<?xml version="1.0" encoding="ISO-8859-1"?><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance">
<front>
<journal-meta>
<journal-id>1794-1237</journal-id>
<journal-title><![CDATA[Revista EIA]]></journal-title>
<abbrev-journal-title><![CDATA[Rev.EIA.Esc.Ing.Antioq]]></abbrev-journal-title>
<issn>1794-1237</issn>
<publisher>
<publisher-name><![CDATA[Escuela de ingenieria de Antioquia]]></publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id>S1794-12372015000200010</article-id>
<title-group>
<article-title xml:lang="en"><![CDATA[COOLING MICROELECTRONIC DEVICES USING OPTIMAL MICROCHANNEL HEAT SINKS: UNA COMPARACIÓN DE DOS ALGORITMOS DE OPTIMIZACIÓN GLOBAL]]></article-title>
<article-title xml:lang="es"><![CDATA[DISEÑO ÓPTIMO DE MICROCANALES: UMA COMPARAÇÃO DOS DOIS ALGORITMOS DE OPTIMIZAÇÃO GLOBAL]]></article-title>
<article-title xml:lang="pt"><![CDATA[DESIGN ÓTIMO DE MICROCANAIS]]></article-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Cruz Duarte]]></surname>
<given-names><![CDATA[Jorge Mario]]></given-names>
</name>
<xref ref-type="aff" rid="A01"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Amaya Contreras]]></surname>
<given-names><![CDATA[Iván Mauricio]]></given-names>
</name>
<xref ref-type="aff" rid="A02"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Correa Cely]]></surname>
<given-names><![CDATA[Carlos Rodrigo]]></given-names>
</name>
<xref ref-type="aff" rid="A03"/>
</contrib>
</contrib-group>
<aff id="A01">
<institution><![CDATA[,Universidad de Guanajuato División de Ingenierías ]]></institution>
<addr-line><![CDATA[Salamanca Guanajuato]]></addr-line>
<country>México</country>
</aff>
<aff id="A02">
<institution><![CDATA[,Universidad Industrial de Santander  ]]></institution>
<addr-line><![CDATA[Bucaramanga ]]></addr-line>
<country>Colombia</country>
</aff>
<aff id="A03">
<institution><![CDATA[,Universidad Industrial de Santander  ]]></institution>
<addr-line><![CDATA[Bucaramanga ]]></addr-line>
<country>Colombia</country>
</aff>
<pub-date pub-type="pub">
<day>00</day>
<month>12</month>
<year>2015</year>
</pub-date>
<pub-date pub-type="epub">
<day>00</day>
<month>12</month>
<year>2015</year>
</pub-date>
<numero>24</numero>
<fpage>151</fpage>
<lpage>166</lpage>
<copyright-statement/>
<copyright-year/>
<self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_arttext&amp;pid=S1794-12372015000200010&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_abstract&amp;pid=S1794-12372015000200010&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_pdf&amp;pid=S1794-12372015000200010&amp;lng=en&amp;nrm=iso"></self-uri><abstract abstract-type="short" xml:lang="en"><p><![CDATA[This article deals with the design of optimum microchannel heat sinks through Unified Particle Swarm Optimisation (UPSO) and Harmony Search (HS). These heat sinks are used for the thermal management of electronic devices, and we analyse the performance of UPSO and HS in their design, both, systematically and thoroughly. The objective function was created using the entropy generation minimisation criterion. In this study, we fixed the geometry of the microchannel, the amount of heat to be removed, and the properties of the cooling fluid. Moreover, we calculated the entropy generation rate, the volume flow rate of air, the channel width, the channel height, and the Knudsen number. The results of several simulation optimizations indicate that both global optimisation strategies yielded similar results, about 0.032 W/K, and that HS required five times more iterations than UPSO, but only about a nineteenth of its computation time. In addition, HS revealed a greater chance (about three times) of finding a better solution than UPSO, but with a higher dispersion rate (about five times). Nonetheless, both algorithms successfully optimised the design for different scenarios, even when varying the material of the heat sink, and for different heat transfer rates.]]></p></abstract>
<abstract abstract-type="short" xml:lang="es"><p><![CDATA[Este artículo trata sobre el diseño óptimo de disipadores de calor de tipo microcanal utilizando los métodos Unified Particle Swarm Optimisation (UPSO) y Harmony Search (HS). Estos disipadores se utilizan en el enfriamiento de componentes microelectrónicos. Por ello analizamos el desempeño de UPSO y HS en su diseño, de forma sistemática y completa. La función objetivo se obtuvo con el criterio de la mínima generación de entropía. En este estudio, se definió la geometría del microcanal, la cantidad de calor a ser retirado y las propiedades del fluido de trabajo. Además, se calculó la tasa de generación de entropía, el flujo volumétrico de aire, el ancho y la altura del canal y el número de Knudsen. Los resultados de las simulaciones indicaron que ambas estrategias de optimización dieron resultados similares, alrededor de 0,032 W / K, y que HS requiere cinco veces más iteraciones que UPSO, pero sólo alrededor de 1/19 de su tiempo de cálculo. Además, HS reveló una mayor probabilidad de encontrar una mejor solución que UPSO, pero con una mayor dispersión. Sin embargo, ambos algoritmos resolvieron exitosamente el diseño para diferentes escenarios, incluso cuando se varía el material del disipador y la tasa de transferencia de calor.]]></p></abstract>
<abstract abstract-type="short" xml:lang="pt"><p><![CDATA[Este artigo discute o projeto ideal de dissipadores de calor de microcanais utilizando os métodos Unified Particle Swarm Optimization (UPSO) e Harmonia Search (HS). Estes resfriadores são utilizados em refrigeração com componentes microeletrônicos. Por isso, vamos analisar o desempenho de UPSO e HS na sua concepção, de uma forma sistemática e completa. A função objetivo foi obtida com o critério de geração mínima de entropia. Neste estudo, definiu-se a geometria de microcanais, a quantidade de calor a ser removida e as propriedades do fluido de trabalho. Além disso, se calculo a taxa de geração de entropia, o caudal volumétrico de ar, a largura e a altura do canal e o número de Knudsen. Os resultados da simulação indicaram que ambas das estratégias de otimização deram resultados semelhantes, cerca de 0.032 W / K, e que HS exige cinco vezes mais iterações UPSO, mas apenas cerca de 1/19 do seu tempo de computação. Também, HS revelou uma maior probabilidade de encontrar uma solução melhor do que UPSO, mas com maior dispersão. No entanto, ambos dos algoritmos resolveram com sucesso o design para diferentes cenários, mesmo quando o material do pia e a taxa de transferência de calor é variada.]]></p></abstract>
<kwd-group>
<kwd lng="en"><![CDATA[Entropy Generation Minimisation]]></kwd>
<kwd lng="en"><![CDATA[Global Optimization Algorithm]]></kwd>
<kwd lng="en"><![CDATA[Microchannel Heat Sink]]></kwd>
<kwd lng="en"><![CDATA[Optimal Design]]></kwd>
<kwd lng="es"><![CDATA[algoritmos de optimización global]]></kwd>
<kwd lng="es"><![CDATA[diseño óptimo]]></kwd>
<kwd lng="es"><![CDATA[disipadores de calor de tipo microcanal]]></kwd>
<kwd lng="es"><![CDATA[mínima generación de entropía]]></kwd>
<kwd lng="pt"><![CDATA[algoritmos de otimização globais]]></kwd>
<kwd lng="pt"><![CDATA[design ideal]]></kwd>
<kwd lng="pt"><![CDATA[dissipadores de calor de tipo microcanal]]></kwd>
<kwd lng="pt"><![CDATA[geração mínima de entropia]]></kwd>
</kwd-group>
</article-meta>
