<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">OJFD</journal-id><journal-title-group><journal-title>Open Journal of Fluid Dynamics</journal-title></journal-title-group><issn pub-type="epub">2165-3852</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ojfd.2015.54036</article-id><article-id pub-id-type="publisher-id">OJFD-62313</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>
 
 
  Effects of Thermal Radiation and Radiation Absorption on Flow Past an Impulsively Started Infinite Vertical Plate with Newtonian Heating and Chemical Reaction
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>wetha</surname><given-names>Ravi</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>Jagdish</surname><given-names>Prakash</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Viswanatha</surname><given-names>Reddy Gottam</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Vijaya</surname><given-names>Kumar Varma Sibyala</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref></contrib></contrib-group><aff id="aff3"><addr-line>Department of Mathematics, S. V. University, Tirupati, India</addr-line></aff><aff id="aff2"><addr-line>Department of Mathematics, University of Botswana, Gaborone, Botswana</addr-line></aff><aff id="aff1"><addr-line>Department of Mathematics, Gudlavalleru Engineering College, Gudlavalleru, India</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>prakashj@mopipi.ub.bw(JP)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>28</day><month>10</month><year>2015</year></pub-date><volume>05</volume><issue>04</issue><fpage>364</fpage><lpage>379</lpage><history><date date-type="received"><day>3</day>	<month>November</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>24</month>	<year>December</year>	</date><date date-type="accepted"><day>29</day>	<month>December</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>
 
 
  A perfect solution to the present natural convective flow problem of a vertical transfinite plate owing to the impulsive motion in the ubiety of first ordered chemical reaction, radiation absorption, radiation, Newtonian heating and species concentration in its plane is evolved by applying the method of Laplace transforms in closed form at the plate. Exact results for velocity, temperature, concentration fields are prevailed and expressions for heat and mass transfer rates are also found. The effects are analyzed for the respective invariables for both ammonia and water vapor.
 
</p></abstract><kwd-group><kwd>Newtonian Heating</kwd><kwd> Natural Convection</kwd><kwd> Chemical Reaction</kwd><kwd> Incompressible Fluid</kwd><kwd> Radiation  Absorption and Radiation</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>On chemical reaction, the field of mass and heat transfer is of good pragmatic importance to applied scientists owing to its general occurrence in various fields of engineering and science. Especially, the subject of mass and heat transfer with heat radiation, chemical reaction has significant role in hydrometallurgical and chemical industries. For a moving plate, a chemical reaction takes place in legion chemical processes between a fluid and foreign mass. This sue is involved in many industrial usages such as glassware or ceramics manufacturing, food processing and production of polymers. The convection study with mass and heat transfer plays a major role in the dispersion and formation of fog, design of chemical processing equipment’s, temperature distribution, and moisture over agricultural fields and in the paper drying process.</p><p>Ahmed et al. [<xref ref-type="bibr" rid="scirp.62313-ref1">1</xref>] have identified the analysis for MHD rotating heat or mass transport phenomenon bounded by a vertical oscillating surface in the Mein of Darcian porous regime by using Numerical/Laplace transform. Characteristics of the heat and mass transfer in the Mien of chemical reaction and thermal radiation for a Newtonian incompressible fluid across an extending vertical surface having temperature dependent viscosity was studied by Kandasamy et al. [<xref ref-type="bibr" rid="scirp.62313-ref2">2</xref>] . Makinde [<xref ref-type="bibr" rid="scirp.62313-ref3">3</xref>] examined the free transient convection interaction of an absorbing, emitting plate with thermal radiation. Mukhopadhyay [<xref ref-type="bibr" rid="scirp.62313-ref4">4</xref>] performed an investigation on the results of heat transfer and thermal radiation on a mixed unsteady convective flow across an extending porous surface in porous medium.</p><p>Heat transfer analysis of a forced convective flow of the fluid past an embedded plate in a porous medium for an incompressible fluid was examined by Mukhopadhyay and Layek [<xref ref-type="bibr" rid="scirp.62313-ref5">5</xref>] . Muthucumaraswamy and Ganesan [<xref ref-type="bibr" rid="scirp.62313-ref6">6</xref>] looked at the impulsively started transient radiation-convection flow with vertical temperature consequences. An analysis of the chemical reaction, theoretically a result, with variable temperature on a vertical oscillating plate was given by Muthucumaraswamy [<xref ref-type="bibr" rid="scirp.62313-ref7">7</xref>] . Reddy et al. [<xref ref-type="bibr" rid="scirp.62313-ref8">8</xref>] investigated the consequences of unsteady natural MHD convective flow in a porous medium with constant mass diffusion and Newtonian heating. The effects of MHD radiating and chemically reacting fluid past a non-isothermal impulsively started vertical surface adjacent to a porous regime by using numerical analysis was discussed by Sahin Ahmed [<xref ref-type="bibr" rid="scirp.62313-ref9">9</xref>] .</p><p>The importance of the present flow problem is to analyze the effects of thermal radiation and radiation absorption on the flow past an impulsively started infinite vertical plate with Newtonian heating and chemical reaction.