{"id":43500,"date":"2021-11-29T12:00:59","date_gmt":"2021-11-29T11:00:59","guid":{"rendered":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/?p=43500"},"modified":"2021-11-28T12:25:49","modified_gmt":"2021-11-28T11:25:49","slug":"winglets-iii-la-resistencia-inducida-y-su-importancia-en-la-aerodinamica","status":"publish","type":"post","link":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/winglets-iii-la-resistencia-inducida-y-su-importancia-en-la-aerodinamica\/","title":{"rendered":"Winglets (III):  La resistencia inducida y su importancia en la aerodin\u00e1mica"},"content":{"rendered":"<p>Continuando con esta serie, hoy vamos a concluir con un t\u00f3pico que iniciamos en el art\u00edculo anterior, la resistencia inducida, y su importancia en la aerodin\u00e1mica, y porqu\u00e9 est\u00e1 ligada a los Winglets.<\/p>\n<h3><strong>Efectos de la resistencia inducida: <em>Upwash<\/em> y <em>downwash<\/em><\/strong><\/h3>\n<p>Cuando un ala se mueve a trav\u00e9s del aire, la corriente de \u00e9ste, al ir aproxim\u00e1ndose al borde de ataque, se divide en dos: una parte pasa por encima del perfil, y la otra por abajo, como ya vimos. Esta corriente que \u201csube\u201d es llamada \u201cupwash\u201d, que en espa\u00f1ol ser\u00eda como decir \u201caguas arriba\u201d. Al llegar la misma corriente al borde de fuga, el aire vuelve a cambiar de direcci\u00f3n, esta vez hacia abajo: a esta corriente de aire descendente se la llama \u201cdownwash\u201d, o \u201caguas abajo\u201d, y es la acci\u00f3n que crea la sustentaci\u00f3n, como su reacci\u00f3n.<\/p>\n<figure id=\"attachment_43504\" aria-describedby=\"caption-attachment-43504\" style=\"width: 800px\" class=\"wp-caption aligncenter\"><a href=\"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/?attachment_id=43504\" rel=\"attachment wp-att-43504\"><img data-recalc-dims=\"1\" loading=\"lazy\" decoding=\"async\" data-attachment-id=\"43504\" data-permalink=\"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/winglets-iii-la-resistencia-inducida-y-su-importancia-en-la-aerodinamica\/fig1-2\/\" data-orig-file=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig1.jpg?fit=800%2C283&amp;ssl=1\" data-orig-size=\"800,283\" data-comments-opened=\"1\" data-image-meta=\"{&quot;aperture&quot;:&quot;0&quot;,&quot;credit&quot;:&quot;&quot;,&quot;camera&quot;:&quot;&quot;,&quot;caption&quot;:&quot;&quot;,&quot;created_timestamp&quot;:&quot;0&quot;,&quot;copyright&quot;:&quot;&quot;,&quot;focal_length&quot;:&quot;0&quot;,&quot;iso&quot;:&quot;0&quot;,&quot;shutter_speed&quot;:&quot;0&quot;,&quot;title&quot;:&quot;&quot;,&quot;orientation&quot;:&quot;0&quot;}\" data-image-title=\"\" data-image-description=\"\" data-image-caption=\"&lt;p&gt;Upwash y Downwash.&lt;\/p&gt;\n\" data-large-file=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig1.jpg?fit=800%2C283&amp;ssl=1\" class=\"size-full wp-image-43504\" src=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig1.jpg?resize=800%2C283&#038;ssl=1\" alt=\"\" width=\"800\" height=\"283\" srcset=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig1.jpg?w=800&amp;ssl=1 800w, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig1.jpg?resize=300%2C106&amp;ssl=1 300w, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig1.jpg?resize=768%2C272&amp;ssl=1 768w\" sizes=\"auto, (max-width: 800px) 100vw, 800px\" \/><\/a><figcaption id=\"caption-attachment-43504\" class=\"wp-caption-text\"><em>Upwash<\/em> y <em>Downwash<\/em>.<\/figcaption><\/figure>\n<p>En resumen, el aire <em><u>cambia de direcci\u00f3n constantemente<\/u><\/em> alrededor del ala, produciendo un \u201clavado\u201d (de ah\u00ed viene la analog\u00eda de llamar a este fen\u00f3meno \u201cwash\u201d). La primera ley de Newton dice que una <em>fuerza<\/em> se produce cuando existe:<\/p>\n<ul>\n<li>Un cambio en la <em>velocidad<\/em> del cuerpo (aceleraci\u00f3n, Fuerzas \u201cG\u201d), o<\/li>\n<li>Un cambio en la <strong>direcci\u00f3n<\/strong> de movimiento del mismo.