{"id":18965,"date":"2025-02-14T12:49:54","date_gmt":"2025-02-14T12:49:54","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18965"},"modified":"2025-02-14T12:49:55","modified_gmt":"2025-02-14T12:49:55","slug":"wind-tunnel-testing-of-a-high-aspect-ratio-wing-model","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/14\/wind-tunnel-testing-of-a-high-aspect-ratio-wing-model\/","title":{"rendered":"Wind Tunnel Testing of a High Aspect Ratio Wing Model"},"content":{"rendered":"\n<p><strong>J.E. Cooper R.G. Cook G. Francois, O. de la Torre, S.A. Neild, M.H. Lowenberg S.S. Alexander, E.B. Coetzee, M. Evans<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2019-094<\/strong><\/p>\n\n\n\n<p>There is much current interest in the development of High Aspect Ratio Wing (HARW) designs for improved aircraft performance. However, there are a lack of relevant data sets available to validate aeroelastic modelling approaches for highly flexible wings. The design and manufacture of a highly flexible 2.4m semi-span wing is described. A series of low speed wind tunnel tests were performed to generate displacement, acceleration, strain gauge, aerodynamic pressure and six component balance measurements for a range of airspeeds and wing root angles of attack. Numerous static and dynamic measurements were made. Preliminary results are shown for the static and dynamic, structural and aerodynamic behaviour over a range of different airspeeds and wing root angles of attack.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/02\/IFASD-2019-094.pdf\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>J.E. Cooper R.G. Cook G. Francois, O. de la Torre, S.A. Neild, M.H. Lowenberg S.S. Alexander, E.B. Coetzee, M. Evans<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-094<\/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],"tags":[2125,698,611],"class_list":["post-18965","post","type-post","status-publish","format-standard","hentry","category-experimental-methods-in-aeroelasticity","category-1-ifasd-2019","tag-high-aspect-ratio-wings","tag-nonlinear-aeroelasticity","tag-wind-tunnel-testing","category-2444","category-2433","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18965","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=18965"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18965\/revisions"}],"predecessor-version":[{"id":18967,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18965\/revisions\/18967"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18965"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18965"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18965"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}