{"id":13603,"date":"2023-10-26T19:55:26","date_gmt":"2023-10-26T19:55:26","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=13603"},"modified":"2024-03-29T11:19:13","modified_gmt":"2024-03-29T11:19:13","slug":"control-of-flow-parameters-in-models-of-precombustion-diffusers-for-ramjet-engine","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2023\/10\/26\/control-of-flow-parameters-in-models-of-precombustion-diffusers-for-ramjet-engine\/","title":{"rendered":"Control of flow parameters in models of precombustion diffusers for ramjet engine"},"content":{"rendered":"\n<p><strong>Natalya V. Guryleva, Mikhail A. Ivankin, Dmitry A. Lapinsky, Alexander M. Tereshin<\/strong><\/p>\n\n\n\n<p><strong>DoI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST 2018-1147<\/strong><\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p>Results of experimental studies of flow in sectioned duct of precombustion diffuser models divided into compartments by longitudinal partitions are presented. It is shown, that the presence of a gasdynamic connection between the channels reduces the flow irregularity, equalizes the flow parameters at the end of the channel, reduces the longitudinal dimensions of the flow deceleration area.<\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_42101147.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_42101147.pdf\">Read the full paper &gt; <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Natalya V. Guryleva, Mikhail A. Ivankin, Dmitry A. Lapinsky, Alexander M. Tereshin<\/b><\/p>\n<p>DoI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST 2018-1147<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[996,994,311,1001],"tags":[965,434,964,963,962],"class_list":["post-13603","post","type-post","status-publish","format-standard","hentry","category-high-speed-aerodynamics-and-aerothermodynamics","category-hisst-2018","category-hypersonic-propulsion","category-propulsion-systems-and-components","tag-experimental-studies","tag-hisst-2018","tag-intake","tag-precombustion-diffuser","tag-shock-train","category-996","category-994","category-311","category-1001","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13603","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=13603"}],"version-history":[{"count":2,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13603\/revisions"}],"predecessor-version":[{"id":15765,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13603\/revisions\/15765"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=13603"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=13603"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=13603"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}