{"id":11450,"date":"2023-07-19T15:17:20","date_gmt":"2023-07-19T15:17:20","guid":{"rendered":"https:\/\/aerospacerepository.org\/?page_id=11450"},"modified":"2026-09-10T12:25:56","modified_gmt":"2026-09-10T12:25:56","slug":"repository-aeronautics-systems","status":"publish","type":"page","link":"https:\/\/aerospacerepository.org\/index.php\/repository-aeronautics-systems\/","title":{"rendered":"Repository Aeronautics Systems"},"content":{"rendered":"\t\t<div data-elementor-type=\"wp-page\" data-elementor-id=\"11450\" class=\"elementor elementor-11450\" data-elementor-post-type=\"page\">\n\t\t\t\t\t\t<section class=\"elementor-section elementor-top-section elementor-element elementor-element-2c9bccf elementor-section-stretched elementor-section-boxed elementor-section-height-default elementor-section-height-default\" data-id=\"2c9bccf\" data-element_type=\"section\" data-e-type=\"section\" data-settings=\"{&quot;stretch_section&quot;:&quot;section-stretched&quot;,&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t\t\t\t<div class=\"elementor-container elementor-column-gap-default\">\n\t\t\t\t\t<div class=\"elementor-column elementor-col-100 elementor-top-column elementor-element elementor-element-b8dafde\" data-id=\"b8dafde\" data-element_type=\"column\" data-e-type=\"column\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-4b8cde6 elementor-widget elementor-widget-spacer\" data-id=\"4b8cde6\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-37c8102 elementor-widget elementor-widget-heading\" data-id=\"37c8102\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"heading.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<h1 class=\"elementor-heading-title elementor-size-default\"><b> Search all Systems Papers<\/b><\/h1>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-6d7d37c elementor-widget elementor-widget-spacer\" data-id=\"6d7d37c\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-bd75123 elementor-widget elementor-widget-spacer\" data-id=\"bd75123\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t<section class=\"elementor-section elementor-top-section elementor-element elementor-element-f5d0bce elementor-section-stretched elementor-section-boxed elementor-section-height-default elementor-section-height-default\" data-id=\"f5d0bce\" data-element_type=\"section\" data-e-type=\"section\" data-settings=\"{&quot;stretch_section&quot;:&quot;section-stretched&quot;,&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t\t\t\t<div class=\"elementor-container elementor-column-gap-default\">\n\t\t\t\t\t<div class=\"elementor-column elementor-col-100 elementor-top-column elementor-element elementor-element-96f2898\" data-id=\"96f2898\" data-element_type=\"column\" data-e-type=\"column\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-fef8474 elementor-widget elementor-widget-spacer\" data-id=\"fef8474\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-28eb3a3 elementor-widget elementor-widget-jet-ajax-search\" data-id=\"28eb3a3\" data-element_type=\"widget\" data-e-type=\"widget\" data-settings=\"{&quot;results_area_columns&quot;:1}\" data-widget_type=\"jet-ajax-search.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<div class=\"elementor-jet-ajax-search jet-search\">\n\t<div class=\"jet_search_listing_grid_hidden_template\" style=\"display: none;\">\n\t\t\t<\/div>\n\n<div class=\"jet-ajax-search\" 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Please, try again later!&quot;,&quot;show_search_suggestions&quot;:&quot;&quot;,&quot;search_suggestions_position&quot;:&quot;&quot;,&quot;search_suggestions_source&quot;:&quot;&quot;,&quot;search_suggestions_limits&quot;:&quot;&quot;,&quot;search_suggestions_item_title_length&quot;:&quot;&quot;,&quot;search_source_terms&quot;:&quot;&quot;,&quot;search_source_terms_title&quot;:&quot;&quot;,&quot;search_source_terms_icon&quot;:&quot;&quot;,&quot;search_source_terms_limit&quot;:&quot;&quot;,&quot;search_source_terms_listing_id&quot;:&quot;&quot;,&quot;search_source_terms_taxonomy&quot;:&quot;&quot;,&quot;search_source_users&quot;:&quot;&quot;,&quot;search_source_users_title&quot;:&quot;&quot;,&quot;search_source_users_icon&quot;:&quot;&quot;,&quot;search_source_users_limit&quot;:&quot;&quot;,&quot;search_source_users_listing_id&quot;:&quot;&quot;}\"><form class=\"jet-ajax-search__form\" method=\"get\" action=\"https:\/\/aerospacerepository.org\/\" role=\"search\" target=\"\">\n\t<div class=\"jet-ajax-search__fields-holder\">\n\t\t<div class=\"jet-ajax-search__field-wrapper\">\n\t\t\t<label for=\"search-input-28eb3a3\" class=\"screen-reader-text\">Search ...<\/label>\n\t\t\t\t\t\t<input id=\"search-input-28eb3a3\" class=\"jet-ajax-search__field\" type=\"search\" placeholder=\"Search all systems papers..\" value=\"\" name=\"s\" autocomplete=\"off\" \/>\n\t\t\t\t\t\t\t<input type=\"hidden\" value=\"{&quot;include_terms_ids&quot;:[3978]}\" name=\"jet_ajax_search_settings\" \/>\n\t\t\t\t\t\t\n\t\t\t\t\t<\/div>\n\t\t\t<\/div>\n\t\n<button class=\"jet-ajax-search__submit\" type=\"submit\" aria-label=\"Search submit\"><span class=\"jet-ajax-search__submit-icon jet-ajax-search-icon\"><i aria-hidden=\"true\" class=\"fas fa-search\"><\/i><\/span><\/button>\n<\/form>\n\n<div class=\"jet-ajax-search__results-area\" >\n\t<div class=\"jet-ajax-search__results-holder\">\n\t\t\t\t\t<div class=\"jet-ajax-search__results-header\">\n\t\t\t\t\n<button class=\"jet-ajax-search__results-count\" aria-label=\"View all results\"><span><\/span> Results<\/button>\n\t\t\t\t<div class=\"jet-ajax-search__navigation-holder\"><\/div>\n\t\t\t<\/div>\n\t\t\t\t\t\t<div class=\"jet-ajax-search__results-list results-area-col-desk-1 results-area-col-tablet-0 results-area-col-mobile-0 results-area-col-mobile-portrait-1\" >\n\t\t\t            <div class=\"jet-ajax-search__results-list-inner \"><\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t\t<div class=\"jet-ajax-search__results-footer\">\n\t\t\t\t\t\t\t\t\t<button class=\"jet-ajax-search__full-results\">See all results<\/button>\t\t\t\t\t\t\t\t<div class=\"jet-ajax-search__navigation-holder\"><\/div>\n\t\t\t<\/div>\n\t\t\t<\/div>\n\t<div class=\"jet-ajax-search__message\"><\/div>\n\t\n<div class=\"jet-ajax-search__spinner-holder\">\n\t<div class=\"jet-ajax-search__spinner\">\n\t\t<div class=\"rect rect-1\"><\/div>\n\t\t<div class=\"rect rect-2\"><\/div>\n\t\t<div class=\"rect rect-3\"><\/div>\n\t\t<div class=\"rect rect-4\"><\/div>\n\t\t<div class=\"rect rect-5\"><\/div>\n\t<\/div>\n<\/div>\n<\/div>\n<\/div>\n<\/div>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-e6a0308 elementor-widget elementor-widget-spacer\" data-id=\"e6a0308\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t<section class=\"elementor-section elementor-top-section elementor-element elementor-element-5406a7d elementor-section-stretched elementor-section-boxed elementor-section-height-default elementor-section-height-default\" data-id=\"5406a7d\" data-element_type=\"section\" data-e-type=\"section\" data-settings=\"{&quot;stretch_section&quot;:&quot;section-stretched&quot;,&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t\t\t\t<div class=\"elementor-container elementor-column-gap-default\">\n\t\t\t\t\t<div class=\"elementor-column elementor-col-25 elementor-top-column elementor-element elementor-element-f9cb2de\" data-id=\"f9cb2de\" data-element_type=\"column\" data-e-type=\"column\" data-settings=\"{&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-1c7c89c elementor-widget elementor-widget-spacer\" data-id=\"1c7c89c\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-d23dc2a elementor-widget elementor-widget-spacer\" data-id=\"d23dc2a\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-8c1dea0 elementor-widget elementor-widget-spacer\" data-id=\"8c1dea0\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-c38b1d9 elementor-widget elementor-widget-spacer\" data-id=\"c38b1d9\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-912ca3b elementor-widget elementor-widget-spacer\" data-id=\"912ca3b\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-f507582 elementor-widget elementor-widget-spacer\" data-id=\"f507582\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-ca061f6 elementor-widget elementor-widget-spacer\" data-id=\"ca061f6\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-b481f81 elementor-widget elementor-widget-spacer\" data-id=\"b481f81\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t<div class=\"elementor-column elementor-col-50 elementor-top-column elementor-element elementor-element-3a3cb99\" data-id=\"3a3cb99\" data-element_type=\"column\" data-e-type=\"column\" data-settings=\"{&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-c7b2ceb elementor-widget elementor-widget-spacer\" data-id=\"c7b2ceb\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-fb80527 elementor-widget elementor-widget-heading\" data-id=\"fb80527\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"heading.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<h2 class=\"elementor-heading-title elementor-size-default\">Results<\/h2>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-424a040 elementor-widget elementor-widget-jet-smart-filters-active hide-widget\" data-id=\"424a040\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"jet-smart-filters-active.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<div class=\"jet-smart-filters-active jet-active-filters jet-filter\" data-label=\"Active filters:\" data-content-provider=\"jet-engine\" data-additional-providers=\"\" data-apply-type=\"ajax\" data-query-id=\"default\"><\/div>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-03c22e8 elementor-widget elementor-widget-jet-smart-filters-sorting\" data-id=\"03c22e8\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"jet-smart-filters-sorting.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<div class=\"jet-smart-filters-sorting jet-filter\"><div\n\tclass=\"jet-sorting jet-sorting--flex-column\"\n\t data-smart-filter=\"sorting\" data-query-type=\"sort\" data-query-var=\"standard\" data-content-provider=\"\" data-query-id=\"default\" data-apply-type=\"ajax\" data-apply-on=\"value\" data-additional-providers=\"\">\n\t\t<select\n\t\tclass=\"jet-sorting-select\"\n\t\tname=\"select-name\"\n\t\t\t\taria-label=\"Sort filter\"\n\t>\n\t\t\t\t\t<option value=\"\">\n\t\t\t\tSort...\t\t\t<\/option>\n\t\t\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;title&quot;,&quot;order&quot;:&quot;ASC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy title from lowest to highest\t\t\t<\/option>\n\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;title&quot;,&quot;order&quot;:&quot;DESC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy title from highest to lowest\t\t\t<\/option>\n\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;date&quot;,&quot;order&quot;:&quot;ASC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy date from lowest to highest\t\t\t<\/option>\n\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;date&quot;,&quot;order&quot;:&quot;DESC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy date from highest to lowest\t\t\t<\/option>\n\t\t\t<\/select>\n<\/div>\n<\/div>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-5b3ecaf elementor-grid-1 elementor-grid-tablet-2 elementor-grid-mobile-1 elementor-posts--thumbnail-top elementor-card-shadow-yes elementor-posts__hover-gradient elementor-widget elementor-widget-posts\" data-id=\"5b3ecaf\" data-element_type=\"widget\" data-e-type=\"widget\" data-settings=\"{&quot;cards_columns&quot;:&quot;1&quot;,&quot;pagination_type&quot;:&quot;load_more_infinite_scroll&quot;,&quot;cards_row_gap&quot;:{&quot;unit&quot;:&quot;px&quot;,&quot;size&quot;:13,&quot;sizes&quot;:[]},&quot;cards_columns_tablet&quot;:&quot;2&quot;,&quot;cards_columns_mobile&quot;:&quot;1&quot;,&quot;cards_row_gap_tablet&quot;:{&quot;unit&quot;:&quot;px&quot;,&quot;size&quot;:&quot;&quot;,&quot;sizes&quot;:[]},&quot;cards_row_gap_mobile&quot;:{&quot;unit&quot;:&quot;px&quot;,&quot;size&quot;:&quot;&quot;,&quot;sizes&quot;:[]},&quot;load_more_spinner&quot;:{&quot;value&quot;:&quot;fas fa-spinner&quot;,&quot;library&quot;:&quot;fa-solid&quot;}}\" data-widget_type=\"posts.cards\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-posts-container elementor-posts elementor-posts--skin-cards elementor-grid\">\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-25535 post type-post status-publish format-standard hentry category-1-aerospace-europe-conference-2023 category-events category-8-human-factors tag-flight-simulator tag-seated-passenger tag-whole-body-vibration homepage_sections-systems category-3766 category-993 category-3774 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2026\/04\/07\/investigation-of-seated-passengers-vibration-using-a-full-flight-simulator\/\" target=&quot;_blank&quot;>\n\t\t\t\tInvestigation