</front><body><![CDATA[  <font face="verdana" size="2">     <p align="center"><font size="4"><b>COOLING MICROELECTRONIC DEVICES USING OPTIMAL MICROCHANNEL HEAT SINKS</b></font></p>     <p align="center"><font size="3"><b>DISE&Ntilde;O &Oacute;PTIMO DE MICROCANALES. UNA COMPARACI&Oacute;N DE DOS ALGORITMOS DE OPTIMIZACI&Oacute;N GLOBAL</b></font></p>     <p align="center"><font size="3"><b>DESIGN &Oacute;TIMO DE MICROCANAIS. UMA COMPARA&Ccedil;&Atilde;O DOS DOIS ALGORITMOS DE OPTIMIZA&Ccedil;&Atilde;O GLOBAL</b></font></p>     <p>&nbsp;</p>     <p><b>Jorge Mario Cruz Duarte<sup>1</sup>, Iv&aacute;n Mauricio Amaya Contreras<sup>2</sup>, Carlos Rodrigo Correa Cely<sup>3</sup></b></p>     <p>1 Ingeniero  electr&oacute;nico, M.Sc., Estudiante de doctorado, Universidad de Guanajuato, Divisi&oacute;n  de Ingenier&iacute;as, Campus Irapuato-Salamanca, Carretera Salamanca-Valle de  Santiago km 3.5 + 1.8 km, Comunidad de Palo Blanco, C.P. 36885, Salamanca,  Guanajuato, M&eacute;xico / Tel.: (521) 464 647 9940, Ext. 2400 / Correo electr&oacute;nico: <a href="mailto:jorge.cruz@ugto.mx">jorge.cruz@ugto.mx</a>.     <br> 2 Ingeniero  mecatr&oacute;nico, Universidad Aut&oacute;noma de Bucaramanga (UAB), Colombia. PhD. en  Ingenier&iacute;a (Ingenier&iacute;a El&eacute;ctrica, Electr&oacute;nica y Gesti&oacute;n &#38; Desarrollo)  Universidad Industrial de Santander (UIS). Profesor c&aacute;tedra, E3T, Universidad  Industrial de Santander, Bucaramanga, Colombia.    <br> 3 Ingeniero qu&iacute;mico Universidad Nacional de Colombia. Mag&iacute;ster en Ingenier&iacute;a  Qu&iacute;mica, Lehigh University, Estados Unidos. PhD. En Ingenier&iacute;a Qu&iacute;mica Lehigh  University USA. Trabajo Postdoctoral, University of Stuttgart, Alemania.  Profesor titular, E3T, Universidad Industrial de Santander, Bucaramanga,  Colombia.</p>     <p>Art&iacute;culo recibido: 22-IV-2015 / Aprobado: 26-VIII-2015    ]]></body>
<body><![CDATA[<br>   Disponible online: 30 de octubre de 2015    <br> Discusi&oacute;n abierta hasta noviembre de 2016</p> <hr size="1" />     <p><b><font size="3">ABSTRACT</font></b></p>     <p>This article  deals with the design of optimum microchannel heat sinks through Unified  Particle Swarm Optimisation (UPSO) and  Harmony Search (HS). These heat sinks are used for the thermal management of  electronic devices, and we analyse the  performance of UPSO and HS in their design, both, systematically and  thoroughly. The objective function was created  using the entropy generation minimisation criterion. In this study, we fixed  the geometry of the microchannel, the amount of  heat to be removed, and the properties of the cooling fluid. Moreover, we  calculated the entropy generation  rate, the volume flow rate of air, the channel width, the channel height, and  the Knudsen number. The results of several  simulation optimizations indicate that both global optimisation strategies  yielded similar results, about 0.032 W/K, and that  HS required five times more iterations than UPSO, but only about a nineteenth  of its computation time. In addition, HS  revealed a greater chance (about three times) of finding a better solution than  UPSO, but with a higher dispersion rate (about  five times). Nonetheless, both algorithms successfully optimised the design for  different scenarios, even when varying the material of the heat sink, and for different heat  transfer rates.</p>     <p><font size="3"><b>KEY WORDS</b></font>: Entropy Generation Minimisation; Global Optimization Algorithm; Microchannel Heat Sink; Optimal Design.</p> <hr size="1" />     <p><font size="3"><b>RESUMEN</b></font></p>     <p>Este art&iacute;culo  trata sobre el dise&ntilde;o &oacute;ptimo de disipadores de calor de tipo microcanal  utilizando los m&eacute;todos <i>Unified</i>   <i>Particle Swarm Optimisation </i>(UPSO) y <i>Harmony Search </i>(HS). Estos disipadores se utilizan en  el enfriamiento de componentes microelectr&oacute;nicos.  Por ello analizamos el desempe&ntilde;o de UPSO y HS en su dise&ntilde;o, de forma sistem&aacute;tica  y completa. La funci&oacute;n objetivo se obtuvo con el criterio de la m&iacute;nima generaci&oacute;n  de entrop&iacute;a. En este estudio, se defini&oacute; la geometr&iacute;a del microcanal, la cantidad de  calor a ser retirado y las propiedades del fluido de trabajo. Adem&aacute;s, se calcul&oacute;  la tasa de generaci&oacute;n de entrop&iacute;a, el flujo volum&eacute;trico  de aire, el ancho y la altura del canal y el n&uacute;mero de Knudsen. Los resultados  de las simulaciones indicaron que ambas  estrategias de optimizaci&oacute;n dieron resultados similares, alrededor de 0,032 W /  K, y que HS requiere cinco veces m&aacute;s iteraciones  que UPSO, pero s&oacute;lo alrededor de 1/19 de su tiempo de c&aacute;lculo. Adem&aacute;s, HS revel&oacute;  una mayor probabilidad de encontrar una  mejor soluci&oacute;n que UPSO, pero con una mayor dispersi&oacute;n. Sin embargo, ambos  algoritmos resolvieron exitosamente el dise&ntilde;o para diferentes escenarios, incluso cuando se var&iacute;a el  material del disipador y la tasa de transferencia de calor.</p>     <p><b><font size="3">PALABRAS CLAVE</font></b>: algoritmos de optimizaci&oacute;n global; dise&ntilde;o &oacute;ptimo; disipadores de calor de tipo microcanal; m&iacute;nima generaci&oacute;n de entrop&iacute;a.</p> <hr size="1" />     <p><font size="3"><b>RESUMO</b></font></p>     <p>Este artigo  discute o projeto ideal de dissipadores de calor de microcanais utilizando os m&eacute;todos  Unified Particle Swarm Optimization (UPSO) e Harmonia Search (HS). Estes  resfriadores s&atilde;o utilizados em refrigera&ccedil;&atilde;o com componentes microeletr&ocirc;nicos. Por isso, vamos  analisar o desempenho de UPSO e HS na sua concep&ccedil;&atilde;o, de uma forma sistem&aacute;tica e  completa. A fun&ccedil;&atilde;o objetivo foi  obtida com o crit&eacute;rio de gera&ccedil;&atilde;o m&iacute;nima de entropia. Neste estudo, definiu-se a  geometria de microcanais, a quantidade de calor a ser  removida e as propriedades do fluido de trabalho. Al&eacute;m disso, se calculo a taxa  de gera&ccedil;&atilde;o de entropia, o caudal volum&eacute;trico  de ar, a largura e a altura do canal e o n&uacute;mero de Knudsen. Os resultados da  simula&ccedil;&atilde;o indicaram que ambas das estrat&eacute;gias  de otimiza&ccedil;&atilde;o deram resultados semelhantes, cerca de 0.032 W / K, e que HS  exige cinco vezes mais itera&ccedil;&otilde;es UPSO, mas  apenas cerca de 1/19 do seu tempo de computa&ccedil;&atilde;o. Tamb&eacute;m, HS revelou uma maior  probabilidade de encontrar uma solu&ccedil;&atilde;o  melhor do que UPSO, mas com maior dispers&atilde;o. No entanto, ambos dos algoritmos  resolveram com sucesso o design para diferentes cen&aacute;rios, mesmo quando o material do pia e a taxa  de transfer&ecirc;ncia de calor &eacute; variada.</p>     ]]></body>
<body><![CDATA[<p><font size="3"><b>PALAVRAS-CHAVE</b></font>: algoritmos de otimiza&ccedil;&atilde;o globais; design ideal; dissipadores de calor de tipo microcanal; gera&ccedil;&atilde;o m&iacute;nima de entropia.