{"id":18543,"date":"2024-11-19T13:20:30","date_gmt":"2024-11-19T13:20:30","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18543"},"modified":"2024-11-19T13:20:30","modified_gmt":"2024-11-19T13:20:30","slug":"accelerated-convergence-of-high-fidelity-aeroelasticity-using-low-fidelity-aerodynamics","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/accelerated-convergence-of-high-fidelity-aeroelasticity-using-low-fidelity-aerodynamics\/","title":{"rendered":"ACCELERATED CONVERGENCE OF HIGH-FIDELITY AEROELASTICITY USING LOW-FIDELITY AERODYNAMICS"},"content":{"rendered":"\n<p><strong>K. Jovanov, R. 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-2015-119<\/strong><\/p>\n\n\n\n<p>This paper presents a methodology on how to effectively solve static high-fidelity aeroelastic problems for high-subsonic and transonic flow regimes. The idea is to employ a low-fidelity aerodynamic model to reduce the computational cost of the high-fidelity aeroelastic problem. The low-fidelity model, in this work a linear aerodynamics model, is used systematically through a model management strategy to accelerate the convergence of the high-fidelity aeroelastic equilibrium. The high-fidelity aerodynamic model is discretized by the finite volume method and the Euler equations are solved in SU2. The structural model is a geometrically non-linear beam element model.<\/p>\n\n\n\n<p><a href=\"https:\/\/www.researchgate.net\/publication\/292972450_ACCELERATED_CONVERGENCE_OF_HIGH-FIDELITY_AEROELASTICITY_USING_LOW-FIDELITY_AERODYNAMICS?enrichId=rgreq-5a077ce3be3bef3289c613854e1e609d-XXX&amp;enrichSource=Y292ZXJQYWdlOzI5Mjk3MjQ1MDtBUzozMjUzMzA2NzA3NjgxMjhAMTQ1NDU3NjI4NDQ4Mg%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>K. Jovanov, R. De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-119<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2413,2419],"tags":[442,2661,2662,2469],"class_list":["post-18543","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-computational-aeroelasticity-1-ifasd-2015","tag-cfd","tag-multi-fidelity-aeroelasticity","tag-panel-aerodynamics","tag-static-aeroelasticity","category-2413","category-2419","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18543","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=18543"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18543\/revisions"}],"predecessor-version":[{"id":18545,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18543\/revisions\/18545"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18543"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18543"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18543"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}