{"id":17959,"date":"2024-08-16T11:38:01","date_gmt":"2024-08-16T11:38:01","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=17959"},"modified":"2024-08-16T11:38:01","modified_gmt":"2024-08-16T11:38:01","slug":"static-fully-coupled-simulation-of-a-transport-aircraft-high-lift-system","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/static-fully-coupled-simulation-of-a-transport-aircraft-high-lift-system\/","title":{"rendered":"STATIC FULLY COUPLED SIMULATION OF A TRANSPORT AIRCRAFT HIGH-LIFT SYSTEM"},"content":{"rendered":"\n<p><strong>Alessandro Lurgo, Robert Jung<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2017-119<\/strong><\/p>\n\n\n\n<p>Whenever the structure of an aircraft component is signi\ufb01cantly \ufb02exible, change in aerodynamic surfaces due to the structural \ufb02exibility must be taken into account in order to accurately model the behaviour of the component under aerodynamic load. This paper describes an industrial quasi steady aeroelastic application of an iteractive Computational Fluid Dynamics (CFD) Computational Structure Mechanics (CSM) co-simulation approach. This kind of approach is expected to represent a substantial improvement in predicting loads on component level. In this paper the outboard \ufb02ap system of a commercial aircraft is analysed. The model is built up with the commercial multibody software Adams. Particular care has been taken to model non-linear elements. The aerodynamic \ufb02ow is modelled through steady non-linear Reynolds Averaged Navier-Stokes (RANS) equations, including the engine jet ef\ufb02ux on the outboard \ufb02ap system. The \ufb02ow \ufb01eld is solved using the DLR (\u2018National Aeronautics and Space Centre\u2019) TAU code. A static analysis of the coupled system is presented. Towards the end of this paper, a test case for an unsteady Adams-TAU co-simulation of a wing is performed. The results are compared to a Nastran-Tau co-simulation of the same wing. This work represents a step towards the realization of an unsteady aeroelastic co-simulation of the outboard \ufb02ap system using the multibody approach.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/08\/IFASD-2017-119.pdf\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Alessandro Lurgo, Robert Jung<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-119<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1957,1953],"tags":[1972,2186,2187,2185,2188],"class_list":["post-17959","post","type-post","status-publish","format-standard","hentry","category-events","category-computational-aeroelasticity","category-ifasd-2017","tag-aeroelasticity","tag-co-simulation","tag-mesh-deformation","tag-multibody","tag-radial-basis-functions","category-993","category-1957","category-1953","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17959","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=17959"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17959\/revisions"}],"predecessor-version":[{"id":17961,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17959\/revisions\/17961"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=17959"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=17959"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=17959"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}