{"id":18316,"date":"2024-11-18T09:36:30","date_gmt":"2024-11-18T09:36:30","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18316"},"modified":"2024-11-18T09:36:31","modified_gmt":"2024-11-18T09:36:31","slug":"unsteady-viscous-inviscid-coupling-simulations-of-separated-laminar-flows-around-2d-airfoils","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/unsteady-viscous-inviscid-coupling-simulations-of-separated-laminar-flows-around-2d-airfoils\/","title":{"rendered":"Unsteady Viscous-Inviscid Coupling Simulations of Separated Laminar Flows Around 2D Airfoils"},"content":{"rendered":"\n<p><strong>Jose I. Rothkegel, Grigorios Dimitriadis<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2015-011<\/strong><\/p>\n\n\n\n<p>An interactive boundary layer model has been developed in 2D in order to solve the unsteady \ufb02ow around an airfoil. The inviscid problem is solved using a panel method, by the discretization of the airfoil into linear-varying vortex panels. The solution of the boundary layer equations is carried out using a \ufb01nite volume scheme. Viscousinviscid coupling is preformed by imposing a permeation velocity on the skin panels of the airfoil and the addition of a free wake at each separation point.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/11\/IFASD-2015-011.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Jose I. Rothkegel, Grigorios Dimitriadis<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-011<\/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":[539,2484,2482,2483,2481,2485],"class_list":["post-18316","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-aerodynamics-cfd","tag-boundary-layer","tag-double-wake","tag-nite-volume","tag-panel-method","tag-separated-ow","tag-vortex-blob","category-2413","category-2416","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18316","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=18316"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18316\/revisions"}],"predecessor-version":[{"id":18318,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18316\/revisions\/18318"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18316"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18316"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18316"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}