<?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">ENG</journal-id><journal-title-group><journal-title>Engineering</journal-title></journal-title-group><issn pub-type="epub">1947-3931</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/eng.2011.312149</article-id><article-id pub-id-type="publisher-id">ENG-9211</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject></subj-group></article-categories><title-group><article-title>
 
 
  Radiation Effects on Free Convection Flow Neara Vertical Plate with Ramped Wall Temperature
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>udra</surname><given-names>Kanta Deka</given-names></name><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Sankar</surname><given-names>Kumar Das</given-names></name><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><author-notes><corresp id="cor1">* E-mail:<email>rkdgu@yahoo.com(UKD)</email>;<email>skdas_jrt@yahoo.co.in(SKD)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>22</day><month>12</month><year>2011</year></pub-date><volume>03</volume><issue>12</issue><fpage>1197</fpage><lpage>1206</lpage><history><date date-type="received"><day>August</day>	<month>15,</month>	<year>2011</year></date><date date-type="rev-recd"><day>September</day>	<month>28,</month>	<year>2011</year>	</date><date date-type="accepted"><day>October</day>	<month>10,</month>	<year>2011</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 the unsteady natural convection flow past an infinite vertical plate is presented, wherein the plate temperature is a ramped one. The fluid considered here is a gray, absorbing/emitting but a non-scattering medium. The influence of the various parameters entering into the problem on the velocity field, temperature field, skin friction and Nusselt number is studied.
 
</p></abstract><kwd-group><kwd>Natural Convection</kwd><kwd> Ramped Wall Temperature</kwd><kwd> Radiation</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The analysis of free convection flow near a vertical plate has been carried out as an important application in many industries. Numerous investigations are performed by using both analytical and numerical methods. The first exact solution of the Navier-Stokes equation was given by Stokes [<xref ref-type="bibr" rid="scirp.9211-ref1">1</xref>] and explains the motion of a viscous incompressible fluid past an impulsively started infinite horizontal plate in its own plane. This is known as Stokes’s first problem in the literature. If the plate is in a vertical direction and gives an impulsive motion in its own plane in a stationary fluid, then the resulting effect of buoyancy force was first studied by Sundalgekar [<xref ref-type="bibr" rid="scirp.9211-ref2">2</xref>] by Laplace transformation technique and the effects of heating or cooling of the plate by free convection currents were discussed. Pohlhausen [<xref ref-type="bibr" rid="scirp.9211-ref3">3</xref>] was among the earlier research workers, who first analyzed the steady free convective flow of a viscous, incompressible fluid past a semi-infinite vertical plate by using integral method. Later on, Ostrach [<xref ref-type="bibr" rid="scirp.9211-ref4">4</xref>] studied the same problem using the similarity solution method. Siegel [<xref ref-type="bibr" rid="scirp.9211-ref5">5</xref>] and Gebhart [<xref ref-type="bibr" rid="scirp.9211-ref6">6</xref>] discussed the unsteady free convective flow of a viscous incompressible fluid, bounded by a semi-infinite vertical wall by using integral and approximation methods, respectively. Several authors (cf. [7-12]) have investigated a number of unsteady free convection flows near a vertical plate under different sets of thermal conditions at the bounding plate.