{"id":18232,"date":"2024-08-29T10:16:40","date_gmt":"2024-08-29T10:16:40","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18232"},"modified":"2024-08-29T10:16:41","modified_gmt":"2024-08-29T10:16:41","slug":"ree-vibration-analysis-of-tapered-wing-structures-using-refined-one-dimensional-models","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/ree-vibration-analysis-of-tapered-wing-structures-using-refined-one-dimensional-models\/","title":{"rendered":"REE-VIBRATION ANALYSIS OF TAPERED WING STRUCTURES USING REFINED ONE-DIMENSIONAL MODELS"},"content":{"rendered":"\n<p><strong>A. Viglietti, E. Zappino, E. Carrera<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2017-230<\/strong><\/p>\n\n\n\n<p>This work presents results from free-vibration analyses on tapered wing box made of composite material. The analyses are performed through a re\ufb01ned one-dimensional model based on the Carrera Uni\ufb01ed Formulation. The displacements over the beam cross-section are evaluated using polynomial expansions. In this way, no geometrical approximations are introduced in the problem and a three-dimensional result can be obtained. Two simple tapered wing boxes have been considered and different laminations have been taking into account. The results are compared with a shell model achieved by a commercial code. The results demonstrate the good accuracy of the model and his use in tailoring analyses.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/08\/IFASD-2017-230.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>A. Viglietti, E. Zappino, E. Carrera<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-230<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1953,1962],"tags":[2392,2396,2393,2394,2395],"class_list":["post-18232","post","type-post","status-publish","format-standard","hentry","category-events","category-ifasd-2017","category-reduced-order-modeling","tag-cuf","tag-free-vibration","tag-one-dimensional-2","tag-tapered","tag-thin-walled","category-993","category-1953","category-1962","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18232","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=18232"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18232\/revisions"}],"predecessor-version":[{"id":18234,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18232\/revisions\/18234"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18232"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18232"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18232"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}