{"id":18962,"date":"2025-02-14T12:45:44","date_gmt":"2025-02-14T12:45:44","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18962"},"modified":"2025-02-14T12:45:45","modified_gmt":"2025-02-14T12:45:45","slug":"investigation-of-gust-loads-on-a-flexible-forward-swept-wing","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/14\/investigation-of-gust-loads-on-a-flexible-forward-swept-wing\/","title":{"rendered":"INVESTIGATION OF GUST LOADS ON A FLEXIBLE FORWARD SWEPT WING"},"content":{"rendered":"\n<p><strong>Vega Handojo, Yasser M. Meddaikar, Johannes K.S. Dillinger, Jurij Sodja, 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-2019-093<\/strong><\/p>\n\n\n\n<p>This paper presents a semi-experimental method which can be used to predict the gust response of a wind tunnel model. The method incorporates transfer functions of the wind tunnel model \u2013 in this case a flexible forward swept wing \u2013 which are obtained using sweep excitations with a gust generator. The prediction results are then compared with those resulting from experimental measurements and numerical simulations. The observed quantities comprise accelerations and loads data. In the ideal case, the advantage of this semiexperimental prediction of the wing\u2019s response to gusts lies mainly in the reduction of wind tunnel time. Instead of testing each gust profile at each frequency, a measurement of several sweep excitations would suffice.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/02\/IFASD-2019-093.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Vega Handojo, Yasser M. Meddaikar, Johannes K.S. Dillinger, Jurij Sodja, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-093<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2444,2433,2449],"tags":[2935,2205,2316],"class_list":["post-18962","post","type-post","status-publish","format-standard","hentry","category-experimental-methods-in-aeroelasticity","category-1-ifasd-2019","category-maneuver-and-gust-loads","tag-dynamic-gust-loads","tag-forward-swept-wing","tag-gust-generator","category-2444","category-2433","category-2449","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18962","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=18962"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18962\/revisions"}],"predecessor-version":[{"id":18964,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18962\/revisions\/18964"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18962"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18962"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18962"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}