of seated passengers vibration using a full-flight simulator\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>ANTONIO ESPOSITO; CALOGERO ORLANDO; ANDREA ALAIMO<\/b><\/p>\n<p>DOI Number: 10.13009\/EUCASS2023-044<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19700 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-active-aeroelastic-control tag-flight-platform tag-flight-test homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/the-simulation-and-flight-verification-of-active-aeroelastic-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tThe simulation and flight verification of active aeroelastic control\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yi Liu, Kaihua Yuan, Xiaolong Cao, Yi Jin, Yang Meng<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-005<\/p>\n<p>Conference number: IFASD-2024-005<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19691 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-aircraft-control tag-aircraft-dynamic-loads homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/wind-law-proposal-for-aircraft-control-in-turbulence\/\" target=&quot;_blank&quot;>\n\t\t\t\tWind Law Proposal for Aircraft Control in Turbulence\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jerome Bazile<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-008<\/p>\n<p>Conference number: IFASD-2024-008<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19685 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-drag-reduction tag-high-aspect-ratio tag-wing-shape-control homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/wing-shape-control-on-the-d150-model-with-aspect-ratio-tradeoffs-for-fuel-efficiency-improvement\/\" target=&quot;_blank&quot;>\n\t\t\t\tWing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Fanglin Yu, Mil\u00e1n Barczi, Carlos Sebastia Saez, B\u00e9la Takarics, Yasser Meddaikar, Mirko Hornung<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-010<\/p>\n<p>Conference number: IFASD-2024-010<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19673 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-composite-wing tag-gust-load-alleviation tag-wingtip-device homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/gust-load-alleviation-efficiency-in-an-optimized-composite-wing-through-the-integration-of-wingtip-devices-incorporating-folding-and-twist-strategies\/\" target=&quot;_blank&quot;>\n\t\t\t\tGust load alleviation efficiency in an optimized composite wing through the integration of wingtip devices: Incorporating folding and twist strategies\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Touraj Farsadi, Majid Ahmadi, Hamed Haddad Khodaparast<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-014<\/p>\n<p>Conference number: IFASD-2024-014<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19646 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-composite-structures tag-gust-loads tag-passive-loads-alleviation tag-structural-dynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/preliminary-investigation-of-the-superelastic-monostable-spoiler-for-dynamic-gust-loads-alleviation\/\" target=&quot;_blank&quot;>\n\t\t\t\tPreliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Andrea Castrichini, Federica Siotto, Xiaoyang Sun, Josh Coppin, Raul Lozano Vargas, Ignacio Ballesteros Ruiz, Enzo Cosentino, Michael Hadjipantelis<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-026<\/p>\n<p>Conference number: IFASD-2024-026<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19636 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-control-design tag-gust-load-alleviation tag-lqg homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/modelling-complex-actuator-and-sensor-architectures-for-gust-alleviation-systems-of-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tModelling complex actuator and sensor architectures for gust alleviation systems of flexible aircraft\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Stefanie D\u00fcssler, Thulasi Mylvaganam, Rafael Palacios<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-029<\/p>\n<p>Conference number: IFASD-2024-029<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19627 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-flexible-wing tag-reinforcement-learning tag-stall-flutter homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/stall-flutter-suppression-with-active-camber-morphing-based-on-reinforcement-learning\/\" target=&quot;_blank&quot;>\n\t\t\t\tStall flutter suppression with active camber morphing based on reinforcement learning\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jinying Li, Yuting Dai, Chao Yang<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-032<\/p>\n<p>Conference number: IFASD-2024-032<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19607 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroservoelasticity tag-geometric-nonlinearity tag-gust-alleviation tag-large-aspect-ratio homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/deep-reinforcement-learning-for-aeroservoelastic-control-of-unmanned-multi-body-aircraft-with-geometric-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tDeep Reinforcement Learning for Aeroservoelastic Control of Unmanned Multi-Body Aircraft with Geometric Nonlinearities\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Zhuolin Ying, Ying Bi, Zijian Zhu, Chen Zhu, Xiaoping Ma<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-038<\/p>\n<p>Conference number: IFASD-2024-038<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19601 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-panel-method tag-unsteady-boundary-layer-method tag-viscous-correction homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/aerodynamic-analysis-of-aircraft-wings-using-a-coupled-pm-bl-approach\/\" target=&quot;_blank&quot;>\n\t\t\t\tAerodynamic analysis of aircraft wings using a coupled PM-BL approach\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Lipeng Zhu, Changchuan Xie, Yang Meng<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-041<\/p>\n<p>Conference number: IFASD-2024-041<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19598 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroservoelasticity tag-high-aspect-ratio tag-load-alleviation tag-servo-dynamics tag-time-delay homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/aeroservoelastic-analysis-and-load-alleviation-control-for-very-flexible-aircraft-tu-flex-study\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroservoelastic Analysis and Load Alleviation Control for Very Flexible Aircraft: TU-Flex Study\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Guilherme Chaves Barbosa, Alvaro Antonio Garc\u00eda Quesada, Pedro Jos\u00e9 Gonz\u00e1lez, Gerrit Stavorinus, Fl\u00e1vio Jos\u00e9 Silvestre<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-042<\/p>\n<p>Conference number: IFASD-2024-042<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19589 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroservoelasticity tag-frequency-time-domain-method tag-nonlinear-dynamics homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/dynamic-analysis-of-nonlinear-aeroservoelasticity-by-a-modified-frequency-time-domain-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tDynamic analysis of nonlinear aeroservoelasticity by a modified frequency-time domain method\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Peihan Wang, Zhigang Wu, Chao Yang<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-045<\/p>\n<p>Conference number: IFASD-2024-045<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19562 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-nonlinear-aeroelasticity tag-sma tag-smart-structures tag-structural-dynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/aeroelastic-analysis-of-a-smart-sma-composite-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic analysis of a smart SMA-composite wing\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Gefferson Silva, Flavio Silvestre, Mauricio Donadon<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-059<\/p>\n<p>Conference number: IFASD-2024-059<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19544 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-active-flutter-suppression tag-aeroservoelasticity tag-cfdcsm-coupling tag-compressible-aerodynamics tag-h-control homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/design-of-flutter-suppression-controllers-for-a-wing-in-compressible-flow-based-on-high-fidelity-aerodynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tDesign of flutter suppression controllers for a wing in compressible flow based on high-fidelity aerodynamics\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Boris Micheli, Jens Neumann, J\u00fcrgen Arnold<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-066<\/p>\n<p>Conference number: IFASD-2024-066<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19541 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-hot-films tag-laminar-turbulent-transition tag-natural-laminar-flow tag-oscillating-airfoil tag-transonic-flow tag-unsteady-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/analysis-of-the-impact-of-forced-pitching-oscillations-in-transonic-flow-on-the-transition-onset-and-the-aeroelastic-behaviour-of-an-airfoil\/\" target=&quot;_blank&quot;>\n\t\t\t\tAnalysis of the impact of forced pitching oscillations in transonic flow on the transition onset and the aeroelastic behaviour of an airfoil\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Italo Cafarelli, Cedric Liauzun, Fabien Mery, Jeanne Methel, Maxime Forte, Arnaud Lepage<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-067<\/p>\n<p>Conference number: IFASD-2024-067<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19505 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-reduced-order-models-1-ifasd-2024 tag-co-rotational tag-harmonic-balance-method tag-reduced-order-model tag-static-aeroelastic-analysis homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-3022 category-3041 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/reduced-order-modeling-analysis-for-flexible-wing-using-a-co-rotational-beam-element\/\" target=&quot;_blank&quot;>\n\t\t\t\tReduced order modeling analysis for flexible wing using a co-rotational beam element\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yali Shao, Changchuan Xie, Chao An, Duoyao Zhang, Yuhui Zhang<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-083<\/p>\n<p>Conference number: IFASD-2024-083<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19459 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-reduced-order-models-1-ifasd-2024 tag-active-control tag-conceptual-aircraft-design tag-reduced-order-modelling homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-3022 category-3041 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/flexible-aircraft-conceptual-co-design-based-on-the-rce-framework\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlexible aircraft conceptual co-design based on the RCE framework\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>B\u00e9la Takarics, B\u00e1lint Patarics, B\u00e1lint Vanek, Fanglin Yu, Yasser M. Meddaikar, Matthias Wuestenhagen, Thiemo Kier<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-099<\/p>\n<p>Conference number: IFASD-2024-099<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19447 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-active-flutter-suppression tag-afs tag-ase tag-control-law-design tag-flight-test-clearance tag-integrated-aeroservoelastic-simulation-models homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/aeroservoelastic-models-for-design-testing-flight-test-clearance-and-validation-of-active-flutter-suppression-control-laws\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Thiemo Kier, Matthias Wuestenhagen, \u00d6zge S\u00fcel\u00f6zgen, Ramesh Konatala, Yasser Meddaikar, Keith Soal, Nicolas Guerin, Julius Bartasevicius, B\u00e9la Takarics, Daniel Balogh, B\u00e1lint Vane<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-103<\/p>\n<p>Conference number: IFASD-2024-103<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19428 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-decentralized-control tag-flexible-aircraft tag-gla tag-gust-load-alleviation tag-optimization homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/decentralized-control-of-ailerons-for-gust-load-alleviation\/\" target=&quot;_blank&quot;>\n\t\t\t\tDecentralized Control of Ailerons for Gust Load Alleviation\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kolja Michel, Simon Schulz, Gertjan Looye, Guido Weber<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-109<\/p>\n<p>Conference