{"id":18307,"date":"2024-11-18T09:26:25","date_gmt":"2024-11-18T09:26:25","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18307"},"modified":"2024-11-18T09:26:26","modified_gmt":"2024-11-18T09:26:26","slug":"flight-loads-and-cumulative-fatique-damages-monitoring-for-each-aircraft-during-service-life","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/flight-loads-and-cumulative-fatique-damages-monitoring-for-each-aircraft-during-service-life\/","title":{"rendered":"FLIGHT LOADS AND CUMULATIVE FATIQUE DAMAGES MONITORING FOR EACH AIRCRAFT DURING SERVICE LIFE"},"content":{"rendered":"\n<p><strong>Victor I. Kleptsov , Vladimir I. Tsimbalyuk , Tatiana I. Orlova<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2015-008<\/strong><\/p>\n\n\n\n<p>The main purpose of this paper is the development of analytical-experimental algorithms based on FDR data to recover variable flight loads with optimal accuracy. This makes it possible to create automatic system for operational flight loads control and consumption of structure service life. In this case, the dependence of variable loads on the load factor in center of gravity (CG) is of statistical nature. Steady-state loads are recovered on the basis of flight parameters. The accuracy of this method is shown. The quality of monitoring is acceptable if numerous flights are processed and is comparable with accuracy of direct stress measurements. It is demonstrated that accuracy improvement can be done by increase of the sampling rate of FDR parameters.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/11\/IFASD-2015-008.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Victor I. Kleptsov , Vladimir I. Tsimbalyuk , Tatiana I. Orlova<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-008<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2413,2420],"tags":[2473,2471,2472],"class_list":["post-18307","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-loads","tag-cumulative-fatigue-damage","tag-flight-parameters","tag-variable-loads","category-2413","category-2420","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18307","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=18307"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18307\/revisions"}],"predecessor-version":[{"id":18309,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18307\/revisions\/18309"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18307"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18307"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18307"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}