{"id":18496,"date":"2024-11-19T12:30:35","date_gmt":"2024-11-19T12:30:35","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18496"},"modified":"2024-11-19T12:30:36","modified_gmt":"2024-11-19T12:30:36","slug":"experimental-identification-of-the-flexibility-influence-matrix-of-the-aircraft-engine-mounted-on-pylon-under-the-wing","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/experimental-identification-of-the-flexibility-influence-matrix-of-the-aircraft-engine-mounted-on-pylon-under-the-wing\/","title":{"rendered":"EXPERIMENTAL IDENTIFICATION OF THE FLEXIBILITY INFLUENCE MATRIX OF THE AIRCRAFT ENGINE MOUNTED ON PYLON UNDER THE WING"},"content":{"rendered":"\n<p><strong>Alexei Grigoriev, Victor Malyutin, Alexei Chizhov, Andrei Gubernatenko<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2015-093<\/strong><\/p>\n\n\n\n<p>In this paper there is a description of the approach of the experimental definition of Elastic influence coefficients\u2019 matrix (ECM) using a number of linear displacements sensors and automated system of load application. Using the definition of the ECM of the engine mounted on wing of the dynamically-scaled model of the passenger aircraft as an example, the key characteristics of its realization are shown, which allow to minimize the main methodological inaccuracies.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/11\/IFASD-2015-093.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Alexei Grigoriev, Victor Malyutin, Alexei Chizhov, Andrei Gubernatenko<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-093<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2413,2421],"tags":[1972,2621,2622,2021],"class_list":["post-18496","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-experimental-methods","tag-aeroelasticity","tag-ecm","tag-stiffness-test","tag-structural-dynamics","category-2413","category-2421","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18496","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=18496"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18496\/revisions"}],"predecessor-version":[{"id":18498,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18496\/revisions\/18498"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18496"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18496"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18496"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}