<\/li>\n<\/ul>\n<p>Como en este caso, el aire cambia de <em>direcci\u00f3n<\/em>, sobre esa porci\u00f3n de aire aparecer\u00e1n fuerzas sobre esta masa, y a su vez las transmitir\u00e1 a su entorno (el ala); a su vez, la tercera ley de Newton dice que hay una fuerza igual y opuesta (reacci\u00f3n), y es la que se ejercer\u00e1 en el ala. Esa es una descripci\u00f3n b\u00e1sica de la <strong>sustentaci\u00f3n<\/strong>. La diferencia de presi\u00f3n (fuerza por unidad de \u00e1rea) a trav\u00e9s del ala es el mecanismo por el cual la sustentaci\u00f3n se transfiere al ala debido al cambio de direcci\u00f3n del aire.<\/p>\n<p>Estos dos efectos, son particularmente importantes en los bordes de las alas, es decir, en las puntas y en el borde de fuga, porque la estela de v\u00f3rtices creada en los extremos de las alas, genera un <em>downwash<\/em> en la parte interior de la envergadura, y un <em>upwash<\/em> en la parte exterior de las mismas.<\/p>\n<figure id=\"attachment_43505\" aria-describedby=\"caption-attachment-43505\" style=\"width: 800px\" class=\"wp-caption aligncenter\"><a href=\"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/?attachment_id=43505\" rel=\"attachment wp-att-43505\"><img data-recalc-dims=\"1\" loading=\"lazy\" decoding=\"async\" data-attachment-id=\"43505\" data-permalink=\"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/winglets-iii-la-resistencia-inducida-y-su-importancia-en-la-aerodinamica\/fig2-2\/\" data-orig-file=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig2.jpg?fit=800%2C627&amp;ssl=1\" data-orig-size=\"800,627\" data-comments-opened=\"1\" data-image-meta=\"{&quot;aperture&quot;:&quot;0&quot;,&quot;credit&quot;:&quot;&quot;,&quot;camera&quot;:&quot;&quot;,&quot;caption&quot;:&quot;&quot;,&quot;created_timestamp&quot;:&quot;0&quot;,&quot;copyright&quot;:&quot;&quot;,&quot;focal_length&quot;:&quot;0&quot;,&quot;iso&quot;:&quot;0&quot;,&quot;shutter_speed&quot;:&quot;0&quot;,&quot;title&quot;:&quot;&quot;,&quot;orientation&quot;:&quot;0&quot;}\" data-image-title=\"\" data-image-description=\"\" data-image-caption=\"&lt;p&gt;Upwash y downwash en los extremos de las alas. (Fuente: ResearchGate (2015). Wingtip vortices cause downwash which reduces the effective angle of attack (Imagen: Researchgate.net).&lt;\/p&gt;\n\" data-large-file=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig2.jpg?fit=800%2C627&amp;ssl=1\" class=\"wp-image-43505 size-full\" src=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig2.jpg?resize=800%2C627&#038;ssl=1\" alt=\"\" width=\"800\" height=\"627\" srcset=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig2.jpg?w=800&amp;ssl=1 800w, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig2.jpg?resize=300%2C235&amp;ssl=1 300w, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig2.jpg?resize=768%2C602&amp;ssl=1 768w\" sizes=\"auto, (max-width: 800px) 100vw, 800px\" \/><\/a><figcaption id=\"caption-attachment-43505\" class=\"wp-caption-text\">Upwash y downwash en los extremos de las alas. (Fuente: <a href=\"https:\/\/www.researchgate.net\/figure\/Wingtip-vortices-cause-downwash-which-reduces-the-effective-angle-of-attack-1_fig1_309476028\" target=\"_blank\" rel=\"noopener\">Researchgate.net<\/a>).<\/figcaption><\/figure>\n<p>Estas estelas vorticosas as\u00ed formadas, generan importantes consecuencias:<\/p>\n<ul>\n<li>Al igual que los frentes de ondas de agua al pasar un barco, que provocan olas laterales, estas estelas generan aire turbulento que persiste incluso despu\u00e9s de haber pasado la aeronave, y las aeronaves circundantes deben tomar distancia prudente para no caer dentro de estos v\u00f3rtices, y perder el control. Esto es muy com\u00fan en despegues y aterrizajes en aeropuertos, donde hay un tiempo espec\u00edfico entre cada aeronave para prevenir incidentes o accidentes.