{"id":19054,"date":"2025-02-17T10:21:06","date_gmt":"2025-02-17T10:21:06","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=19054"},"modified":"2025-02-17T10:21:07","modified_gmt":"2025-02-17T10:21:07","slug":"numerical-and-experimental-study-of-aeroelastic-tailoring-effect-using-flexible-composite-laminates-for-haps-application","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/17\/numerical-and-experimental-study-of-aeroelastic-tailoring-effect-using-flexible-composite-laminates-for-haps-application\/","title":{"rendered":"NUMERICAL AND EXPERIMENTAL STUDY OF AEROELASTIC TAILORING EFFECT USING FLEXIBLE COMPOSITE LAMINATES FOR HAPS APPLICATION"},"content":{"rendered":"\n<p><strong>B. Kirsch, O. Montagnier, T.M. Faure, E. Benard<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2019-131<\/strong><\/p>\n\n\n\n<p>The enhancement of high altitude drone endurance compels to design very \ufb02exible high-aspect-ratio composite airframe vulnerable to destructive \ufb02uid\/structure interaction like \ufb02utter or torsional divergence. Extensive research has been conducted to increase critical speed without being at the expense of weight balance. One of the promising solutions is the aeroelastic tailoring which consists in a speci\ufb01c con\ufb01guration of laminated composite layup. The present work uses an aeroelastic reduced order model, namely GEBTAero, suitable for the non linear anisotropic behavior of this kind of composite wing, able to quickly compute aeroelastic critical speeds. Particular focus is put on a wind tunnel test campaign conducted on a set of \ufb02exible plates, both metallic and composite, in order to assess the accuracy of GEBTAero.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/02\/IFASD-2019-131.pdf\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>B. Kirsch, O. Montagnier, T.M. Faure, E. Benard<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-131<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2433,2452],"tags":[2004,2240,2567,684],"class_list":["post-19054","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2019","category-reduced-order-models","tag-aeroelastic-tailoring","tag-composite-materials","tag-high-aspect-ratio-wing","tag-wind-tunnel-test","category-2433","category-2452","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19054","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=19054"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19054\/revisions"}],"predecessor-version":[{"id":19056,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19054\/revisions\/19056"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=19054"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=19054"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=19054"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}