{"id":16083,"date":"2024-04-12T08:27:03","date_gmt":"2024-04-12T08:27:03","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16083"},"modified":"2024-04-12T08:28:04","modified_gmt":"2024-04-12T08:28:04","slug":"design-and-testing-of-a-low-mass-flow-rde-running-on-ethylene-oxygen","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/design-and-testing-of-a-low-mass-flow-rde-running-on-ethylene-oxygen\/","title":{"rendered":"Design and testing of a low mass flow RDE running on ethylene-oxygen"},"content":{"rendered":"\n<p><strong>Hamilton Law, Tom Baxter, Charlie Ryan, Ralf Deiterding<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-371<\/strong><\/p>\n\n\n\n<p>A modular laboratory rotating detonation engine (RDE) for combined mass flow rates below 10 g\/s has<br>been designed. Since a large chamber diameter to width ratio is used, first tests with stoichiometric<br>ethylene\u00adoxygen mixtures have revealed detonation modes with one, two and three separate detonation<br>heads, depending on mass flow rate. Spectrograms from high\u00adfrequency pressure data and high\u00adspeed<br>photography are used to confirm successful operation and identify the operational modes reliably.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-371.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-371.pdf\">Read the full paper > <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Hamilton Law, Tom Baxter, Charlie Ryan, Ralf Deiterding<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-371<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1006,1013],"tags":[1017,1018,1016],"class_list":["post-16083","post","type-post","status-publish","format-standard","hentry","category-events","category-hisst-2022","category-propulsion-systems-and-components-hisst-2022","tag-ethyleneoxygen","tag-minimal-chamber-design","tag-rotating-detonation-engine-experiment","category-993","category-1006","category-1013","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16083","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=16083"}],"version-history":[{"count":2,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16083\/revisions"}],"predecessor-version":[{"id":16085,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16083\/revisions\/16085"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16083"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16083"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16083"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}