</p><p>Practical problems usually occupy wall conditions that are non-uniform or arbitrary. Therefore, it is very useful to investigate problems subject to step change in wall temperature. Schetz [13,14] developed an approximate analytical model for natural convection flow from a vertical plate with discontinuous wall temperature conditions. However, different techniques were attempted on this problem. Hayday et al. [<xref ref-type="bibr" rid="scirp.9211-ref10">10</xref>] used a numerical approach, Kelleher et al. [<xref ref-type="bibr" rid="scirp.9211-ref11">11</xref>] and Kao [<xref ref-type="bibr" rid="scirp.9211-ref15">15</xref>] used series expansions. Lee and Yovanovich [<xref ref-type="bibr" rid="scirp.9211-ref12">12</xref>] have attempted to improve the earlier results for step change in wall temperature.</p><p>The interaction of natural convection with thermal radiation has increased greatly during the last decade due to its importance in many practical involvements. When free convection flows occur at high temperature, radiation effects on the flow become significant. Radiation effects on the free convection flow are important in context of space technology, processes in engineering areas occur at high temperature. Soundalgekar and Takhar [<xref ref-type="bibr" rid="scirp.9211-ref16">16</xref>] have considered the radiative free convective flow of an optically thin gray-gas past a semi-infinite vertical plate. Radiation effects on mixed convection along an isothermal vertical plate were studied by Hossain and Takhar [<xref ref-type="bibr" rid="scirp.9211-ref17">17</xref>]. Raptis and Perdikis [<xref ref-type="bibr" rid="scirp.9211-ref18">18</xref>] studied the effects of thermal radiation and free convection flow past a moving vertical plate. Das et al. [<xref ref-type="bibr" rid="scirp.9211-ref19">19</xref>] have analyzed radiation effects on flow past an impulsively started infinite isothermal vertical plate by the Laplace transform technique.</p><p>Recently, Muthucumaraswamy and Janakiraman [<xref ref-type="bibr" rid="scirp.9211-ref20">20</xref>] studied MHD and radiation effects on moving isothermal vertical plate with variable mass diffusion. Also, Chandran et al. [<xref ref-type="bibr" rid="scirp.9211-ref8">8</xref>] have analyzed the unsteady natural convection flow of a viscous incompressible fluid near a vertical plate with ramped wall temperature and they have compared the results with the case of constant wall temperature. The fluid convection resulting from such a wall temperature profile is likely to be of relevance in several industrial applications, especially, where the initial temperature profiles assume importance in design processes. Saha et al. [<xref ref-type="bibr" rid="scirp.9211-ref21">21</xref>] investigated the natural convection boundary layer adjacent to an inclined semi-infinite flat plate subjected to ramp heating. Recently, Deka et al. [<xref ref-type="bibr" rid="scirp.9211-ref22">22</xref>] have analyzed the unsteady free convection flow of a viscous incompressible fluid past an infinite vertical plate with ramped wall temperature in presence of heat source.</p><p>In the present problem, it is proposed to study the effect of thermal radiation on the unsteady free convection flow of a viscous incompressible fluid past an infinite vertical plate containing a ramped type temperature profile with respect to time. Two different solutions corresponding to ramped as well as constant wall temperature, are obtained by Laplace transform technique have been shown separately.