{"id":19682,"date":"2025-05-13T10:43:56","date_gmt":"2025-05-13T10:43:56","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=19682"},"modified":"2025-09-10T10:16:18","modified_gmt":"2025-09-10T10:16:18","slug":"wind-tunnel-test-of-gust-response-for-distributed-propeller-wing-system","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/wind-tunnel-test-of-gust-response-for-distributed-propeller-wing-system\/","title":{"rendered":"Wind tunnel test of gust response for distributed propeller-wing system"},"content":{"rendered":"\n<p><strong>Kunhui Huang, Zhitao Zhang, Dawei Liu, Changchuan Xie<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-011<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2024-011<\/strong><\/p>\n\n\n\n<p>High-efficiency distributed propellers have emerged as a propulsion option for future transportation, necessitating a thorough understanding of the propellers&#8217; slipstream performance and aerodynamic interaction with a wing under a variety of operating situations. At low subsonic speed and typical rotational speed, an experimental gust wind study was carried out to examine the impacts of the distributed propellers&#8217; thrust and slipstream on a flexible wing with a 300 mm wing-chord. A fiber optic sensing system was designed and deployed on the beam surface aimed to measure the time-domain response of wingtip deformation. The results demonstrate the accuracy of the measurement system in predicting structural deformation and aerodynamic performance under various gust situations.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/05\/11.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Kunhui Huang, Zhitao Zhang, Dawei Liu, Changchuan Xie<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-011<\/p>\n<p>Conference number: IFASD-2024-011<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,3022,3046],"tags":[1972,3335,2132,684,3336],"class_list":["post-19682","post","type-post","status-publish","format-standard","hentry","category-events","category-ifasd-2024","category-wind-tunnel-testing-1-ifasd-2024","tag-aeroelasticity","tag-distributed-propeller","tag-gust-response","tag-wind-tunnel-test","tag-wing-deformation","category-993","category-3022","category-3046","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19682","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=19682"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19682\/revisions"}],"predecessor-version":[{"id":20393,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19682\/revisions\/20393"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=19682"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=19682"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=19682"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}