<\/li>\n<li>Como se mencion\u00f3 al principio, estas estelas son \u201carrastradas\u201d como cadenas por la aeronave en su paso, es decir, quedan vinculadas a la misma, <strong>por lo que la aeronave debe incrementar su potencia para vencer esta resistencia extra<\/strong>.<\/li>\n<li><u>La sustentaci\u00f3n tambi\u00e9n se ve afectada<\/u>: la resistencia inducida que provocan estos v\u00f3rtices en las puntas de las alas reducen la sustentaci\u00f3n de la aeronave, por el \u201cbarrido\u201d sobre el extrad\u00f3s que provoca el downwash en las puntas de las alas.<\/li>\n<\/ul>\n<h3><strong>Envergadura \u201cefectiva\u201d y \u201cGeom\u00e9trica<\/strong>\u201d.<\/h3>\n<p>Como se mencion\u00f3 en el \u00faltimo punto del p\u00e1rrafo anterior, el downwash provocado por los v\u00f3rtices de punta de ala provocan un soplado de la capa l\u00edmite sobre esa porci\u00f3n del extrad\u00f3s, haciendo que la sustentaci\u00f3n en esa \u00e1rea se vea afectada. Esto hace que la envergadura <em>geom\u00e9trica<\/em> (la que medimos con una cinta m\u00e9trica) sea muy distinta de la envergadura <em>efectiva<\/em> (la envergadura donde hay sustentaci\u00f3n \u00fatil). Es decir, con un ala de una cierta envergadura (geom\u00e9trica), la sustentaci\u00f3n que obtengamos ser\u00e1 mucho <em>menor<\/em> en la realidad que la calculada en teor\u00eda: esto es debido a la reducci\u00f3n provocada por el downwash a ambos extremos de las alas, que \u201crecorta\u201d la sustentaci\u00f3n, haciendo el efecto como si el ala fuera m\u00e1s corta. Esto provoca que, cuando se dise\u00f1a un ala para una aeronave, se debe prever un incremento extra en la envergadura, para luego obtener la sustentaci\u00f3n deseada en la teor\u00eda, caso contrario el ala no sustentar\u00eda lo suficiente.<\/p>\n<p>En la siguiente imagen\u00a0se muestra la diferencia entre la envergadura geom\u00e9trica y efectiva, debida al downwash:<\/p>\n<figure id=\"attachment_43507\" aria-describedby=\"caption-attachment-43507\" style=\"width: 773px\" class=\"wp-caption aligncenter\"><a href=\"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/?attachment_id=43507\" rel=\"attachment wp-att-43507\"><img data-recalc-dims=\"1\" loading=\"lazy\" decoding=\"async\" data-attachment-id=\"43507\" data-permalink=\"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/winglets-iii-la-resistencia-inducida-y-su-importancia-en-la-aerodinamica\/fig3-2\/\" data-orig-file=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig3.jpg?fit=773%2C326&amp;ssl=1\" data-orig-size=\"773,326\" data-comments-opened=\"1\" data-image-meta=\"{&quot;aperture&quot;:&quot;0&quot;,&quot;credit&quot;:&quot;&quot;,&quot;camera&quot;:&quot;&quot;,&quot;caption&quot;:&quot;&quot;,&quot;created_timestamp&quot;:&quot;0&quot;,&quot;copyright&quot;:&quot;&quot;,&quot;focal_length&quot;:&quot;0&quot;,&quot;iso&quot;:&quot;0&quot;,&quot;shutter_speed&quot;:&quot;0&quot;,&quot;title&quot;:&quot;&quot;,&quot;orientation&quot;:&quot;0&quot;}\" data-image-title=\"\" data-image-description=\"\" data-image-caption=\"&lt;p&gt;El downwash provoca un soplado de la capa limite en el extrad\u00f3s, disminuyendo la sustentaci\u00f3n, creando el efecto de un ala m\u00e1s corta.&lt;\/p&gt;\n\" data-large-file=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig3.jpg?fit=773%2C326&amp;ssl=1\" class=\"size-full wp-image-43507\" src=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig3.jpg?resize=773%2C326&#038;ssl=1\" alt=\"\" width=\"773\" height=\"326\" srcset=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig3.jpg?w=773&amp;ssl=1 773w, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig3.jpg?resize=300%2C127&amp;ssl=1 300w, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig3.jpg?resize=768%2C324&amp;ssl=1 768w\" sizes=\"auto, (max-width: 773px) 100vw, 773px\" \/><\/a><figcaption id=\"caption-attachment-43507\" class=\"wp-caption-text\">El downwash provoca un soplado de la capa limite en el extrad\u00f3s, disminuyendo la sustentaci\u00f3n, creando el efecto de un ala m\u00e1s corta.