</p></sec><sec id="s2"><title>2. Mathematical Formulation</title><p>We consider a two-dimensional flow of a viscous incompressible fluid past an infinite vertical flat plate. The fluid considered here is a gray, absorbing/emitting but a non-scattering medium. With respect to an arbitrarily chosen origin on this plate, the <img src="8-8101510\16ecb6b0-5f7e-4e6e-b25b-282f1d82e525.jpg" />-axis is taken along the wall in the vertically upward direction, and the <img src="8-8101510\07465f6e-b78a-4651-a907-a7593b1d41a3.jpg" />- axis is taken normal to the plate into the fluid. Initially, for time<img src="8-8101510\351d6d53-4b8c-4584-98c9-1435991d4de6.jpg" />, both the fluid and the plate are at rest and assumed to be at the same temperature<img src="8-8101510\922ed821-6590-47f8-ab1e-07390a68559a.jpg" />. At time<img src="8-8101510\c412e8a8-be7b-4e8e-8d52-bab8b8d4bd5f.jpg" />, the temperature of the plate is raised or lowered to <img src="8-8101510\49c26b8d-aabb-4d7e-ada8-0d141ab3da0e.jpg" /> and thereafter maintained at the constant temperature <img src="8-8101510\f4254c4f-0890-4704-8838-d5707d70f32b.jpg" /> for<img src="8-8101510\e89e5e99-99f7-4c77-9293-dc230737007e.jpg" />.</p><p>We assume that the flow is laminar and is such that the effects of the convective and pressure gradient terms in the momentum equations can be neglected (see Currie et al. [<xref ref-type="bibr" rid="scirp.9211-ref23">23</xref>]). It is also assumed that the effect of viscous dissipation is negligible. Moreover, as the plate is infinite in extent in the<img src="8-8101510\d3d7da54-faa7-4412-8fa2-46aaeedcf2ad.jpg" />-direction, the derivatives of all the flow variables with respect to <img src="8-8101510\a2cf5da6-db55-4cf0-93b3-5a0a11073547.jpg" /> vanish and as a result of the boundary layer approximations, the physical variables are functions of <img src="8-8101510\680aae61-a625-4dd0-a4af-a9cf98cecab6.jpg" /> only. Thus the motion is one dimensional with only non-zero vertical velocity <img src="8-8101510\06f19b25-9fc3-49c9-ab02-dc8f46f601bd.jpg" /> varying with <img src="8-8101510\e855197a-3d39-4ff6-81bc-08853e0c078d.jpg" /> and <img src="8-8101510\a2a2479c-9b7f-423f-a2b2-f9155185b3ba.jpg" /> only. Due to one-dimensional nature, the equation of continuity is trivially satisfied.</p><p>Then under usual Boussinesq’s approximation, the unsteady flow is governed by,</p><disp-formula id="scirp.9211-formula147104"><label>(1)</label><graphic position="anchor" xlink:href="8-8101510\9950ac64-7064-4b4a-a145-d5478bf5339e.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.9211-formula147105"><label>(2)</label><graphic position="anchor" xlink:href="8-8101510\a2ddd4e1-12c9-4b25-9b67-17d067340cfa.jpg"  xlink:type="simple"/></disp-formula><p>The initial and boundary conditions are,</p><disp-formula id="scirp.9211-formula147106"><label>(3)</label><graphic position="anchor" xlink:href="8-8101510\18db9d97-cc48-423b-bdf1-feaf2e88c4c9.jpg"  xlink:type="simple"/></disp-formula><p>The local radiant for the case of an optically thin gray gas is expressed by,</p><disp-formula id="scirp.9211-formula147107"><label>(4)</label><graphic position="anchor" xlink:href="8-8101510\8cf96644-298c-4932-92dc-c4f89ce7b24d.jpg"  xlink:type="simple"/></disp-formula><p>It is assumed that the temperature differences with the flow are sufficiently small so that <img src="8-8101510\83e1de00-b9de-4d86-bff1-7effe39fcb54.jpg" /> may be expressed as a linear function of the temperature, which