<?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>0012-7353</journal-id>
<journal-title><![CDATA[DYNA]]></journal-title>
<abbrev-journal-title><![CDATA[Dyna rev.fac.nac.minas]]></abbrev-journal-title>
<issn>0012-7353</issn>
<publisher>
<publisher-name><![CDATA[Universidad Nacional de Colombia]]></publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id>S0012-73532021000400210</article-id>
<article-id pub-id-type="doi">10.15446/dyna.v88n219.93809</article-id>
<title-group>
<article-title xml:lang="en"><![CDATA[Numerical analysis of aircraft flow exhaust gases to design a curved deflector for Mexico City international airport]]></article-title>
<article-title xml:lang="es"><![CDATA[Análisis numérico del flujo de gases de escape de aviones para diseñar un deflector curvo para el aeropuerto internacional de la Ciudad de México]]></article-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Garrido-Téllez]]></surname>
<given-names><![CDATA[Jorge Luis]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Hernández-Martínez]]></surname>
<given-names><![CDATA[Eusebio Eduardo]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Jiménez-Escalona]]></surname>
<given-names><![CDATA[José Carlos]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
</contrib-group>
<aff id="Af1">
<institution><![CDATA[,Instituto Politecnico Nacional  ]]></institution>
<addr-line><![CDATA[Mexico ]]></addr-line>
<country>Mexico</country>
</aff>
<pub-date pub-type="pub">
<day>00</day>
<month>12</month>
<year>2021</year>
</pub-date>
<pub-date pub-type="epub">
<day>00</day>
<month>12</month>
<year>2021</year>
</pub-date>
<volume>88</volume>
<numero>219</numero>
<fpage>210</fpage>
<lpage>217</lpage>
<copyright-statement/>
<copyright-year/>
<self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_arttext&amp;pid=S0012-73532021000400210&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_abstract&amp;pid=S0012-73532021000400210&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_pdf&amp;pid=S0012-73532021000400210&amp;lng=en&amp;nrm=iso"></self-uri><abstract abstract-type="short" xml:lang="en"><p><![CDATA[Abstract The numerical simulation results of the flow exhaust gases emitted by different aircraft engines are presented in this work. These results permitted the design of the most appropriate circular arc for a curved deflector to correctly direct the flow at the time planes are taking-off on the left runway number five of Mexico City International Airport (AICM) and not to affect the operability and route of the inter-terminal train, called as &#8220;Aerotren&#8221;. This train has four carriages of 25 passengers each and transports users of Mexico City International Airport from terminal T-1 to terminal T-2 and vice versa. For the numerical simulation, several engine models of different aircraft were used, including the Boeing 747-400, the Boeing 777-200LR/-300ER, the Airbus A340-600, and the McDonnell Douglas MD11. The results presented here are those from the McDonnell Douglas MD11 airplane, which is the most critical case since it has an engine in the rear part of the fuselage on the vertical empennage, and this causes the flow of exhaust gases to arrive in a direction from top to bottom on the upper part of the Aerotren, which for safety should not exceed 15.0 m/s (54 km/hr). The impact of the explosion of these engine models was used to choose the most appropriate deflector curvature angle in the take-off area. The numerical simulation was carried out through the Fluent CFD program, solving the Navier-Stokes equations, the standard (-( model, turbulence, and atmospheric conditions in Mexico City. An experimental stage and the visualization of the behavior of the flow of exhaust gases within a wind tunnel are also presented. A 1: 125 scale model was used for both the deflectors with the radius of curvature obtained and the train car, in an area of one square meter and a grid background screen.]]></p></abstract>
<abstract abstract-type="short" xml:lang="es"><p><![CDATA[Resumen En este trabajo se presentan los resultados obtenidos de la simulación numérica del flujo sobre un deflector curvo, con la finalidad de obtener el arco circular más apropiado para direccionar el flujo de los gases de escape en el momento de despegue de los aviones en la pista 05 izquierda del Aeropuerto Internacional de la Ciudad de México (AICM) y no afectar la operatividad y vialidad del tren inter-terminales, también llamado como Aerotrén. Este tren cuenta con cuatro vagones de 25 pasajeros cada uno y tiene la finalidad de transportar a los usuarios del aeropuerto de la terminal T-1 Internacional a la terminal T-2 Nacional y viceversa. Para la simulación numérica se utilizaron varios modelos de motores de diferentes aviones entre ellos: el Boeing 747-400, el Boeing 777-200LR/-300ER, el Airbus A340-600 y el McDonnell Douglas MD11. Los resultados que se presentan en este trabajo son del avión McDonnell Douglas MD11 por ser el caso crítico ya que cuenta con un motor en la parte posterior del fuselaje sobre el empenaje vertical y esto provoca que el flujo de los gases de escape llegue en una dirección desde arriba hacia abajo sobre la parte superior del tren, el cual por seguridad no deben sobrepasar la velocidad de 15.0 m/s (54 Km/hr). También se presentan los resultados experimentales de la visualización del comportamiento del flujo dentro de un túnel de viento, para esto se utilizó un modelo a escala de 1:125 tanto del deflector como del vagón del tren, en un área de 1 m2 y una pantalla de fondo cuadriculada.]]></p></abstract>
<kwd-group>
<kwd lng="en"><![CDATA[numerical analysis]]></kwd>
<kwd lng="en"><![CDATA[aircraft gas turbine engine flow]]></kwd>
<kwd lng="en"><![CDATA[computational fluid dynamics]]></kwd>
<kwd lng="en"><![CDATA[curved deflector]]></kwd>
<kwd lng="en"><![CDATA[Mexico City international airport]]></kwd>
<kwd lng="en"><![CDATA[wind tunnel test]]></kwd>
<kwd lng="en"><![CDATA[visualization]]></kwd>
<kwd lng="es"><![CDATA[análisis numérico]]></kwd>
<kwd lng="es"><![CDATA[flujo de motores de turbina de gas en aviones]]></kwd>
<kwd lng="es"><![CDATA[dinámica computacional de fluidos]]></kwd>
<kwd lng="es"><![CDATA[deflector curvo]]></kwd>
<kwd lng="es"><![CDATA[aeropuerto internacional de la Ciudad de México]]></kwd>
<kwd lng="es"><![CDATA[prueba en túnel de viento]]></kwd>
<kwd lng="es"><![CDATA[visualización]]></kwd>
</kwd-group>
</article-meta>
</front><back>
<ref-list>
<ref id="B1">
<label>[1]</label><nlm-citation citation-type="confpro">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Nadal-Mora]]></surname>
<given-names><![CDATA[V.]]></given-names>
</name>
<name>
<surname><![CDATA[Pezzotti]]></surname>
<given-names><![CDATA[S.]]></given-names>
</name>
<name>
<surname><![CDATA[Di Barnardi]]></surname>
<given-names><![CDATA[A.]]></given-names>
</name>
<name>
<surname><![CDATA[Di Gregorio]]></surname>
<given-names><![CDATA[P.]]></given-names>
</name>
<name>
<surname><![CDATA[Pesarini]]></surname>
<given-names><![CDATA[A.]]></given-names>
</name>
</person-group>
<source><![CDATA[Theoretical analysis and experimental validation of the interaction between the exhaust flow of aircraft engines in take-off operations, an anti-jet barrier and a vehicular route]]></source>
<year>2007</year>
<conf-name><![CDATA[ Proceedings of the First Congress of the Ibero-American Network for Research in Air Transport (RIDITA)]]></conf-name>
<conf-loc> </conf-loc>
<page-range>339-58</page-range></nlm-citation>
</ref>
<ref id="B2">
<label>[2]</label><nlm-citation citation-type="book">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Morrison]]></surname>
<given-names><![CDATA[R.]]></given-names>
</name>
</person-group>
<source><![CDATA[Ground jet blast hazard]]></source>
<year>1993</year>
<numero>6</numero>
<issue>6</issue>
<publisher-name><![CDATA[ASRS Directline]]></publisher-name>
</nlm-citation>
</ref>
<ref id="B3">
<label>[3]</label><nlm-citation citation-type="book">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Hayden]]></surname>
<given-names><![CDATA[H.J.]]></given-names>
</name>
</person-group>
<source><![CDATA[Jet engine exhaust deflector]]></source>
<year>1958</year>
<publisher-name><![CDATA[U.S. Patent 2,826,382]]></publisher-name>
</nlm-citation>
</ref>
<ref id="B4">
<label>[4]</label><nlm-citation citation-type="book">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Stanley]]></surname>
<given-names><![CDATA[B.L.]]></given-names>
</name>
<name>
<surname><![CDATA[Dunes]]></surname>
<given-names><![CDATA[P.]]></given-names>
</name>
</person-group>
<source><![CDATA[Split exhaust jet blast deflector fence]]></source>
<year>1995</year>
<publisher-loc><![CDATA[U.S ]]></publisher-loc>
<publisher-name><![CDATA[Patent]]></publisher-name>
</nlm-citation>
</ref>
<ref id="B5">
<label>[5]</label><nlm-citation citation-type="book">
<source><![CDATA[Campion, G.P. Blast deflector]]></source>
<year>2004</year>
<publisher-name><![CDATA[U.S]]></publisher-name>
</nlm-citation>
</ref>
<ref id="B6">
<label>[6]</label><nlm-citation citation-type="journal">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Kuishi]]></surname>
<given-names><![CDATA[Y.]]></given-names>
</name>
<name>
<surname><![CDATA[Liangliang]]></surname>
<given-names><![CDATA[C.]]></given-names>
</name>
<name>
<surname><![CDATA[Hu]]></surname>
<given-names><![CDATA[L.]]></given-names>
</name>
<name>
<surname><![CDATA[Yunliang]]></surname>
<given-names><![CDATA[W.]]></given-names>
</name>
</person-group>
