{"id":19595,"date":"2025-05-12T10:42:22","date_gmt":"2025-05-12T10:42:22","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=19595"},"modified":"2025-09-10T11:01:49","modified_gmt":"2025-09-10T11:01:49","slug":"ground-vibration-testing-and-model-update-of-a-transonic-flutter-wind-tunnel-model","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/ground-vibration-testing-and-model-update-of-a-transonic-flutter-wind-tunnel-model\/","title":{"rendered":"Ground Vibration Testing and Model Update of a Transonic Flutter Wind Tunnel Model"},"content":{"rendered":"\n<p><strong>Anders Ellmo<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: 10.82439\/ceas-ifasd-2024-043<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2024-043<\/strong><\/p>\n\n\n\n<p>Using complex composite structures in a wind tunnel model means that small differences in layup, thickness and other manufacturing outcomes will result in significant consequences for the structural dynamic properties of the model, and subsequently its aeroelastic behaviour. The KTH-NASA wind tunnel model has interchangeable wings composite wings, and it is shown that finite element representations of each individual wing are needed to match experimental data, and produce accurate predictions of flutter behaviour.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/05\/43.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Anders Ellmo<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-043<\/p>\n<p>Conference number: IFASD-2024-043<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,3033,3022],"tags":[1972,2854,2021],"class_list":["post-19595","post","type-post","status-publish","format-standard","hentry","category-events","category-experimental-methods-in-aeroelasticity-1-ifasd-2024","category-ifasd-2024","tag-aeroelasticity","tag-model-update","tag-structural-dynamics","category-993","category-3033","category-3022","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19595","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=19595"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19595\/revisions"}],"predecessor-version":[{"id":20421,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19595\/revisions\/20421"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=19595"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=19595"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=19595"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}