is accomplished by expanding <img src="8-8101510\90b63e3e-865c-49c9-9604-abd7a2e3e2dc.jpg" /> in a Taylor series about <img src="8-8101510\f741b733-1b16-4e7b-a2d9-beb8874bbccd.jpg" /> and neglecting the higher order terms. Thus,</p><disp-formula id="scirp.9211-formula147108"><label>(5)</label><graphic position="anchor" xlink:href="8-8101510\f386d8ad-769d-4919-9a0a-6f4dc6e002f8.jpg"  xlink:type="simple"/></disp-formula><p>By using Equations (4) and (5), Equation (2) reduces to,</p><disp-formula id="scirp.9211-formula147109"><label>(6)</label><graphic position="anchor" xlink:href="8-8101510\ec9d4ff4-9319-4b76-b3a4-35c00b394df0.jpg"  xlink:type="simple"/></disp-formula><p>Introducing the non-dimensional quantities,</p><disp-formula id="scirp.9211-formula147110"><label>(7)</label><graphic position="anchor" xlink:href="8-8101510\e19a1743-c229-4957-a2c6-8916e74e69c6.jpg"  xlink:type="simple"/></disp-formula><p>the Equations (1) and (2) reduce to,</p><disp-formula id="scirp.9211-formula147111"><label>(8)</label><graphic position="anchor" xlink:href="8-8101510\e6e07e5b-81a6-482a-9fd1-062cb30ac913.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.9211-formula147112"><label>(9)</label><graphic position="anchor" xlink:href="8-8101510\3d2fc323-f580-4bd5-8bee-1958a9842367.jpg"  xlink:type="simple"/></disp-formula><p>According to the above non-dimensional process, the characteristic time t<sub>0</sub> can be defined as,</p><disp-formula id="scirp.9211-formula147113"><label>(10)</label><graphic position="anchor" xlink:href="8-8101510\51436a28-c39a-4386-84bd-81bec8c7467c.jpg"  xlink:type="simple"/></disp-formula><p>and then the initial and boundary conditions in non-dimensional form are,</p><disp-formula id="scirp.9211-formula147114"><label>(10)</label><graphic position="anchor" xlink:href="8-8101510\e69480a7-1c53-4765-b54a-5b3d8a7e16e6.jpg"  xlink:type="simple"/></disp-formula><p>All the physical quantities are mentioned in Nomenclature.</p></sec><sec id="s3"><title>3. Method of Solution</title><p>The Equations (8) and (9) subject to the conditions (10) are solved by the usual Laplace-transform technique and the solutions are as follows:</p><p>Case I: Pr ≠ 1</p><p>The exact solutions for temperature and velocity are given by,</p><disp-formula id="scirp.9211-formula147115"><label>(11)</label><graphic position="anchor" xlink:href="8-8101510\a5d1f6af-588b-4958-81ff-3836b5b5a7a5.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.9211-formula147116"><label>(12)</label><graphic position="anchor" xlink:href="8-8101510\7545525f-ed9f-446c-805f-c825289c4cae.jpg"  xlink:type="simple"/></disp-formula><p>where, (see the equation at the bottom of this page).</p><p>where<img src="8-8101510\ad1290d1-87f2-4124-aec6-2dd35cadde03.jpg" />.</p><p>Case II: Pr = 1.</p><p>The exact solutions for temperature and velocity are,</p><disp-formula id="scirp.9211-formula147117"><label>(13)</label><graphic position="anchor" xlink:href="8-8101510\cdc2d4a8-482a-4ce3-a272-47c2f462c678.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.9211-formula147118"><label>(14)</label><graphic position="anchor" xlink:href="8-8101510\c65dc738-abef-49b8-a0c8-50561714afd8.jpg"  xlink:type="simple"/></disp-formula><p>where,</p><p><img src="8-8101510\6d23044b-6d01-4843-b09b-d5741b5deb92.jpg" /></p><p><img src="8-8101510\5f09fab6-a40d-46b4-999c-fc7643455784.jpg" /></p><p>Here, <img src="8-8101510\cbb70681-e818-4417-9acf-0cf6f599a218.jpg" />is the unit step function defined, in general as,</p><p><img src="8-8101510\851b0aec-0619-4c61-815b-6836eff0fc29.jpg" /></p><p>To differentiate the effect