{"id":17433,"date":"2024-06-13T12:52:25","date_gmt":"2024-06-13T12:52:25","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=17433"},"modified":"2024-06-14T13:10:25","modified_gmt":"2024-06-14T13:10:25","slug":"a-method-for-predicting-multivariate-random-loads-and-a-discrete-appoximation-of-the-mutidimensional-design-load-envelope","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/a-method-for-predicting-multivariate-random-loads-and-a-discrete-appoximation-of-the-mutidimensional-design-load-envelope\/","title":{"rendered":"A method for predicting multivariate random loads and a discrete appoximation of the mutidimensional design load envelope"},"content":{"rendered":"\n<p><strong>C.Aquilini, D.Parisse<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference Number: IFASD-2017-005<\/strong><\/p>\n\n\n\n<p>Random loads are of greatest concern during the design phase of new aircraft. They<br>can either result from a stationary Gaussian process, such as continuous turbulence, or from a<br>random process, such as buffet. Buffet phenomena are especially relevant for fighters flying in<br>the transonic regime at high angles of attack or when the turbulent, separated air flow induces<br>fluctuating pressures on structures like wing surfaces, horizontal tail planes, vertical tail planes,<br>airbrakes, flaps or landing gear doors.<br>In this paper a method is presented for predicting n-dimensional combined loads in the presence<br>of massively separated flows. This method can be used both early in the design process, when<br>only numerical data are available, and later, when test data measurements have been performed.<br>Moreover, the two-dimensional load envelope for combined load cases and its discretization,<br>which are well documented in the literature, are generalized to n dimensions, n \u2265 3.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/06\/IFASD-2017-005.pdf\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>C.Aquilini, D.Parisse<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference Number: IFASD-2017-005<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1958,1953],"tags":[1972,1970,1971,1973],"class_list":["post-17433","post","type-post","status-publish","format-standard","hentry","category-events","category-dynamic-loads","category-ifasd-2017","tag-aeroelasticity","tag-buffeting","tag-combined-random-loads","tag-multidimensional-design-load-envelope","category-993","category-1958","category-1953","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17433","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=17433"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17433\/revisions"}],"predecessor-version":[{"id":17486,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17433\/revisions\/17486"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=17433"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=17433"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=17433"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}