{"id":18600,"date":"2024-11-19T14:18:09","date_gmt":"2024-11-19T14:18:09","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18600"},"modified":"2024-11-19T14:18:10","modified_gmt":"2024-11-19T14:18:10","slug":"cfd-csd-approach-to-evaluate-the-aeroelastic-response-of-hypersonic-vehicle-wing","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/cfd-csd-approach-to-evaluate-the-aeroelastic-response-of-hypersonic-vehicle-wing\/","title":{"rendered":"CFD\/CSD APPROACH TO EVALUATE THE AEROELASTIC RESPONSE OF HYPERSONIC VEHICLE WING"},"content":{"rendered":"\n<p><strong>Jinan Lv, Li Guo, Fangjian Wang, Ziqiang Liu<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2015-146<\/strong><\/p>\n\n\n\n<p>A coupling numerical simulation technology which combined computational fluid dynamics (CFD) method with computational structure dynamic (CSD) is developed. Several kinds of mode to exchange data for CFD\/CSD coupled computation is designed. Aeroelastic response of hypersonic wing under Ma 5 wind tunnel experimental condition is calculated as an example. The coupling of bending and torsion mode is captured. The computed result indicates that CFD\/CSD method of aeroelastic simulation is feasible and credible.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/11\/IFASD-2015-146.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Jinan Lv, Li Guo, Fangjian Wang, Ziqiang Liu<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-146<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2413,2430],"tags":[682,2140,2687],"class_list":["post-18600","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-poster-presentations","tag-aeroelastic","tag-cfd-csd","tag-coupling-simulation","category-2413","category-2430","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18600","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=18600"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18600\/revisions"}],"predecessor-version":[{"id":18602,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18600\/revisions\/18602"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18600"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18600"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18600"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}