{"id":16260,"date":"2024-04-12T13:28:34","date_gmt":"2024-04-12T13:28:34","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16260"},"modified":"2024-04-12T13:28:35","modified_gmt":"2024-04-12T13:28:35","slug":"numerical-analysis-of-the-flow-in-a-generic-scramjet-engine-model-flow-without-injection","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/numerical-analysis-of-the-flow-in-a-generic-scramjet-engine-model-flow-without-injection\/","title":{"rendered":"Numerical analysis of the flow in a generic scramjet engine model \u2013 Flow without injection"},"content":{"rendered":"\n<p><strong>F\u00e1bio Henrique Eug\u00eanio Ribeiro, Andr\u00e9 Carlos Fraile J\u00fanior<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-389<\/strong><\/p>\n\n\n\n<p>Scramjet engines are high-speed airbreathing propulsion systems with no moving parts, which compress the air dynamically through a supersonic intake, increasing temperature and pressure levels so<br>combustion can occur. Flow dynamics in a generic scramjet combustion chamber is studied based on a<br>representative experiment run at the Institute for Advanced Studies. The computations are performed<br>with an in-house solver that is being developed to perform simulations of compressible reactive multicomponent flows. The present simulations are performed within the LES framework and WALE model<br>is retained as the SGS viscosity closure, and the geometry of the combustor is modeled using the IBM<br>algorithm.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-389.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-389.pdf\">Read the full paper ><\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>F\u00e1bio Henrique Eug\u00eanio Ribeiro, Andr\u00e9 Carlos Fraile J\u00fanior<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-389<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1006,1014],"tags":[442,614,561],"class_list":["post-16260","post","type-post","status-publish","format-standard","hentry","category-events","category-hisst-2022","category-testing-and-evaluation-hisst-2022","tag-cfd","tag-scramjet","tag-turbulence","category-993","category-1006","category-1014","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16260","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=16260"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16260\/revisions"}],"predecessor-version":[{"id":16261,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16260\/revisions\/16261"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16260"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16260"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16260"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}