{"id":160122,"date":"2022-09-26T10:00:32","date_gmt":"2022-09-26T10:00:32","guid":{"rendered":"\/knowledge\/forums\/topic\/discovery-aim-tutorial-modal-analysis-of-a-wing\/"},"modified":"2023-08-16T06:33:33","modified_gmt":"2023-08-16T06:33:33","slug":"discovery-aim-tutorial-modal-analysis-of-a-wing","status":"publish","type":"topic","link":"https:\/\/innovationspace.ansys.com\/knowledge\/forums\/topic\/discovery-aim-tutorial-modal-analysis-of-a-wing\/","title":{"rendered":"Discovery AIM tutorial &#8211; Modal Analysis of a Wing"},"content":{"rendered":"<p><strong>This example is taken from\u00a0<u><a href=\"https:\/\/confluence.cornell.edu\/display\/SIMULATION\/ANSYS+AIM+-+Modal+Analysis+of+a+Wing\" target=\"_blank\" rel=\"nofollow noopener noreferrer\">Cornell University&#8217;s ANSYS AIM Learning Modules<\/a><\/u><\/strong><\/p>\n<hr \/>\n<nav class=\"toc -selected\">Contents<\/p>\n<ol class=\"toc__section -lev0\">\n<li class=\"toc__item -lev0\">Problem Specification<\/li>\n<li class=\"toc__item -lev0\">Geometry<\/li>\n<li class=\"toc__item -lev0\">Mesh<\/li>\n<li class=\"toc__item -lev0\">Physics Setup<\/li>\n<li class=\"toc__item -lev0\">Results Evaluation<\/li>\n<li class=\"toc__item -lev0\">Verification &amp; Validation<\/li>\n<\/ol>\n<\/nav>\n<h4 content_id=\"problem-specification\" class=\"toc__permalink\" content_id=\"problem-specification\" class=\"toc__permalink\"  id=\"PROBLEM-SPECIFICATION\">Problem Specification<\/h4>\n<p>A wing with a NACA 0012 airfoil section is supported such that one end is fixed and the other end is free. The wing has a chord of 1 meter, a span of 5 meters, and a thickness of 0.01 meters. The wing is Aluminum 6061-T6. Find the first 6 modes of vibration of the airfoil using ANSYS AIM.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignnone size-full wp-image-156981\" src=\"\/knowledge\/wp-content\/uploads\/sites\/4\/2022\/08\/HM-5.png\" alt=\" width=\"805\" height=\"415\" \/><\/p>\n<hr \/>\n<h4 content_id=\"geometry\" class=\"toc__permalink\" content_id=\"geometry\" class=\"toc__permalink\"  id=\"GEOMETRY\">Geometry<\/h4>\n<p>In this video, you will learn how to:<\/p>\n<ul>\n<li>Import the geometry in Discovery AIM<\/li>\n<li>Specify thickness of the wing surface to be 0.01m<\/li>\n<\/ul>\n<p><iframe loading=\"lazy\" class=\"vidyard_iframe\" src=\"\/\/play.vidyard.com\/uT7HvSRMGB1UUveBqniSSM.html?\" width=\"700\" height=\"400\" frameborder=\"0\" scrolling=\"no\" allowfullscreen=\"allowfullscreen\"><\/iframe><\/p>\n<hr \/>\n<h4 content_id=\"mesh\" class=\"toc__permalink\" content_id=\"mesh\" class=\"toc__permalink\"  id=\"MESH\"><strong>Mesh<\/strong><\/h4>\n<p>In this tutorial, we will be using\u00a0<strong>Physics-Aware Meshing<\/strong>. Physics-aware meshing helps automate and simplify your problem setup. With physics-aware meshing, the computational mesh is generated automatically based on the solution fidelity setting and the physics inputs.<\/p>\n<hr \/>\n<h4 content_id=\"physics-setup\" class=\"toc__permalink\" content_id=\"physics-setup\" class=\"toc__permalink\"  id=\"PHYSICS-SETUP\">Physics Setup<\/h4>\n<p>In this video, you will learn how to:<\/p>\n<ul>\n<li>Change the material of the wing to a new material with the name Aluminum 6061-T6<\/li>\n<li>Add a density property of 2700 kg\/m^3<\/li>\n<li>Add an Isotropic Elasticity property, with Young&#8217;s Modulus = 1e7 psi and Poisson&#8217;s ratio = 0.33<\/li>\n<li>Add a fixed support on two edges of the wing&#8217;s end<\/li>\n<\/ul>\n<p><iframe loading=\"lazy\" class=\"vidyard_iframe\" src=\"\/\/play.vidyard.com\/yRPbV8NTA7ryCnUq5KpDL5.html?