{"id":19087,"date":"2025-02-17T11:40:47","date_gmt":"2025-02-17T11:40:47","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=19087"},"modified":"2025-02-17T11:40:47","modified_gmt":"2025-02-17T11:40:47","slug":"experimental-evaluation-of-fuel-sloshing-effects-on-wing-dynamics","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/17\/experimental-evaluation-of-fuel-sloshing-effects-on-wing-dynamics\/","title":{"rendered":"EXPERIMENTAL EVALUATION OF FUEL SLOSHING EFFECTS ON WING DYNAMICS"},"content":{"rendered":"\n<p><strong>F. Gambioli, R. Alegre Usach, J. Kirby, T. Wilson, P. Behruzi<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2019-142<\/strong><\/p>\n\n\n\n<p>We provide an overview of a series of experimental tests performed by the Loads &amp; Aeroelastics department at Airbus in support of a broader research activity, aiming at modelling the dissipative effects of fuel sloshing on the dynamic behavior of wing-like structures. We describe the test setup, its similarity with the actual wing-structure of a large civil aircraft, the scaling rules applied, the measuring equipment and the practical considerations which drove the design of the test rig. The free vibration of this wing-like structure is compared for cases with and without sloshing, showing the potential of exploiting the dissipation inherent to the \ufb02uid structure interaction process for dynamic load alleviation.<\/p>\n\n\n\n<p><a href=\"https:\/\/www.researchgate.net\/publication\/333560557_EXPERIMENTAL_EVALUATION_OF_FUEL_SLOSHING_EFFECTS_ON_WING_DYNAMICS?enrichId=rgreq-ba1ba0632b0ab7357e68bb096655d3b5-XXX&amp;enrichSource=Y292ZXJQYWdlOzMzMzU2MDU1NztBUzo3NzExNzUzNDkyMjc1MjdAMTU2MDg3MzkzOTY0OQ%3D%3D&amp;el=1_x_2\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>F. Gambioli, R. Alegre Usach, J. Kirby, T. Wilson, P. Behruzi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-142<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2445,2433],"tags":[2008,2406,2021],"class_list":["post-19087","post","type-post","status-publish","format-standard","hentry","category-experimental-methods-in-structural-dynamics","category-1-ifasd-2019","tag-fluid-structure-interaction-2","tag-sloshing","tag-structural-dynamics","category-2445","category-2433","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19087","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=19087"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19087\/revisions"}],"predecessor-version":[{"id":19088,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19087\/revisions\/19088"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=19087"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=19087"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=19087"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}