</p></sec><sec id="s2"><title>2. Mathematical Analysis</title><p>Free convective unsteady flow of the fluid for a vertical transfinite plate with Newtonian heating, past an impulsively started incompressible viscous fluid in the Mien of radiation and radiation absorption is studied. Along the plate and in the vertical upward direction, axis <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x7.png" xlink:type="simple"/></inline-formula> is chosen and normal to the plate, axis <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x8.png" xlink:type="simple"/></inline-formula> is considered. Initially the fluid and the plate are having same temperature <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x9.png" xlink:type="simple"/></inline-formula> and the concentration <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x10.png" xlink:type="simple"/></inline-formula> at all points in a stationary state for time<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x11.png" xlink:type="simple"/></inline-formula>. The coordinate system and the flow model are shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>. The plate is fixed with a velocity <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x12.png" xlink:type="simple"/></inline-formula> in the vertical direction into impulsive motion versus the gravitational field at time<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x13.png" xlink:type="simple"/></inline-formula>. We assumed that i) heat transfer rate and the local surface temperature <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x14.png" xlink:type="simple"/></inline-formula> are proportional to one another from the surface, and near the plate concentration rises to <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x15.png" xlink:type="simple"/></inline-formula> and ii) the consequences of viscous dissipation are negligible in the energy equation. Among the fluid and diffusing species, there is a first order chemical reaction. Since all the physical quantities are expressed in terms of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x16.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x17.png" xlink:type="simple"/></inline-formula>only and are free from <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x18.png" xlink:type="simple"/></inline-formula> and in the direction of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x19.png" xlink:type="simple"/></inline-formula>, the plate is considered transfinite.</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> A sketch of flowmodel and coordinate system</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x20.png"/></fig><p>The equations for this present flow, by the Boussinesq estimation are as follows</p><disp-formula id="scirp.62313-formula2003"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x21.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2004"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x22.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2005"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x23.png"  xlink:type="simple"/></disp-formula><p>and the connected conditions for this flow are</p><disp-formula id="scirp.62313-formula2006"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x24.png"  xlink:type="simple"/></disp-formula><p>Here <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x25.png" xlink:type="simple"/></inline-formula></p><p>The term of radiative heat flux by the Rosseland estimation is given by</p><disp-formula id="scirp.62313-formula2007"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x26.png"  xlink:type="simple"/></disp-formula><p>But here with in the flow, presuming that the deviation in temperatures can be showed as a linear combination of the temperatures and around<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x27.png" xlink:type="simple"/></inline-formula>, which is found by expanding <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x28.png" xlink:type="simple"/></inline-formula> in a Taylor’s series as follows:</p><disp-formula id="scirp.62313-formula2008"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x29.png"  xlink:type="simple"/></disp-formula><p>and ignoring the higher ordered terms, beyond the first degree, we get</p><disp-formula id="scirp.62313-formula2009"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x30.png"  xlink:type="simple"/></disp-formula><p>Differentiating Equation (5) with respect to <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x31.png" xlink:type="simple"/></inline-formula> and applying Equation (6), we get</p><disp-formula id="scirp.62313-formula2010"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x32.png"  xlink:type="simple"/></disp-formula><p>We have inserted the non-dimensional succeeding measures</p><disp-formula id="scirp.62313-formula2011"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x33.png"  xlink:type="simple"/></disp-formula><p>The Equations (1)-(3) are reduced into the following forms by using the Equations (8) and (9) as follows</p><disp-formula id="scirp.62313-formula2012"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x34.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2013"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x35.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2014"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x36.png"  xlink:type="simple"/></disp-formula><p>In non-dimensional form, the conditions reduce to as follows</p><disp-formula id="scirp.62313-formula2015"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x37.png"  xlink:type="simple"/></disp-formula></sec><sec id="s3"><title>3. Solution of the Problem</title><p>The non-dimensional Equations (10)-(12) associated with the conditions given by Equations (13) are evolved by the method of Laplace transforms, and therefore the results of concentration, temperature and velocity are given by</p><disp-formula id="scirp.62313-formula2016"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x38.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2017"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x39.