{"id":19072,"date":"2025-02-17T11:20:00","date_gmt":"2025-02-17T11:20:00","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=19072"},"modified":"2025-02-17T11:20:01","modified_gmt":"2025-02-17T11:20:01","slug":"numerical-analysis-of-limit-cycle-oscillation-of-a-supersonic-transport-wind-tunnel-test-model","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/17\/numerical-analysis-of-limit-cycle-oscillation-of-a-supersonic-transport-wind-tunnel-test-model\/","title":{"rendered":"NUMERICAL ANALYSIS OF LIMIT CYCLE OSCILLATION OF A SUPERSONIC TRANSPORT WIND TUNNEL TEST MODEL"},"content":{"rendered":"\n<p><strong>Kenichi SAITOH, Hamidreza KHEIRANDISH, Norio YOSHIMOTO<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2019-137<\/strong><\/p>\n\n\n\n<p>In the previous experimental research of aeroelasticity for supersonic transport wing model, limit cycle oscillation (LCO) boundary and amplitude characteristics have been obtained. The LCO started from smaller amplitude and grew up suddenly as dynamic pressure increased. Numerical analysis was performed for it, and large amplitude LCO was captured by Euler simulation. Bifurcation diagram was obtained by Harmonic balance method, and LCO amplitude is estimated.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/02\/IFASD-2019-137.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Kenichi SAITOH, Hamidreza KHEIRANDISH, Norio YOSHIMOTO<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-137<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2433,2448],"tags":[2997,2110,2065,2995,2996],"class_list":["post-19072","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2019","category-limit-cycle-oscillation","tag-euler-analysis","tag-harmonic-balance-method","tag-lco","tag-super-sonic-transport","tag-transonic-speed","category-2433","category-2448","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19072","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=19072"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19072\/revisions"}],"predecessor-version":[{"id":19074,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/19072\/revisions\/19074"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=19072"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=19072"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=19072"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}