of the ramped temperature distribution from the constant wall temperature on the flow, we compare both solutions obtained. The solutions for temperature and velocity for the flow near an isothermal stationary plate can be obtained as,</p><disp-formula id="scirp.9211-formula147119"><label>(15)</label><graphic position="anchor" xlink:href="8-8101510\af44224b-c75d-4875-8e4a-d0ec049ef23d.jpg"  xlink:type="simple"/></disp-formula><p><img src="8-8101510\39cd0fa2-ff9f-451c-8d96-7d4c550f6cc9.jpg" /></p><disp-formula id="scirp.9211-formula147120"><label>(16)</label><graphic position="anchor" xlink:href="8-8101510\2ef56ae7-4eb1-4674-a89c-e1e838fa48c1.jpg"  xlink:type="simple"/></disp-formula><p><img src="8-8101510.files/image001.gif" /> <img src="8-8101510.files/image002.gif" /></p><p><img src="8-8101510\fcf11cae-3e1c-46e9-a04c-cbfc2bd560e7.jpg" /></p><p><img src="8-8101510\b40299b7-6251-422c-959f-124ff797c3c1.jpg" /></p><p>where,</p><p><img src="8-8101510\94d27bc7-13e5-481b-a15b-a7a7e1aba711.jpg" /></p><p><img src="8-8101510\d9f6510b-4310-4d71-b3c2-7a7477217c76.jpg" /></p><p><img src="8-8101510\3c2330a2-e707-419c-b8bb-bd02399f9f8a.jpg" /></p></sec><sec id="s4"><title>4. Nusselt Number and Skin-Friction</title><p>We now study the heat transfer coefficient, i.e. Nusselt number, which is given in non-dimensional form by,</p><p><img src="8-8101510\b23a353c-35ce-4f53-90a0-9f1b17042491.jpg" /></p><p>where,</p><p><img src="8-8101510\55c7b6cb-31a3-4648-b385-d74d51168aaa.jpg" /></p><p>while, for the isothermal plate,</p><p><img src="8-8101510\550d0119-1a2c-49c3-abee-afdfeee55575.jpg" /></p><p>From the velocity field, we now study the skin friction. The non-dimensional form of skin-friction is given by,</p><p><img src="8-8101510\17aeb14c-6578-4563-b51c-7f0f80080321.jpg" /></p><p>where,</p><p><img src="8-8101510\3a9d9c07-03a7-405d-94b8-e3093a264443.jpg" /></p><p><img src="8-8101510\6d4065bb-b00f-4242-9776-054868e8b807.jpg" /></p><p>Again, the skin friction for isothermal plate is given by,</p><p><img src="8-8101510\b40ac0c3-a9be-4a27-8669-b4f1020c0ba5.jpg" /></p><p>where,</p><p><img src="8-8101510\a6f47e62-3a8d-40ac-bcd2-032f767a56c7.jpg" /></p><p><img src="8-8101510\0fd74594-dab2-4183-b5d1-a5c5786d4c6a.jpg" /></p></sec><sec id="s5"><title>5. Results and Discussions</title><p>In order to understand the effects of different physical parameters, namely; <img src="8-8101510\f7c4f8ad-7a08-42ac-a4f9-cf67d4792e73.jpg" />(Prandtl number), <img src="8-8101510\68542b2a-0881-44ff-a12d-77a9ce5b9441.jpg" />(radiation parameter) and <img src="8-8101510\49f92260-600f-4f80-9de7-1ac0ba3e2784.jpg" /> (time), on the nature of the flow, computations are carried out for velocity, temperature, Nusselt number and skin friction. The computed results are presented graphically. In all the figures, dotted lines correspond to solutions without ramped wall temperature.</p><p>Figures 1-3 display the effect of <img src="8-8101510\c7ce2a0a-91cd-4bbb-8238-f161e1016734.jpg" /> (time) on the temperature field for the case of air (Pr = 0.71). It is observed that temperature increases with an increase in <img src="8-8101510\22039e8c-4dc7-47c7-b337-df467b97f1fb.jpg" /> (time). It is also found that the temperature decreases with <img src="8-8101510\14306dba-c59e-4aa4-9466-cae0bfe83b61.jpg" /> from its ramped value on the plate to its free stream value for all values of time<img src="8-8101510\4ce55d4c-9ba1-4629-a307-7266c75285c0.jpg" />.