{"id":16957,"date":"2024-05-24T13:58:15","date_gmt":"2024-05-24T13:58:15","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16957"},"modified":"2025-09-21T14:26:19","modified_gmt":"2025-09-21T14:26:19","slug":"conceptual-design-of-hypersonic-combined-cycle-engines","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/05\/24\/conceptual-design-of-hypersonic-combined-cycle-engines\/","title":{"rendered":"Conceptual Design of Hypersonic Combined Cycle Engines"},"content":{"rendered":"\n<p><strong>Hideyuki TAGUCHI, Hidemi TAKAHASHI, Shunsuke IMAMURA, Sadatake TOMIOKA<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: 10.82241\/ceas-hisst-2024-157<\/strong><\/p>\n\n\n\n<p><strong>Conference number: HiSST-2024-157<\/strong><\/p>\n\n\n\n<p>Conceptual design of hypersonic combined cycle engines is investigated. A pre-cooled turbojet engine and a scramjet engine are combined to a turbine-based combined cycle (TBCC) engine. The pre-cooled turbojet engine is assumed to be operated from Mach 0 to Mach 5. The scramjet engine is assumed to be operated from Mach 5 to Mach 6. The operating condition of the pre-cooled turbojet engine is confirmed using the results of propulsion wind tunnel test at Mach 4 flight simulating condition. A light weight mode change mechanism is proposed to change the engine cycle from the pre-cooled turbojet engine to the scramjet engine. A waverider shape airframe is designed and the flight performance is calculated for a hypersonic aircraft using the TBCC engine.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/05\/HiSST-2024-157.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Hideyuki TAGUCHI, Hidemi TAKAHASHI, Shunsuke IMAMURA, Sadatake TOMIOKA<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82241\/ceas-hisst-2024-157<\/p>\n<p>Conference number: HiSST-2024-157<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1407,1414],"tags":[1658,440,933],"class_list":["post-16957","post","type-post","status-publish","format-standard","hentry","category-events","category-11-hisst-2024","category-propulsion-systems-and-components-11-hisst-2024","tag-air-breathing","tag-hypersonic","tag-propulsion","category-993","category-1407","category-1414","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16957","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=16957"}],"version-history":[{"count":5,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16957\/revisions"}],"predecessor-version":[{"id":21271,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16957\/revisions\/21271"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16957"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16957"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16957"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}