{"id":16149,"date":"2024-04-12T10:23:51","date_gmt":"2024-04-12T10:23:51","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16149"},"modified":"2024-04-12T10:23:52","modified_gmt":"2024-04-12T10:23:52","slug":"one-dimensional-sequential-combustor-model-for-scramjet-engines","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/one-dimensional-sequential-combustor-model-for-scramjet-engines\/","title":{"rendered":"One-Dimensional Sequential Combustor Model for Scramjet Engines\u00a0"},"content":{"rendered":"\n<p><strong>Johannes C. Riehmer, Andreas K. Flock<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-136<\/strong><\/p>\n\n\n\n<p>Reliable and accurate combustor modeling is a key element for scramjet vehicle design. Especially in<br>the early design and concept phase this requires a fast, adaptable, and robust model. This paper<br>presents a straightforward approach to model such scramjet combustors on a discrete one-dimensional<br>mesh by serializing the different flow and combustion processes in individual cells. This way the<br>implementation effort is significantly decreased while the numerical stability is increased in comparison<br>to more common finite-difference modeling. Additionally, it allows direct implementation of correction<br>terms and empirical factors fitting the model to detailed numerical simulations or experimental data.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-136.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-136.pdf\">Read the full paper > <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Johannes C. Riehmer, Andreas K. Flock<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-136<\/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":[712,1093,614],"class_list":["post-16149","post","type-post","status-publish","format-standard","hentry","category-events","category-hisst-2022","category-propulsion-systems-and-components-hisst-2022","tag-combustion","tag-one-dimensional","tag-scramjet","category-993","category-1006","category-1013","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16149","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=16149"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16149\/revisions"}],"predecessor-version":[{"id":16150,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16149\/revisions\/16150"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16149"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16149"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16149"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}