{"id":19667,"date":"2025-05-13T10:26:16","date_gmt":"2025-05-13T10:26:16","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=19667"},"modified":"2025-09-10T10:19:34","modified_gmt":"2025-09-10T10:19:34","slug":"exploring-the-effect-of-different-shock-impingement-angles-on-aeroelastic-response-for-a-thin-panel","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/exploring-the-effect-of-different-shock-impingement-angles-on-aeroelastic-response-for-a-thin-panel\/","title":{"rendered":"Exploring the Effect of Different Shock Impingement Angles on Aeroelastic Response for a Thin Panel"},"content":{"rendered":"\n<p><strong>Luisa Piccolo Serafim, Earl Dowell<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-016<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2024-016<\/strong><\/p>\n\n\n\n<p>In this study, a novel dynamically linearized Euler time-domain approach is used to compute the generalized aerodynamic force from a CFD simulation. The aerodynamic forcing term is implemented in a theoretical\/computational nonlinear aeroelastic model to assess the dynamic response of a flexible clamped-clamped panel considering the pressure profile due to different shock wedge angles. One benefit of this approach is the possibility to perform the same analysis to solve the Navier-Stokes Equation via RANS simulation and consider the viscous boundary layer effect for near transonic regimes. Different shock wedge configurations will be explored in this study in the CFD\/ROM simulation and the aeroelastic solution using an inviscid solver. These results will also be compared with the same structural configuration considering a modified Piston Theory model, exploring the limitations and opportunities of this simpler and faster solution.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/05\/16.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Luisa Piccolo Serafim, Earl Dowell<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-016<br \/>\nConference number: IFASD-2024-016<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,3028,3022],"tags":[1972,3328,3003,1353],"class_list":["post-19667","post","type-post","status-publish","format-standard","hentry","category-events","category-computational-aeroelasticity-1-ifasd-2024","category-ifasd-2024","tag-aeroelasticity","tag-fluid-structural-interaction-fsi","tag-limit-cycle-oscillation-lco","tag-shock-impingement","category-993","category-3028","category-3022","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19667","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=19667"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19667\/revisions"}],"predecessor-version":[{"id":20398,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19667\/revisions\/20398"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=19667"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=19667"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=19667"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}