{"id":18036,"date":"2024-08-21T10:43:37","date_gmt":"2024-08-21T10:43:37","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18036"},"modified":"2024-08-21T10:43:38","modified_gmt":"2024-08-21T10:43:38","slug":"effect-of-angle-of-attack-gas-composition-and-reynolds-number-on-flutter-boundary-of-benchmark-super-critical-wing","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/effect-of-angle-of-attack-gas-composition-and-reynolds-number-on-flutter-boundary-of-benchmark-super-critical-wing\/","title":{"rendered":"EFFECT OF ANGLE OF ATTACK, GAS COMPOSITION AND REYNOLDS NUMBER ON FLUTTER BOUNDARY OF BENCHMARK SUPER-CRITICAL WING"},"content":{"rendered":"\n<p><strong>Jan Navr\u00e1til, Adam Jir\u00e1sek, Peter Hamlington, Lt. Col. Andrew Lofthouse<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2017-142<\/strong><\/p>\n\n\n\n<p>This paper presents results of the second Aeroelastic Prediction Workshop which uses the Benchmark Super-Critical Wing, BSCW at \ufb02utter conditions as a common test case. The primary purpose of this study is to evaluate the effect of angle of attack. To do so, we analyzed BSCW wing at three angles of attack \u03b1 = 0deg, \u03b1 = 1deg and \u03b1 = 5deg. The second task is to evaluate the effect of gas composition on \ufb02utter boundary. The two gases are R-12 heavy gas, used as a test medium for the wind tunnel test, and air.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/08\/IFASD-2017-142.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Jan Navr\u00e1til, Adam Jir\u00e1sek, Peter Hamlington, Lt. Col. Andrew Lofthouse<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-142<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1957,1953],"tags":[2239,1972,2213,2236,2238,2237,2235,683],"class_list":["post-18036","post","type-post","status-publish","format-standard","hentry","category-events","category-computational-aeroelasticity","category-ifasd-2017","tag-aepw","tag-aeroelasticity","tag-bscw","tag-computational","tag-dynamics","tag-uid","tag-utter","tag-transonic","category-993","category-1957","category-1953","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18036","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\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=18036"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18036\/revisions"}],"predecessor-version":[{"id":18038,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18036\/revisions\/18038"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18036"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18036"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18036"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}