{"id":13467,"date":"2023-10-26T18:25:33","date_gmt":"2023-10-26T18:25:33","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=13467"},"modified":"2024-05-03T14:27:31","modified_gmt":"2024-05-03T14:27:31","slug":"optimum-trim-of-an-experimental-hypersonic-glider","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2023\/10\/26\/optimum-trim-of-an-experimental-hypersonic-glider\/","title":{"rendered":"Optimum Trim of an Experimental Hypersonic Glider"},"content":{"rendered":"\n<p><strong>Victor F. Villace&nbsp; , Sergey A. Takovitskii<\/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_11201006<\/strong><\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p>Single point trimming of the hypersonic glider is not sufficient to accomplish the mission requirements and attain maximum performance. Applied to a hypersonic flight experiment, the present research shows that drifts of +\/-4% around the centre of gravity imply large penalties on the aerodynamic efficiency along the intended glider trajectory. The analysis is based upon a three degrees of freedom trajectory analysis. Beyond the current parametric analysis, the final manuscript will address the optimization of the vehicle trim to maximize the trajectory performance.<\/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_11201006.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_11201006.pdf\">Read the full paper &gt; <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Victor F. Villace\u00a0 , Sergey A. Takovitskii<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<br \/>\nConference Number HiSST 2018_11201006<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[997,994,198,257,1000],"tags":[434,807,660,806],"class_list":["post-13467","post","type-post","status-publish","format-standard","hentry","category-high-speed-missions-and-vehicles","category-hisst-2018","category-hypersonic-aerodynamics","category-hypersonic-flight-dynamics","category-operations-and-environment","tag-hisst-2018","tag-optimization","tag-trajectory","tag-trim","category-997","category-994","category-198","category-257","category-1000","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13467","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=13467"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13467\/revisions"}],"predecessor-version":[{"id":16548,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13467\/revisions\/16548"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=13467"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=13467"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=13467"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}