{"id":18672,"date":"2024-11-20T11:46:59","date_gmt":"2024-11-20T11:46:59","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18672"},"modified":"2024-11-20T11:47:00","modified_gmt":"2024-11-20T11:47:00","slug":"an-advanced-panel-method-for-compressible-subsonic-unsteady-flow-past-complex-geometries","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/an-advanced-panel-method-for-compressible-subsonic-unsteady-flow-past-complex-geometries\/","title":{"rendered":"AN ADVANCED PANEL METHOD FOR COMPRESSIBLE SUBSONIC UNSTEADY FLOW PAST COMPLEX GEOMETRIES"},"content":{"rendered":"\n<p><strong>Steven P. Fiddes, Chris W. Burkett, Thiemo Kier<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2015-181<\/strong><\/p>\n\n\n\n<p>This paper describes the development of a new boundary-element method for predicting the unsteady compressible flow past general configurations in subsonic flow. It permits the actual geometry of the configuration to be represented and computes the cou- pling between the steady and unsteady flow components. It adopts a description of the unsteady deformation of the geometry that avoids many of the limitations inherent with vortex- and doublet-lattice methods. The paper describes the issues that have been ad- dressed in developing the method and, through 2D and 3D validation cases, demonstrates advantages over some established methods.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/11\/IFASD-2015-181.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Steven P. Fiddes, Chris W. Burkett, Thiemo Kier<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-181<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2413,2416],"tags":[],"class_list":["post-18672","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-aerodynamics-cfd","category-2413","category-2416","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18672","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=18672"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18672\/revisions"}],"predecessor-version":[{"id":18674,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18672\/revisions\/18674"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18672"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18672"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18672"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}