<article-title xml:lang=""><![CDATA[Analysis of jet blast impact of embarked aircraft on deck takeoff zone]]></article-title>
<source><![CDATA[Aerospace Science and Technology]]></source>
<year>2015</year>
<volume>45</volume>
<page-range>60-6</page-range></nlm-citation>
</ref>
<ref id="B7">
<label>[7]</label><nlm-citation citation-type="journal">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Kuishi]]></surname>
<given-names><![CDATA[Y.]]></given-names>
</name>
<name>
<surname><![CDATA[Yicheng]]></surname>
<given-names><![CDATA[S.]]></given-names>
</name>
<name>
<surname><![CDATA[Hu]]></surname>
<given-names><![CDATA[L.]]></given-names>
</name>
<name>
<surname><![CDATA[Weigang]]></surname>
<given-names><![CDATA[G.]]></given-names>
</name>
</person-group>
<article-title xml:lang=""><![CDATA[Analysis of the flow of carrier-based aircraft exhaust jets impact on the flight deck]]></article-title>
<source><![CDATA[International Journal of Aeronautical and Space Sciences]]></source>
<year>2015</year>
<volume>16</volume>
<numero>1</numero>
<issue>1</issue>
<page-range>1-7</page-range></nlm-citation>
</ref>
<ref id="B8">
<label>[8]</label><nlm-citation citation-type="journal">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Fu-Dong]]></surname>
<given-names><![CDATA[G.]]></given-names>
</name>
<name>
<surname><![CDATA[De-Xin]]></surname>
<given-names><![CDATA[W.]]></given-names>
</name>
<name>
<surname><![CDATA[Hai-Dong]]></surname>
<given-names><![CDATA[W.]]></given-names>
</name>
<name>
<surname><![CDATA[Ming-Ming]]></surname>
<given-names><![CDATA[J.]]></given-names>
</name>
</person-group>
<article-title xml:lang=""><![CDATA[Numerical analysis and verification of the gas jet from aircraft engines impacting a jet blast deflector]]></article-title>
<source><![CDATA[Chinese Journal of Mechanical Engineering]]></source>
<year>2018</year>
<volume>31</volume>
<numero>86</numero>
<issue>86</issue>
<page-range>1-11</page-range></nlm-citation>
</ref>
<ref id="B9">
<label>[9]</label><nlm-citation citation-type="journal">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Song]]></surname>
<given-names><![CDATA[M.]]></given-names>
</name>
<name>
<surname><![CDATA[Jianguo]]></surname>
<given-names><![CDATA[T.]]></given-names>
</name>
<name>
<surname><![CDATA[Xiankai]]></surname>
<given-names><![CDATA[L.]]></given-names>
</name>
<name>
<surname><![CDATA[Hao]]></surname>
<given-names><![CDATA[J.]]></given-names>
</name>
</person-group>
<article-title xml:lang=""><![CDATA[The effect analysis of an engine jet on an aircraft blast deflector]]></article-title>
<source><![CDATA[Transactions of the Institute of Measurement and Control Journal of Mechanical Engineering]]></source>
<year>2018</year>
<volume>41</volume>
<numero>4</numero>
<issue>4</issue>
<page-range>990-1001</page-range></nlm-citation>
</ref>
<ref id="B10">
<label>[10]</label><nlm-citation citation-type="">
<source><![CDATA[Manual de usuario de Fluent, s.a]]></source>
<year></year>
</nlm-citation>
</ref>
<ref id="B11">
<label>[11]</label><nlm-citation citation-type="book">
<source><![CDATA[Airplane characteristics for airport planning manuals: Boeing 747-400, Boeing 777-200LR/-300ER, Airbus A340-600]]></source>
<year></year>
<publisher-name><![CDATA[McDonnell Douglas MD11, s.a]]></publisher-name>
</nlm-citation>
</ref>
<ref id="B12">
<label>[12]</label><nlm-citation citation-type="book">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Launder]]></surname>
<given-names><![CDATA[B.E.]]></given-names>
</name>
<name>
<surname><![CDATA[Spalding]]></surname>
<given-names><![CDATA[D.B.]]></given-names>
</name>
</person-group>
<source><![CDATA[Lectures in mathematical models of turbulence]]></source>
<year>1972</year>
<publisher-loc><![CDATA[London, U.K. ]]></publisher-loc>
<publisher-name><![CDATA[Academic Press]]></publisher-name>
</nlm-citation>
</ref>
<ref id="B13">
<label>[13]</label><nlm-citation citation-type="">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Sarkar]]></surname>
<given-names><![CDATA[S.]]></given-names>
</name>
<name>
<surname><![CDATA[Balakrishnan]]></surname>
<given-names><![CDATA[L.]]></given-names>
</name>
</person-group>
<source><![CDATA[Application of a Reynolds-stress turbulence model to the compressible shear layer]]></source>
<year>1990</year>
<page-range>90-18</page-range></nlm-citation>
</ref>
<ref id="B14">
<label>[14]</label><nlm-citation citation-type="book">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Baxter]]></surname>
<given-names><![CDATA[L.L.]]></given-names>
</name>
</person-group>
<source><![CDATA[Turbulent transport of particles]]></source>
<year>1989</year>
<publisher-loc><![CDATA[Provo, Utah, USA ]]></publisher-loc>
<publisher-name><![CDATA[Brigham Young University]]></publisher-name>
</nlm-citation>
</ref>
</ref-list>
</back>
</article>
