{"id":17222,"date":"2024-06-06T12:44:15","date_gmt":"2024-06-06T12:44:15","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=17222"},"modified":"2025-09-21T13:52:30","modified_gmt":"2025-09-21T13:52:30","slug":"some-recent-developments-in-hypersonic-flow-stability-analyses","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/06\/some-recent-developments-in-hypersonic-flow-stability-analyses\/","title":{"rendered":"Some Recent Developments in Hypersonic Flow Stability Analyses"},"content":{"rendered":"\n<p><strong>Liang WANG, Song FU<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: 10.82241\/ceas-hisst-2024-280<\/strong><\/p>\n\n\n\n<p><strong>Conference number: HiSST-2024-280<\/strong><\/p>\n\n\n\n<p>This paper presents the authors&#8217; advancements in the investigation of flow instabilities encountered during hypersonic flight. It encapsulates several significant findings, as follows: 1) Elucidation of the excitation mechanisms governing the evolution of the three-dimensional boundary layer at the vehicle nose, with particular emphasis on the impact of thermal\u2013chemical nonequilibrium effects. 2) Observation of a notable decay in disturbance growth-rate oscillation downstream of the turning point, where the unstable supersonic mode transitions back to the subsonic regime. 3) Discovery of novel modes of crossflow vortices occurring on the surface of swept wings.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/06\/HiSST-2024-280.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Liang WANG, Song FU<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82241\/ceas-hisst-2024-280<\/p>\n<p>Conference number: HiSST-2024-280<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1407,1411],"tags":[719,546,669,1825],"class_list":["post-17222","post","type-post","status-publish","format-standard","hentry","category-events","category-11-hisst-2024","category-hypersonic-fundamentals-and-history-11-hisst-2024","tag-high-enthalpy-flow","tag-hypersonics","tag-stability-analyses","tag-swept-leading-edge-flow","category-993","category-1407","category-1411","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17222","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=17222"}],"version-history":[{"count":4,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17222\/revisions"}],"predecessor-version":[{"id":21229,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17222\/revisions\/21229"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=17222"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=17222"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=17222"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}