\" width=\"700\" height=\"400\" frameborder=\"0\" scrolling=\"no\" allowfullscreen=\"allowfullscreen\"><\/iframe><\/p>\n<hr \/>\n<h4 content_id=\"results-evaluation\" class=\"toc__permalink\" content_id=\"results-evaluation\" class=\"toc__permalink\"  id=\"RESULTS-EVALUATION\">Results Evaluation<\/h4>\n<p>In this video\u00a0you will learn how to:<\/p>\n<ul>\n<li>View Displacement Magnitude contours for each mode<\/li>\n<li>Look at the calculated modal frequencies<\/li>\n<li>Refine the mesh and investigate any change in modal frequencies<\/li>\n<\/ul>\n<p><iframe loading=\"lazy\" class=\"vidyard_iframe\" src=\"\/\/play.vidyard.com\/k3Wtzxyow6ErzKBuCiBq5p.html?\" width=\"700\" height=\"400\" frameborder=\"0\" scrolling=\"no\" allowfullscreen=\"allowfullscreen\"><\/iframe><\/p>\n<hr \/>\n<h4 content_id=\"verification-amp-validation\" class=\"toc__permalink\" content_id=\"verification-amp-validation\" class=\"toc__permalink\"  id=\"VERIFICATION-VALIDATION\">Verification &amp; Validation<\/h4>\n<p>One of the ways we can check the validity of our analysis is by refining our mesh. If the values for our frequencies approach a limit, then we have arrived at our answer. If the values change drastically when we refine the mesh, then we need to refine the mesh further and we have not yet found an acceptable solution. We will refine the mesh by increasing the Mesh resolution, as in the Numerical Results video. \u00a0The table below shows the results from the video. \u00a0Since the frequencies do not change, we do not have the refine the mesh further.<\/p>\n<table>\n<tbody>\n<tr>\n<td><strong>Mode<\/strong><strong> Number<\/strong><\/td>\n<td><strong>Frequency (Unrefined Mesh)<\/strong><\/td>\n<td><strong>Frequency (Refined Mesh)<\/strong><\/td>\n<\/tr>\n<tr>\n<td>1<\/td>\n<td>4.6563<\/td>\n<td>4.7554<\/td>\n<\/tr>\n<tr>\n<td>2<\/td>\n<td>24..785<\/td>\n<td>25.087<\/td>\n<\/tr>\n<tr>\n<td>3<\/td>\n<td>31.701<\/td>\n<td>32.087<\/td>\n<\/tr>\n<tr>\n<td>4<\/td>\n<td>37.989<\/td>\n<td>38.247<\/td>\n<\/tr>\n<tr>\n<td>5<\/td>\n<td>51.152<\/td>\n<td>49.506<\/td>\n<\/tr>\n<tr>\n<td>6<\/td>\n<td>59.988<\/td>\n<td>56.756<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n","protected":false},"template":"","class_list":["post-160122","topic","type-topic","status-publish","hentry","topic-tag-aim-tutotrial","topic-tag-discovery-aim","topic-tag-structures"],"aioseo_notices":[],"aioseo_head":"\n\t\t<!-- All in One SEO 4.9.10 - aioseo.com -->\n\t<meta name=\"description\" content=\"This example is taken from Cornell University&#039;s ANSYS AIM Learning Modules Contents Problem Specification Geometry Mesh Physics Setup Results Evaluation Verification &amp; Validation Problem Specification A wing with a NACA 0012 airfoil section is supported such that one end is fixed and the other end is free. 