</p> <hr size="1" />     <p><b><font size="3">NOMENCLATURE</font></b></p> <table width="580" border="0" cellspacing="0" cellpadding="0">   <tr>     <td width="80"><font size="-1"><i>C</i></font></td>     <td width="500"><font size="-1">Adimensional parameter</font></td>   </tr>   <tr>     <td><font size="-1"><i>C<sub>p</sub></i></font></td>     <td><font size="-1">Specific heat at constant pressure (<i>J/kg&middot;K</i>)</font></td>   </tr>     <tr>     <td><font size="-1"><i>C<sub>v</sub></i></font></td>     <td><font size="-1">Specific heat at constant volume (<i>J/kg&middot;K</i>)</font></td>   </tr>     <tr>     <td><font size="-1"><i>D<sub>h</sub></i></font></td>     <td><font size="-1">Hydraulic diameter <img src="img/revistas/eia/n24/n24a10for11.gif"> 4<i>H<sub>c</sub>w<sub>c</sub></i>/(<i>H<sub>c</sub> </i>+ 2<i>w<sub>c</sub></i>)(<i>m</i>)</font></td>   </tr>     <tr>     <td><font size="-1"><i>FW</i></font></td>     <td><font size="-1">Fretwidth</font></td>   </tr>   <tr>     <td><font size="-1"><i>F</i></font></td>     <td><font size="-1">Friction factor</font></td>   </tr>   <tr>     <td><font size="-1"><i>G</i></font></td>     <td><font size="-1">Volume flow rate (<i>m</i><sup>3</sup>/<i>s</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><img src="img/revistas/eia/n24/n24a10for12.gif"></font></td>     <td><font size="-1"> Global velocity component</font></td>   </tr>   <tr>     <td><font size="-1"><i>H<sub>c</sub></i></font></td>     <td><font size="-1">Channel height (<i>m</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>HMCR</i></font></td>     <td><font size="-1">Harmony Memory Consideration Rate</font></td>   </tr>   <tr>     <td><font size="-1"><i>HMS</i></font></td>     <td><font size="-1">Harmony Memory Size</font></td>   </tr>   <tr>     <td><font size="-1"><i>h<sub>avg</sub></i></font></td>     <td><font size="-1">Average heat transfer coefficient (<i>W/m</i><sup>2</sup><i>&middot;K</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>Kn</i></font></td>     <td><font size="-1">Knudsen number</font></td>   </tr>   <tr>     <td><font size="-1"><i>k</i></font></td>     <td><font size="-1">Thermal conductivity of solid (<i>W/m&middot;K</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>k<sub>ce</sub></i></font></td>     <td><font size="-1">Sum of entrance and exit losses</font></td>   </tr>   <tr>     <td><font size="-1"><i>k<sub>f</sub></i></font></td>     <td><font size="-1">Thermal conductivity of fluid (<i>W/m&middot;K</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>L</i></font></td>     <td><font size="-1">Length of cannel in flow direction (<i>m</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><img src="img/revistas/eia/n24/n24a10for13.gif"></font></td>     <td><font size="-1">Local velocity component</font></td>   </tr>   <tr>     <td><font size="-1"><i>N</i></font></td>     <td><font size="-1">Total number of microchannels</font></td>   </tr>   <tr>     <td><font size="-1"><i>Nu<sub>Dh</sub></i></font></td>     <td><font size="-1">Nusselt number base on hydraulic diameter <img src="img/revistas/eia/n24/n24a10for11.gif"> <i>D<sub>h</sub>h<sub>avg</sub>/k<sub>f</sub></i></font></td>   </tr>   <tr>     <td><font size="-1"><i>n</i></font></td>     <td><font size="-1">Total number of design variables</font></td>   </tr>   <tr>     <td><font size="-1"><i>P</i></font></td>     <td><font size="-1">Pressure (Pa)</font></td>   </tr>   <tr>     <td><font size="-1"><i>PAR</i></font></td>     <td><font size="-1">Pitch Adjusting Rate</font></td>   </tr>   <tr>     <td><font size="-1"><i>Pe<sub>Dh</sub></i></font></td>     <td><font size="-1">Peclet number base on hydraulic diameter <img src="img/revistas/eia/n24/n24a10for11.gif"> <i>D_h U_{avg} /  \alpha_{th}</i></font></td>   </tr>   <tr>     <td><font size="-1"><i>Pr</i></font></td>     <td><font size="-1">Prandtl number</font></td>   </tr>   <tr>     <td><font size="-1"><i><img src="img/revistas/eia/n24/n24a10for14.gif"><sub>g</sub></i></font></td>     <td><font size="-1">Best position for whole swarm</font></td>   </tr>   <tr>     <td><font size="-1"><i><img src="img/revistas/eia/n24/n24a10for14.gif"><sub>gp</sub></i></font></td>     <td><font size="-1">Best position for each neighbourhood</font></td>   </tr>   <tr>     <td><font size="-1"><i><img src="img/revistas/eia/n24/n24a10for14.gif"><sub>p</sub></i></font></td>     <td><font size="-1">Best position for each particle</font></td>   </tr>   <tr>     <td><font size="-1"><i><img src="img/revistas/eia/n24/n24a10for15.gif"></i></font></td>     <td><font size="-1">Total heat transfer rate (<i>W</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>R<sub>th</sub></i></font></td>     <td><font size="-1">Total thermal resistance (<i>K</i>/<i>W</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>Re<sub>Dh</sub></i></font></td>     <td><font size="-1">Reynolds number base on hydraulic diameter</font></td>   </tr>   <tr>     <td><font size="-1"><i>rand</i></font></td>     <td><font size="-1">Random number, uniformly distributed  between zero and one</font></td>   </tr>   <tr>     <td><font size="-1"><i><img src="img/revistas/eia/n24/n24a10for16.gif"><sub>gen</sub></i></font></td>     <td><font size="-1">Total entropy generation rate</font></td>   </tr>   <tr>     <td><font size="-1"><i><img src="img/revistas/eia/n24/n24a10for16.gif"><sub>gen,ht</sub></i></font></td>     <td><font size="-1">Entropy generation rate due to  heat transfer (W/K)</font></td>   </tr>   <tr>     <td><font size="-1"><i><img src="img/revistas/eia/n24/n24a10for16.gif"><sub>gen,ff</sub></i></font></td>     <td><font size="-1"> Entropy generation rate due to  fluid friction (W/K)</font></td>   </tr>   <tr>     <td><font size="-1"><i>T<sub>a</sub></i></font></td>     <td><font size="-1">Ambient temperature (K)</font></td>   </tr>   <tr>     <td><font size="-1"><i>T<sub>b</sub></i></font></td>     <td><font size="-1">Heat sink base temperature (<i>K</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>U<sub>avg</sub></i></font></td>     <td><font size="-1">Average velocity in channels (<i>m/s</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>V</i></font></td>     <td><font size="-1">Total velocity</font></td>   </tr>   <tr>     <td><font size="-1"><i>W</i></font></td>     <td><font size="-1">Width of heat sink (<i>m</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>w<sub>c</sub></i></font></td>     <td><font size="-1">Half of the channel width (<i>m</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>w<sub>w</sub></i></font></td>     <td><font size="-1">Half of the fin thickness (<i>m</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>X<sub>i</sub></i></font></td>     <td><font size="-1">Design variables</font></td>   </tr> </table>      <p><b><i>Greek symbols</i></b></p> <table width="580" border="0" cellspacing="0" cellpadding="0">   <tr>     <td width="80"><font size="-1"><i>&alpha;</i></font></td>     <td width="500"><font size="-1">Slip parameter</font></td>   </tr>   <tr>     <td><font size="-1"><i>&alpha;<sub>c</sub></i></font></td>     <td><font size="-1">Channel  aspect ratio <img src="img/revistas/eia/n24/n24a10for11.gif"> 2<i>w<sub>c</sub></i>/<i>H<sub>c</sub></i></font></td>   </tr>   <tr>     <td><font size="-1"><i>&alpha;<sub>hs</sub></i></font></td>     <td><font size="-1">Heat sink  aspect ratio <img src="img/revistas/eia/n24/n24a10for11.gif"><i> L</i>/2<i>w<sub>c</sub></i></font></td>   </tr>   <tr>     <td><font size="-1"><i>&alpha;<sub>th</sub></i></font></td>     <td><font size="-1">Thermal  diffusivity <img src="img/revistas/eia/n24/n24a10for11.gif"><i> k_f / \rho \cdot c_p</i> (<i>m</i><sup>2</sup><i>/s</i>)</font></td>   </tr>   <tr>     <td><font size="-1">&gamma;</font></td>     <td><font size="-1">Ratio of specific heats <img src="img/revistas/eia/n24/n24a10for11.gif"><i> c<sub>p</sub></i>/c<i><sub>v</sub></i></font></td>   </tr>   <tr>     <td><font size="-1">&Delta;<i>P</i></font></td>     <td><font size="-1">Pressure drop across microchannel  (<i>Pa</i>)</font></td>   </tr>   <tr>     <td><font size="-1">&eta;<i><sub>fin</sub></i></font></td>     <td><font size="-1">Fin efficiency</font></td>   </tr>   <tr>     <td><font size="-1">&nu;</font></td>     <td><font size="-1">Kinematic viscosity of fluid (<i>m<sup>2</sup>/s</i>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>&rho;</i></font></td>     <td><font size="-1">Fluid density (<i>kg/m</i><sup>3</sup>)</font></td>   </tr>   <tr>     <td><font size="-1"><i>&sigma;</i></font></td>     <td><font size="-1">Tangential momentum accommodation  coefficient</font></td>   </tr>   <tr>     <td><font size="-1"><i>&sigma;<sub>t</sub></i></font></td>     <td><font size="-1">Energy  accommodation coefficient</font></td>   </tr>   <tr>     <td><font size="-1"><i>&phi;</i><sub>1</sub></font></td>     <td><font size="-1">Cognitive  parameter</font></td>   </tr>   <tr>     <td><font size="-1"><i>&phi;</i><sub>2</sub></font></td>     <td><font size="-1">Social  parameter</font></td>   </tr>   <tr>     <td><font size="-1">&chi;</font></td>     <td><font size="-1">Constriction factor</font></td>   </tr>   <tr>     <td><font size="-1"><i>&Psi;</i></font></td>     <td><font size="-1">Swarm size</font></td>   </tr> </table>      <p><font size="3"><b>1. INTRODUCTION</b></font></p>     <p>Modern electronics pack lots of  semiconductors in a reduced area and execute specific  tasks at high clock rates, magnifying the  dissipated power and forcing designers to encompass heat  transfer phenomena. What began with the era of  Large Scale Integration (LSI) has led to different  design strategies, and has produced different commercial  options to deal with it.