{"id":11434,"date":"2023-07-19T15:13:22","date_gmt":"2023-07-19T15:13:22","guid":{"rendered":"https:\/\/aerospacerepository.org\/?page_id=11434"},"modified":"2026-09-10T12:00:48","modified_gmt":"2026-09-10T12:00:48","slug":"repository-aeronautics-aircraft-design","status":"publish","type":"page","link":"https:\/\/aerospacerepository.org\/index.php\/repository-aeronautics-aircraft-design\/","title":{"rendered":"Repository Aeronautics Aircraft Design"},"content":{"rendered":"\t\t<div data-elementor-type=\"wp-page\" data-elementor-id=\"11434\" class=\"elementor elementor-11434\" 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 Aircraft Design 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\" data-settings=\"{&quot;symbols_for_start_searching&quot;:2,&quot;search_by_empty_value&quot;:&quot;&quot;,&quot;submit_on_enter&quot;:&quot;&quot;,&quot;search_source&quot;:&quot;any&quot;,&quot;search_logging&quot;:&quot;&quot;,&quot;search_results_url&quot;:&quot;&quot;,&quot;search_taxonomy&quot;:&quot;&quot;,&quot;include_terms_ids&quot;:[3970],&quot;exclude_terms_ids&quot;:[],&quot;exclude_posts_ids&quot;:[],&quot;custom_fields_source&quot;:&quot;&quot;,&quot;limit_query&quot;:5,&quot;limit_query_tablet&quot;:&quot;&quot;,&quot;limit_query_mobile&quot;:&quot;&quot;,&quot;limit_query_in_result_area&quot;:25,&quot;results_order_by&quot;:&quot;relevance&quot;,&quot;results_order&quot;:&quot;asc&quot;,&quot;sentence&quot;:&quot;&quot;,&quot;search_in_taxonomy&quot;:&quot;&quot;,&quot;search_in_taxonomy_source&quot;:&quot;&quot;,&quot;results_area_width_by&quot;:&quot;form&quot;,&quot;results_area_custom_width&quot;:&quot;&quot;,&quot;results_area_custom_position&quot;:&quot;&quot;,&quot;results_area_columns&quot;:1,&quot;results_area_columns_tablet&quot;:&quot;&quot;,&quot;results_area_columns_mobile&quot;:&quot;&quot;,&quot;results_area_columns_mobile_portrait&quot;:&quot;&quot;,&quot;thumbnail_visible&quot;:&quot;yes&quot;,&quot;thumbnail_size&quot;:&quot;thumbnail&quot;,&quot;thumbnail_placeholder&quot;:{&quot;url&quot;:&quot;https:\\\/\\\/aerospacerepository.org\\\/wp-content\\\/plugins\\\/elementor\\\/assets\\\/images\\\/placeholder.png&quot;,&quot;id&quot;:&quot;&quot;,&quot;size&quot;:&quot;&quot;},&quot;post_content_source&quot;:&quot;content&quot;,&quot;post_content_custom_field_key&quot;:&quot;&quot;,&quot;post_content_length&quot;:30,&quot;show_product_price&quot;:&quot;&quot;,&quot;show_product_rating&quot;:&quot;&quot;,&quot;show_add_to_cart&quot;:&quot;&quot;,&quot;show_result_new_tab&quot;:&quot;&quot;,&quot;highlight_searched_text&quot;:&quot;&quot;,&quot;listing_id&quot;:&quot;&quot;,&quot;bullet_pagination&quot;:&quot;&quot;,&quot;number_pagination&quot;:&quot;&quot;,&quot;navigation_arrows&quot;:&quot;in_header&quot;,&quot;navigation_arrows_type&quot;:&quot;angle&quot;,&quot;show_title_related_meta&quot;:&quot;&quot;,&quot;meta_title_related_position&quot;:&quot;&quot;,&quot;title_related_meta&quot;:&quot;&quot;,&quot;show_content_related_meta&quot;:&quot;&quot;,&quot;meta_content_related_position&quot;:&quot;&quot;,&quot;content_related_meta&quot;:&quot;&quot;,&quot;negative_search&quot;:&quot;Sorry, but nothing matched your search terms.&quot;,&quot;server_error&quot;:&quot;Sorry, but we cannot handle your search query now. 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 aircraft design papers..\" value=\"\" name=\"s\" autocomplete=\"off\" \/>\n\t\t\t\t\t\t\t<input type=\"hidden\" value=\"{&quot;include_terms_ids&quot;:[3970]}\" 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-7b79ae9 elementor-widget elementor-widget-spacer\" data-id=\"7b79ae9\" 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-1bca2b8 elementor-widget elementor-widget-spacer\" data-id=\"1bca2b8\" 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-94f1ab8 elementor-widget elementor-widget-spacer\" data-id=\"94f1ab8\" 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-6371a06 elementor-widget elementor-widget-spacer\" data-id=\"6371a06\" 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-4966878 elementor-widget elementor-widget-spacer\" data-id=\"4966878\" 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-722a8ac elementor-widget elementor-widget-spacer\" data-id=\"722a8ac\" 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-19709 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-cfd tag-closed-loop-gust-encounter tag-gust-loads tag-military-fighter-aircraft homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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-encounter-of-a-supersonic-fighter-aircraft-using-cfd-methods\/\" target=&quot;_blank&quot;>\n\t\t\t\tGust Encounter of a Supersonic Fighter Aircraft using CFD Methods\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Arne Voss<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-001<\/p>\n<p>Conference number: IFASD-2024-001<\/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-19703 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-altitude-variation tag-continuous-turbulence tag-flight-loads tag-load-collectives homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/influence-of-cruise-altitude-variation-on-the-turbulence-loads-of-a-medium-range-transport-configuration\/\" target=&quot;_blank&quot;>\n\t\t\t\tInfluence of Cruise Altitude Variation on the Turbulence Loads of a Medium-Range Transport 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>Vega Handojo, Sunpeth Cumnuantip<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-004<\/p>\n<p>Conference number: IFASD-2024-004<\/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-19697 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aerodynamic-gap