{"id":74279,"date":"2005-02-06T00:00:00","date_gmt":"2005-02-06T00:00:00","guid":{"rendered":"https:\/\/www.deberes.net\/tesis\/sin-categoria\/comportamiento-aerodinamico-de-sondas-atmosfericas-en-entornos-aeroportuarios\/"},"modified":"2005-02-06T00:00:00","modified_gmt":"2005-02-06T00:00:00","slug":"comportamiento-aerodinamico-de-sondas-atmosfericas-en-entornos-aeroportuarios","status":"publish","type":"post","link":"https:\/\/www.deberes.net\/tesis\/ciencias-tecnologicas\/comportamiento-aerodinamico-de-sondas-atmosfericas-en-entornos-aeroportuarios\/","title":{"rendered":"Comportamiento aerodinamico de sondas atmosfericas en entornos aeroportuarios"},"content":{"rendered":"<h2>Tesis doctoral de <strong>  Nadal Mora Vicente Javier <\/strong><\/h2>\n<p>El objetivo del trabajo es el estudio del comportamiento aerodin\u00e1mico de un tipo de sondas basadas en el concepto de pararrotor, para su empleo en la exploraci\u00f3n y medici\u00f3n de caracter\u00edsticas de la atm\u00f3sfera en entornos aeroportuarias. Se espera que las caracter\u00edsticas de este tipo de sondas permitan controlar su ca\u00edda en una forma m\u00e1s precisa que las basadas en paraca\u00eddas y puedan formar parte de un sistema meteorol\u00f3gico de terminal integrado (ver apartado 1.3.4).  el pararrotor es un decelerador aerodin\u00e1mico (frena la ca\u00edda de cuerpos en la atm\u00f3sfera), que vuela en r\u00e9gimen de autorrotaci\u00f3n. Aunque el r\u00e9gimen de autorrotaci\u00f3n es ampliamente conocido (y, sin embargo, contin\u00faa siendo objeto de investigaci\u00f3n) por su aplicaci\u00f3n al caso de las aeronaves de ala giratoria (p.E., Los helic\u00f3pteros), el problema estudiado aqu\u00ed se diferencia fundamentalmente del estudio cl\u00e1sico en el alargamiento de las palas, siendo en el presente caso de alargamiento peque\u00f1o (de orden de la unidad), por lo que son aplicables los conceptos desarrollados en el caso de helic\u00f3pteros. el alargamiento es peque\u00f1o por razones de almacenamiento para su transporte: las palas deben ir plegada sobre el cuerpo de la sonda, que suele ser cil\u00edndrico, y cuya altura est\u00e1 limitada por razones de estabilidad girosc\u00f3pica.  el desarrollo te\u00f3rico comienza con la elaboraci\u00f3n de un modelo de la acci\u00f3n de las fuerzas aerodin\u00e1micas sobre el movimiento del cuerpo en rotaci\u00f3n alrededor de un eje fijo, basado en aspectos de la teor\u00eda de cantidad de movimiento y la teor\u00eda de alas esbeltas. Este modelo permite predecir la variaci\u00f3n en el \u00e1ngulo de incidencia del flujo de la velocidad tangencial dimensional, la velocidad de la corriente adimensinal, el \u00e1ngulo de paso, el par\u00e1metro adimensional de relaci\u00f3n de velocidades y el \u00e1ngulo de ataque, para diferentes caracter\u00edsticas aerodin\u00e1micas de las palas. El modelo permite identificar los factores de los<\/p>\n<p>&nbsp;<\/p>\n<h3>Datos acad\u00e9micos de la tesis doctoral \u00ab<strong>Comportamiento aerodinamico de sondas atmosfericas en entornos aeroportuarios<\/strong>\u00ab<\/h3>\n<ul>\n<li><strong>T\u00edtulo de la tesis:<\/strong>\u00a0 Comportamiento aerodinamico de sondas atmosfericas en entornos aeroportuarios <\/li>\n<li><strong>Autor:<\/strong>\u00a0  Nadal Mora Vicente Javier <\/li>\n<li><strong>Universidad:<\/strong>\u00a0 Polit\u00e9cnica de Madrid<\/li>\n<li><strong>Fecha de lectura de la tesis:<\/strong>\u00a0 02\/06\/2005<\/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>Angel Sanz Andres<\/li>\n<\/ul>\n<\/li>\n<li><strong>Tribunal<\/strong>\n<ul>\n<li>Presidente del tribunal: rafael Sanjurjo navarro <\/li>\n<li>anibal Isidoro carmona (vocal)<\/li>\n<li>Jos\u00e9 Meseguer ruiz (vocal)<\/li>\n<li>dami\u00e1n Rivas rivas (vocal)<\/li>\n<\/ul>\n<\/li>\n<\/ul>\n<p>&nbsp;<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Tesis doctoral de Nadal Mora Vicente Javier El objetivo del trabajo es el estudio del comportamiento aerodin\u00e1mico de un tipo [&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 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