</p>     <p>Some years ago, Tuckerman and Pease urged the incorporation of heat sinks in  electronics, since an inadequate thermal management leads to  inefficiency and even failure of the devices. They considered  an electric equivalent for designing  microchannels and rocketed their use (nowadays, they are  broadly used in microelectronics). Later, some researchers  proposed an alternative design for microchannels,  considering entropy generation as a metric of the  irreversibility in a system (in a way that its  minimisation represents the maximisation of the operating  efficiency), but using traditional optimisation approaches.  Recently, the use of the entropy generation  minimisation (EGM) criterion has grown in different thermal  management scenarios. We believe this is partly due  to the evolution of modern optimisation and  partly due to its straightforward application, Rao and  Waghmare (2014), Hamadneh <i>et al</i>. (2013), Adham, Mohd-Ghazali and Ahmad (2012), Mohammed Adham, Mohd-Ghazali and Ahmad (2013),  Karathanassis <i>et</i> <i>al</i>. (2013), Chen and Chen (2013). However,  these two (EGM and modern optimisation) have not  been broadly applied to the design of  microchannels until relatively recent years. For example,  Adham, Mohd-Ghazali and Ahmad (2014) used Genetic  Algorithm (GA), and a modification of Khan's <i>et al</i>. model; and Khan, Kadri and Ali (2013) compared  results achieved using GA against previously  reported ones, obtained through NR. Additionally, Cruz,  Amaya and Correa (2015) designed microchannel heat  sinks with a more comprehensive mathematical  model, using algorithms such as Simulated  Annealing (SA), Unified Particle Swarm Optimisation  (UPSO) and Spiral Optimisation. This article  focuses on the aforementioned gap, designing a microchannel heat sink (MCHS) through entropy  generation minimisation (EGM), and optimising it with  two different modern techniques. From the vast  supply of available methods, and for the need of a  valid strategy to accomplish our designs in a short  period of time and in a reliable way, we chose the Harmony  Search (HS) and the Unified Particle Swarm  Optimisation (UPSO) algorithms, due to their interesting  characteristics, and to the good results they have achieved  for different applications, Abdel-Raouf and  Abdel-Baset Metwally (2013), Satpati, Koley and Datta  (2014), Amaya, Cruz and Correa (2015). Furthermore we have already had good experience with  those algorithms in other engineering  applications. We begin by explaining some of the  fundamentals around MCHS and about modern optimisation  techniques, and then move on to the methodology  section, where we discuss the procedure followed in this  study. Moving on to the results, we first show  the data of a Monte Carlo analysis and some preliminary  tests with the algorithms, in order to obtain a first  glance of the parameters and to define a set of values  that allow both algorithms to achieve good results.  Afterwards, we compare the performance of HS and UPSO  under specific scenarios, and for multiple materials  and heat generation configurations. We finish this  manuscript through the conclusions and  recommendations for future research.</p>     <p><b><font size="3">2. FUNDAMENTALS</font></b></p>     <p>Nowadays, integrated circuits (IC) are  fabricated   using vast amounts of semiconductors so  that they   can operate at high frequencies. However,  the power   dissipated by a chip increases with the  operating frequency,   and since their performance is temperature   sensitive, it is vital to remove it. Heat  sinks provide   a thermal support to electronic devices,  allowing the   heat to flow from the device and to the  environment,   and thus extending their lifetime.</p>     <p><b><font size="3">2.1. Model of the microchannel  heat sink</font></b></p>     <p>Heat sinks may have diverse geometries,  but   they all perform the same task and are  based on the   same main principle: extended superficial  area available   for heat transfer. Among them,  microchannel   heat sinks (MCHS) are commonly used when  space,   temperature and heat flux are constrained  by the   specification of the problem (e.g.  biomedical systems,   laptops and gadgets). The main features of  these devices   relate to their base structure (which  confines   a fluid flow to channels and thus allows a  high heat   transfer flux), as well as, to their small  temperature   increase, high heat transfer coefficients  and negligible   effects related to mass transfer. MCHS  have been   broadly used in literature, Rimbault,  Nguyen and   Galanis (2014), Karunanithi and  Hassanipour (2014),   Hatami and Ganji (2014), Leng <i>et al</i>. (2015), Hajialigol   <i>et al</i>. (2015), Khan, Kadri and Ali (2013),  Adham,   Mohd-Ghazali and Ahmad (2014). A general  scheme   of their base structure is shown in <a href="#fig1">Figure 1</a> where   the geometric parameters <i>L </i>and <i>W </i>relate to the length   and width of the device, respectively; <i>H</i><i><sub>c</sub> </i>and <i>w</i><i><sub>c</sub> </i>represent   the height and half-width of each channel;  and <i>w</i><i><sub>w</sub></i>   is half the separation between two  channels.</p>       ]]></body>
<body><![CDATA[<p align="center"><a name="fig1"></a><img src="img/revistas/eia/n24/n24a10fig1.gif"></p>     <p>In order to obtain the mathematical model, Khan <i>et al</i>. (2013) considered the top surface as adiabatic, while the lower plate allowed  for a uniform heat flow from the chip. They assumed that  the walls of the channels are smooth and with  adiabatic extremes, and that the material of the  heat sink is isotropic. Both, the cooling fluid and the  thermal energy flow, are considered as stationary,  laminar two-dimensional and fully  developed. The effects due to fluid drag can be overlooked when 0.001 &le; <i>Kn</i> &le; 0.1. Moreover, the flow is uncompressible with constant thermophysical properties and the axial conduction of the fin and the fluid is neglected, as well as the variations of kinetic and potential energies. This model also assumes an equal area available for heat transfer, between the microchannel and the electronic device. This last aspect seems a rather particular limitation of this model, due that it is not a common situation in real life. Khan <i>et al</i>. developed the model shown in (<a href="#for1">1</a>), which describes the entropy generation rate of a MCHS. This equation correlates the entropy generated due to the irreversibility of heat transfer  (in the heat sink and in the fluid) and to the fluid  friction, defined as <i><img