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The wing has a chord of 1 meter, a"},"aioseo_meta_data":{"post_id":"160122","title":null,"description":null,"keywords":null,"keyphrases":null,"primary_term":null,"canonical_url":null,"og_title":null,"og_description":null,"og_object_type":"default","og_image_type":"default","og_image_url":null,"og_image_width":null,"og_image_height":null,"og_image_custom_url":null,"og_image_custom_fields":null,"og_video":null,"og_custom_url":null,"og_article_section":null,"og_article_tags":null,"twitter_use_og":false,"twitter_card":"default","twitter_image_type":"default","twitter_image_url":null,"twitter_image_custom_url":null,"twitter_image_custom_fields":null,"twitter_title":null,"twitter_description":null,"schema":{"blockGraphs":[],"customGraphs":[],"default":{"data":{"Article":[],"Course":[],"Dataset":[],"FAQPage":[],"Movie":[],"Person":[],"Product":[],"ProductReview":[],"Car":[],"Recipe":[],"Service":[],"SoftwareApplication":[],"WebPage":[]},"graphName":"","isEnabled":true},"graphs":[]},"schema_type":"default","schema_type_options":null,"pillar_content":false,"robots_default":true,"robots_noindex":false,"robots_noarchive":false,"robots_nosnippet":false,"robots_nofollow":false,"robots_noimageindex":false,"robots_noodp":false,"robots_notranslate":false,"robots_max_snippet":null,"robots_max_videopreview":null,"robots_max_imagepreview":"large","priority":null,"frequency":null,"local_seo":null,"limit_modified_date":false,"created":"2025-10-17 18:52:47","updated":"2026-07-30 11:05:04","ai":null,"breadcrumb_settings":null,"seo_analyzer_scan_date":null},"aioseo_breadcrumb":"<div class=\"aioseo-breadcrumbs\"><span class=\"aioseo-breadcrumb\">\n\t\t\t<a href=\"https:\/\/innovationspace.ansys.com\/knowledge\" title=\"Home\">Home<\/a>\n\t\t<\/span><span class=\"aioseo-breadcrumb-separator\">&raquo;<\/span><span class=\"aioseo-breadcrumb\">\n\t\t\t<a href=\"https:\/\/innovationspace.ansys.com\/knowledge\/topics\/\" title=\"Topics\">Topics<\/a>\n\t\t<\/span><span class=\"aioseo-breadcrumb-separator\">&raquo;<\/span><span class=\"aioseo-breadcrumb\">\n\t\t\t<a href=\"https:\/\/innovationspace.ansys.com\/knowledge\/forums\/topic-tag\/discovery-aim\/\" title=\"discovery-aim\">discovery-aim<\/a>\n\t\t<\/span><span class=\"aioseo-breadcrumb-separator\">&raquo;<\/span><span class=\"aioseo-breadcrumb\">\n\t\t\tDiscovery AIM tutorial \u2013 Modal Analysis of a Wing\n\t\t<\/span><\/div>","aioseo_breadcrumb_json":[{"label":"Home","link":"https:\/\/innovationspace.ansys.com\/knowledge"},{"label":"Topics","link":"https:\/\/innovationspace.ansys.com\/knowledge\/topics\/"},{"label":"discovery-aim","link":"https:\/\/innovationspace.ansys.com\/knowledge\/forums\/topic-tag\/discovery-aim\/"},{"label":"Discovery AIM tutorial &#8211; Modal Analysis of a Wing","link":"https:\/\/innovationspace.ansys.com\/knowledge\/forums\/topic\/discovery-aim-tutorial-modal-analysis-of-a-wing\/"}],"acf":[],"custom_fields":[{"0":{"_wp_page_template":["default"],"_bbp_last_active_time":["09-13-2022  20:20:28"],"_bbp_forum_id":["159552"],"_btv_view_count":["805"],"family":[""],"application_name":[""],"product_version":[""],"_bbp_likes_count":["1"]},"test":"watchlearnansys-com"}],"_links":{"self":[{"href":"https:\/\/innovationspace.ansys.com\/knowledge\/wp-json\/wp\/v2\/topics\/160122","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/innovationspace.ansys.com\/knowledge\/wp-json\/wp\/v2\/topics"}],"about":[{"href":"https:\/\/innovationspace.ansys.com\/knowledge\/wp-json\/wp\/v2\/types\/topic"}],"version-history":[{"count":0,"href":"https:\/\/innovationspace.ansys.com\/knowledge\/wp-json\/wp\/v2\/topics\/160122\/revisions"}],"wp:attachment":[{"href":"https:\/\/innovationspace.ansys.com\/knowledge\/wp-json\/wp\/v2\/media?parent=160122"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}