tag-box-pressure-modifications tag-doublet-lattice-method-dlm tag-flutter tag-gust tag-static-lift-and-moment tag-zaero homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/flutter-and-gust-response-of-a-wing-with-aerodynamic-gaps\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlutter and Gust Response of a Wing with Aerodynamic Gaps\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Dale Pitt<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-006<\/p>\n<p>Conference number: IFASD-2024-006<\/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-19694 post type-post status-publish format-standard hentry category-events category-aeroelastic-design-applications-1-ifasd-2024 category-ifasd-2024 tag-aeroelastic-stability tag-high-aspect-ratio-wing-aircraft tag-preliminary-design homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3024 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\/assessment-of-aeroelastic-stability-of-high-aspect-wing-aircraft-during-the-preliminary-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tAssessment of aeroelastic stability of high aspect wing aircraft during the preliminary 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>Sunpeth Cumnuantip, Matthias Schulze, Wolf R. Krueger<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-007<\/p>\n<p>Conference number: IFASD-2024-007<\/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-19688 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-conceptual-aircraft-design tag-gradient-based-optimization tag-multi-disciplinary-design-optimization tag-time-domain homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/aeroelastic-mission-optimization-of-very-flexible-vehicles-including-take-off-and-climb-constraints\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic Mission Optimization of Very Flexible Vehicles including Take-Off and Climb Constraints\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christopher Lupp<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-009<\/p>\n<p>Conference number: IFASD-2024-009<\/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-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-19670 post type-post status-publish format-standard hentry category-events category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelastic-tailoring tag-composite-material tag-high-aspect-ratio-wing tag-multi-disciplinary-design-optimization tag-numerical-simulation homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3038 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\/optimizing-high-aspect-ratio-composite-wings-through-geometrically-nonlinear-aeroelastic-tailoring\/\" target=&quot;_blank&quot;>\n\t\t\t\tOptimizing high aspect ratio composite wings through geometrically nonlinear aeroelastic tailoring\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-2024-015<\/p>\n<p>Conference number: IFASD-2024-015<\/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-19667 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-fluid-structural-interaction-fsi tag-limit-cycle-oscillation-lco tag-shock-impingement homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/exploring-the-effect-of-different-shock-impingement-angles-on-aeroelastic-response-for-a-thin-panel\/\" target=&quot;_blank&quot;>\n\t\t\t\tExploring the Effect of Different Shock Impingement Angles on Aeroelastic Response for a Thin Panel\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Luisa Piccolo Serafim, Earl Dowell<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-016<br \/>\nConference number: IFASD-2024-016<\/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-19664 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-constrained-optimisation tag-efficient-global-optimisation tag-lamination-parameters tag-reliability-based-design-optimisation homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/aeroelastic-reliability-based-optimisation-of-composite-plates-via-surrogate-modeling\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic reliability based optimisation of composite plates via surrogate modeling\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Roger Ballester Claret, Nicolo Fabbiane, Christian Fagiano, Cedric Julien, Didier Lucor<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-017<\/p>\n<p>Conference number: IFASD-2024-017<\/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-19652 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-cfd tag-control-surfaces tag-dlm tag-unsteady-aerodynamics tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/experimental-and-numerical-assessment-on-the-aeroelastic-behavior-of-a-nlf-airfoil-with-oscillating-control-surfaces\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental and numerical assessment on the aeroelastic behavior of a NLF airfoil with oscillating control surfaces\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Carlos Sebastia Saez, Mirko Hornung<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-024<\/p>\n<p>Conference number: IFASD-2024-024<\/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-19649 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity-in-conceptual-aircraft-design tag-computational-aeroelasticity tag-flutter tag-highly-flexible-aircraft-structures tag-loads-alleviation tag-mdo homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/control-surface-sizing-and-design-through-integrated-mdo-approach-enhancing-load-alleviation-while-preserving-handling-quality-criteria\/\" target=&quot;_blank&quot;>\n\t\t\t\tControl surface sizing and design through integrated MDO approach: Enhancing load alleviation while preserving handling quality