number: IFASD-2024-109<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19425 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-kalman-state-estimator tag-sensor-fusion tag-slender tag-state-space homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/estimation-of-slender-body-elastic-rates-and-accelerations-using-a-combination-of-measured-data\/\" target=&quot;_blank&quot;>\n\t\t\t\tEstimation of slender body elastic rates and accelerations using a combination of measured data\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ilya Genkin, Daniella E. Raveh<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-110<\/p>\n<p>Conference number: IFASD-2024-110<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19387 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-active-control tag-flared-folding-wingtips tag-flutter tag-flutter-suppression homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/active-flutter-suppression-and-gust-load-alleviation-of-wings-incorporating-floating-wingtips\/\" target=&quot;_blank&quot;>\n\t\t\t\tActive flutter suppression and gust load alleviation of wings incorporating floating wingtips\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>William Mansey, Fintan Healy, Huaiyuan Gu, Djamel Rezgui, Jonathan Cooper<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-125<\/p>\n<p>Conference number: IFASD-2024-125<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19384 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-active-flutter-suppression tag-aeroelasticity tag-flight-flutter-testing tag-model-updating tag-system-identification tag-uav homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/post-flight-system-identification-and-aeroservoelastic-model-updating-for-prediction-and-validation-of-the-onset-of-flutter\/\" target=&quot;_blank&quot;>\n\t\t\t\tPost-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>\u00d6zge S\u00fcel\u00f6zgen, Gertjan Looye, Thiemo Kier, Matthias Wuestenhagen, Ramesh Konatala, Keith Soal, Nicolas Gu\u00e9rin, B\u00e1lint Vanek<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-128<\/p>\n<p>Conference number: IFASD-2024-128<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19372 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-reduced-order-models-1-ifasd-2024 tag-gust-load-analysis tag-machine-learning tag-nonlinear-parametric-model-order-reduction homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-3022 category-3041 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/machine-learning-based-parametric-model-order-reduction-for-the-gust-load-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tMachine learning-based parametric model order reduction for the gust load analysis\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sangmin Lee, SiHun Lee, Younggeun Park, Seung-Hoon Kang, Kijoo Jang, Haeseong Cho, SangJoon Shin<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-135<\/p>\n<p>Conference number: IFASD-2024-135<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19352 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-reduced-order-models-1-ifasd-2024 tag-flexible-wing tag-large-amplitude-motion tag-model-order-reduction tag-nonlinear homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-3022 category-3041 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/nonlinear-dynamic-response-of-a-pazy-wing-variant-using-koiter-newton-model-reduction\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear dynamic response of a pazy wing variant using Koiter-Newton model reduction\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kautuk Sinha, Farbod Alijani, Wolf Krueger, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-142<\/p>\n<p>Conference number: IFASD-2024-142<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19318 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-gust-load-alleviation tag-lidar tag-two-degree-of-freedom-controller homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/09\/lidar-based-gust-load-alleviation-increasing-the-load-reduction-potential-through-a-two-degree-of-freedom-controller-architecture\/\" target=&quot;_blank&quot;>\n\t\t\t\tLidar-based gust load alleviation &#8211; increasing the load reduction potential through a two-degree-of-freedom controller architecture\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christian Wallace, Nicolas Fezans<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-163<\/p>\n<p>Conference number: IFASD-2024-163<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19306 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-folding-wing-tip tag-gust-load-alleviation tag-passive-and-semi-active-control homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/09\/passive-and-active-load-alleviation-technologies-for-uharw-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tPassive and active load alleviation technologies for UHARW wings\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Francesco Toffol<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-167<\/p>\n<p>Conference number: IFASD-2024-167<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19273 post type-post status-publish format-standard hentry category-events category-aeroelastic-analysis-frameworks-1-ifasd-2024 category-ifasd-2024 tag-incremental-nonlinear-dynamic-inversion tag-limit-cycle-oscillation tag-robust-nonlinear-model-predictive-control homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3023 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/24\/nonlinear-incremental-robust-model-predictive-control-for-a-nonlinear-aeroservoelastic-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear Incremental Robust Model Predictive Control for a Nonlinear Aeroservoelastic System\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Tingyu Zhang, Xuerui Wang<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-181<\/p>\n<p>Conference number: IFASD-2024-181<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19270 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroservoelasticity tag-describing-function tag-gust-load-alleviation tag-onset-frequency tag-saturation-regime homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/24\/nonlinear-analysis-of-combined-rate-and-acceleration-limits-effect-on-actuator-performance\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear analysis of combined rate and acceleration limits effect on actuator performance\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Luca Marino, Xuerui Wang, Jurij Sodja<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-183<\/p>\n<p>Conference number: IFASD-2024-183<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19252 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelastic-control tag-flight-control tag-load-alleviation homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/24\/automated-tuning-of-a-baseline-flight-control-system-with-maneuver-load-alleviation-for-an-energy-efficient-passenger-airplane\/\" target=&quot;_blank&quot;>\n\t\t\t\tAutomated Tuning of a Baseline Flight Control System with Maneuver Load Alleviation for an Energy-Efficient Passenger Airplane\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Till Strothteicher, Nicolas Fezans<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-191<\/p>\n<p>Conference number: IFASD-2024-191<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19230 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-flight-dynamics tag-flight-testing tag-system-identification tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-3027 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/20\/flexible-aircraft-flight-dynamics-and-loads-model-identification-from-flight-test-data-in-unsteady-conditions\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlexible aircraft flight dynamics and loads model identification from flight test data in unsteady conditions\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Andres Jurisson, Bart Eussen, Coen de Visser, Roeland de Breuker<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-198<\/p>\n<p>Conference number: IFASD-2024-198<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19165 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-reduced-order-models-1-ifasd-2024 tag-aeroelastic-tailoring tag-aeroelasticity tag-concurrent-design tag-mdo tag-rom tag-symbolic-model tag-tensor-product-model homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-3022 category-3041 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/28\/mathematical-method-for-prediction-aeroelastic-phenomena-and-multidisciplinary-optimization-lifting-surfaces-of-flight-vehicle-at-preliminary-stage-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tMathematical method for prediction aeroelastic phenomena and multidisciplinary optimization lifting surfaces of flight vehicle at preliminary stage design\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Oleh Havaza, Vitalii Sukhov, Ruslan Nikitin<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-235<\/p>\n<p>Conference number: IFASD-2024-235<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18720 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-reduced-order-modelling tag-aircraft-loads tag-flexible-aircraft tag-load-alleviation tag-nonlinear-aeroelasticity tag-parametric-rom homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2418 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/parametric-reduced-order-model-for-rapid-prediction-of-dynamic-loads-and-aeroelastic-response-with-structural-nonlinearitie\/\" target=&quot;_blank&quot;>\n\t\t\t\tPARAMETRIC REDUCED ORDER MODEL FOR RAPID PREDICTION OF DYNAMIC LOADS AND AEROELASTIC RESPONSE WITH STRUCTURAL NONLINEARITIE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Michele Castellani, Yves Lemmens, Jonathan E. Cooper<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-208<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18717 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/limit-cycle-oscillations-of-a-pretensed-membrane-strip\/\" target=&quot;_blank&quot;>\n\t\t\t\tLimit-cycle Oscillations of a pretensed Membrane Strip\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ariel Drachinsky, Daniella E. Raveh<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-207<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18714 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/reynolds-averaged-navier-stokes-study-of-thetransonic-limit-cycle-oscillation-phenomenon-onthe-f-16-fighter-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tReynolds-averaged Navier-Stokes Study of theTransonic Limit Cycle Oscillation Phenomenon onthe F-16 Fighter Aircraft\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Michael Iovnovich, Daniella E. Raveh, Dan Michaels, Motti Adar<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-206<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18711 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-approximation-of-unsteady-aerodynamic-coefficients tag-flutter-calculation-method tag-non-linear-transonic-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/non-linear-unsteady-aerodynamics-application-for-airliner-flutter-research\/\" target=&quot;_blank&quot;>\n\t\t\t\tNON-LINEAR UNSTEADY AERODYNAMICS APPLICATION FOR AIRLINER FLUTTER RESEARCH\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Chuban A.V., Chuban V.D.