{"id":18947,"date":"2025-02-14T12:20:11","date_gmt":"2025-02-14T12:20:11","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18947"},"modified":"2025-02-14T12:20:12","modified_gmt":"2025-02-14T12:20:12","slug":"a-full-potential-static-aeroelastic-solver-for-preliminary-aircraft-design","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/14\/a-full-potential-static-aeroelastic-solver-for-preliminary-aircraft-design\/","title":{"rendered":"A FULL POTENTIAL STATIC AEROELASTIC SOLVER FOR PRELIMINARY AIRCRAFT DESIGN"},"content":{"rendered":"\n<p><strong>Adrien Crovato, Romain Boman, Huseyin Guner, Vincent E. Terrapon, Grigorios Dimitriadis, Hugo S. Almeida, Alex P. Prado, Carlos Breviglieri, Pedro H. Cabral, Gustavo H. Silva<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2019-087<\/strong><\/p>\n\n\n\n<p>There is a consensus in the aerospace research community that future aircraft will be more \ufb02exible and their wings will be more highly loaded. While this development is likely to increase aircraft ef\ufb01ciency, it poses several aeroelastic questions. Current aeroelastic tailoring practice for early preliminary aircraft design relies on linear aerodynamic modeling, unable to predict shocks. On the other hand, nonlinear solvers, although they provide a wide range of functionality and are reliable, often consist in monolithic code structures and cannot be ef\ufb01ciently coupled to external structural mechanics codes. They are therefore usually not readily usable for coupled \ufb02uid-structure interaction computations. The objective of the present work is to carry out aerodynamic and static aeroelastic computations in the context of preliminary aircraft design. To this end, an open-source, fast and reliable, unstructured \ufb01nite element, Full Potential solver has been developed. Preliminary results are presented and show a signi\ufb01cant improvement over the classical linear potential method and are in good agreement with higher \ufb01delity nonlinear solvers.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/02\/IFASD-2019-087.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Adrien Crovato, Romain Boman, Huseyin Guner, Vincent E. Terrapon, Grigorios Dimitriadis, Hugo S. Almeida, Alex P. Prado, Carlos Breviglieri, Pedro H. Cabral, Gustavo H. Silva<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-087<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2437,2433],"tags":[766,1972,2203,2930,2108],"class_list":["post-18947","post","type-post","status-publish","format-standard","hentry","category-aeroelastic-optimization","category-1-ifasd-2019","tag-aerodynamics","tag-aeroelasticity","tag-aircraft-design","tag-full-potential","tag-transonic-ow","category-2437","category-2433","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18947","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=18947"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18947\/revisions"}],"predecessor-version":[{"id":18949,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18947\/revisions\/18949"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18947"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18947"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18947"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}