{"id":13618,"date":"2023-10-26T20:03:43","date_gmt":"2023-10-26T20:03:43","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=13618"},"modified":"2024-04-22T20:37:28","modified_gmt":"2024-04-22T20:37:28","slug":"noise-reduction-using-optimal-takeoff-thrust-management-for-supersonic-business-jet","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2023\/10\/26\/noise-reduction-using-optimal-takeoff-thrust-management-for-supersonic-business-jet\/","title":{"rendered":"Noise Reduction Using Optimal Takeoff Thrust Management for Supersonic Business Jet"},"content":{"rendered":"\n<p><strong>\u0410.\u0410. Mirzoyan<\/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_43401176<\/strong><\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p>Optimization of thrust management (TM) at initial climb may give an important reserve to improve noise performance of Supersonic Business Jet (SSBJ). A variable engine nozzle with a variable throat and exhaust area is often used as a component of supersonic propulsion system. Optimization of nozzle throat variation for jet noise reduction may significantly increase the environmental friendliness of SSBJ. Such optimal (low noise) variation of nozzle throat area at engine throttling provides fixed air flow and corresponding additional reduction of engine exhaust jet velocity.<\/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_43401176.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_43401176.pdf\">Read the full paper &gt; <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>\u0410.\u0410. Mirzoyan<\/b><\/p>\n<p>DoI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST 2018_43401176<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[997,994,313,1000],"tags":[434],"class_list":["post-13618","post","type-post","status-publish","format-standard","hentry","category-high-speed-missions-and-vehicles","category-hisst-2018","category-noise-reduction-technolgies","category-operations-and-environment","tag-hisst-2018","category-997","category-994","category-313","category-1000","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13618","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=13618"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13618\/revisions"}],"predecessor-version":[{"id":16361,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13618\/revisions\/16361"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=13618"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=13618"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=13618"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}