src="img/revistas/eia/n24/n24a10for16.gif"><sub>gen,ht</sub> </i>and <i><img src="img/revistas/eia/n24/n24a10for16.gif"></i><i><sub>gen,ff</sub></i>, respectively. This correlation was obtained through the methodology laid out by Bejan (1995) who dictates that the minimum entropy generation of a real system can be found through an analysis based on heat transfer, fluid mechanics and thermodynamics,</p>     <p><a name="for1"></a><img src="img/revistas/eia/n24/n24a10for1.gif"></p>     <p>The first part of the entropy generation, <i><img src="img/revistas/eia/n24/n24a10for16.gif"></i><i><sub>gen,ht</sub></i>,   depends on the heat transfer rate (<img src="img/revistas/eia/n24/n24a10for15.gif">), as well as on   the absolute temperature of the base plate (<i>T</i><i><sub>b</sub></i>) and   of the ambient (<i>T</i><i><sub>a</sub></i>), and the total thermal  resistance   of the device. The latter relates to a correlation of  parameters:   (2<i>&alpha;</i><i><sub>hs</sub></i><i>C</i><sub>3</sub>)/(<i>Lk</i><i><sub>f</sub></i><i>C</i><sub>1</sub><i>C</i><sub>2</sub>), where <i>&alpha;</i><i><sub>hs</sub> </i>and <i>L </i>are the aspect   ratio and the length (in the direction of the heat   flow). <i>k</i><i><sub>f</sub> </i>is the thermal  conductivity of the fluid and <i>C</i><sub>1</sub>, <i>C</i><sub>2</sub> and <i>C</i><sub>3</sub> are correlations of the number of channels   (<i>N </i>= (<i>W</i>/2 - 2<i>w</i><i><sub>w</sub></i>)/(<i>w</i><i><sub>c</sub> </i>+ <i>w</i><i><sub>w</sub></i>)), the aspect ratio of the   heat sink and the channel (<i>&alpha;</i><i><sub>hs</sub></i> = <i>L</i>/2<i>w</i><i><sub>c</sub> </i>and &alpha;<i><sub>c</sub> </i>= 2<i>w</i><i><sub>c</sub></i>/<i>H</i><i><sub>c</sub></i>,   respectively), the fin's efficiency (&eta;<i><sub>fin</sub></i>), and dimensionless   groups such as Nusselt's (<i>Nu</i><i><sub>Dh</sub></i> ) and Peclet's (<i>Pe<sub>Dh</sub></i> )   numbers, shown in (<a href="#for2">2</a>),</p>       <p><a name="for2"></a><img src="img/revistas/eia/n24/n24a10for2.gif"></p>     <p>The second part of the entropy generation, <i><img src="img/revistas/eia/n24/n24a10for16.gif"></i><i><sub>gen,ff</sub></i>,   depends on <i>N </i>and <i>T</i><i><sub>a</sub></i>, as well as on the fluid density   (<i>&rho;</i>), the channel geometry (<i>w</i><i><sub>c</sub> </i>and <i>H</i><i><sub>c</sub></i>), the average velocity   of the flow (<i>U</i><i><sub>avg</sub></i>) and the parameter <i>C</i><sub>4</sub>, that correlates   the losses on the channels with the effects due to friction, as shown in (<a href="#for3">3</a>).</p>     <p><a name="for3"></a><img src="img/revistas/eia/n24/n24a10for3.gif"></p>     <p>Once a single-objective function based on (<a href="#for1">1</a>) has been defined, the heat sink is designed by finding the variables (i.e. the design vector) <i>H<sub>c</sub></i>, <i>w</i><i><sub>c</sub></i>, <i>w</i><i><sub>w</sub></i>, <i>Kn </i>and <i>G </i>that minimise the entropy generation rate. Thus, the restricted optimisation problem given in (<a href="#for4">4</a>) appears. For this research, we also considered, for comparison purposes, the restrictions previously reported in  literature Adham, Mohd-Ghazali and Ahmad (2012).</p>     <p><a name="for4"></a><img src="img/revistas/eia/n24/n24a10for4.gif"></p>     <p><b><font size="3">2.2. Modern global  optimization methods</font></b></p>     ]]></body>
<body><![CDATA[<p>These techniques generally require simple  calculations,   making them versatile and easy to  implement,   as opposed to traditional gradient-based  approaches.</p>     <p><b><i><font size="3">Harmony Search  algorithm (HS)</font></i></b></p>     <p>About fifteen years ago, as presented  Amaya, <i>et</i>   <i>al</i>. (2015), Geen proposed the HS algorithm  inspired by the improvisation expert musicians carry  out. This process is modelled through three possible  choices regarding a piece of music: reproduce an  already famous one, a variant or a brand new one.  Since a piece of music is a sequence of tones playing in  harmony, HS relates them to the design vector of an  optimisation problem. In its most basic form, HS  depends on four parameters. The first one is the Harmony  Memory Size (<i>MHS</i>), or simply put, the maximum number of pieces that can be stored in memory. The second parameter is the Harmony Memory Considering Rate (<i>HMCR</i>), that determines if an already stored piece should be selected, or not. The third parameter is the Pitch Adjusting Rate (<i>PAR</i>) and defines how often a selected piece must be adjusted using (<a href="#for5">5</a>) and the fourth parameter, known as Fretwidth (<i>FW</i>). The modified solution,, is the same piece that was selected, but shifted around <i>FW</i>, using a uniformly distributed random number between zero and one (<i>rand</i>). It is worth mentioning that this is the only equation HS requires, as opposed to other approaches,</p>     <p><a name="for5"></a><img src="img/revistas/eia/n24/n24a10for5.gif"></p>     <p>A general algorithm can thus be laid out as:</p> <ol>       <li>Define <i>HMCR, PAR, FW</i>, the search domain <i>X</i><i><sub>min</sub></i> &le; <i>X </i>&le;<i> X</i><i><sub>max</sub></i>, and the objective function <i>f</i><i><sub>obj</sub></i>(<i>X</i><sub>1</sub>, <i>X</i><sub>2</sub>,..., <i>X</i><i><sub>n</sub></i>). Also, define the stop criteria.</li>       <li>Randomly populate the memory matrix (<i>HM</i>), of     size <i>HMS </i>&times; <i>n</i>.</li>       <li>Generate a random number with <i>HMCR </i>probability     of being successful. If it is, go to step four. Otherwise, select a random value and go to step     six.</li>       <li>Select the element located at a random row of <i>HM </i>and at the column corresponding to the dimension     being updated.</li>       <li>Generate a random number with <i>PAR </i>probability     of being successful. If it is, update the value     using (<a href="#for5">5</a>).</li>       ]]></body>
<body><![CDATA[<li>Move on to the next dimension and repeat for all <i>n </i>dimensions.</li>       <li>Check stop criteria. If it complies, stop and print     results. Otherwise, return to step three.</li>     </ol>     <p><b><i><font size="3">Unified Particle Swarm Optimisation  algorithm</font></i></b>   <font size="3"><b><i>(UPSO)</i></b></font></p>     <p>UPSO was proposed by Parsopoulos and Vrahatis,   and it is an improvement of the traditional PSO   algorithm, originally proposed by Kennedy and Eberhart. This technique is based on swarm intelligence and it was inspired by the natural process of food search carried out by bird flocks and fish shoals. The main difference between UPSO and PSO is that in the former, the agents (also known as particles) can form subsets (or neighbourhoods), in order to strengthen the exploration (global behaviour) and exploitation (local behaviour) of the search domain. The total  velocity of a particle is composed of a global and a local dynamic, respectively known as <img src="img/revistas/eia/n24/n24a10for12.gif">, (<a href="#for6">6</a>), and <img src="img/revistas/eia/n24/n24a10for13.gif">, (<a href="#for6">7</a>),</p>     <p><a name="for6"></a><img src="img/revistas/eia/n24/n24a10for6.gif"></p>     <p>These two elements directly depend on parameters   such as the constriction factor, &chi;, that limits the velocity   of the particles to avoid an explosion of the swarm;   the self and swarm confidence, <i>&phi;</i><sub>1</sub> and <i>&phi;</i><sub>2</sub> respectively;   and four uniformly distributed random numbers between   zero and one, <i>rand</i>1. UPSO also considers the   position, <i>&chi;<sub>p</sub><sup>t</sup></i>, and the total velocity, <i>V<sub>p</sub><sup>t</sup></i>, at