<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-204<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18690 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 tag-aerodynamics tag-morphing tag-shear-layer tag-time-resolved-piv tag-turbulence homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/time-resolved-piv-measurements-of-a-hybrid-morphing-naca4412-airfoil\/\" target=&quot;_blank&quot;>\n\t\t\t\tTime resolved PIV measurements of a hybrid morphing NACA4412 airfoil\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Johannes Scheller, Karl-Joseph Rizzo, Gurvan Jodin, Eric Duhayon, Jean-Francois Rouchon, Giles Harran, Marianna Braza<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-190<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18687 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-blade-shape-optimization tag-disk-weight-minimization tag-structural-optimization homepage_sections-helicopters homepage_sections-materials-and-structures homepage_sections-propulsion homepage_sections-systems category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/compressor-blade-and-disc-optimal-structural-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPRESSOR BLADE AND DISC OPTIMAL STRUCTURAL DESIGN\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Joury M. Temis, , Denis A. Yakushev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-188<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18681 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-dlr-tau-code tag-flutter tag-gcro-dr tag-gmres tag-gust-response tag-krylov-subspace-recycling tag-linearised-computational-fluid-dynamics tag-shock-buet homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/krylov-subspace-recycling-for-linearised-aerodynamics-analysis-using-dlr-tau\/\" target=&quot;_blank&quot;>\n\t\t\t\tKRYLOV SUBSPACE RECYCLING FOR LINEARISED AERODYNAMICS ANALYSIS USING DLR\u2013TAU\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>S. Xu, S. Timme, K. J. Badcock<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-186<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18675 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-aeroelasticity tag-arbitrary-polynomial-chaos tag-composite-materials tag-polar-method homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/uncertainty-quantification-in-aeroelastic-response-of-an-idealized-composite-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tUNCERTAINTY QUANTIFICATION IN AEROELASTIC RESPONSE OF AN IDEALIZED COMPOSITE WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christian T. Nitschke, Jonas Maruani, Angela Vincenti, Didier Lucor, Jean-Camille Chassaing<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-182<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18669 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-abaqus tag-aeroelasticy tag-aircraft tag-exible tag-simulation homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/aeroelastic-simulations-of-flexible-aircraft-with-the-commercial-structural-solver-abaqus\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC SIMULATIONS OF FLEXIBLE AIRCRAFT WITH THE COMMERCIAL STRUCTURAL SOLVER ABAQUS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Marcos C. Ruggeri, Roberto G. A. da Silva, Carlos E. de Souza<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-180<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18663 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-cfd-csm tag-coupling tag-fluid-structure tag-gust tag-openfsi homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/openfsi-interface-for-strongly-coupled-steady-and-unsteady-aeroelasticity\/\" target=&quot;_blank&quot;>\n\t\t\t\tOPENFSI INTERFACE FOR STRONGLY COUPLED STEADY AND UNSTEADY AEROELASTICITY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>C. Valente, D. Jones, A. Gaitonde, J. E. Cooper, Y. Lemmens<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-178<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18657 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-computational-aeroelastic-analysis tag-euler-analysis-of-unsteady-flows tag-flutter-flight-test tag-real-time-damping-estimation homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/a-correlation-study-of-modal-parameters-between-flutter-testing-and-cfd-simulation\/\" target=&quot;_blank&quot;>\n\t\t\t\tA CORRELATION STUDY OF MODAL PARAMETERS BETWEEN FLUTTER TESTING AND CFD SIMULATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>S. Orlando, M. Brughmans, T. Karaa\u011fa\u00e7l\u0131, \u00dc. Ceyhan, \u00d6. S\u00fcmer, M.E. Cerit, B. Durak<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-175<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18643 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-boundary-layer tag-panel-utter homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/influence-of-the-boundary-layer-on-flutter-of-elastic-plate-in-supersonic-gas-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF THE BOUNDARY LAYER ON FLUTTER OF ELASTIC PLATE IN SUPERSONIC GAS FLOW\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vsevolod O. Bondarev, Vasily V. Vedeneev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-168<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18640 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-action tag-aerodynamic-non-linearities tag-uid-structure-inter tag-p-k-method-limit-cycle-oscillations homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/prediction-of-aeroelastic-limit-cycle-oscillations-based-on-harmonic-forced-motion-oscillations\/\" target=&quot;_blank&quot;>\n\t\t\t\tPREDICTION OF AEROELASTIC LIMIT-CYCLE OSCILLATIONS BASED ON HARMONIC FORCED MOTION OSCILLATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A.C.L.M van Rooij, J. Nitzsche, R.P. Dwight<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-166<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18637 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-compact-gas-turbine tag-foil-gasdynamic-bearings tag-nonlinear-vibrations tag-rotor-dynamics tag-test-rig homepage_sections-helicopters homepage_sections-materials-and-structures homepage_sections-propulsion homepage_sections-systems category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/rotor-dynamics-of-compact-gas-turbine-unit-with-gas-bearings-investigation\/\" target=&quot;_blank&quot;>\n\t\t\t\tROTOR DYNAMICS OF COMPACT GAS TURBINE UNIT WITH GAS BEARINGS INVESTIGATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>D. Sc., Prof. Temis J.M., PhD Temis M.J., Egorov A.M.<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-164<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18631 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-structural-dynamics-shimmy tag-aerial-delivery tag-loads tag-structural-dynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2432 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/aerial-delivery-dynamic-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tAERIAL DELIVERY DYNAMIC LOADS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. P\u00e9rez de la Serna, A. J. Rodr\u00edguez Jim\u00e9nez, M. Oliver, H. Climent<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-160<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18628 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-engine-imbalance tag-ground-vibration-tests tag-rotating-inertial-force tag-simulation homepage_sections-avionics homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/airplane-ground-tests-with-rotating-force-simulation\/\" target=&quot;_blank&quot;>\n\t\t\t\tAIRPLANE GROUND TESTS WITH ROTATING FORCE SIMULATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Regina V. Leonteva<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-158<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18622 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-structural-dynamics-shimmy tag-frequency-response tag-nonlinear-dynamics tag-rubber tag-softening-effect tag-structural-dynamic-modification homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2432 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/nonlinear-dynamic-analysis-of-assembled-aircraft-structures-with-concentrated-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR DYNAMIC ANALYSIS OF ASSEMBLED AIRCRAFT STRUCTURES WITH CONCENTRATED NONLINEARITIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>E. Menga, S. Hernandez, S. Moledo, C. Lopez<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-155<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18619 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-cfd-csm-interaction tag-nonlinear-structure tag-oscillations tag-tau tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/limit-cylcle-oscillation-simulations-of-aerostabil-windtunnel-experiments\/\" target=&quot;_blank&quot;>\n\t\t\t\tLIMIT-CYLCLE-OSCILLATION SIMULATIONS OF AEROSTABIL WINDTUNNEL EXPERIMENTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Bernd Stickan, Johannes Dillinger, Jens Nitzsche<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-154<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18606 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods-bridges tag-adaptive-wing tag-aeroelastic-analysis tag-videogrammetry homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2427 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/structural-dynamic-investigation-of-adaptive-wing-demonstrator-within-sade-project\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTRUCTURAL DYNAMIC INVESTIGATION OF ADAPTIVE WING DEMONSTRATOR WITHIN SADE PROJECT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Gennady A. Amiryants, Vladimir P. Kulesh, Victor A. Malyutin, Andrey V. Smotrov, Alexander V. Chedrik<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-148<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18603 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-hale tag-large-deformation tag-static tag-uvlm homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/efficient-analysis-of-hale-aircraft-structure-for-static-and-dynamic-aeroelastic-behavior\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT ANALYSIS OF HALE AIRCRAFT STRUCTURE FOR STATIC AND DYNAMIC AEROELASTIC BEHAVIOR\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Lu LIU, Taehyoun KIM, Kwok Leung LAI<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-147<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18597 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-aeroelastic-galloping tag-narmax tag-system-identification homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/bifurcation-analysis-of-the-aeroelastic-galloping-problem-via-input-output-parametric-modelling\/\" target=&quot;_blank&quot;>\n\t\t\t\tBifurcation Analysis of the Aeroelastic Galloping Problem via Input-Output Parametric Modelling\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nicholas F. Giannelis, Gareth A. Vio<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-144<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18594 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-reduced-order-modelling tag-aic-correction tag-dynamic-loads tag-gust-encounter tag-rom homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2418 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/a-reduced-order-model-for-dynamic-loads-prediction-including-aerodynamic-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tA REDUCED ORDER MODEL FOR DYNAMIC LOADS PREDICTION INCLUDING AERODYNAMIC NONLINEARITIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>David Quero, Wolf Kr\u00fcger and Guillermo Jenaro<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-141<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18591 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-aeroelasticity tag-gvt-ground-vibration-tests tag-ifasd tag-structural-dynamics homepage_sections-avionics homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/state-of-the-art-of-gvt-technology-in-russia-and-possible-directions-to-increase-accuracy-and-reliability\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTATE OF THE ART OF GVT TECHNOLOGY IN RUSSIA AND POSSIBLE DIRECTIONS TO INCREASE ACCURACY AND RELIABILITY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Petr G. Karkle, Michail A. Pronin, Michail M. Bogatyrev, Gleb V. Liseykin, Klaas Dijkstra<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-140<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18588 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-crashworthiness tag-ditching tag-fluid-structure-interaction tag-structural-dynamics homepage_sections-aircraft-design homepage_sections-systems category-2413 category-2426 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/experimental-ditching-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL DITCHING LOADS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>H. Climent, G. Pastor, J.T. Viana, L. Ben\u00edtez, A. Iafrati<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-139<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18573 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-circulation-control tag-utter tag-modal-reduction tag-reduced-order-model homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/dynamic-instabilities-of-circulation-controlled-aerofoils\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC INSTABILITIES OF CIRCULATION CONTROLLED AEROFOILS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ian Krukow, Nora Neuert, Dieter Dinkler<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-134<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18567 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-aeroelasticity tag-health-monitoring tag-loads tag-observer tag-state-estimation homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/embedding-a-multi-body-model-of-a-fixed-wing-aircraft-in-a-nonlinear-state-observer\/\" target=&quot;_blank&quot;>\n\t\t\t\tEMBEDDING A MULTI-BODY MODEL OF A FIXED-WING AIRCRAFT IN A NONLINEAR STATE OBSERVER\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Tuur L. Benoit, Yves C. Lemmens, Wim A. Desmet<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-130<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18555 