<\/figcaption><\/figure>\n<p>Debajo se muestra una gr\u00e1fica en donde se ven los resultados experimentales de un ala sin y con Winglets:<\/p>\n<figure id=\"attachment_43508\" aria-describedby=\"caption-attachment-43508\" style=\"width: 800px\" class=\"wp-caption aligncenter\"><a href=\"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/?attachment_id=43508\" rel=\"attachment wp-att-43508\"><img data-recalc-dims=\"1\" loading=\"lazy\" decoding=\"async\" data-attachment-id=\"43508\" data-permalink=\"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/winglets-iii-la-resistencia-inducida-y-su-importancia-en-la-aerodinamica\/fig4\/\" data-orig-file=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig4.jpg?fit=800%2C491&amp;ssl=1\" data-orig-size=\"800,491\" data-comments-opened=\"1\" data-image-meta=\"{&quot;aperture&quot;:&quot;0&quot;,&quot;credit&quot;:&quot;&quot;,&quot;camera&quot;:&quot;&quot;,&quot;caption&quot;:&quot;&quot;,&quot;created_timestamp&quot;:&quot;0&quot;,&quot;copyright&quot;:&quot;&quot;,&quot;focal_length&quot;:&quot;0&quot;,&quot;iso&quot;:&quot;0&quot;,&quot;shutter_speed&quot;:&quot;0&quot;,&quot;title&quot;:&quot;&quot;,&quot;orientation&quot;:&quot;0&quot;}\" data-image-title=\"\" data-image-description=\"\" data-image-caption=\"&lt;p&gt;Distribuci\u00f3n de sustentaci\u00f3n en una semiala con y sin Winglets. La zona sombreada en celeste es la sustentaci\u00f3n ganada gracias al agregado de Winglets \/ Sharklets.&lt;\/p&gt;\n\" data-large-file=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig4.jpg?fit=800%2C491&amp;ssl=1\" class=\"size-full wp-image-43508\" src=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig4.jpg?resize=800%2C491&#038;ssl=1\" alt=\"\" width=\"800\" height=\"491\" srcset=\"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig4.jpg?w=800&amp;ssl=1 800w, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig4.jpg?resize=300%2C184&amp;ssl=1 300w, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2021\/11\/fig4.jpg?resize=768%2C471&amp;ssl=1 768w\" sizes=\"auto, (max-width: 800px) 100vw, 800px\" \/><\/a><figcaption id=\"caption-attachment-43508\" class=\"wp-caption-text\">Distribuci\u00f3n de sustentaci\u00f3n en una semiala con y sin Winglets. La zona sombreada en celeste es la sustentaci\u00f3n ganada gracias al agregado de Winglets \/ Sharklets.<\/figcaption><\/figure>\n<p>En el pr\u00f3ximo art\u00edculo, veremos otro tema que seguro usted se lo habr\u00e1 preguntado muchas veces: \u00bfPor qu\u00e9 se forman esas estelas vorticosas, (conocidas como \u201ctrailing vortex\u201d)?<\/p>\n<hr \/>\n<p>&nbsp;<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Continuando con esta serie, hoy vamos a concluir con un t\u00f3pico que iniciamos en el art\u00edculo anterior, la resistencia inducida, y su importancia en la aerodin\u00e1mica, y porqu\u00e9 est\u00e1 ligada a los Winglets.<\/p>\n","protected":false},"author":91,"featured_media":43502,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"_jetpack_newsletter_access":"","_jetpack_dont_email_post_to_subs":false,"_jetpack_newsletter_tier_id":0,"_jetpack_memberships_contains_paywalled_content":false,"_jetpack_memberships_contains_paid_content":false,"footnotes":"","jetpack_post_was_ever_published":false},"categories":[5],"tags":[644],"class_list":["post-43500","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-general","tag-winglets"],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v27.7 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>Winglets (III): La resistencia inducida y su importancia en la aerodin\u00e1mica - Gaceta Aeronautica<\/title>\n<meta name=\"description\" content=\"La resistencia inducida, y su importancia en la aerodin\u00e1mica, y porqu\u00e9 est\u00e1 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Continuamos comprendiendo su evoluci\u00f3n hist\u00f3rica y t\u00e9cnica. 