{"id":16088,"date":"2024-04-12T09:02:58","date_gmt":"2024-04-12T09:02:58","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16088"},"modified":"2024-04-12T09:02:59","modified_gmt":"2024-04-12T09:02:59","slug":"aerodynamic-characterization-of-stratofly-hypersonic-vehicle-by-means-of-engineering-methods-and-cfd-simulations","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/aerodynamic-characterization-of-stratofly-hypersonic-vehicle-by-means-of-engineering-methods-and-cfd-simulations\/","title":{"rendered":"Aerodynamic Characterization of Stratofly Hypersonic Vehicle by means of engineering methods and CFD simulations"},"content":{"rendered":"\n<p><strong>Pietro Roncioni, Marco Marini, Roberta Fusaro, Nicole Viola<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-422<\/strong><\/p>\n\n\n\n<p>In the framework of European Commission Horizon2020 STRATOFLY Project, the aerodynamic<br>characterization of external aeroshape of the hypersonic vehicle MR3 was conducted by means of<br>engineering tools in order to rapidly sizing the control surfaces for stability and maneuverability all over<br>the range of Mach number. One important aspect is the trimmability of the vehicle and so the correct<br>dimensioning of longitudinal control surfaces. The results of this activity are presented in terms of global<br>aerodynamic coefficients, control surfaces effects and stability derivatives. Sensitivity analysis with<br>respect to the available engineering methods and comparisons with CFD simulations will be shown too,<br>in order to provide reliable uncertainty ranges around the nominal data.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-422.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-422.pdf\">Read the full paper > <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Pietro Roncioni, Marco Marini, Roberta Fusaro, Nicole Viola<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-422<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1009,1006],"tags":[766,730,1021,655],"class_list":["post-16088","post","type-post","status-publish","format-standard","hentry","category-events","category-high-speed-missions-and-vehicles-hisst-2022","category-hisst-2022","tag-aerodynamics","tag-design","tag-flight-control","tag-hypersonic-vehicle","category-993","category-1009","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16088","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=16088"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16088\/revisions"}],"predecessor-version":[{"id":16089,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16088\/revisions\/16089"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16088"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16088"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16088"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}