the time step <i>t</i>, as well as the best position found by each particle, <i><img src="img/revistas/eia/n24/n24a10for14.gif"></i><i><sub>p</sub></i>, by each neighbourhood, <i><img src="img/revistas/eia/n24/n24a10for14.gif"></i><i><sub>gp</sub></i>, and by the swarm, <i><img src="img/revistas/eia/n24/n24a10for14.gif"></i><i><sub>g</sub></i>, during the whole search. Note that the index <i>p </i>relates   to a particle in the swarm, where <i>p </i>= 1,...,<i>&Psi;</i>, and <i>&Psi; </i>is the total number of agents. The total velocity of   each particle for the next time step, <i>V<sub>p</sub><sup>t+1</sup></i>, is obtained   through (<a href="#for7">8</a>) where <i>u </i>is the unification factor and represents   a constant between zero and one, whose objective   is to balance the global and local behaviour of   each particle. Finally, (<a href="#for7">9</a>) is used to find the new  position   of the swarm,</p>     <p><a name="for7"></a><img src="img/revistas/eia/n24/n24a10for7.gif"></p>     <p>A general algorithm can thus be laid out as:</p> <ol>       <li>Define &chi;, <i>&phi;</i><sub>1</sub>, <i>&phi;</i><sub>1</sub>, <i>&Psi; </i>and the selection criteria of the     neighbourhoods, the search domain <i>X</i><i><sub>min </sub></i>&le;<i> X</i><i><sub>p</sub></i>&le;<i> X</i><i><sub>max</sub></i>, and the objective function <i>f</i><i><sub>obj</sub></i>(&chi;).</li>       ]]></body>
<body><![CDATA[<li>Randomly assign the initial position of each  particle,     <i>&chi;<sub>p</sub></i><sup>1</sup>, over the search domain and assign an     initial value for the velocity <i>V<sub>p</sub></i><sup>1</sup>.</li>       <li>Evaluate each position, &chi;<sub>p</sub>, in <i>f</i><i><sub>obj</sub> </i>and find <i><img src="img/revistas/eia/n24/n24a10for14.gif"></i><i><sub>p</sub></i><i>, <img src="img/revistas/eia/n24/n24a10for14.gif"></i><i><sub>gp</sub></i> and <i><img src="img/revistas/eia/n24/n24a10for14.gif"></i><i><sub>g</sub></i>.</li>       <li>Use (<a href="#for7">8</a>) and (<a href="#for7">9</a>) to calculate and,  respectively.</li>       <li>Evaluate each new position in the  objective function     and update <i><img src="img/revistas/eia/n24/n24a10for14.gif"></i><i><sub>p</sub></i><i>, <img src="img/revistas/eia/n24/n24a10for14.gif"></i><i><sub>gp</sub> </i>and <i><img src="img/revistas/eia/n24/n24a10for14.gif"></i><i><sub>g</sub></i>.</li>       <li>Check stop criteria. If it complies,  stop and print     results. Otherwise, make <i>t = t </i>+1 and go to step four.</li>     </ol>     <p><b><i><font size="3">2.3. Solution of a  constrained</font></i></b>   <font size="3"><b><i>optimisation problem</i></b></font></p>     <p>A constrained optimisation problem is  defined   as shown in (<a href="#for8">10</a>), and the design vector &chi;* with <i>n </i>components   is known as the solution, or optimum  design   variable, which represents the design  vector &chi; that   minimises the single-objective function <i>f</i><i><sub>obj</sub></i>(&chi;) inside   the feasible region defined by the  restrictions <img src="img/revistas/eia/n24/n24a10for17.gif"><i><sub>i</sub> </i>and   the boundaries of each dimension. Any  number of   restrictions, <i>n</i><i><sub>g</sub></i>, can be implemented and they might   represent either equalities or  inequalities,</p>     <p><a name="for8"></a><img src="img/revistas/eia/n24/n24a10for8.gif"></p>     <p>There are, at least, two general  approaches for   solving these kind of problems through  global optimisation   algorithms. The first one repositions the   agents into the feasible region whenever  an update   takes them out, and the kind of reposition  varies according   to the optimisation algorithm. The second   one modifies the objective function  through penalty   factors, which in turn vary according to  each specific   problem.</p>     ]]></body>
<body><![CDATA[<p><b><font size="3">3. METHODOLOGY</font></b></p>     <p>During this study, simulation data was  gathered   using an ASUS&reg; S46C personal computer with   the following specifications: Intel&reg; Core<sup>TM</sup>  i7-3537U   CPU @ 2.00 GHz - 2.50 GHz, 6 GB RAM,  operating under   Microsoft&reg; Windows<sup>TM</sup> 8.1 Single - 64 bits.  This   work was split into different stages, and  in all tests we   stopped the algorithms if they did not  improve after a   given number of iterations (saturation) or  if excessive   iterations were carried out.</p>     <p><b><font size="3">3.1. Monte Carlo simulation</font></b></p>     <p>The first stage was a set of Monte Carlo  simulations   to observe the relative importance of the  design   parameters, from a known distribution of  entropy   generation rate, and the influence of heat  and mass   transfer phenomena on it. We first  analysed the final   equation and then began deepening into the  definition   of each variable, via their respective  equations. For each one of these tests, 10<sup>10</sup> samples were generated so the data was significant.</p>     <p><b><font size="3">3.2. Selection of parameters</font></b></p>     <p>The second stage was a parameter search to   tune each algorithm, so their performances  could   be properly addressed. On this regard, we  used the   design parameters shown in <a href="#tab1">Table 1</a>, considering air   as cooling fluid and a total heat transfer  of 150 W from   the chip. We also used the set of  parameters shown   in <a href="#tab2">Table 2</a>, and ran 40 repetitions of each  parameter   configuration, for each algorithm,  considering the   objective function given in (<a href="#for1">1</a>), and the  design vector   as <i>X</i>= (<i>H<sub>c</sub>, w<sub>c</sub>, w<sub>w</sub>, Kn, G</i>) all this in order to solve the   minimisation problem given in (<a href="#for4">4</a>). We  measured   the convergence rate of each  configuration, which is   simply the ratio of the tests that  satisfied the main stop   criterion, over the total number of tests.  It is worth   mentioning that we used three different  components   for the fretwidth (<i>FW</i>1, <i>FW</i>2 and <i>FW</i>3), where each   one relates to a specific design variable.  This was done   because there is a difference in the order  of magnitude   of the design variables and because a bad  scaling of <i>FW</i>   could jeopardize HS's performance. After  finding the   best parameters for each algorithm, 1000  repetitions   were run for each one and we analysed  their benefits   and drawbacks.</p>       <p align="center"><a name="tab1"></a><img src="img/revistas/eia/n24/n24a10tab1.gif"></p>       <p align="center"><a name="tab2"></a><img src="img/revistas/eia/n24/n24a10tab2.gif"></p>     <p>We also performed the Wilcoxon signed-rank test for the difference of <i><img src="img/revistas/eia/n24/n24a10for16.gif"></i><i><sub>gen,min</sub> </i>obtained through HS and UPSO,  using equality of mean values as the null hypothesis (<img src="img/revistas/eia/n24/n24a10for18.gif"><sub>0</sub> : &mu;<i><sub>HS</sub> </i>= &mu;<i><sub>UPSO</sub></i>) and a significance level of 0.05 for two tails Derrac <i>et al</i>. (2011).</p>     <p><b><font size="3">3.3. Design scenarios</font></b></p>     ]]></body>