criteria\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Daniel Muradas Odriozola, Sylvie Marquier, Joseph Morlier, Christian Gogu<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-025<\/p>\n<p>Conference number: IFASD-2024-025<\/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-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-19633 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-flutter tag-high-aspect-ratio-wing tag-machine-learning tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/machine-learning-to-forecast-unsteady-motion-induced-unsteady-forces\/\" target=&quot;_blank&quot;>\n\t\t\t\tMachine learning to forecast unsteady, motion-induced unsteady forces\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Reik Thormann, Hans Martin Bleecke<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-030<\/p>\n<p>Conference number: IFASD-2024-030<\/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-19630 post type-post status-publish format-standard hentry category-events category-aeroelastic-design-applications-1-ifasd-2024 category-ifasd-2024 tag-aeroelastic-optimization tag-nonlinear-structural-stability tag-wingbox-structures homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3024 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\/influence-of-load-introduction-method-on-wingbox-optimization-with-nonlinear-structural-stability-constraints\/\" target=&quot;_blank&quot;>\n\t\t\t\tInfluence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints\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 M. A. Mitrotta, Alberto Pirrera, Terence Macquart, Jonathan E. Cooper, Alex Pereira do Prado, Pedro Higino Cabral<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-031<\/p>\n<p>Conference number: IFASD-2024-031<\/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-19624 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-hybrid-testing tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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-hybrid-testing-for-industrial-applications\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic hybrid testing for industrial applications\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Davide Balatti, Hamed Haddad Khodaparast, Shakir Jiffri, Michael Friswell, Sebastiano Fichera, Alessandra Vizzaccaro, Andrea Castrichini<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-033<\/p>\n<p>Conference number: IFASD-2024-033<\/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-19621 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-adjoint-tsm tag-gust-response tag-harmonic-balance tag-time-spectral-method tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/a-modular-tsm-solver-for-aeroelastic-analysis-and-optimizations\/\" target=&quot;_blank&quot;>\n\t\t\t\tA modular TSM solver for aeroelastic analysis and optimizations\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Cedric Liauzun, Christophe Blondeau<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-034 <\/p>\n<p>Conference number: IFASD-2024-034<\/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-19618 post type-post status-publish format-standard hentry category-events category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelastic-prediction tag-gust-response tag-large-deflections tag-very-flexible-wing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3038 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\/evaluation-of-aeroelastic-models-for-gust-response-prediction-in-very-flexible-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tEvaluation of Aeroelastic Models for Gust Response Prediction in Very Flexible 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>Divya Sanghi, Cristina Riso, Carlos Cesnik<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-035<\/p>\n<p>Conference number: IFASD-2024-035<\/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-19615 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/advances-in-aeroelastic-prediction-and-design-optimization-for-next-generation-aerospace-vehicles\/\" target=&quot;_blank&quot;>\n\t\t\t\tAdvances in Aeroelastic Prediction and Design Optimization for Next-Generation Aerospace Vehicles\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sai Vishal Gali, Cristina Riso<\/b><\/p>\n<p>DOI Number: 10.82439\/ceas-ifasd-2024-036<\/p>\n<p>Conference number: IFASD-2024-036<\/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-19612 post type-post status-publish format-standard hentry category-events category-aeroelastic-design-applications-1-ifasd-2024 category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelastic-analysis tag-free-play tag-unmanned-multi-body-aircraft homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3024 category-3028 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\/nonlinear-aeroelastic-response-analysis-of-unmanned-multi-body-aircraft-with-free-play\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear Aeroelastic Response Analysis of Unmanned Multi-body Aircraft with Free Play\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Chen Zhu, Ying Bi, Zijian Zhu, Zhuolin Ying, Xiaoping Ma<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-037<\/p>\n<p>Conference number: IFASD-2024-037<\/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-19595 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-model-update tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/ground-vibration-testing-and-model-update-of-a-transonic-flutter-wind-tunnel-model\/\" target=&quot;_blank&quot;>\n\t\t\t\tGround Vibration Testing and Model Update of a Transonic Flutter Wind Tunnel Model\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Anders