{"id":13473,"date":"2023-10-26T18:29:23","date_gmt":"2023-10-26T18:29:23","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=13473"},"modified":"2024-05-03T18:43:43","modified_gmt":"2024-05-03T18:43:43","slug":"method-for-solving-the-equations-describing-the-interaction-of-a-3-d-boundary-layer-with-an-outer-inviscid-supersonic-flow","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2023\/10\/26\/method-for-solving-the-equations-describing-the-interaction-of-a-3-d-boundary-layer-with-an-outer-inviscid-supersonic-flow\/","title":{"rendered":"Method for Solving the Equations Describing the Interaction of a 3-D Boundary Layer with an Outer Inviscid Supersonic Flow"},"content":{"rendered":"\n<p><strong>G. L. Korolev<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST 2018_13401004<\/strong><\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p>Advanced computational method is developed for solving the three-dimensional time-independent equations describing the interaction of a laminar boundary layer with an outer inviscid flow. By applying the method, the problem of the three-dimensional viscous supersonic gas flow over a roughness element (a hump and a cavity) is solved for the first time within the framework of the classical triple-deck theory. The asymptotic height of the roughness element corresponding to the non-separated flow is determined, and separated flow patterns are constructed.<\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p><a href=\"https:\/\/link.springer.com\/article\/10.1134\/S0965542507030128\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_13401004.pdf\">Read the full paper from the Springer website &gt;<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>G. L. Korolev<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<br \/>\nConference Number HiSST 2018_13401004<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[193,996,994,198],"tags":[813,434,815,814,744],"class_list":["post-13473","post","type-post","status-publish","format-standard","hentry","category-boundary-layer-control","category-high-speed-aerodynamics-and-aerothermodynamics","category-hisst-2018","category-hypersonic-aerodynamics","tag-3-d-interaction","tag-hisst-2018","tag-numerical-method","tag-separation","tag-supersonic-flow","category-193","category-996","category-994","category-198","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13473","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\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=13473"}],"version-history":[{"count":4,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13473\/revisions"}],"predecessor-version":[{"id":16607,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13473\/revisions\/16607"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=13473"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=13473"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=13473"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}