<body><![CDATA[<p>The third stage considered two variations  of the   model and its constraints. We analyse the  solutions   and the way in which the algorithms  behaved. The first   one dealt with bigger search domains, but  preserving   the context of the design, as shown in  (<a href="#for9">11</a>). Here, it is   important to note that the limits of <i>Kn </i>were not varied   since the effects due to fluid drag were  disregarded. The second one dealt with different  materials (<a href="#tab3">Table 3</a>), based on the information provided in  Mohammed Adham, Mohd-Ghazali and Ahmad (2013) for  microchannel structures, and with different heat  generation rates (<i><img src="img/revistas/eia/n24/n24a10for15.gif"></i>),</p>     <p><a name="for9"></a><img src="img/revistas/eia/n24/n24a10for9.gif"></p>     <p align="center"><a name="tab3"></a><img src="img/revistas/eia/n24/n24a10tab3.gif"></p>     <p><b>3.4. Data Comparison</b></p>     <p>In the final stage of this work, <i>Kn </i>as well as <i>G</i>,   were fixed in an interval, as shown by the  constraints   given in (<a href="#for10">12</a>). A material with <i>k = </i>148 <i>W/m</i><i>&middot;K </i>was also   considered. The resulting designs were  compared   with some of the data provided by Khan,  Kadri and Ali   (2013),</p>     <p><a name="for10"></a><img src="img/revistas/eia/n24/n24a10for10.gif"></p>     <p><b><font size="3">4. RESULTS AND DISCUSSION</font></b></p>     <p><font size="3"><b>4.1. Monte Carlo analysis</b></font></p>     <p><a href="#tab4">Table 4</a> shows the values found with Monte   Carlo, which provides us with an insight  about the order   of magnitude of each parameter and their  relative   importance. In this case, we obtained a  feasible MCHS   design (choosing each parameter from the  intervals   given in <a href="#tab4">Table 4</a>), but not the optimum one.</p>       <p align="center"><a name="tab4"></a><img src="img/revistas/eia/n24/n24a10tab4.gif"></p>     ]]></body>
<body><![CDATA[<p><b><font size="3">4.2. Parameter selection</font></b></p>     <p>When using HS, it was found that a reduced   memory size (<i>HMS</i>) and a high considering rate   (<i>HMCR</i>) yielded  a high convergence rate (<a href="#fig2">Figure 2a</a>). Regarding the pitch rate (<i>PAR</i>), we found that smaller values tended to favour convergence for almost all <i>HMS </i>values (<a href="#fig2">Figure  2b</a>) as well as for every <i>HMCR</i>, even though in the latter the effect was more  important for lower values (<a href="#fig3">Figure 3a</a>). The remaining parameter, i.e. the fretwidth (<i>FW</i>), provided an improvement in the average convergence rate when using the first configuration, even though its effect was not as strong as for the other ones (<a href="#fig3">Figure 3b</a>). Therefore, we selected 10, 0.9, 0.2 and <i>FW</i>3 as the values for <i>HMS</i>, <i>HMCR</i>, <i>PAR </i>and <i>FW</i>.</p>     <p align="center"><a name="fig2"></a><a href="img/revistas/eia/n24/n24a10fig2.gif" target="_blank">Figure 2</a></p>     <p align="center"><a name="fig3"></a><a href="img/revistas/eia/n24/n24a10fig3.gif" target="_blank">Figure 3</a></p>     <p>With respect to UPSO, we found that bigger swarms and a unification factor (<i>u</i>) between 0.4 and 0.6 yielded better convergence rates (<a href="#fig4">Figure 4a</a>). In order to clarify this idea some more, we calculated a global convergence rate, considering the average of  all tests (including all combinations of parameters) as a function of the unification factor. We found that <i>u</i> = 0.4 and <i>u </i>= 0.6 yield 82.2% and  82.3%, respectively, while <i>u </i>= 0.2 yields 81.2% and <i>u </i>= 0.8 yields 81.5%. We  also found that no matter the size of the swarm, smaller constriction values (&chi;) provide better convergence rates (<a href="#fig4">Figure 4b</a>). Since <i>&phi;</i><sub>1</sub> and <i>&phi;</i><sub>2</sub> are both part of the same equation, we looked for a good combination and not for a tendency, finding that <i>&phi;</i><sub>1 </sub>= 3.0 and <i>&phi;</i><sub>1 </sub>= 2.2 yielded the highest convergence rates (<a href="#fig5">Figure 5</a>).</p>     <p align="center"><a name="fig4"></a><a href="img/revistas/eia/n24/n24a10fig4.gif" target="_blank">Figura 4</a></p>     <p align="center"><a name="fig5"></a><img src="img/revistas/eia/n24/n24a10fig5.gif"></p>     <p><a href="#tab5">Table 5</a> summarizes the parameters that work best for both algorithms, based on what was previously discussed and the best results achieved with each algorithm are laid out in <a href="#tab6">Table 6</a>. <a href="#fig6">Figure 6</a> shows the normalised frequency distribution for the minimum entropy generation rates found with HS and UPSO, using the same bins for both techniques (calculated using UPSO's span). In the first case, we considered only 959 executions in the plot, striving to simplify  the plot. We noted that the probability of obtaining a <i><img src="img/revistas/eia/n24/n24a10for16.gif">gen,min</i> between 32.26 and 33.68 <i>mW/K </i>using HS and UPSO is of 23.5% and of 9.6%, respectively. Also, we found that the mean value of <i><img src="img/revistas/eia/n24/n24a10for16.gif"></i><i>gen,min </i>is virtually the same for both methods, but HS showed a standard deviation of 5 <i>mW/K</i>, more  than twice that of UPSO's; and HS requires almost five times more iterations than UPSO, but it does them in a time about 20 times smaller.</p>     <p align="center"><a name="tab5"></a><img src="img/revistas/eia/n24/n24a10tab5.gif"></p>     <p align="center"><a name="tab6"></a><img src="img/revistas/eia/n24/n24a10tab6.gif"></p>     ]]></body>
<body><![CDATA[<p align="center"><a name="fig6"></a><img src="img/revistas/eia/n24/n24a10fig6.gif"></p>     <p>In addition, the Wilcoxon signed-rank  test, a non-parametric statistical hypothesis  test, was used to compare the difference of <i><img src="img/revistas/eia/n24/n24a10for16.gif"></i><i>gen,min </i>obtained using both methods (i.e., HS and UPSO). It was  concluded that there is insufficient evidence to  reject the null hypothesis (<img src="img/revistas/eia/n24/n24a10for18.gif"><sub>0</sub> : &mu;<i><sub>HS</sub> </i>= &mu;<i><sub>UPSO</sub></i>), with a significance level of 0.05. The power of the test was 0.1912. <a href="#fig7">Figure 7</a> shows the distribution of this difference  with mean, standard deviation, skewness and kurtosis  equal to 0.89 <i>mW</i>/<i>K</i>, 5.34 <i>mW</i>/<i>K</i>, 3.52 and 28.67,respectively.</p>     <p align="center"><a name="fig7"></a><img src="img/revistas/eia/n24/n24a10fig7.gif"></p>     <p><b><font size="3">4.3. Design scenarios</font></b></p>     <p><font size="3"><b><i>4.3.1. Search domain  expansion</i></b></font></p>     <p>After expanding the search domain, both  approaches   achieved minimum entropy values quite   similar to those of the smaller domain (<a href="#tab7">Table 7</a>),   although the values of the design  parameters are   somewhat different. Even so, we found that  the average   minimum entropy generation rate increased   for both algorithms and that the big data  dispersion   of HS is still present (<a href="#tab8">Table 8</a>).</p>       <p align="center"><a name="tab7"></a><img src="img/revistas/eia/n24/n24a10tab7.gif"></p>       <p align="center"><a name="tab8"></a><img src="img/revistas/eia/n24/n24a10tab8.gif"></p>     <p><b><i><font size="3">4.3.2. Tests for  different materials</font></i></b></p>     <p>We found that the convergence rate of both  approaches   is not affected by the material which the   heat sinks are made of, since higher  conductivity   values returned lower entropy generation  rates, as   expected (<a href="#tab9">Table 9</a>). Nevertheless, there is a clear   dependence of the values of the design  parameters   with that variable. In <a href="#fig8">Figure 8</a>, UPSO yielded a   slightly lower average minimum entropy  generation   rate for all materials but copper.  Nonetheless, HS   was able to achieve a better answer in all  cases, so   we consider that the difference in the  data is mainly   due to HS's high dispersion. Moreover, we  observed   that the number of required iterations  remains   quite steady for all materials, and even  though HS   did almost six times more iterations than  UPSO, it   was about 20 times faster.</p>       ]]></body>
