{"id":13380,"date":"2023-10-13T14:42:58","date_gmt":"2023-10-13T14:42:58","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=13380"},"modified":"2024-05-03T14:43:17","modified_gmt":"2024-05-03T14:43:17","slug":"drag-reduction-of-hypersonic-spiked-blunt-body-with-sideward-jets","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2023\/10\/13\/drag-reduction-of-hypersonic-spiked-blunt-body-with-sideward-jets\/","title":{"rendered":"Drag Reduction of Hypersonic Spiked Blunt Body with Sideward Jets"},"content":{"rendered":"\n<p><strong>Guilai Han , Zonglin Jiang<\/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_2010873<\/strong><\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p>Drag reduction for blunt body flying at hypersonic speed were numerically investigated in this paper, with spikes and sideward jets applied to re-configurated the flow field. The spikes and the sideward jets led to the formation of the conical shock, the reattached shock, and the circumfluence, instead of a bow shock in front of the blunt body. The flow field reconfiguration played a dominant role in drag reduction. This paper proposed a parameter for the design of drag reduction of the spiked bodies, by combing the locations of the reattached shock and its interaction with the conical shock.<\/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_2010873.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_2010873.pdf\">Read the Full Paper&gt;<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Guilai Han , Zonglin Jiang<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<br \/>\nConference Number HiSST 2018_2010873<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[994,198,999,236],"tags":[690,434,440,492,691,689],"class_list":["post-13380","post","type-post","status-publish","format-standard","hentry","category-hisst-2018","category-hypersonic-aerodynamics","category-materials-and-structures-hisst-2018","category-supersonic-and-hypersonic-aircraft-design","tag-drag-reduction","tag-hisst-2018","tag-hypersonic","tag-numerical-simulation","tag-sideward-jet","tag-spike","category-994","category-198","category-999","category-236","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13380","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=13380"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13380\/revisions"}],"predecessor-version":[{"id":16568,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13380\/revisions\/16568"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=13380"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=13380"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=13380"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}