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods tag-computational-fluid-dynamics tag-experimental-aerodynamics tag-experimental-aeroelasticity tag-fluid-structure-interaction tag-gust-generator homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2421 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/design-and-testing-of-a-low-subsonic-wind-tunnel-gust-generator\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN AND TESTING OF A LOW SUBSONIC WIND TUNNEL GUST GENERATOR\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>P.M.G.J. Lancelot, J. Sodja, N.P.M. Werter, R. De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-124<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18549 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-ground-vibration-testing tag-strain-modal-analysis tag-strain-sensors homepage_sections-avionics homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/the-use-of-dynamic-strain-sensors-and-measurements-on-the-ground-vibration-testing-of-an-f-16-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHE USE OF DYNAMIC STRAIN SENSORS AND MEASUREMENTS ON THE GROUND VIBRATION TESTING OF AN F-16 AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Fabio L. M. dos Santos, Bart Peeters, Jan Debille, Carmine Salzano, Luiz Carlos, S. Goes, Wim Desmet<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-122<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18543 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-cfd tag-multi-fidelity-aeroelasticity tag-panel-aerodynamics tag-static-aeroelasticity homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/accelerated-convergence-of-high-fidelity-aeroelasticity-using-low-fidelity-aerodynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tACCELERATED CONVERGENCE OF HIGH-FIDELITY AEROELASTICITY USING LOW-FIDELITY AERODYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>K. Jovanov, R. De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-119<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18535 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods tag-data-acquisition tag-experimental-modal-analysis tag-noise tag-piezoelectric-materials homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2421 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/on-the-data-acquisiton-for-aeroelastic-analysis-using-pzt-lead-zirconate-titanate-excitation-and-test-parameters-definition\/\" target=&quot;_blank&quot;>\n\t\t\t\tON THE DATA ACQUISITON FOR AEROELASTIC ANALYSIS USING PZT (LEAD ZIRCONATE TITANATE) EXCITATION AND TEST PARAMETERS DEFINITION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>\u00c9der L. Oliveira, Roberto G. A. da Silva, Nuno M. M Maia, Adolfo G. Marto, Frederico J. Afonso, Afzal Suleman<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-115<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18532 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-structural-dynamics-shimmy tag-aeroelasticity tag-structural-dynamics tag-unsteady-aerodynamics tag-vibrations homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2432 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/main-landing-gear-door-dynamic-loads-due-to-unsteady-aerodynamics-a-predictive-and-validated-methodology\/\" target=&quot;_blank&quot;>\n\t\t\t\tMAIN LANDING GEAR DOOR DYNAMIC LOADS DUE TO UNSTEADY AERODYNAMICS: A PREDICTIVE AND VALIDATED METHODOLOGY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>R. Abarca, D. Arenillas, O. Castro, B. Masi\u00e1, E. Menga, M. Barth<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-114<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18523 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-aerodynamic-analysis tag-aerodynamic-singularities tag-blade tag-campbells-diagramm tag-design-process-flutter tag-elastic-modes tag-helicopter-aeroelasticity tag-rotor homepage_sections-helicopters homepage_sections-materials-and-structures homepage_sections-propulsion homepage_sections-systems category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/alternative-problem-formulations-for-identification-of-mathematical-model-of-helicopter-rotor-blade-and-some-problems-of-aeroelasticity-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tALTERNATIVE PROBLEM FORMULATIONS FOR IDENTIFICATION OF MATHEMATICAL MODEL OF HELICOPTER ROTOR BLADE AND SOME PROBLEMS OF AEROELASTICITY ANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vadim Yu.Eremin, Sergei E.Paryshev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-105<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18514 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-best-linear-approximation tag-nonlinear-distortions tag-system-identification homepage_sections-avionics homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/nonlinear-ground-vibration-identification-of-an-f-16-aircraft-part-i-fast-nonparametric-analysis-of-distortions-in-frf-measurements\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR GROUND VIBRATION IDENTIFICATION OF AN F-16 AIRCRAFT PART I: FAST NONPARAMETRIC ANALYSIS OF DISTORTIONS IN FRF MEASUREMENTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M. Vaes, J. Schoukens, Y. Rolain, B. Peeters, J. Debille, T. Dossogne3, J.P. No\u00ebl, C. Grappasonni, G. Kerschen<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-101<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18511 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-structural-dynamics-shimmy tag-dampers tag-development-testing tag-ground-testing tag-ground-vibration-testing tag-landing-gear tag-resonant-characteristics tag-shimmy homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2432 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/experimental-methods-of-studying-of-dynamic-characteristics-of-airplane-landing-gear\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL METHODS OF STUDYING OF DYNAMIC CHARACTERISTICS OF AIRPLANE LANDING GEAR\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A.V. Krapivko, V.N. Zadonskay, E.S. Kolyshev, S.E. Paryshev, E.A. Dubovsky<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-099<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18505 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-aeroservoelasticity tag-generalized-aerodynamic-forces tag-linearized-euler-solver homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/linearized-fun3d-for-rapid-aeroelastic-design-and-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tLINEARIZED FUN3D FOR RAPID AEROELASTIC DESIGN AND ANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Shuchi Yang, P.C. Chen, Zhicun Wang<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-097<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18499 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-flutter-testing tag-free-decays tag-modal-analysis tag-system-identification homepage_sections-avionics homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/an-efficient-approach-for-in-operation-modal-analysis-of-flutter-flight-tests\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN EFFICIENT APPROACH FOR IN-OPERATION MODAL ANALYSIS OF FLUTTER FLIGHT TESTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>B. Jacquier, P. Vacher, S. Leroy, D. Walker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-095<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18496 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods tag-aeroelasticity tag-ecm tag-stiffness-test tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2421 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/experimental-identification-of-the-flexibility-influence-matrix-of-the-aircraft-engine-mounted-on-pylon-under-the-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL IDENTIFICATION OF THE FLEXIBILITY INFLUENCE MATRIX OF THE AIRCRAFT ENGINE MOUNTED ON PYLON UNDER THE WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alexei Grigoriev, Victor Malyutin, Alexei Chizhov, Andrei Gubernatenko<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-093<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18478 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-structural-dynamics-shimmy tag-coupling tag-landing-gear tag-modal-analysis tag-shimmy tag-structural-dynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2432 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/study-of-shimmy-in-industrial-context\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTUDY OF SHIMMY IN INDUSTRIAL CONTEXT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ludovic MARTIN, Vincent JACQUES, Yves MARTIN-SIEGFRIED<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-083<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18475 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-reduced-order-modelling tag-aeroelasticity tag-neural-networks tag-reduced-order-modeling tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2418 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/nonlinear-reduced-order-modeling-of-unsteady-aerodynamic-loads-based-on-dynamic-local-linear-neuro-fuzzy-models\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR REDUCED-ORDER MODELING OF UNSTEADY AERODYNAMIC LOADS BASED ON DYNAMIC LOCAL LINEAR NEURO-FUZZY MODELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Maximilian Winter, Christian Breitsamter<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-082<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18460 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-aeroelastic tag-flutter tag-geometric-nonlinearity tag-high-aspect-ratio homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/geometrical-nonlinear-aeroelastic-analysis-of-large-aircraft-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tGEOMETRICAL NONLINEAR AEROELASTIC ANALYSIS OF LARGE AIRCRAFT WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Zhang Chao, He Jingwu , Xie Changchuan, Liu Yi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-076<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18454 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 tag-damping-coefficients tag-natural-frequencies tag-refueling-system homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/dynamic-stability-of-a-hose-drogue-wing-system-for-aerial-refueling\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC STABILITY OF A HOSE-DROGUE-WING SYSTEM FOR AERIAL REFUELING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>P. Garc\u00eda-Fogeda, F. Ar\u00e9valo<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-074<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18448 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 tag-dielectric-elastomers tag-feedback-control tag-fluid-structure-interaction tag-hyperelastic tag-low-reynolds tag-reduced-order-modelling tag-system-identication homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/reduced-order-modelling-and-feedback-control-of-integrally-actuated-membrane-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tREDUCED-ORDER MODELLING AND FEEDBACK CONTROL OF INTEGRALLY ACTUATED MEMBRANE WINGS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Stefano Buoso, Rafael Palacios<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-072<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18441 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-crashworthiness tag-a400m tag-dynamic-loads tag-landing-gear tag-uerf homepage_sections-aircraft-design homepage_sections-systems category-2413 category-2426 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/certification-of-landing-gear-structure-under-uerf-event\/\" target=&quot;_blank&quot;>\n\t\t\t\tCERTIFICATION OF LANDING GEAR STRUCTURE UNDER UERF EVENT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Gomez Vinas, Esteban, Chorro Matinez. J.Manuel, Martinez Perez Angel, Perez Hernandez, J.M, Perez San Jose, Jorge<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-069<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18432 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-continuous-turbulence tag-flutter tag-gust tag-small-disturbance-cfd tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/verification-of-the-use-of-small-disturbance-cfd-aerodynamics-in-flutter-and-gust-analyses-for-simple-to-highly-complex-configurations\/\" target=&quot;_blank&quot;>\n\t\t\t\tVerification of the use of small-disturbance CFD aerodynamics in flutter and gust analyses for simple to highly complex configurations\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Cyrille Vidy, Lukas Katzenmeier, Maximilian Winter, Christian Breitsamter<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-066<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18429 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-aeroelastic