{"id":67712,"date":"2018-03-09T22:56:10","date_gmt":"2018-03-09T22:56:10","guid":{"rendered":"https:\/\/www.deberes.net\/tesis\/sin-categoria\/bala%c2%adstica-externa-de-cohete-sonda-considerando-los-fenomenos-de-interferencia-aerodinamica\/"},"modified":"2018-03-09T22:56:10","modified_gmt":"2018-03-09T22:56:10","slug":"bala%c2%adstica-externa-de-cohete-sonda-considerando-los-fenomenos-de-interferencia-aerodinamica","status":"publish","type":"post","link":"https:\/\/www.deberes.net\/tesis\/mecanica-de-fluidos\/bala%c2%adstica-externa-de-cohete-sonda-considerando-los-fenomenos-de-interferencia-aerodinamica\/","title":{"rendered":"Bal\u00edstica externa de cohete sonda considerando los fen\u00f3menos de interferencia aerodin\u00e1mica"},"content":{"rendered":"<h2>Tesis doctoral de <strong> Jony Oliver Lazo Ramos <\/strong><\/h2>\n<p>El desarrollo de un cohete sonda involucra varios aspectos como son: &#8211;\tel sistema de propulsi\u00f3n, &#8211;\tla estructura &#8211;\tla aerodin\u00e1mica y bal\u00edstica del cohete. &#8211;\tla instrumentaci\u00f3n cient\u00edfica entonces el objetivo general planteado en el presente trabajo es desarrollar un programa y un modelo matem\u00e1tico para el c\u00e1lculo de la aerodin\u00e1mica y de la bal\u00edstica que nos permita dise\u00f1ar la configuraci\u00f3n externa de un cohete sonda que tenga un buen comportamiento en vuelo y adem\u00e1s nos permita predecir de forma exacta su trayectoria el primer objetivo es desarrollar un modelo matem\u00e1tico integral para el c\u00e1lculo de los coeficientes aerodin\u00e1micos que tome cuenta la gran variedad de factores de los cuales estos dependen y que se presentan durante el vuelo del cohete sonda. El conocimiento de estos coeficientes nos permitir\u00e1: 1.-Garantizar un buen comportamiento del veh\u00edculo en el aire. 2.-Tener una base completa de datos para su uso durante el c\u00e1lculo de la bal\u00edstica externa. El segundo objetivo es la predicci\u00f3n de la trayectoria de vuelo del veh\u00edculo con un enfoque nuevo que es el uso de la base de datos en forma de matrices en 2d y 3d. Esto nos permitir\u00e1 obtener resultados con exactitud superior a los m\u00e9todos actuales, ya que estos utilizan durante el c\u00f3mputo de la trayectoria datos en forma de tablas \u00f3 de ecuaciones que var\u00edan en funci\u00f3n a una sola variable ya sea la velocidad, de la altura \u00f3 del tiempo. Este grado de precisi\u00f3n ira aumentando a medida que los valores de los intervalos tiempo, as\u00ed como intervalos de altitud en el programa desarrollado se vayan haciendo cada vez m\u00e1s peque\u00f1os.<\/p>\n<p>&nbsp;<\/p>\n<h3>Datos acad\u00e9micos de la tesis doctoral \u00ab<strong>Bal\u00edstica externa de cohete sonda considerando los fen\u00f3menos de interferencia aerodin\u00e1mica<\/strong>\u00ab<\/h3>\n<ul>\n<li><strong>T\u00edtulo de la tesis:<\/strong>\u00a0 Bal\u00edstica externa de cohete sonda considerando los fen\u00f3menos de interferencia aerodin\u00e1mica <\/li>\n<li><strong>Autor:<\/strong>\u00a0 Jony Oliver Lazo Ramos <\/li>\n<li><strong>Universidad:<\/strong>\u00a0 Polit\u00e9cnica de Madrid<\/li>\n<li><strong>Fecha de lectura de la tesis:<\/strong>\u00a0 30\/10\/2008<\/li>\n<\/ul>\n<p>&nbsp;<\/p>\n<h3>Direcci\u00f3n y tribunal<\/h3>\n<ul>\n<li><strong>Director de la tesis<\/strong>\n<ul>\n<li>Vassili Samsonov<\/li>\n<\/ul>\n<\/li>\n<li><strong>Tribunal<\/strong>\n<ul>\n<li>Presidente del tribunal: Antonio Vizan idoipe <\/li>\n<li>julio Hernandez rodriguez (vocal)<\/li>\n<li>Luis Antonio Lastra espinoza (vocal)<\/li>\n<li>rodrigo Martinez val pe\u00f1alosa (vocal)<\/li>\n<\/ul>\n<\/li>\n<\/ul>\n<p>&nbsp;<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Tesis doctoral de Jony Oliver Lazo Ramos El desarrollo de un cohete sonda involucra varios aspectos como son: &#8211; el [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"site-sidebar-layout":"default","site-content-layout":"","ast-site-content-layout":"","site-content-style":"default","site-sidebar-style":"default","ast-global-header-display":"","ast-banner-title-visibility":"","ast-main-header-display":"","ast-hfb-above-header-display":"","ast-hfb-below-header-display":"","ast-hfb-mobile-header-display":"","site-post-title":"","ast-breadcrumbs-content":"","ast-featured-img":"","footer-sml-layout":"","theme-transparent-header-meta":"","adv-header-id-meta":"","stick-header-meta":"","header-above-stick-meta":"","header-main-stick-meta":"","header-below-stick-meta":"","astra-migrate-meta-layouts":"default","ast-page-background-enabled":"default","ast-page-background-meta":{"desktop":{"background-color":"var(--ast-global-color-4)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-gradient":""},"tablet":{"background-color":"","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-gradient":""},"mobile":{"background-color":"","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-gradient":""}},"ast-content-background-meta":{"desktop":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-gradient":""},"tablet":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-gradient":""},"mobile":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-gradient":""}},"footnotes":""},"categories":[51119,1192,16008],"tags":[39131,148863,9028,148865,16369,148864],"class_list":["post-67712","post","type-post","status-publish","format-standard","hentry","category-aerodinamica","category-mecanica-de-fluidos","category-politecnica-de-madrid","tag-antonio-vizan-idoipe","tag-jony-oliver-lazo-ramos","tag-julio-hernandez-rodriguez","tag-luis-antonio-lastra-espinoza","tag-rodrigo-Martinez-val-penalosa","tag-vassili-samsonov"],"_links":{"self":[{"href":"https:\/\/www.deberes.net\/tesis\/wp-json\/wp\/v2\/posts\/67712","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.deberes.net\/tesis\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/www.deberes.net\/tesis\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/www.deberes.net\/tesis\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/www.deberes.net\/tesis\/wp-json\/wp\/v2\/comments?post=67712"}],"version-history":[{"count":0,"href":"https:\/\/www.deberes.net\/tesis\/wp-json\/wp\/v2\/posts\/67712\/revisions"}],"wp:attachment":[{"href":"https:\/\/www.deberes.net\/tesis\/wp-json\/wp\/v2\/media?parent=67712"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.deberes.net\/tesis\/wp-json\/wp\/v2\/categories?post=67712"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.deberes.net\/tesis\/wp-json\/wp\/v2\/tags?post=67712"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}