{"id":18663,"date":"2024-11-20T11:37:47","date_gmt":"2024-11-20T11:37:47","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18663"},"modified":"2024-11-20T11:37:47","modified_gmt":"2024-11-20T11:37:47","slug":"openfsi-interface-for-strongly-coupled-steady-and-unsteady-aeroelasticity","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/openfsi-interface-for-strongly-coupled-steady-and-unsteady-aeroelasticity\/","title":{"rendered":"OPENFSI INTERFACE FOR STRONGLY COUPLED STEADY AND UNSTEADY AEROELASTICITY"},"content":{"rendered":"\n<p><strong>C. Valente, D. Jones, A. Gaitonde, J. E. Cooper, Y. Lemmens<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2015-178<\/strong><\/p>\n\n\n\n<p>The main objective of this paper is to present the implementation of a new OpenFSI methodology to strongly couple the structural solver MSC Nastran and the CFD code DLR TAU. To achieve this, a dedicated interface has been created to allow both the exchange of information between the two codes and the time synchronization necessary for a strongly coupled analysis. The framework is demonstrated to be a valuable means to accurately simulate steady and unsteady aeroelastic problems. Numerical results obtained from a simulation of an AGARD 445.6 wing example have been used as a benchmark problem to show the applicability of the framework. This framework has then been used for static and gust calculations for the FFAST wing, which is representative of a modern civil transport wing.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/11\/IFASD-2015-178.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>C. Valente, D. Jones, A. Gaitonde, J. E. Cooper, Y. Lemmens<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-178<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2413,2419],"tags":[1972,2740,1142,2739,2005,2741],"class_list":["post-18663","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-computational-aeroelasticity-1-ifasd-2015","tag-aeroelasticity","tag-cfd-csm-2","tag-coupling","tag-fluid-structure","tag-gust","tag-openfsi","category-2413","category-2419","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18663","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=18663"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18663\/revisions"}],"predecessor-version":[{"id":18665,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18663\/revisions\/18665"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18663"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18663"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18663"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}