{"id":18666,"date":"2024-11-20T11:42:01","date_gmt":"2024-11-20T11:42:01","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18666"},"modified":"2024-11-20T11:42:02","modified_gmt":"2024-11-20T11:42:02","slug":"integrated-flexible-dynamic-loads-models-based-on-aerodynamic-influence-coefficients-of-a-3d-panel-method","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/integrated-flexible-dynamic-loads-models-based-on-aerodynamic-influence-coefficients-of-a-3d-panel-method\/","title":{"rendered":"INTEGRATED FLEXIBLE DYNAMIC LOADS MODELS BASED ON AERODYNAMIC INFLUENCE COEFFICIENTS OF A 3D PANEL METHOD"},"content":{"rendered":"\n<p><strong>Thiemo M. Kier, Mark J. Verveld, Chris W. Burkett<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2015-179<\/strong><\/p>\n\n\n\n<p>The integration of loads analysis models using so called aerodynamic in-\ufb02uence coe\ufb03cients (AICs) is described. These AICs relate a change of normal velocity at panel control points to a change in panel pressure distribution, allowing to consider aeroelastic e\ufb00ects in a straight forward manner. The aerodynamic method employed for aeroelastic applications is typically the Vortex or Doublet Lattice Method, discretizing mean lifting surfaces. In this paper, the AICs are obtained by a 3D panel method, which signi\ufb01cantly increases the geometric \ufb01delity and accounts for previously unmodeled \ufb02ight mechanical e\ufb00ects. These e\ufb00ects are veri\ufb01ed by comparison with the Vortex Lattice Method and CFD results. Further, an interpolation scheme is required, since the AICs of 3D panel methods depend nonlinearly on the underlying \ufb02ight state. The setup of a reduced order aerodynamic model for AICs (AIC-ROM), based on proper orthogonal decomposition is presented and results are assessed.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/11\/IFASD-2015-179.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Thiemo M. Kier, Mark J. Verveld, Chris W. Burkett<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-179<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2413,2416],"tags":[1153,2742,2743,2483],"class_list":["post-18666","post","type-post","status-publish","format-standard","hentry","category-1-ifasd-2015","category-aerodynamics-cfd","tag-3d","tag-aerodynamic-inuence-coecients-integrated-exible-ight-dynamics-model","tag-manoeuvre-loads-analysis","tag-panel-method","category-2413","category-2416","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18666","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=18666"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18666\/revisions"}],"predecessor-version":[{"id":18668,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18666\/revisions\/18668"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18666"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18666"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18666"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}