{"id":18871,"date":"2025-02-13T13:35:16","date_gmt":"2025-02-13T13:35:16","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18871"},"modified":"2025-02-13T13:35:17","modified_gmt":"2025-02-13T13:35:17","slug":"aeroelastic-tailoring-of-flexible-composite-aircraft","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/13\/aeroelastic-tailoring-of-flexible-composite-aircraft\/","title":{"rendered":"AEROELASTIC TAILORING OF FLEXIBLE COMPOSITE AIRCRAFT"},"content":{"rendered":"\n<p><strong>Mario Natella, Roeland De Breuker<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2019-055<\/strong><\/p>\n\n\n\n<p>This paper presents a uni\ufb01ed framework for aeroelastic tailoring of fully-\ufb02exible free-\ufb02ying composite aircraft. A continuous-time state-space model is used to describe the \ufb02ow. The 3D composite wing structure is condensed into a Timoshenko beam model utilizing a cross-sectional modeler. The aerodynamic and structural models are tightly coupled with the longitudinal \ufb02ight dynamic equations of motion in the state-space formulation. This paper refers to the clamped-wing aeroelastic tailoring as classic aeroelastic tailoring. Hence, the term aeroelastic tailoring will point at the novel approach that models the \ufb02exible, free-\ufb02ying composite aircraft. With this paper, the author investigates the effects on the tailored structural design in terms of optimum mass and stiffness distribution due to the \ufb02exibility of the composite aircraft.<\/p>\n\n\n\n<p><a href=\"https:\/\/pure.tudelft.nl\/ws\/files\/73091064\/IFASD_2019_055.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Mario Natella, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-055<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2437,2433],"tags":[2004,2873,2373,807],"class_list":["post-18871","post","type-post","status-publish","format-standard","hentry","category-aeroelastic-optimization","category-1-ifasd-2019","tag-aeroelastic-tailoring","tag-composite-aircraft","tag-load-alleviation","tag-optimization","category-2437","category-2433","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18871","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=18871"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18871\/revisions"}],"predecessor-version":[{"id":18873,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18871\/revisions\/18873"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18871"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18871"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18871"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}