{"id":18214,"date":"2024-08-29T09:49:32","date_gmt":"2024-08-29T09:49:32","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18214"},"modified":"2024-08-29T09:49:33","modified_gmt":"2024-08-29T09:49:33","slug":"nonlinear-static-aeroelastic-analysis-of-high-aspect-ratio-wing-based-on-cfd-csd-coupling-solution","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/nonlinear-static-aeroelastic-analysis-of-high-aspect-ratio-wing-based-on-cfd-csd-coupling-solution\/","title":{"rendered":"NONLINEAR STATIC AEROELASTIC ANALYSIS OF HIGH-ASPECT RATIO WING BASED ON CFD\/CSD COUPLING SOLUTION"},"content":{"rendered":"\n<p><strong>Yang Lan , Xie Changchuan , Yang Chao , Zhang Bing , Andrea Da Rouch<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2017-221<\/strong><\/p>\n\n\n\n<p>This paper discussed the implementation of a nonlinear static aeroelastic analysis framework based on CFD\/CSD coupling method. For fluid-structure interaction (FSI) problems, a conventional serial staggered (CSS) procedure is applied to generate a loosely-coupled scheme. The Reynolds-averaged Navier-Stokes equations are solved for the fluid, and a geometrical nonlinear finite element method is used for the structure. The morphing of the mesh is achieved using a spring-TFI (trans-finite interpolation) hybrid approach with rotation correction. The proposed nonlinear static aeroelastic framework is demonstrated on a very flexible high-aspect ratio wing, which is currently undergoing wind tunnel testing.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/08\/IFASD-2017-221.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Yang Lan , Xie Changchuan , Yang Chao , Zhang Bing , Andrea Da Rouch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-221<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1961,1953],"tags":[2152,2380,2379],"class_list":["post-18214","post","type-post","status-publish","format-standard","hentry","category-events","category-highly-flexible-aircraft-structures","category-ifasd-2017","tag-fsi","tag-geometrical-nonlinear-fem","tag-static-aeroelastic","category-993","category-1961","category-1953","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18214","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=18214"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18214\/revisions"}],"predecessor-version":[{"id":18216,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18214\/revisions\/18216"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18214"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18214"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18214"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}