{"id":13346,"date":"2023-10-13T14:14:15","date_gmt":"2023-10-13T14:14:15","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=13346"},"modified":"2024-05-03T14:48:29","modified_gmt":"2024-05-03T14:48:29","slug":"investigation-of-the-stream-traced-intake-starting-within-the-hexafly-int-project","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2023\/10\/13\/investigation-of-the-stream-traced-intake-starting-within-the-hexafly-int-project\/","title":{"rendered":"Investigation of the Stream-Traced Intake Starting within the HEXAFLY-INT Project"},"content":{"rendered":"\n<p><strong>Anatoly A. Gubanov&nbsp; , Natalya V. Guryleva , Mikhail A. Ivankin , Vadim A. Talyzin , Alexander V. Fedorov<\/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_1701070<\/strong><\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p>Investigation of starting process of the stream-traced intake is presented. It\u2019s shown that starting of the intake could significantly correlate with boundary layer state at the compression surface. Results of the experimental investigation of the internal characteristics with different boundary layer tripping devices and vortex generators (and without them) are presented.<\/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_1701070.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_1701070.pdf\">Read the full paper &gt; <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Anatoly A. Gubanov\u00a0 , Natalya V. Guryleva , Mikhail A. Ivankin , Vadim A. Talyzin , Alexander V. Fedorov<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<br \/>\nConference Number HiSST 2018_1701070<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[193,996,997,994],"tags":[539,630,434,628,627,629],"class_list":["post-13346","post","type-post","status-publish","format-standard","hentry","category-boundary-layer-control","category-high-speed-aerodynamics-and-aerothermodynamics","category-high-speed-missions-and-vehicles","category-hisst-2018","tag-boundary-layer","tag-experimental-investigation","tag-hisst-2018","tag-stream-traced-intake","tag-tripping-device","tag-vortex-generator","category-193","category-996","category-997","category-994","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13346","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=13346"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13346\/revisions"}],"predecessor-version":[{"id":16572,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13346\/revisions\/16572"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=13346"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=13346"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=13346"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}