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2018"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x40.png"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. The Rate of Heat Transfer</title><p>In dimensionless form, heat transfer rate from the temperature gradient is</p><disp-formula id="scirp.62313-formula2019"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x41.png"  xlink:type="simple"/></disp-formula><p>From Equations (15) and (17), we get</p><disp-formula id="scirp.62313-formula2020"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x42.png"  xlink:type="simple"/></disp-formula></sec><sec id="s5"><title>5. The Rate of Mass Transfer</title><p>In dimensionless form, mass transfer rate from the concentration gradient is</p><disp-formula id="scirp.62313-formula2021"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x43.png"  xlink:type="simple"/></disp-formula><p>From Equations (14) and (19), we get</p><disp-formula id="scirp.62313-formula2022"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/8-2320251x44.png"  xlink:type="simple"/></disp-formula></sec><sec id="s6"><title>6. Deduction</title><p>The effects of this analysis are in good agreement with the results given by Rajesh [<xref ref-type="bibr" rid="scirp.62313-ref8">8</xref>] in the absence of parameters radiation absorption (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x45.png" xlink:type="simple"/></inline-formula>) and radiation (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x45.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x46.png" xlink:type="simple"/></inline-formula>),</p><p>where</p><disp-formula id="scirp.62313-formula2023"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x47.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2024"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x48.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2025"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x49.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2026"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x50.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2027"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x51.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2028"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x52.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2029"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x53.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2030"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x54.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2031"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x55.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2032"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x56.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x57.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x57.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x58.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x57.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x59.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x57.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x59.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x60.png" xlink:type="simple"/></inline-formula>,</p><disp-formula id="scirp.62313-formula2033"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x61.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x62.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x62.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x63.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x62.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x63.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x64.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x62.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x63.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x64.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x65.png" xlink:type="simple"/></inline-formula>,</p><disp-formula id="scirp.62313-formula2034"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x66.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2035"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x67.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2036"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x68.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2037"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x69.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2038"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x70.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x71.png" xlink:type="simple"/></inline-formula>,</p><disp-formula id="scirp.62313-formula2039"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x72.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2040"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x73.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2041"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x74.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2042"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x75.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2043"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x76.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2044"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x77.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2045"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x78.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2046"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x79.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.62313-formula2047"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x80.png"  xlink:type="simple"/></disp-formula></sec><sec id="s7"><title>7. Results and Discussion</title><p>In this field of study, in order to examine the consequences of velocity field, temperature profile and concentration profiles by allotting numerical values for several arguments for both water vapor and ammonia, Prandtl number (Pr) and Schmidt number (Sc) values are considered.