. The positive values of S correspond to cooling of the plate increases Nusselt number increases and the negative values of S correspond to heating of the plate decreases Nusselt number decreases. When R and Pr are increased the Nusselt number decreases.</p></sec><sec id="s6"><title>6. Conclusions</title><p>・ Fluid flow slows down in the vicinity of the permeable plate while enhances in region close to nonpermeable</p><fig id="fig11"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>1</label><caption><title> Variation in velocity with <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x90.png" xlink:type="simple"/></inline-formula> and distance from the plate at S = 0.5, Gr = 5, M = 5, Da = 0.1, Pr = 1, R = 2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x89.png"/></fig><fig id="fig12"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>2</label><caption><title> Variation in temperature with <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/4-2320275x92.png" xlink:type="simple"/></inline-formula> and distance from the plate at S = 0.5, Pr = 1, R = 2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/4-2320275x91.png"/></fig><p>wall on increasing suction parameter correspond to cooling of the plate.</p><p>・ Fluid velocity profiles increase in the vicinity of the permeable plate while decrease in region close to non permeable wall with the increase in Grashof number correspond to cooling of the plate</p><p>・ Fluid velocity profiles increase in the vicinity of the permeable plate while decrease in region close to non permeable wall when Prandtl number and radiation parameter is increased.</p><p>・ Fluid velocity and temperature in the porous medium through the one period of oscillation oscillates up to a certain distance from the plate and this oscillation disappears far away from the plate.</p><p>・ The values of skin friction increase when magnetic parameter, Prandtl number and radiation parameter are increased while the values of skin friction decrease when Darcy number is increased.</p><p>・ Nusselt number decreases when Prandtl number and radiation parameter are increased.</p></sec><sec id="s7"><title>Cite this paper</title><p>Monika Miglani,Net Ram Garg,Mukesh Kumar Sharma, (2016) Radiative Effect on Flow and Heat Transfer over a Vertically Oscillating Porous Flat Plate Embedded in Porous Medium with Oscillating Surface Temperature. 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