{"id":13626,"date":"2023-10-26T20:09:08","date_gmt":"2023-10-26T20:09:08","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=13626"},"modified":"2024-04-22T20:08:59","modified_gmt":"2024-04-22T20:08:59","slug":"starting-and-heating-of-rectangular-hypersonic-inlet-with-blunted-leading-edges","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2023\/10\/26\/starting-and-heating-of-rectangular-hypersonic-inlet-with-blunted-leading-edges\/","title":{"rendered":"Starting and heating of rectangular hypersonic inlet with blunted leading edges"},"content":{"rendered":"\n<p><strong>V. Borovoy , V. Mosharov , A. Skuratov and V. Radchenko<\/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_47601548<\/strong><\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p>Experimental investigation of the flow in a schematic rectangular air inlet mounted on a plate is carried out. The influence of leading edges bluntness and narrowing degree of the internal channel on the inlet starting and on the heat transfer inside it are studied. The experiments are carried out at two Mach numbers (M\u221e=5 and 8) and different Reynolds numbers Re\u221eL from 2.8\u00d7106 to 23\u00d7106 .<\/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_47601548.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_47601548.pdf\">Read the full paper &gt; <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>V. Borovoy , V. Mosharov , A. Skuratov and V. Radchenko<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST 2018_47601548<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[996,994,198,257,311,999,1001],"tags":[985,987,513,988,986],"class_list":["post-13626","post","type-post","status-publish","format-standard","hentry","category-high-speed-aerodynamics-and-aerothermodynamics","category-hisst-2018","category-hypersonic-aerodynamics","category-hypersonic-flight-dynamics","category-hypersonic-propulsion","category-materials-and-structures-hisst-2018","category-propulsion-systems-and-components","tag-air-inlet","tag-entropy-layer","tag-heat-transfer-2","tag-ludwieg-wind-tunnel","tag-starting","category-996","category-994","category-198","category-257","category-311","category-999","category-1001","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13626","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=13626"}],"version-history":[{"count":4,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13626\/revisions"}],"predecessor-version":[{"id":16356,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13626\/revisions\/16356"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=13626"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=13626"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=13626"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}