{"id":13481,"date":"2023-10-26T18:34:28","date_gmt":"2023-10-26T18:34:28","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=13481"},"modified":"2024-05-03T14:24:29","modified_gmt":"2024-05-03T14:24:29","slug":"active-flow-control-of-wide-envelope-air-breathing-engine-inlet","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2023\/10\/26\/active-flow-control-of-wide-envelope-air-breathing-engine-inlet\/","title":{"rendered":"Active Flow Control of Wide-envelope Air-breathing Engine Inlet"},"content":{"rendered":"\n<p><strong>Wang Jianlei , Li Tiangang , Wei Zhen , Chen Bing , Gong Chunlin , Gu Liangxian<\/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_15101002<\/strong><\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p>Wide-envelope spacecraft need to operate at the Mach number far away from the design point. For better engine inlet performance at those operation states active flow control technology is needed to be used. Both NS-DBD plasma flow control and jet flow control methods were studied. Results shows both methods and improve the engine inlet performance. The flow rate and total pressure recovery ability is increased and drag is reduced. More results with unsteady control and optimized control parameters will present in the final article<\/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_15101002.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_15101002.pdf\">Read the full paper &gt; <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Wang Jianlei , Li Tiangang , Wei Zhen , Chen Bing , Gong Chunlin , Gu Liangxian<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<br \/>\nConference Number HiSST 2018_15101002<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[996,994,198,311,1001],"tags":[729,434,824,822,823],"class_list":["post-13481","post","type-post","status-publish","format-standard","hentry","category-high-speed-aerodynamics-and-aerothermodynamics","category-hisst-2018","category-hypersonic-aerodynamics","category-hypersonic-propulsion","category-propulsion-systems-and-components","tag-active-flow-control","tag-hisst-2018","tag-jet-flow-control","tag-ns-dbd-plasma-flow-control","tag-wide-envelope-inlet","category-996","category-994","category-198","category-311","category-1001","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13481","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=13481"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13481\/revisions"}],"predecessor-version":[{"id":16542,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13481\/revisions\/16542"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=13481"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=13481"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=13481"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}