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Tambi\u00e9n veremos una breve historia de c\u00f3mo los Winglets cruzaron el atl\u00e1ntico, y en Europa se transformaron\u2026","rel":"","context":"En \u00abAviaci\u00f3n general\u00bb","block_context":{"text":"Aviaci\u00f3n general","link":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/category\/general\/"},"img":{"alt_text":"","src":"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/11\/winglets11-2.jpg?fit=1024%2C683&ssl=1&resize=350%2C200","width":350,"height":200,"srcset":"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/11\/winglets11-2.jpg?fit=1024%2C683&ssl=1&resize=350%2C200 1x, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/11\/winglets11-2.jpg?fit=1024%2C683&ssl=1&resize=525%2C300 1.5x, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/11\/winglets11-2.jpg?fit=1024%2C683&ssl=1&resize=700%2C400 2x"},"classes":[]},{"id":48475,"url":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/winglets-xii-raked-wingtips-la-competencia-continua\/","url_meta":{"origin":43500,"position":2},"title":"Winglets (XII): \u201cRaked Wingtips\u201d, la competencia contin\u00faa&#8230;","author":"Pedro Alejandro Wikarczuk","date":"09\/01\/2023","format":false,"excerpt":"En este art\u00edculo exploraremos otras soluciones al problema de la resistencia inducida, que al ir los Winglets \/ Sharklets populariz\u00e1ndose y expandi\u00e9ndose a aeronaves de mayor porte, requirieron nuevas soluciones en la aviaci\u00f3n comercial.","rel":"","context":"En \u00abAviaci\u00f3n general\u00bb","block_context":{"text":"Aviaci\u00f3n general","link":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/category\/general\/"},"img":{"alt_text":"winglets","src":"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2023\/01\/winglets12-6.jpg?fit=1024%2C683&ssl=1&resize=350%2C200","width":350,"height":200,"srcset":"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2023\/01\/winglets12-6.jpg?fit=1024%2C683&ssl=1&resize=350%2C200 1x, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2023\/01\/winglets12-6.jpg?fit=1024%2C683&ssl=1&resize=525%2C300 1.5x, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2023\/01\/winglets12-6.jpg?fit=1024%2C683&ssl=1&resize=700%2C400 2x"},"classes":[]},{"id":45626,"url":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/winglets-ix-mejoras-en-la-performance\/","url_meta":{"origin":43500,"position":3},"title":"Winglets (IX): Mejoras en la performance","author":"Pedro Alejandro Wikarczuk","date":"23\/06\/2022","format":false,"excerpt":"Ya vimos en el cap\u00edtulo anterior el nacimiento y la r\u00e1pida aceptaci\u00f3n de los Winglets, gracias al talento creador de su inventor, Richard T. Whitcomb. Hoy veremos por qu\u00e9 se difundieron con tanta rapidez en la aviaci\u00f3n comercial, y fueron bien recibidos.","rel":"","context":"En \u00abAviaci\u00f3n general\u00bb","block_context":{"text":"Aviaci\u00f3n general","link":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/category\/general\/"},"img":{"alt_text":"","src":"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/06\/winglets9-1.jpg?fit=800%2C469&ssl=1&resize=350%2C200","width":350,"height":200,"srcset":"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/06\/winglets9-1.jpg?fit=800%2C469&ssl=1&resize=350%2C200 1x, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/06\/winglets9-1.jpg?fit=800%2C469&ssl=1&resize=525%2C300 1.5x, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/06\/winglets9-1.jpg?fit=800%2C469&ssl=1&resize=700%2C400 