</p><p>For several values of different arguments the velocities are analyzed and are presented in Figures 2-7 at time t = 0.4 respectively, for both the types of heating (Gr &lt; 0, Gm &lt; 0) plate and cooling (Gr &gt; 0, Gm &gt; 0) plate. <xref ref-type="fig" rid="fig2">Figure 2</xref> depicts the result of Schmidt number (Sc) at time t = 0.4 on the flow. With an increase in Sc, it is noticed that the velocity increases for heating of the plate and decreases for cooling of the plate and as Sc increases at t = 0.4 from 0.22 - 0.30 and to 0.60, the maximum velocity of the fluid decreases by 5.7% - 10% for ammonia and by 5.6% - 10.9% for water vapor in the case of cooling plate and the minimum velocity of the fluid increases by 10% and 16.58% for ammonia and by 10.26% - 17% for water vapor in the case of heating plate. Prandtl number (Pr) effects on the flow are expressed in <xref ref-type="fig" rid="fig4">Figure 4</xref> at time t = 0.4. It is identified that there is an increase in velocity near the plate and then decreases with a point of separation moving far away from the plate in the type of</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Velocity profile shows the effect of Sc and Pr = 0.71, K = 0.2, Nr = 0.1, Q<sub>1</sub> = 0.1, t = 0.4</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x81.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Velocity profile displays the result of Sc and Pr = 0.71, K = 0.2, Nr = 0, Q<sub>1</sub> = 0, t = 0.4</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x82.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Velocity profile shows the effect of Pr and Sc = 0.22, K = 0.2, Nr = 0.1, Q<sub>1</sub> = 0.1, t = 0.4</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x83.png"/></fig><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Velocity profile displays the result of Pr and Sc = 0.22, K = 0.2, Nr = 0, Q<sub>1</sub> = 0, t = 0.4</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x84.png"/></fig><p>heating and in the instance of cooling plate, the reverse effect is found with the increase of Pr. Owing to the variation in parameter of chemical reaction (K), <xref ref-type="fig" rid="fig6">Figure 6</xref> reveals the consequence of velocity profiles at time t = 0.4. As K increases, it is found that, there is an increase velocity in the plate of heating type and the velocity decreases in the plate of cooling type and as K increases at t = 0.4 from 0.2 - 2 and to 5, the maximum velocity of</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Velocity profile shows the effect of K and Sc = 0.22, Pr = 0.71, Nr = 0.1, Q<sub>1</sub> = 0.1, t = 0.4</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x85.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Velocity profile displays the result of K and Sc = 0.22, Pr = 0.71, Nr = 0, Q<sub>1</sub> = 0, t = 0.4</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x86.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Velocity profile shows the effect of K and Sc = 0.22, Pr = 0.71, Nr = 0.1, Q<sub>1</sub> = 0.1, t = 0.4</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x87.png"/></fig><p>the fluid decreases by 7.4% - 6.8% for ammonia and by 7.1% - 7.4% for water vapor in the case of cooling plate and the minimum velocity of the fluid increases by 8.4% - 9.04% for ammonia and by 5.56% - 9.61% for water vapor in the case of heating plate.</p><p>For various values of Nr (radiation parameter), the velocity profile is shown in <xref ref-type="fig" rid="fig8">Figure 8</xref> at t = 0.4. It is seen that there is a decrease in velocity near the plate and then increases with a point of separation moving away from the plate in the cooling case and the phenomenon is reversed in the case of heating type with the decrease of Nr. <xref ref-type="fig" rid="fig9">Figure 9</xref> describes the effects of Q<sub>1</sub> (radiation absorption parameter) at t = 0.4. As Q<sub>1</sub> decreases, it is observed that the velocity increases for heating plate and decreases for cooling plate. <xref ref-type="fig" rid="fig1">Figure 1</xref>0 reveals the result of velocity profile at several times (t = 0.4, 0.6, 0.8). It is identified that there is a considerable decrease in velocity in the heating type and increase when the plate is cooled as time (t) increases. The same results are noticed in the absence of thermal radiation and radiation absorption for different values of Sc, Pr, K, t which are shown in <xref ref-type="fig" rid="fig3">Figure 3</xref>, <xref ref-type="fig" rid="fig5">Figure 5</xref>, <xref ref-type="fig" rid="fig7">Figure 7</xref>, and <xref ref-type="fig" rid="fig1">Figure 1</xref>1. Hence, these results are in good agreement with the results of Rajesh [<xref ref-type="bibr" rid="scirp.62313-ref10">10</xref>] .</p><p>The effect of temperature profile for several values of various parameters are studied and shown in Figures 12-17 at time t = 0.2. It is observed from Figures 12-14 that the temperature rises with the fall in Sc and K. In Figures 15-17, it is observed that the temperature rises with the increase of Nr, Q<sub>1</sub>, and t. Moreover <xref ref-type="fig" rid="fig1">Figure 1</xref>3 shows the results of velocity for different values of Pr. It is noticed from the values that, velocity increases near the</p><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Velocity profile displays the result of K and Sc = 0.22, Pr = 0.71, Nr = 0, Q1 = 0, t = 0.4</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x88.png"/></fig><fig id="fig10"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>0</label><caption><title> The effect of velocity profile fortand Pr = 0.71, K = 0.2, Nr = 0.1, Sc = 0.22, Q<sub>1</sub> = 0.1</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x89.png"/></fig><fig id="fig11"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>1</label><caption><title> The result of velocity profile for tand Sc = 0.22, K = 0.2, Nr = 0.1, Q<sub>1</sub> = 0.1, Pr = 0.71</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x90.png"/></fig><fig id="fig12"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>2</label><caption><title> Temperature profile presents the effect of Sc and Pr = 0.71, K = 0.2, Nr = 0.1, Q<sub>1</sub> = 0.1, t = 0.2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x91.png"/></fig><fig id="fig13"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>3</label><caption><title> Temperature profile shows the resultof Pr and Sc = 0.22, K = 0.2, Nr = 0.1, Q<sub>1</sub> = 0.1, t = 0.2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x92.png"/></fig><fig id="fig14"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>4</label><caption><title> Temperature profile displays ensue of K and Sc = 0.22, Pr = 0.71, Nr = 0.1, Q<sub>1</sub> = 0.1, t = 0.2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x93.png"/></fig><fig id="fig15"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>5</label><caption><title> Temperature profile indicates the effect of Nr and 0.22, K = 0.2, Q<sub>1</sub> = 0.1, Pr = 0.71, t = 0.2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x94.png"/></fig><fig id="fig16"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>6</label><caption><title> The effect of temperature profile for Q<sub>1</sub> and Pr = 0.71, Sc = 0.22, Nr = 0.1, K = 0.2, t = 0.2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x95.png"/></fig><fig id="fig17"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>7</label><caption><title> Theresult of temperature profile for tand Sc = 0.22, K = 0.2, Q<sub>1</sub> = 0.1, Pr = 0.1, Nr = 0.1</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x96.png"/></fig><fig id="fig18"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>8</label><caption><title> Concentration profile displays the effect of Sc and K = 0.2, t = 0.2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x97.png"/></fig><p>plate and falls far away from the plate with a point of separation.</p><p>The effect of concentration profile for several values of various parameters is studied and is presented in Figures 18-20 at times 0.4. From <xref ref-type="fig" rid="fig1">Figure 1</xref>8 and <xref ref-type="fig" rid="fig1">Figure 1</xref>9, it is identified that with the decrease in Sc and K, the concentration increases. And from <xref ref-type="fig" rid="fig2">Figure 2</xref>0, it is found that there is a rise in concentration with the rise in time t. For several values of various arguments, the Sherwood number versus time is presented in <xref ref-type="fig" rid="fig2">Figure 2</xref>1 and <xref ref-type="fig" rid="fig2">Figure 2</xref>2. It is identified that, there is an increase in Sherwood number for both hydrogen and water vapor with the increase of Sc and K.</p><p>For different values of various arguments for both hydrogen and water vapor, the Nusselt number versus time is shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>3. From this figure, it is observed that, there is a rise in Nusselt number with the fall in Pr.</p><fig id="fig19"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>9</label><caption><title> Concentration profile shows theresult of K and Sc = 0.22, t = 0.2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x98.png"/></fig><fig id="fig20"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref>0</label><caption><title> Concentration profile presents theensue of t and Sc = 0.22, K = 0.2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x99.png"/></fig><fig id="fig21"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref>1</label><caption><title> Effect of Sc on the real part of Sherwood number and K = 0.2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x100.png"/></fig><fig id="fig22"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref>2</label><caption><title> Result of K on the real part of Sherwood number and Sc = 0.22</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x101.png"/></fig><fig id="fig23"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref>3</label><caption><title> Effect of Pr on the real part of nusselt number and K = 0.2, Sc = 0.22, Nr = 0.1, Q<sub>1</sub> = 0.1</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x102.png"/></fig><fig id="fig24"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref>4</label><caption><title> Result of Pr on the real part of nusselt number and K = 0.2, Sc = 0.22, Nr = 0, Q<sub>1</sub> = 0</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/8-2320251x103.png"/></fig><p>And the same results are noticed in the absence of thermal radiation and radiation absorption for different values of Pr which is shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>4. Hence, these results are in good agreement with the results of Rajesh [<xref ref-type="bibr" rid="scirp.62313-ref10">10</xref>] .</p></sec><sec id="s8"><title>Cite this paper</title><p>SwethaRavi,JagdishPrakash,Viswanatha ReddyGottam,Vijaya Kumar VarmaSibyala, (2015) Effects of Thermal Radiation and Radiation Absorption on Flow Past an Impulsively Started Infinite Vertical Plate with Newtonian Heating and Chemical Reaction. Open Journal of Fluid Dynamics,05,364-379. doi: 10.4236/ojfd.2015.54036</p></sec><sec id="s9"><title>Nomenclature</title><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x104.png" xlink:type="simple"/></inline-formula>: concentration far away from the plate;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x105.png" xlink:type="simple"/></inline-formula>: concentration;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x106.png" xlink:type="simple"/></inline-formula>: non-dimensional species concentration;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x107.png" xlink:type="simple"/></inline-formula>: concentration at the plate;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x108.png" xlink:type="simple"/></inline-formula>: molecular diffusivity;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x109.png" xlink:type="simple"/></inline-formula>: specific heat at constant pressure;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x110.png" xlink:type="simple"/></inline-formula>: thermal grashoff number;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x111.png" xlink:type="simple"/></inline-formula>: mass grashoff number;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x112.png" xlink:type="simple"/></inline-formula>: coefficient of heat transfer;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x113.png" xlink:type="simple"/></inline-formula>: acceleration due to gravity;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x114.png" xlink:type="simple"/></inline-formula>: parameter of chemical reaction;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x115.png" xlink:type="simple"/></inline-formula>: non-dimensional parameter of chemical reaction;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x116.png" xlink:type="simple"/></inline-formula>: radiative heat flux;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x117.png" xlink:type="simple"/></inline-formula>: parameter of radiation absorption;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x118.png" xlink:type="simple"/></inline-formula>: mean absorption coefficient;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x119.png" xlink:type="simple"/></inline-formula>: Stefan-Boltzmann constant;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x120.png" xlink:type="simple"/></inline-formula>: parameter of radiation;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x121.png" xlink:type="simple"/></inline-formula>: Prandtl number;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x122.png" xlink:type="simple"/></inline-formula>: Schmidt number;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x123.png" xlink:type="simple"/></inline-formula>: Sherwood number;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x124.png" xlink:type="simple"/></inline-formula>: Nusselt number;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x125.png" xlink:type="simple"/></inline-formula>: temperature;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x126.png" xlink:type="simple"/></inline-formula>, ambient temperature;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x127.png" xlink:type="simple"/></inline-formula>: non-dimensional time;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x128.png" xlink:type="simple"/></inline-formula>: time;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x129.png" xlink:type="simple"/></inline-formula>: non-dimensional velocity of the in the<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x129.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x130.png" xlink:type="simple"/></inline-formula>, direction;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x131.png" xlink:type="simple"/></inline-formula>: velocity of the fluid;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x132.png" xlink:type="simple"/></inline-formula>: plate velocity;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x133.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x133.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x134.png" xlink:type="simple"/></inline-formula>: Cartesian coordinates along the plate and normal to the plate;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x135.png" xlink:type="simple"/></inline-formula>: non-dimensional coordinate;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x136.png" xlink:type="simple"/></inline-formula>: volumetric coefficient of thermal expansion;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x137.png" xlink:type="simple"/></inline-formula>: volumetric coefficient of expansion with concentration;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x138.png" xlink:type="simple"/></inline-formula>: viscosity;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x139.png" xlink:type="simple"/></inline-formula>: density;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x140.png" xlink:type="simple"/></inline-formula>: non-dimensional temperature;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x141.png" xlink:type="simple"/></inline-formula>: thermal conductivity;</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x142.png" xlink:type="simple"/></inline-formula>: kinematic viscosity.</p></sec><sec id="s10"><title>Appendix</title><disp-formula id="scirp.62313-formula2048"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x143.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x144.png" xlink:type="simple"/></inline-formula>,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x145.png" xlink:type="simple"/></inline-formula>,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x146.png" xlink:type="simple"/></inline-formula>,</p><disp-formula id="scirp.62313-formula2049"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x147.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x148.png" xlink:type="simple"/></inline-formula>,</p><disp-formula id="scirp.62313-formula2050"><graphic  xlink:href="http://html.scirp.org/file/8-2320251x149.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x150.png" xlink:type="simple"/></inline-formula>,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x151.png" xlink:type="simple"/></inline-formula>,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x152.png" xlink:type="simple"/></inline-formula>,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x153.png" xlink:type="simple"/></inline-formula>,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x154.png" xlink:type="simple"/></inline-formula>,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/8-2320251x155.png" xlink:type="simple"/></inline-formula>.</p></sec><sec id="s11"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.62313-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Ahmed, S., Batin, A. and Chamka, A.J. (2015) Numerical/Laplace Transform Analysis for MHD Rotating Heat/ Mass Transport in a Darcian Porous Regime Bounded by an Oscillating Vertical Surface. Alexandria Engineering Journal, 54, 45-54. http://dx.doi.org/10.1016/j.aej.2014.11.006</mixed-citation></ref><ref id="scirp.62313-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Kandasamy, R., Muhaimin, I. and Saim, H.B. (2010) Group Analysis for the Effects of the Temperature Dependent Fluid Viscosity and Chemical Reaction on Free Convective Heat and Mass Transfer. Journal of Applied Mechanics and Technical Physics, 51, 887-897.http://dx.doi.org/10.1007/s10808-010-0110-2</mixed-citation></ref><ref id="scirp.62313-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Makinde, O.D. (2005) Free Convection Flow with Thermal Radiation and Mass Transfer Past a Moving Vertical Porous Plate. 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