<body><![CDATA[<p align="center"><a name="tab9"></a><img src="img/revistas/eia/n24/n24a10tab9.gif"></p>       <p align="center"><a name="fig8"></a><img src="img/revistas/eia/n24/n24a10fig8.gif"></p>     <p><b><i><font size="3">4.3.3. Tests for different dissipated power</font></i></b></p>     <p>We fixed the material to copper (since it  allowed for   the minimum entropy) and varied the heat  generation,   ranging from 150 W and up to 1000 W, with  50 W steps. In order to facilitate data comparison, we  use the same organization style as in Khan, Kadri and  Ali (2013), Adham, Mohd-Ghazali and Ahmad (2014). Thus, <a href="#tab10">Table 10</a> shows the optimal designs achieved with HS  and UPSO in terms of three design variables (i.e., <i>Kn</i>, <i>&alpha;</i><i><sub>c</sub> </i>and &beta;) and three performance parameters (i.e., <i>R</i><i><sub>th</sub></i>, &Delta;<i>P </i>and <i><img src="img/revistas/eia/n24/n24a10for16.gif"></i><i><sub>gen</sub></i>).</p>     <p align="center"><a name="tab10"></a><a href="img/revistas/eia/n24/n24a10tab10.gif" target="_blank">Table 10</a></p>     <p>For all designs, we found that the channel  height and the volume flow rate remains close to  the upper limits (50 <i>mm </i>and 0.01 <i>m</i><sup>3</sup>/<i>s</i>, respectively), as expected. In the same way, higher heat flow rates  lead to higher entropy generation rates. The thermal  resistance diminishes as the generated heat rises, since a fixed  flow requires that the minimum resistance  decreases in order to satisfy the increased power dissipation  from the chip. The pressure drop estimated by HS  was consistently higher than the reported by UPSO although  there is some kind of oscillation in their  values. Additionally, we observed that the optimal channel  aspect ratio (<i>&alpha;</i><i><sub>c</sub></i>) decreases when the heat transfer rate  increases, with an approximate rate of 4 &times; 10<sup>-6</sup> 1/<i>W</i>, making channels highly rectangular.</p>     <p>It was also observed that the pressure  drop increases at a rate of 1.15 <i>Pa/W </i>and that a high fraction of <i><img src="img/revistas/eia/n24/n24a10for16.gif"><sub>gen,min</sub> </i>is due to heat transfer (<a href="#fig9">Figure 9</a>), while the contribution of mass transfer (<i><img src="img/revistas/eia/n24/n24a10for16.gif"><sub>gen,ff</sub></i>) is reduced. As it was anticipated, these results show a  system highly dependent of the heat transfer mechanism.  Moreover, we appreciated a rise in the heat sink  base temperature (<i>T<sub>b</sub></i>) with the increased heat flow (<a href="#fig10">Figure 10</a>). For a traditional electronic device, <i>T<sub>b</sub> </i>&gt; 345 K may compromise its performance, so special care must be  taken into account. On this regard, we show that for heat  transfer rates over 500 W (piecewise box), the  device will misbehave, so additional variables, such as the  properties of the fluid, must be included in the model.</p>     <p align="center"><a name="fig9"></a><img src="img/revistas/eia/n24/n24a10fig9.gif"></p>     <p align="center"><a name="fig10"></a><img src="img/revistas/eia/n24/n24a10fig10.gif"></p>     <p>Those simulation results could guide us in defining safe operational conditions.</p>     ]]></body>
<body><![CDATA[<p><b><i><font size="3">4.3.4. Data Comparison</font></i></b></p>     <p>Finally, we compare our simulated designs  (using   HS and UPSO) against those reported by  Khan,   Kadri and Ali (2013) using Genetic  Algorithm (GA). In the same way as Khan <i>et al</i>. did, we varied <i>Kn </i>and   <i>G</i>, and assumed the same design variables (<i>H</i><i><sub>c</sub></i>, <i>w</i><i><sub>c</sub></i>, and <i>w<sub>w</sub></i>). Results are shown in <a href="#tab11">Table 11</a>. For a given value of <i>Kn </i>and <i>G</i>, we obtained quite different aspect ratios (<i>&alpha;</i><i><sub>c</sub> </i>and <i>&beta;</i>), even though they share the same trend. Unfortunately, analysing their  data it is easy to observe that their results are  above the upper limit imposed for their simulations  (<a href="#tab2">Table 2</a> in Khan, Kadri and Ali (2013)). This  hinders a more detailed comparison.</p>     <p align="center"><a name="tab11"></a><a href="img/revistas/eia/n24/n24a10tab11.gif" target="_blank">Table 11</a></p>     <p><b><font size="3">5. CONCLUSIONS AND</font></b>   <font size="3"><b>RECOMMENDATIONS</b></font></p>     <p>It was accomplished a systematic and   thorough analysis, related to the  effectiveness of the   optimization algorithms HS and UPSO for  the design   of optimal microchannels<i>. </i>It was also evident that   the Monte Carlo strategy, a well-known  powerful   technique, can be used as a first approach  in design   engineering, especially to grasp an idea  of the   order of magnitude and of the relative  importance   of the parameters. During this study we  explored   two modern algorithms for optimising the  design of a microchannel heat sink. We found that both   approaches yielded precise results, even  though they   have some particularities. In the case of  Harmony   Search (HS), we found that it always  provided the   best answer (i.e. the one with the minimum  entropy   generation rate), but its data dispersion  was higher   (about two times), thus allowing Unified  Particle   Swarm Optimisation (UPSO) to generate  results with   a lower average minimum entropy generation  rate. We also noted that HS presented a greater  chance (24%) of finding a better solution than  PSO (10%). Moreover, we determined that HS requires  several times more iterations than UPSO (about  five for this particular research) but since each  iteration has quite a straightforward logic, the  convergence time of HS ends up being way shorter than UPSO's  (about 19 times according to our data). We also  determined that both algorithms seem to be stable  when varying the material of the heat sink and the heat  generation rate, providing practical values for the  designs. Of all the materials tested, it was determined  that copper generates the minimum entropy. However, a  proper selection of the material must not only  consider thermal conductivity, but also variables  such as manufacturing costs, operating conditions,  and other factors relevant to the design  specifications, even its own weight. Nonetheless, HS and  UPSO behaved quite well for this application,  so we recommend using them and invite the reader to test them with a multi-objective model that  incorporates the aforementioned variables in order to  achieve a more realistic and buildable design.  Finally, we think these findings can be used by  microchannels design engineers to significantly shorten  the time consuming optimal design process.</p>     <p><b><font size="3">ACKNOWLEDGEMENTS</font></b></p>     <p>The authors would like to express their  gratitude   to  Vicerrector&iacute;a de Investigaci&oacute;n y Extensi&oacute;n,   at  Universidad Industrial de Santander (Colombia),   for the support granted through project  1807.</p>     <p><b><font size="3">REFERENCES</font></b></p>     <!-- ref --><p>Abdel-Raouf, O. y Abdel-Baset-Metwally, M.  (2013). A   Survey of Harmony Search Algorithm. <i>International</i>   <i>Journal of Computer Applications</i>, 70(28), pp.17-26.    &nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=3056079&pid=S1794-1237201500020001000001&lng=','','width=640,height=500,resizable=yes,scrollbars=1,menubar=yes,');">Links</a>&#160;]<!-- end-ref --></p>     ]]></body>
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