2x"},"classes":[]},{"id":45133,"url":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/winglets-viii-como-nacieron-y-porque\/","url_meta":{"origin":43500,"position":4},"title":"Winglets (VIII): C\u00f3mo nacieron y porqu\u00e9","author":"Pedro Alejandro Wikarczuk","date":"02\/05\/2022","format":false,"excerpt":"En este nuevo cap\u00edtulo de la serie, vamos a ver como nacieron, y porque, los ya conocidos \u201cWinglets\u201d. Todo comenz\u00f3 con la necesidad de ahorrar combustible y energ\u00eda, obligada por la crisis del petr\u00f3leo de 1973, y el aporte de un talentoso Ingeniero llamado Richard Travis Whitcomb, quien fue el\u2026","rel":"","context":"En \u00abAviaci\u00f3n general\u00bb","block_context":{"text":"Aviaci\u00f3n general","link":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/category\/general\/"},"img":{"alt_text":"","src":"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/05\/foto2.jpg?fit=800%2C481&ssl=1&resize=350%2C200","width":350,"height":200,"srcset":"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/05\/foto2.jpg?fit=800%2C481&ssl=1&resize=350%2C200 1x, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/05\/foto2.jpg?fit=800%2C481&ssl=1&resize=525%2C300 1.5x, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/05\/foto2.jpg?fit=800%2C481&ssl=1&resize=700%2C400 2x"},"classes":[]},{"id":46893,"url":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/winglets-x-el-diseno-de-whitcomb-y-sus-variantes\/","url_meta":{"origin":43500,"position":5},"title":"Winglets (X): El dise\u00f1o de Whitcomb y sus variantes","author":"Pedro Alejandro Wikarczuk","date":"29\/08\/2022","format":false,"excerpt":"En el art\u00edculo anterior se expusieron las ventajas del uso de los Winglets, y el porqu\u00e9 de su r\u00e1pida difusi\u00f3n y popularidad en el mundo de la aviaci\u00f3n comercial. Hoy veremos que, adem\u00e1s del dise\u00f1o original presentado por Whitcomb, las distintas empresas constructoras comenzaron una febril competencia por la mejora\u2026","rel":"","context":"En \u00abAviaci\u00f3n general\u00bb","block_context":{"text":"Aviaci\u00f3n general","link":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/category\/general\/"},"img":{"alt_text":"","src":"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/08\/winglets10-5.jpg?fit=1024%2C707&ssl=1&resize=350%2C200","width":350,"height":200,"srcset":"https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/08\/winglets10-5.jpg?fit=1024%2C707&ssl=1&resize=350%2C200 1x, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/08\/winglets10-5.jpg?fit=1024%2C707&ssl=1&resize=525%2C300 1.5x, https:\/\/i0.wp.com\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-content\/uploads\/2022\/08\/winglets10-5.jpg?fit=1024%2C707&ssl=1&resize=700%2C400 2x"},"classes":[]}],"jetpack_likes_enabled":true,"jetpack_sharing_enabled":true,"jetpack_shortlink":"https:\/\/wp.me\/p1P39s-bjC","_links":{"self":[{"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/posts\/43500","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/users\/91"}],"replies":[{"embeddable":true,"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/comments?post=43500"}],"version-history":[{"count":4,"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/posts\/43500\/revisions"}],"predecessor-version":[{"id":43509,"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/posts\/43500\/revisions\/43509"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/media\/43502"}],"wp:attachment":[{"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/media?parent=43500"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/categories?post=43500"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.gacetaeronautica.com\/gaceta\/wp-101\/wp-json\/wp\/v2\/tags?post=43500"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}