{"id":18404,"date":"2024-11-18T14:47:08","date_gmt":"2024-11-18T14:47:08","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18404"},"modified":"2024-11-18T14:47:09","modified_gmt":"2024-11-18T14:47:09","slug":"designing-of-elastically-scaled-model-of-a-high-acpect-ratio-wing-using-digital-technologies","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/designing-of-elastically-scaled-model-of-a-high-acpect-ratio-wing-using-digital-technologies\/","title":{"rendered":"DESIGNING OF ELASTICALLY SCALED MODEL OF A HIGH ACPECT RATIO WING USING DIGITAL TECHNOLOGIES"},"content":{"rendered":"\n<p><strong>O. Orlova<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2015-053<\/strong><\/p>\n\n\n\n<p>Designing of an elastically scaled model of a high aspect ratio wing, which made using of digital technologies is considered. Model is made on the basis of rigid core and polymeric material with low modulus of elasticity. It is possible to use numerical control (NC) machines or 3D \u2013 printers during manufacturing. The search of required construction is carried out on the basis of finite element method (FEM) with the aid of optimization through influence coefficient matrix.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/11\/IFASD-2015-053.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>O. Orlova<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-053<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2413,2430],"tags":[2552,1623,2553,807,2469],"class_list":["post-18404","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-poster-presentations","tag-elastically-scaled-models","tag-fem","tag-influence-coefficient-matrix","tag-optimization","tag-static-aeroelasticity","category-2413","category-2430","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18404","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=18404"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18404\/revisions"}],"predecessor-version":[{"id":18407,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18404\/revisions\/18407"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18404"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18404"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18404"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}