</p><p><xref ref-type="fig" rid="fig2">Figure 2</xref> represents the temperature profiles for different values of <img src="8-8101510\315abe7f-f63e-4c6e-8277-e1509b042ec2.jpg" /> at <img src="8-8101510\d41ee3ea-b04a-4f52-aaed-651e5ee50100.jpg" /> and<img src="8-8101510\d4f8ce4a-807d-4c6b-b9e4-39945e269c34.jpg" />. It is found that the temperature decreases with an increase in<img src="8-8101510\68199daf-13fc-4232-bbe1-71b841d6e207.jpg" />. <xref ref-type="fig" rid="fig3">Figure 3</xref> shows the effect of radiation parameter R on the temperature field for fixed values of <img src="8-8101510\bcf11e5d-4618-4f70-944f-fbdd38812ae2.jpg" /> and <img src="8-8101510\c0c6d69d-3795-4d2e-bba1-294ca5c2c49d.jpg" /> and demonstrates that the temperature decreases gradually with increasing values of<img src="8-8101510\5ed9df9a-2b14-405a-a21b-35aa86f51183.jpg" />.</p><p>From Figures 1-3 we have presented the temperature variation with the two types of boundary conditions,</p><p>ramped and constant plate temperature. We observe that the fluid temperature is greater in the case of isothermal plate than in the case of ramped temperature at the plate. This should be expected since in the latter case, the heating of the fluid takes place more gradually than in the isothermal case. Also, we observe that the temperature is maximum near the plate and decreases away from the plate and finally takes free stream value for all values of<img src="8-8101510\56a1f7c3-2288-4c73-a20b-c254f068aded.jpg" />, <img src="8-8101510\ec2954d2-c017-4e27-ab1c-03207cfc1eba.jpg" />and<img src="8-8101510\cd2df24c-6bd7-4e03-999a-f79a3fb4953b.jpg" />.</p><p>In Figures 4 and 5, the velocity profiles are shown for different values of physical parameters involved. <xref ref-type="fig" rid="fig4">Figure 4</xref> reveals velocity variations with <img src="8-8101510\4e7f7d46-afa8-430c-8e0c-fa9e986c5df2.jpg" />and <img src="8-8101510\918d6b59-7075-4a85-881d-e0427ef1eaaf.jpg" /> at<img src="8-8101510\cab754b7-9cab-415a-9669-ee62d424f726.jpg" />. It demonstrates that the velocity decreases with increaseing the Prandtl number. <xref ref-type="fig" rid="fig5">Figure 5</xref> illustrates the influence of <img src="8-8101510\18611975-0d92-45d2-b5fe-6b5d9155566e.jpg" /> on the velocity field for both ramped temperature and isothermal plate. It is observed that the fluid velocity decreases on increasing radiation parameter <img src="8-8101510\6792eac3-1480-437e-8c17-9d2318340bdd.jpg" /> in the boundary layer region. This implies that the radiation decelerates fluid velocity for both ramped temperature and isothermal plate. Figures 4 and 5 also demonstrate that the velocity increases with an increase in time<img src="8-8101510\1509c1d0-baa7-41ad-81e9-fb77bdbc7df9.jpg" />. Again, from Figures 4 and 5, we observe that the velocity increases with <img src="8-8101510\c3754668-5ea1-4704-92d6-01bd6c090978.jpg" /> near the plate, becomes maximum and then decreases away from the plate and finally takes asymptotic value for all values of<img src="8-8101510\00118199-c2a4-49f5-99fa-515e4babbd82.jpg" />. Lastly, it is seen that the velocity in case of ramped temperature plate is always less than the flow induced by a plate of constant temperature.</p><p><img src="8-8101510\c58bff44-04d0-41ff-ba9c-d6044fb97e76.jpg" />is calculated for different<img src="8-8101510\bdc3857e-21aa-4679-aeae-5e778258b265.jpg" />, <img src="8-8101510\40fefc6e-8bc9-4a02-8cc8-13ec3593dc4e.jpg" />and <img src="8-8101510\110bc870-00be-4b76-acec-71657cadbeba.jpg" /> and presented in Figures 6 and 7. It is clear from the figures that for the ramped plate temperature, the Nusselt number increases for a range <img src="8-8101510\0e35d27c-87aa-4a40-9c74-e28fb481e1f3.jpg" /> and decreases for <img src="8-8101510\6cd1ca95-23b1-40b9-b095-10a0573990c1.jpg" /> for all <img src="8-8101510\dbc1d396-7320-4a0e-bc71-5586908a8712.jpg" /> and<img src="8-8101510\a77a62fc-3172-4baf-9d87-685a594d547c.jpg" />. But in case of constant wall temperature, the Nusselt number decreases with respect to<img src="8-8101510\6dd7a88a-9668-4e2c-ad1e-851b4ee42375.jpg" />.