tag-geometric-nonlinearity tag-static-stability tag-trim homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/the-aeroelastic-trim-and-static-stability-analysis-of-highly-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHE AEROELASTIC TRIM AND STATIC STABILITY ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Hu Rui, Xie Changchuan, Liu Yi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p> Conference Number: IFASD-2015-064<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18408 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/nonlinear-actuator-modeling-for-aeroservoelastic-dynamic-loads-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear Actuator Modeling for Aeroservoelastic Dynamic Loads Simulations\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Rami Veiberman, Martin Weiss, Moti Karpel<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-054<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18397 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods-bridges tag-aatb tag-nonlinear tag-transfer-function tag-unsteady-aerodynamics tag-wind-tunnel-testing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2427 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/experiments-on-the-active-aeroelastic-test-bench-aatb-for-the-identification-of-unsteady-aerodynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTS ON THE ACTIVE AEROELASTIC TEST BENCH (AATB) FOR THE IDENTIFICATION OF UNSTEADY AERODYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>J. Ertveldt , J. Schoukens , R. Pintelon, S. Vanlanduit<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-050<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18391 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aileron-buzz tag-computational-aeroelasticity tag-describing-function tag-uid-structure-interaction tag-limit-cycle-oscillation homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/multiple-input-dscribing-function-analysis-of-non-classical-aileron-buzz\/\" target=&quot;_blank&quot;>\n\t\t\t\tMULTIPLE INPUT DSCRIBING FUNCTION ANALYSIS OF NON-CLASSICAL AILERON BUZZ\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M. Irfan Zafar, Francesca Fusi, Giuseppe Quaranta<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-048<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18383 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-aeroelasticity tag-experimental tag-structural-dynamics tag-validation homepage_sections-helicopters homepage_sections-materials-and-structures homepage_sections-propulsion homepage_sections-systems category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/cror-blade-deformation-part-2-aeroelastic-computations-and-comparison-with-experiments\/\" target=&quot;_blank&quot;>\n\t\t\t\tCROR BLADE DEFORMATION, PART 2: AEROELASTIC COMPUTATIONS AND COMPARISON WITH EXPERIMENTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Y. Mauffrey, A. Geeraert, S. Verley<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-043<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18380 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-aeroelasticity tag-experimental tag-polynomial-chaos-expansion-structural-dynamics tag-validation homepage_sections-helicopters homepage_sections-materials-and-structures homepage_sections-propulsion homepage_sections-systems category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/sensor-calibration-for-calculation-of-loads-on-a-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tSENSOR CALIBRATION FOR CALCULATION OF LOADS ON A FLEXIBLE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Marcus Vinicius P. Viana<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-042<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18377 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-apu tag-flap-door tag-flight-test tag-strength-and-fatigue-justification tag-structural-dynamics tag-unsteady-aerodynamic tag-vibrations tag-wind-tunnel-test homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/combined-unsteady-aerodynamics-and-structural-response-on-auxiliary-power-unit-flap-door-strength-and-fatigue-justification-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMBINED UNSTEADY AERODYNAMICS AND STRUCTURAL RESPONSE ON AUXILIARY POWER UNIT FLAP DOOR: STRENGTH AND FATIGUE JUSTIFICATION METHOD\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>PALOMARES A., ABARCA R., BARTH M<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-041<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18371 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods-bridges tag-amplitude-frequency-spectrum tag-pressure-oscillation tag-wake tag-wing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2427 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/loading-parameters-of-a-long-range-aircraft-wing-in-wind-tunnel-close-to-buffet-boundary\/\" target=&quot;_blank&quot;>\n\t\t\t\tLOADING PARAMETERS OF A LONG-RANGE AIRCRAFT WING IN WIND TUNNEL CLOSE TO BUFFET BOUNDARY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nikolay Bragin, Mansur Garifulin, Sergey Skomorokhov, Vitaliy Yanin<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-038<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18362 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-f-16-aircraft tag-ground-vibration-testing tag-sine-sweep-excitation tag-structural-nonlinearities homepage_sections-avionics homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/nonlinear-ground-vibration-identification-of-an-f-16-aircraft-part-ii-understanding-nonlinear-behaviour-in-aerospace-structures-using-sine-sweep-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR GROUND VIBRATION IDENTIFICATION OF AN F-16 AIRCRAFT PART II: UNDERSTANDING NONLINEAR BEHAVIOUR IN AEROSPACE STRUCTURES USING SINE-SWEEP TESTING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Dossogne, J.P. No\u00ebl, C. Grappasonni, G. Kerschen, B. Peeters, J. Debille, M. Vaes, J. Schoukens<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-035<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18356 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-composite tag-isogeometric tag-multi-fidelity tag-optimization tag-wind-turbine homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/isogeometric-framework-for-aeroelastic-wind-turbine-rotor-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tIsogeometric Framework for Aeroelastic Wind Turbine Rotor Analysis\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Etana Ferede, Mostafa M. Abdalla, Johannes K.S. Dillinger<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-030<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18353 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-crashworthiness tag-ditching tag-fluid-structure-interaction tag-structural-dynamics homepage_sections-aircraft-design homepage_sections-systems category-2413 category-2426 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/numerical-simulation-of-ditching-dynamic-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL SIMULATION OF DITCHING DYNAMIC LOADS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>J. T. Viana, J. Romera, G. Pastor, L. Ben\u00edtez, H. Climent, M. H. Siemann<\/b><\/p>\n<p>DOI Number; N\/A<\/p>\n<p>Conference number: IFASD-2015-028<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18350 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods-bridges tag-artificial-flow tag-dynamic-aeroelasticity tag-electromechanical-modeling tag-flutter homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2427 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/research-on-dynamic-stability-of-an-elastic-model-using-tests-in-artificial-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tRESEARCH ON DYNAMIC STABILITY OF AN ELASTIC MODEL USING TESTS IN ARTIFICIAL FLOW\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Gleb V.Liseykin, Mikhail M.Bogatyrev, Mikhail A.Pronin, Vsevolod I.Smyslov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-027<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18347 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-active-twist-blade tag-individual-blade-control tag-output-feedback tag-periodic-control homepage_sections-helicopters homepage_sections-materials-and-structures homepage_sections-propulsion homepage_sections-systems category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/periodic-output-feedback-control-for-helicopter-vibration-reduction\/\" target=&quot;_blank&quot;>\n\t\t\t\tPERIODIC OUTPUT FEEDBACK CONTROL FOR HELICOPTER VIBRATION REDUCTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Claudio Brillante, Marco Morandini, Paolo Mantegazza<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-025<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18344 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-finite-element-model-updating tag-ground-vibration-testing tag-modal-identification tag-phase-resonance-method tag-phase-separation-method tag-structural-nonlinearities homepage_sections-avionics homepage_sections-flight-mechanics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/airbus-a320-neo-gvt-and-fem-updating-state-of-the-art-techniques-to-perform-an-industrial-vibration-test-campaign-and-a-rapid-process-to-update-renewed-fem-for-clearance-of-first-flight-test\/\" target=&quot;_blank&quot;>\n\t\t\t\tAIRBUS A320 NEO GVT AND FEM UPDATING STATE-OF-THE-ART TECHNIQUES TO PERFORM AN INDUSTRIAL VIBRATION TEST CAMPAIGN AND A RAPID PROCESS TO UPDATE RENEWED FEM FOR CLEARANCE OF FIRST FLIGHT TEST\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>C. Stephan , T-P Vo-Hoang , S. Giclais , Y. Govers , P. Lubrina , M. Boeswald , A. Laporte<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-024<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18341 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-aeroelastic-deformation tag-cror tag-experimental-measurement tag-spa homepage_sections-helicopters homepage_sections-materials-and-structures homepage_sections-propulsion homepage_sections-systems category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/cror-blade-deformation-part-1-experimental-results-by-strain-pattern-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tCROR BLADE DEFORMATION, PART 1: EXPERIMENTAL RESULTS BY STRAIN PATTERN ANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. GEERAERT, C. STEPHAN<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-023<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18328 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods tag-buffet-control tag-closed-loop tag-fluidic-trailing-edge-device tag-fluidic-vortex-generator tag-open-loop tag-transonic-flow homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2421 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/an-experimental-demonstration-of-active-transonic-buffet-control-using-a-closed-loop-methodology\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN EXPERIMENTAL DEMONSTRATION OF ACTIVE TRANSONIC BUFFET CONTROL USING A CLOSED-LOOP METHODOLOGY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Arnaud Lepage, Julien Dandois, Arnaud Geeraert, Pascal Molton, Frederic Ternoy, Jean Bernard Dor, Eric Coustols<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-015<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18325 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods-bridges tag-aeroelasticity tag-buffeting tag-control tag-flaps tag-flutter tag-long-span-bridge tag-winglets homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2427 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/flutter-and-buffeting-of-long-span-suspension-bridges-in-fully-erected-and-partially-erected-conditions\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER AND BUFFETING OF LONG SPAN SUSPENSION BRIDGES IN FULLY ERECTED AND PARTIALLY ERECTED CONDITIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M. Massaro, K.N. Bakis, D.J.N. Limebeer, M.J.R. Graham<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-014<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18319 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods tag-dynamic-stall tag-leishman-beddoes tag-nonlinear-aeroelasticity tag-stall-utter tag-wind-tunnel-testing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2421 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/theoretical-and-experimental-investigation-of-a-structurally-and-aerodynamically-nonlinear-pitch-and-%ef%ac%82ap-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tTheoretical and experimental investigation of a structurally and aerodynamically nonlinear pitch and \ufb02ap wing\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Edouard Verstraelen, Johan Boutet, Chiara Grappasonni, Gaetan Kerschen, Grigorios