{"id":18675,"date":"2024-11-20T11:49:40","date_gmt":"2024-11-20T11:49:40","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18675"},"modified":"2024-11-20T11:49:40","modified_gmt":"2024-11-20T11:49:40","slug":"uncertainty-quantification-in-aeroelastic-response-of-an-idealized-composite-wing","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/uncertainty-quantification-in-aeroelastic-response-of-an-idealized-composite-wing\/","title":{"rendered":"UNCERTAINTY QUANTIFICATION IN AEROELASTIC RESPONSE OF AN IDEALIZED COMPOSITE WING"},"content":{"rendered":"\n<p><strong>Christian T. Nitschke, Jonas Maruani, Angela Vincenti, Didier Lucor, Jean-Camille Chassaing<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2015-182<\/strong><\/p>\n\n\n\n<p>The aeroelastic response of a cantilevered composite plate wing in incompressible \ufb02ow is studied. Uncertainties of the laminate ply angles are taken into account, with special regard to desymmetrisation of the laminate by the uncertainties. The polar method is employed for preliminary analysis as well as parameter space reduction. Arbitrary polynomial chaos is used to decrease the number of calls to the aeroelastic solver.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/11\/IFASD-2015-182.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Christian T. Nitschke, Jonas Maruani, Angela Vincenti, Didier Lucor, Jean-Camille Chassaing<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-182<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2413,2417],"tags":[1972,2747,2240,2748],"class_list":["post-18675","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-nonlinearities-uncertainties","tag-aeroelasticity","tag-arbitrary-polynomial-chaos","tag-composite-materials","tag-polar-method","category-2413","category-2417","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18675","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=18675"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18675\/revisions"}],"predecessor-version":[{"id":18677,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18675\/revisions\/18677"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18675"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18675"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18675"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}