{"id":288869,"date":"2023-06-15T09:16:45","date_gmt":"2023-06-15T09:16:45","guid":{"rendered":"\/forum\/forums\/topic\/static-structural-ansys\/"},"modified":"2023-06-15T09:16:45","modified_gmt":"2023-06-15T09:16:45","slug":"static-structural-ansys","status":"closed","type":"topic","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/static-structural-ansys\/","title":{"rendered":"Static Structural Ansys"},"content":{"rendered":"<p>I would like to ask about Total Deformation in Static Structural. I&#8217;m doing an analysis on a wing structure of an aircraft model. As seen in the pictures below, I&#8217;ve applied 9.81N downward force at the surface of both propellers attached to a carbon fiber pylon and there are also several fixed supports. The problem now is that the maximum deformation obtained is 0.2 mm which is non-logical as the pylon should deform at least 10 mm or around that range. Is there any way to increase the total deformation exerted to the pylon without any major modifications? Thank you.<\/p>\n<p>Below are the picture of total deformation with the force and fixed support set for the analysis.<\/p>\n<p><img decoding=\"async\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2023\/06\/15-06-2023-1686820328-mceclip0.png\"><\/p>\n<p><img decoding=\"async\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2023\/06\/15-06-2023-1686820420-mceclip3.png\"><\/p>\n<p><img decoding=\"async\" src=\"\/forum\/wp-content\/uploads\/sites\/2\/2023\/06\/15-06-2023-1686820563-mceclip4.png\"><\/p>\n","protected":false},"template":"","class_list":["post-288869","topic","type-topic","status-closed","hentry"],"aioseo_notices":[],"aioseo_head":"\n\t\t<!-- All in One SEO 4.9.10 - aioseo.com -->\n\t<meta name=\"description\" content=\"I would like to ask about Total Deformation in Static Structural. I&#039;m doing an analysis on a wing structure of an aircraft model. As seen in the pictures below, I&#039;ve applied 9.81N downward force at the surface of both propellers attached to a carbon fiber pylon and there are also several fixed supports. The problem\" \/>\n\t<meta name=\"robots\" content=\"max-image-preview:large\" \/>\n\t<link rel=\"canonical\" href=\"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/static-structural-ansys\/\" \/>\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=\"Static Structural Ansys | Ansys Learning Forum\" \/>\n\t\t<meta property=\"og:description\" content=\"I would like to ask about Total Deformation in Static Structural. I&#039;m doing an analysis on a wing structure of an aircraft model. 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