{"id":18411,"date":"2024-11-18T14:53:08","date_gmt":"2024-11-18T14:53:08","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18411"},"modified":"2024-11-18T14:53:08","modified_gmt":"2024-11-18T14:53:08","slug":"evolutionary-approach-to-structural-design-of-wing-under-stress-buckling-and-aeroelasticity-requirements","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/evolutionary-approach-to-structural-design-of-wing-under-stress-buckling-and-aeroelasticity-requirements\/","title":{"rendered":"EVOLUTIONARY APPROACH TO STRUCTURAL DESIGN OF WING UNDER STRESS, BUCKLING AND AEROELASTICITY REQUIREMENTS"},"content":{"rendered":"\n<p><strong>Vasily V. Chedrik, Sergey A. Tuktarov<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2015-055<\/strong><\/p>\n\n\n\n<p>An evolutionary approach to synthesis of optimal aircraft component layouts has been developed. It is based on combined application of topology optimization, an engineering interpretation and optimum sizing of load-bearing structural elements. The developed approach gives possibility to include stress, buckling and aeroelasticity constraints altogether in unified design procedure and to get an optimal wing structure.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/11\/IFASD-2015-055.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Vasily V. Chedrik, Sergey A. Tuktarov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-055<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2413,2415],"tags":[1972,642,2555,1982,2554,695],"class_list":["post-18411","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-aeroelastic-optimisation","tag-aeroelasticity","tag-buckling","tag-finite-element-model-layout","tag-structural-optimization","tag-structural-strength","tag-topology-optimization","category-2413","category-2415","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18411","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=18411"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18411\/revisions"}],"predecessor-version":[{"id":18413,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18411\/revisions\/18413"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18411"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18411"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18411"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}