{"id":16383,"date":"2024-04-24T12:20:47","date_gmt":"2024-04-24T12:20:47","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16383"},"modified":"2024-04-26T15:08:10","modified_gmt":"2024-04-26T15:08:10","slug":"simulating-hypersonic-fluid-structural-interaction-of-an-inclinedcantilever-panel-using-the-conservation-element-solution-element-method","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/24\/simulating-hypersonic-fluid-structural-interaction-of-an-inclinedcantilever-panel-using-the-conservation-element-solution-element-method\/","title":{"rendered":"Simulating Hypersonic Fluid Structural Interaction of an InclinedCantilever Panel Using the Conservation Element Solution Element Method"},"content":{"rendered":"\n<p><strong>L. Pollock, G. Wild<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-400<\/strong><\/p>\n\n\n\n<p>This manuscript presents the simulation of the Fluid Structural Interaction (FSI) of a cantilever<br>compliant panel in hypersonic flow. The problem is resolved through multiphysics coupling in the<br>commercial software package LS-DYNA and employs the use of the Immersed Boundary Method (IBM)<br>within the Conservation Element Solution Element (CESE) solver framework using explicit time stepping.<br>The CESE method encompasses many non-traditional features that makes it aptly suited for the study<br>of hypersonic flows, including, a unified treatment of space and time, and a Riemann-free shock solver.<br>The study of hypersonic FSI is of high importance due to restrictive weight requirements resulting in<br>thin panels that are prone to deformation. The understanding of the aeroelastic effects is important to<br>ensure continued operation of geometry sensitive regions such as inlets and control surfaces.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/04\/HiSST-2022-400.pdf\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>L. Pollock, G. Wild<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-400<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[1008,1006],"tags":[682,1284,1285,440,1216],"class_list":["post-16383","post","type-post","status-publish","format-standard","hentry","category-high-speed-aerodynamics-and-aerothermodynamics-hisst-2022","category-hisst-2022","tag-aeroelastic","tag-conservation-element-solution-element","tag-fluid-structural-interaction","tag-hypersonic","tag-immersed-boundary-method","category-1008","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16383","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=16383"}],"version-history":[{"count":2,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16383\/revisions"}],"predecessor-version":[{"id":16506,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16383\/revisions\/16506"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16383"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16383"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16383"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}