Dimitriadis<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-012<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18313 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 tag-co-design tag-control-vector-parametrisation tag-gebm tag-mdo tag-mdsdo tag-open-loop-control tag-optimisation tag-single-shooting homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/co-design-of-very-flexible-actuated-structures\/\" target=&quot;_blank&quot;>\n\t\t\t\tCO-DESIGN OF VERY FLEXIBLE ACTUATED STRUCTURES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Salvatore Maraniello, Rafael Palacios<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-010<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18310 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-bifurcation tag-freeplay tag-limit-cycle-oscillations tag-nonlinear-aeroelasticity homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/asymmetric-limit-cycle-oscillations-in-systems-with-symmetric-freeplay\/\" target=&quot;_blank&quot;>\n\t\t\t\tAsymmetric limit cycle oscillations in systems with symmetric freeplay\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Grigorios Dimitriadis<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-009<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18301 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-reduced-order-modelling tag-geometric-nonlinearities tag-reduced-order-model tag-static-aeroelasticity tag-trim-analysis homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2418 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/static-aeroelastic-analysis-including-geometric-nonlinearities-based-on-reduced-ordered-model-rom\/\" target=&quot;_blank&quot;>\n\t\t\t\tStatic aeroelastic analysis including geometric nonlinearities based on Reduced Ordered Model (ROM)\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>An Chao, Xie Changchuan, Liu Yi, Yang Chao<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-006<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18298 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-high-aspect-ratio-wings tag-nonlinear-aeroelasticity tag-simulation homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/aeroelastic-modeling-and-simulation-of-flexible-jet-transport-aircraft-with-high-aspect-ratio-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC MODELING AND SIMULATION OF FLEXIBLE JET TRANSPORT AIRCRAFT WITH HIGH-ASPECT-RATIO WINGS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ryan C. Kitson, Carlos E. S. Cesnik<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-005<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18289 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 tag-model-updation tag-multi-objective-optimization tag-servoelastic-response homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/multiobjective-optimization-for-servoelastic-response-predictions-of-a-fly-by-wire-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tMULTIOBJECTIVE OPTIMIZATION FOR SERVOELASTIC RESPONSE PREDICTIONS OF A FLY-BY-WIRE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Prabha Srinivasan, Ashok Joshi, Hemalatha E<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-001<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18238 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aeroelasticity tag-flexible-flying-wing tag-flight-dynamics tag-nonlinear-coupled-stability homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/stability-analysis-for-a-very-flexible-flying\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTABILITY ANALYSIS FOR A VERY FLEXIBLE FLYING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Liu Yi, Xie Changchuan, Xu Yuntao, Zhou Danjie<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-236<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18235 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aerodynamic-hearting tag-ase-stability tag-unsteady-thrust homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/aeroservoelastic-stability-analysis-of-an-air-breathing-hypersonic-vehicle\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROSERVOELASTIC STABILITY ANALYSIS OF AN AIR-BREATHING HYPERSONIC VEHICLE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Huangda Zhao, Chao Yang, Zhigang Wu<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-232<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18232 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-cuf tag-free-vibration tag-one-dimensional tag-tapered tag-thin-walled homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/ree-vibration-analysis-of-tapered-wing-structures-using-refined-one-dimensional-models\/\" target=&quot;_blank&quot;>\n\t\t\t\tREE-VIBRATION ANALYSIS OF TAPERED WING STRUCTURES USING REFINED ONE-DIMENSIONAL MODELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. Viglietti, E. Zappino, E. Carrera<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-230<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18211 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-limit-cycle-oscillation tag-neural-network tag-openfoam tag-stall-flutter tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/nonlinear-aerodynamic-identification-and-stall-flutter-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR AERODYNAMIC IDENTIFICATION AND STALL FLUTTER ANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>XIANG ZhengPing , DAI YuTing<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-219<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18208 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-complex-conguration tag-crm tag-reduced-order-modeling tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/application-of-unsteady-aerodynamic-reduced-order-modeling-techniques-to-a-complex-configuration\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF UNSTEADY AERODYNAMIC REDUCED-ORDER MODELING TECHNIQUES TO A COMPLEX CONFIGURATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Maximilian Winter, Christian Breitsamter<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-217<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18205 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-aeroelastic tag-flutter tag-gusts tag-hinged-folding-wing-tips tag-load-alleviation tag-manoeuvres homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/aeroelastic-behaviour-of-hinged-wing-tips\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC BEHAVIOUR OF HINGED WING TIPS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>T. Wilson, A. Castrichini, A. Azabal, J.E. Cooper, R. Ajaj, M. Herring<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-216<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18171 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-geometric-nonlinearity tag-hyper-reduction tag-model-order-reduction tag-simulation-free-trainingj146 tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/simulation-free-hyper-reduced-models-for-geometrically-nonlinear-structural-dynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tSIMULATION-FREE HYPER-REDUCED MODELS FOR GEOMETRICALLY NONLINEAR STRUCTURAL DYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>S. Jain, P. Tiso<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-197<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18159 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-control-system-nonlinearities tag-lyapunov-exponents tag-stability homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/quantitative-aeroelastic-stability-evaluation-of-control-surfaces-with-structural-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tQUANTITATIVE AEROELASTIC STABILITY EVALUATION OF CONTROL SURFACES WITH STRUCTURAL NONLINEARITIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Aykut Tamer, Pierangelo Masarati<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-192<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18156 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-adaptive-wing tag-aeroelasticity tag-structural-analysis homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/study-on-adaptive-wing-structure-for-compromising-structural-strength-and-aerodynamic-performance\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTUDY ON ADAPTIVE WING STRUCTURE FOR COMPROMISING STRUCTURAL STRENGTH AND AERODYNAMIC PERFORMANCE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>TAMAYAMA Masato, FUJII Kanata, YOKOZEKI Tomohiro, ARIZONO Hitoshi<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-191<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18127 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-aeroelastic-analysys tag-cfd tag-rom homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/aerom-nasas-unsteady-aerodynamic-and-aeroelastic-reduced-order-modeling-software\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROM: NASA\u2019S UNSTEADY AERODYNAMIC AND AEROELASTIC REDUCED-ORDER MODELING SOFTWARE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Walter A. Silva<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-181<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18121 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-dynamic-wake-inow tag-helicopter-ight-dynamics tag-reduced-order-modeling homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/application-of-low-order-wake-inflow-models-to-rotorcraft-aeromechanics\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF LOW-ORDER WAKE INFLOW MODELS TO ROTORCRAFT AEROMECHANICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>J. Serafini, F. Cardito, G. Bernardini, M. Gennaretti<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-179<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18118 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-aeroelasticity tag-control tag-repetitive tag-structural-dynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/individual-blade-repetitive-control-for-horizontal-axis-wind-turbines\/\" target=&quot;_blank&quot;>\n\t\t\t\tINDIVIDUAL BLADE REPETITIVE CONTROL FOR HORIZONTAL-AXIS WIND TURBINES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Riccardo Fratini, Jacopo Serafini, Massimo Gennaretti, Riccardo Santini, Stefano Panzieri<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-177<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18103 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aeroservoelasticity tag-flutter tag-lco homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/aeroservoelastic-stability-analysis-using-response-based-parametric-flutter-margins\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROSERVOELASTIC STABILITY ANALYSIS USING RESPONSE-BASED PARAMETRIC FLUTTER MARGINS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Federico Roizner, Moti Karpel<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-172<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18085 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-increased-order-modeling tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/increased-order-aeroservoelastic-modeling-in-practice\/\" target=&quot;_blank&quot;>\n\t\t\t\tINCREASED-ORDER AEROSERVOELASTIC MODELING IN PRACTICE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Manuel Reyes, Hector Climent, Moti Karpel, Felix Ar\u00e9valo, Carlos Maderuelo<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-165<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18066 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-continuous-turbulence tag-gust-encounter tag-nonlinear tag-rom tag-volterra-series homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/a-nonlinear-frequency-domain-aerodynamic-model-for-continuous-turbulence-encounter-based-on-functional-series-expansion\/\" target=&quot;_blank&quot;>\n\t\t\t\tA NONLINEAR FREQUENCY DOMAIN AERODYNAMIC MODEL FOR CONTINUOUS TURBULENCE ENCOUNTER BASED ON FUNCTIONAL SERIES EXPANSION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>David Quero, Wolf Kr\u00fcger<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-159<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18063 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-adaptive-structures tag-gust tag-morphing tag-passive-and-semi-active-control homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/camber-morphing-airfoils-to-reduce-gust-susceptibility\/\" target=&quot;_blank&quot;>\n\t\t\t\tCAMBER-MORPHING AIRFOILS TO REDUCE GUST SUSCEPTIBILITY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Giuliano Tuzzi, Giuseppe Quaranta<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-158<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18057 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-aeroelasticity-real-time-simulation tag-exible-aircraft tag-ight-dynamics tag-reduced-order-modeling homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/application-of-nonlinear-model-order-reduction-technique-to-a-flexible-aircraft-for-real-time-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF NONLINEAR MODEL ORDER REDUCTION TECHNIQUE TO A FLEXIBLE AIRCRAFT FOR REAL-TIME SIMULATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Juliano A. Paulino, Fl\u00e1vio J. Silvestre, Ant\u00f4nio B. Guimar\u00e3es Neto, Tiago P. Monteiro, Roberto Gil A. da Silva, Andrea Da Ronch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-152<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18045 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-computational-uid-dynamics tag-ight-dynamics tag-model-reduction homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/model-reduction-for-gust-load-analysis-of-free-flying-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODEL REDUCTION FOR GUST LOAD ANALYSIS OF FREE-FLYING AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>G. Pagliuca, P. Bekemeyer, R. Thormann, S. Timme<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-148<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18021 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-active-utter-control tag-linear-compressor-cascade tag-plasma-actuators tag-virtual-surfaces homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/numerical-investigation-of-virtual-control-surfaces-for-aeroelastic-control-on-compressor-blades\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL INVESTIGATION OF VIRTUAL CONTROL SURFACES FOR AEROELASTIC CONTROL ON COMPRESSOR BLADES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Valentina Motta, Leonie Malzacher, Dieter Peitsch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-137<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18018 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-computational-aeroelasticity tag-reduced-order-models homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/self-adaptive-pod-based-rom-aeroelastic-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tSELF ADAPTIVE POD BASED ROM AEROELASTIC SIMULATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Rub\u00e9n Moreno-Ramos, Fernando Varas, Jos\u00e9 M. Vega<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-136<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18009 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-business-jet tag-comfort tag-model-reduction tag-vibration-control homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/demonstration-of-innovative-vibration-control-on-a-falcon-business-jet\/\" target=&quot;_blank&quot;>\n\t\t\t\tDEMONSTRATION OF INNOVATIVE VIBRATION CONTROL ON A FALCON BUSINESS JET\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Claire MEYER, Gabriel BROUX, Julien PRODIGUE, Olivier CANTINAUD, Charles POUSSOT-VASSAL<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-133<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17987 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-aeroelasticity tag-airbrake tag-buffet tag-hankel tag-mitigation tag-uncertainty homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/19\/development-of-a-buffet-load-mitigation-system-based-on-multi-surface-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tDEVELOPMENT OF A BUFFET LOAD MITIGATION SYSTEM BASED ON MULTI-SURFACE CONTROL\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sheharyar Malik, Luca Riccobene, Sergio Ricci, Daniele Monti<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-122<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17857 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-degenerate-transformation tag-dynamic-eigenmodes tag-modally-equivalent-perturbed-system tag-modes tag-nonlinear-system tag-reduced-order-model homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/parametrically-rich-nonlinear-reduced-order-modeling-anapplication-in-viscous-incompressible-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tPARAMETRICALLY RICH NONLINEAR REDUCED-ORDER MODELING: AN APPLICATION IN VISCOUS INCOMPRESSIBLE FLOW\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>T. Kim, E.H. Dowell<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-085<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17841 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aeroservoelasticity tag-control-of-exible-aircraft tag-gain-scheduling homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/x-hale-autopilot-with-stability-augmentation-andshape-control-based-on-loop-separation\/\" target=&quot;_blank&quot;>\n\t\t\t\tX-HALE AUTOPILOT WITH STABILITY AUGMENTATION AND SHAPE CONTROL BASED ON LOOP SEPARATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Pedro J. Gonz\u00e1lez, Ant\u00f4nio B. Guimar\u00e3es Neto, Guilherme Chaves Barbosa, Rafael M. Bertolin, Fl\u00b4avio J. Silvestre, Carlos E. S. Cesnik<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-077<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17829 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-morphing tag-robust-optimization tag-rotorcraft tag-uncertainty-quantication homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/robust-aerodynamic-optimization-for-helicopterblade-morphing-airfoils\/\" target=&quot;_blank&quot;>\n\t\t\t\tROBUST AERODYNAMIC OPTIMIZATION FOR HELICOPTER BLADE MORPHING AIRFOILS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Francesca Fusi, Giuseppe Quaranta, Pietro M. Congedo<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-070<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17826 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-hypersonic-aerothermoelasticity tag-linearized-stability-analysis tag-reduced-order-modeling tag-scaling-laws homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/efficient-reduced-order-modeling-for-skin-panels-inhypersonic-flow-and-its-application-to-generatingaerothermoelastic-scaling-laws\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT REDUCED-ORDER MODELING FOR SKIN PANELS IN HYPERSONIC FLOW AND ITS APPLICATION TO GENERATING AEROTHERMOELASTIC SCALING LAWS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Daning Huang, Tomer Rokita, Peretz P. Friedmann<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-069<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17769 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aeroelasticity tag-control-system tag-flutter tag-frequency-response homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/investigation-of-flutter-characteristics-of-aircraftwith-control-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATION OF FLUTTER CHARACTERISTICS OF AIRCRAFT WITH CONTROL SYSTEM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M. Zichenkov, A. Chizhov, S. Kuzmina, F. Ishmuratov, A. Zubakov<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-043<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17766 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-flutter-boundary tag-proper-orthogonal-decomposition tag-reduced-order-model tag-structural-dynamic-reanalysis tag-transonic-aeroelasticity homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/consideration-of-pod-interpolation-for-aeroelasticdesign-with-large-global-structural-variations-usestructural-dynamic-reanalysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tCONSIDERATION OF POD INTERPOLATION FOR AEROELASTIC DESIGN WITH LARGE GLOBAL STRUCTURAL VARIATIONS USE STRUCTURAL DYNAMIC REANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Dongfeng Li, Gang Chen, A.Da Ronch, Qiang Zhou, Yueming Li<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-040<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17760 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-geometric-nonlinearities tag-reduced-order-model tag-response-analysis homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/efficient-aeroelastic-response-analysis-includinggeometric-nonlinearities-based-on-structural-rom\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT AEROELASTIC RESPONSE ANALYSIS INCLUDING GEOMETRIC NONLINEARITIES BASED ON STRUCTURAL ROM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>An Chao, Xie Changchuan, Meng Yang, Yang Chao<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-037<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17757 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-nonlinear-modal-analysis tag-reduced-order-modeling tag-very-exible-aircraft homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/modal-formulation-for-geometrically-nonlinearstructural-dynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODAL FORMULATION FOR GEOMETRICALLY NONLINEAR STRUCTURAL DYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Renato R. Medeiros, Carlos E. S. Cesnik, Etienne B. Coetzee<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-035<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17457 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-adaptive-control tag-control-of-flexible-aircraft tag-hale-aircraft tag-lyapunov-direct-method tag-model-reference-adaptive-control homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/dynamic-gain-scheduling-of-highly-flexible-aircraft-applying-adaptive-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tDynamic Gain Scheduling of Highly Flexible Aircraft Applying Adaptive Control\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>R.M.Bertolin, F.J.Silvestre, A.B.Guimaraes Neto, P.J.Gonzalez, G.C.Barbosa, C.E.S.Cesnik<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-017<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17448 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aeroelasticity tag-dynamic-loads tag-flight-control-system tag-structural-coupling homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-systems category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/flight-control-design-to-improve-aircraft-performance-by-reducing-the-flutter-and-dynamic-loads-margins\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlight control design to improve aircraft performance by reducing the flutter and dynamic loads margins\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>L.Benassi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-014<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<\/div>\n\t\t\t\t\t<span class=\"e-load-more-spinner\">\n\t\t\t\t<i aria-hidden=\"true\" class=\"fas fa-spinner\"><\/i>\t\t\t<\/span>\n\t\t\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-c8c877b elementor-widget elementor-widget-spacer\" data-id=\"c8c877b\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t<div class=\"elementor-column elementor-col-25 elementor-top-column elementor-element elementor-element-4b92472\" data-id=\"4b92472\" data-element_type=\"column\" data-e-type=\"column\" data-settings=\"{&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t<div class=\"elementor-widget-wrap\">\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t<section class=\"elementor-section elementor-top-section elementor-element elementor-element-5f254a1 elementor-section-stretched elementor-section-boxed elementor-section-height-default elementor-section-height-default\" data-id=\"5f254a1\" data-element_type=\"section\" data-e-type=\"section\" data-settings=\"{&quot;stretch_section&quot;:&quot;section-stretched&quot;,&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t\t\t\t<div class=\"elementor-container elementor-column-gap-default\">\n\t\t\t\t\t<div class=\"elementor-column elementor-col-100 elementor-top-column elementor-element elementor-element-ff101ec\" data-id=\"ff101ec\" data-element_type=\"column\" data-e-type=\"column\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-bbafcf0 elementor-widget elementor-widget-spacer\" data-id=\"bbafcf0\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-9389dce elementor-widget elementor-widget-spacer\" data-id=\"9389dce\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t<\/div>\n\t\t","protected":false},"excerpt":{"rendered":"<p>Search all Systems Papers Search &#8230; Results See all results Results Sort&#8230; By title from lowest to highest By title from highest to lowest By date from lowest to highest By date from highest to lowest<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"footnotes":""},"class_list":["post-11450","page","type-page","status-publish","hentry","category-993","category-1956","category-1953","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/11450","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=11450"}],"version-history":[{"count":67,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/11450\/revisions"}],"predecessor-version":[{"id":27540,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/11450\/revisions\/27540"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=11450"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}