{"id":396474,"date":"2024-12-05T16:14:56","date_gmt":"2024-12-05T16:14:56","guid":{"rendered":"https:\/\/innovationspace.ansys.com\/forum\/forums\/reply\/396474\/"},"modified":"2024-12-05T16:14:56","modified_gmt":"2024-12-05T16:14:56","slug":"396474","status":"publish","type":"reply","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/reply\/396474\/","title":{"rendered":"Reply To: Different results for inlet boundary conditions."},"content":{"rendered":"<p>&lt;p&gt;When titing the geometry if you want to maintain same AOA the chord of the wing should be rotated with respect to horizintal axis. If the wing is twisted titling might make it difficult to get desired AOA. Usually velocity component approach is preferable.&nbsp;&lt;\/p&gt;<\/p>\n","protected":false},"template":"","class_list":["post-396474","reply","type-reply","status-publish","hentry"],"aioseo_notices":[],"aioseo_head":"\n\t\t<!-- All in One SEO 4.9.10 - aioseo.com -->\n\t<meta name=\"description\" content=\"When titing the geometry if you want to maintain same AOA the chord of the wing should be rotated with respect to horizintal axis. If the wing is twisted titling might make it difficult to get desired AOA. Usually velocity component approach is preferable.\" \/>\n\t<meta name=\"robots\" content=\"max-image-preview:large\" \/>\n\t<link rel=\"canonical\" href=\"https:\/\/innovationspace.ansys.com\/forum\/forums\/reply\/396474\/\" \/>\n\t<meta name=\"generator\" content=\"All in One SEO (AIOSEO) 4.9.10\" \/>\n\t\t<meta property=\"og:locale\" content=\"en_US\" \/>\n\t\t<meta property=\"og:site_name\" content=\"Ansys Learning Forum | Ansys Innovation Space\" \/>\n\t\t<meta property=\"og:type\" content=\"article\" \/>\n\t\t<meta property=\"og:title\" content=\"Reply To: Different results for inlet boundary conditions. | Ansys Learning Forum\" \/>\n\t\t<meta property=\"og:description\" content=\"When titing the geometry if you want to maintain same AOA the chord of the wing should be rotated with respect to horizintal axis. If the wing is twisted titling might make it difficult to get desired AOA. Usually velocity component approach is preferable.\" \/>\n\t\t<meta property=\"og:url\" content=\"https:\/\/innovationspace.ansys.com\/forum\/forums\/reply\/396474\/\" \/>\n\t\t<meta property=\"article:published_time\" content=\"2024-12-05T16:14:56+00:00\" \/>\n\t\t<meta property=\"article:modified_time\" content=\"2024-12-05T16:14:56+00:00\" \/>\n\t\t<meta name=\"twitter:card\" content=\"summary_large_image\" \/>\n\t\t<meta name=\"twitter:title\" content=\"Reply To: Different results for inlet boundary conditions. | Ansys Learning Forum\" \/>\n\t\t<meta name=\"twitter:description\" content=\"When titing the geometry if you want to maintain same AOA the chord of the wing should be rotated with respect to horizintal axis. If the wing is twisted titling might make it difficult to get desired AOA. Usually velocity component approach is preferable.\" \/>\n\t\t<script type=\"application\/ld+json\" class=\"aioseo-schema\">\n\t\t\t{\"@context\":\"https:\\\/\\\/schema.org\",\"@graph\":[{\"@type\":\"BreadcrumbList\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/forums\\\/reply\\\/396474\\\/#breadcrumblist\",\"itemListElement\":[{\"@type\":\"ListItem\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum#listItem\",\"position\":1,\"name\":\"Home\",\"item\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\",\"nextItem\":{\"@type\":\"ListItem\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/forums\\\/reply\\\/396474\\\/#listItem\",\"name\":\"Reply To: Different results for inlet boundary conditions.\"}},{\"@type\":\"ListItem\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/forums\\\/reply\\\/396474\\\/#listItem\",\"position\":2,\"name\":\"Reply To: Different results for inlet boundary conditions.\",\"previousItem\":{\"@type\":\"ListItem\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum#listItem\",\"name\":\"Home\"}}]},{\"@type\":\"Organization\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/#organization\",\"name\":\"Ansys Learning Forum\",\"description\":\"Ansys Innovation Space\",\"url\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/\"},{\"@type\":\"WebPage\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/forums\\\/reply\\\/396474\\\/#webpage\",\"url\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/forums\\\/reply\\\/396474\\\/\",\"name\":\"Reply To: Different results for inlet boundary conditions. | Ansys Learning Forum\",\"description\":\"When titing the geometry if you want to maintain same AOA the chord of the wing should be rotated with respect to horizintal axis. 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