{"id":16893,"date":"2024-05-16T13:27:35","date_gmt":"2024-05-16T13:27:35","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16893"},"modified":"2025-09-21T14:35:24","modified_gmt":"2025-09-21T14:35:24","slug":"internal-flow-path-analysis-of-the-scramjet-hypersonic-experimental-vehicle","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/05\/16\/internal-flow-path-analysis-of-the-scramjet-hypersonic-experimental-vehicle\/","title":{"rendered":"Internal Flow Path Analysis of the Scramjet Hypersonic Experimental Vehicle"},"content":{"rendered":"\n<p><strong>Oreste RUSSO, Pietro RONCIONI, Marco MARINI, Sara DI BENEDET TO, Giuliano RANUZZI, Simone PIZZURRO<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: 10.82241\/ceas-hisst-2024-126<\/strong><\/p>\n\n\n\n<p><strong>Conference number: HiSST-2024-126<\/strong><\/p>\n\n\n\n<p>The paper focuses on the assessment of propulsive and combustion performances of a scramjet engine in hypersonic cruise conditions and its emission indexes for various species involved in the combustion process. Nose-to-tail CFD analysis of the entire internal flow path (inlet, combustor and nozzle) are performed in flight-cruise configuration, for both power-off and power-on conditions, by using ANSYS FLUENT software with steady RANS model with available literature chemical schemes. The performance parameters (combustion efficiency and kinetic and thermodynamic quantities) revealed a significant improvement as well as the achievement of very high combustion efficiency by the end of the engine cycle is achieved.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/05\/HiSST-2024-126.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Oreste RUSSO, Pietro RONCIONI, Marco MARINI, Sara DI BENEDET TO, Giuliano RANUZZI, Simone PIZZURRO<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82241\/ceas-hisst-2024-126<\/p>\n<p>Conference number: HiSST-2024-126<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1409,1407],"tags":[442,440,614,470],"class_list":["post-16893","post","type-post","status-publish","format-standard","hentry","category-events","category-high-speed-aerodynamics-and-aerothermodynamics-11-hisst-2024","category-11-hisst-2024","tag-cfd","tag-hypersonic","tag-scramjet","tag-supersonic-combustion","category-993","category-1409","category-1407","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16893","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=16893"}],"version-history":[{"count":4,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16893\/revisions"}],"predecessor-version":[{"id":21283,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16893\/revisions\/21283"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16893"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16893"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16893"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}