</p><p>The numerical values of t are evaluated for different values of<img src="8-8101510\82d0309b-c613-4087-a1c7-d8b6597d207c.jpg" />; <img src="8-8101510\9f16c105-2328-4154-b41e-970aa130af45.jpg" />and depicted in <xref ref-type="fig" rid="fig8">Figure 8</xref> The effects of ramped and constant wall temperature on skin friction are also presented in this figure. We have seen that due to the presence of radiation, the skin-friction is greater in case of ramped temperature of the plate than the case of an isothermal plate. It is also noticed that for small values of t &lt; 1, there is a quick fall in the skin friction in the case of ramped temperature of the plate, whereas the skin friction decreases more gradually with time for the case of isothermal plate. Further, we observe that the skin friction co-efficient increases with <img src="8-8101510\b157e265-0e35-4c78-a186-cc9c85424e0d.jpg" /> for both ramped temperature and isothermal plate, which illustrates that radiation has tendency to enhance the skin friction. It is also observed that the skin friction is enhanced with<img src="8-8101510\96bca29c-a380-465e-92b6-8468c101eebb.jpg" />. Lastly, we find that the ber.perayure skin-friction is more in water as compared to that in air.</p></sec><sec id="s6"><title>6. Conclusions</title><p>An analysis is performed to study the effect of radiation on unsteady free convection flow past an infinite vertical plate with ramped wall temperature. The non-dimensional forms of the governing equations of the fluid flow are solved by Laplace-transform technique. The solutions for velocity, temperature are studied graphically. Also, the Nusselt number and skin friction have been discu-ssed.</p><p>Following observations are made from the study:</p><p>1) Temperature of the fluid increases with an increase in time <img src="8-8101510\abef78f7-b2ff-406c-b877-697e0a1aaad5.jpg" /> but as <img src="8-8101510\7dd39fc4-b53f-4a44-8d3d-0df1796a3e6e.jpg" /> increases, temperature decreases. Also, the temperature decreases gradually with<img src="8-8101510\53cdf112-bd7a-49e4-a079-ad37b808fb90.jpg" />.</p><p>2) The temperature decreases with <img src="8-8101510\ce1f3b45-ac80-46cd-ab26-d2f8634348d4.jpg" /> from its ramped value on the plate to its free stream value.</p><p>3) The presence of radiation tends to decelerate the fluid flow for both ramped temperature and isothermal plate. Also, fluid velocity accelerates as time progresses.</p><p>4) The velocity decreases with increasing the Prandtl number.</p><p>5) Nusselt number increases for <img src="8-8101510\21e575e2-4d11-493c-ba2f-2fe746a06475.jpg" />and decreases for <img src="8-8101510\d93a84c5-873e-4827-8299-34f1f30c17e0.jpg" /> for all <img src="8-8101510\b838e360-5573-46eb-8cfe-5655448f075b.jpg" /> and<img src="8-8101510\8082765d-25a2-4f3b-bc05-110e29e3029c.jpg" />.</p><p>6) Skin friction increases with increasing <img src="8-8101510\b6edae0a-bf9b-4f3c-a315-75afab4a8319.jpg" /> and<img src="8-8101510\9d2bb2e3-5e01-40e4-b52d-2b1b9e1e0585.jpg" />.</p></sec><sec id="s7"><title>7. REFERENCES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.9211-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">G. G. 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