Ellmo<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-043<\/p>\n<p>Conference number: IFASD-2024-043<\/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-19592 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-buffet tag-design tag-pod tag-random-loads tag-turbulence homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/robust-design-through-identification-of-main-components-from-multivariate-random-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tRobust design through identification of main components from multivariate random 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>Cyrille Vidy, Carlo Aquilini<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-044<\/p>\n<p>Conference number: IFASD-2024-044<\/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-19586 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-doublet-lattice-method tag-uav tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/doublet-lattice-modelling-and-analysis-of-unsteady-aerodynamic-effects-for-a-flexible-unmanned-aircraft-during-maneuvers-and-gust-encounters\/\" target=&quot;_blank&quot;>\n\t\t\t\tDoublet lattice modelling and analysis of unsteady aerodynamic effects for a flexible unmanned aircraft during maneuvers and gust encounters\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Leif Rieck, Benjamin Herrmann, Frank Thielecke<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-046<br \/>\nConference number: IFASD-2024-046<\/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-19583 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-buffet tag-design tag-nodal-loads tag-random-loads tag-stress tag-turbulence homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/from-multivariate-random-loads-to-deterministic-load-distributions-an-exact-method-for-aeroelastic-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tFrom Multivariate Random Loads To Deterministic Load Distributions: An Exact Method For Aeroelastic 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>Carlo Aquilini, Gabriele Grasso, Cyrille Vidy<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-047<\/p>\n<p>Conference number: IFASD-2024-047<\/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-19574 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-correlation-based-transition-modeling tag-transition-model-validation tag-turbulent-wedges tag-unsteady-transonic-flow homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/effect-of-turbulent-wedges-on-the-steady-and-unsteady-aerodynamics-of-a-forward-swept-laminar-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tEffect of Turbulent Wedges on the Steady and Unsteady Aerodynamics of a Forward Swept Laminar 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>Michael Fehrs, Christoph Kaiser<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-054<\/p>\n<p>Conference number: IFASD-2024-054<\/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-19568 post type-post status-publish format-standard hentry category-events category-aeroelastic-design-applications-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-b-spline tag-doublet-lattice-method-dlm tag-movables homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3024 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\/continuous-parametrisation-of-wing-movable-layout-for-design-optimisation\/\" target=&quot;_blank&quot;>\n\t\t\t\tContinuous parametrisation of wing movable layout for design optimisation\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Stefan de Boer, Jurij Sodja, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-057<\/p>\n<p>Conference number: IFASD-2024-057<\/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-19556 post type-post status-publish format-standard hentry category-events category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-cfd tag-control tag-flexible-aircraft tag-flight-dynamics tag-fluid-structure-coupling tag-gla tag-gust-response tag-maneuver homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3038 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\/highly-flexible-aircraft-flight-dynamics-using-cfd\/\" target=&quot;_blank&quot;>\n\t\t\t\tHighly Flexible Aircraft Flight Dynamics using CFD\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alain Dugeai<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-062<\/p>\n<p>Conference number: IFASD-2024-062<\/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-19553 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aero-thermo-elasticity tag-cfd-method tag-fem-method tag-hypersonic tag-partitioned-loose-coupling-strategy homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/a-cfd-ctd-csd-based-aero-thermo-elastic-framework-for-full-vehicle-scale-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tA CFD\/CTD\/CSD based aero-thermo-elastic framework for full-vehicle scale 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>Liang Ma, Zhiqiang Wan, Xiaozhe Wang, Keyu Li, Chang Li, Longfei He<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-063<\/p>\n<p>Conference number: IFASD-2024-063<\/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-19550 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelastic-tailoring tag-commercial-aircraft tag-kriging-surrogate-model homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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-optimization-of-commercial-aircraft-considering-high-precision-aerodynamic-performance\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic optimization of commercial aircraft considering high-precision 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>Keyu Li, Chao Yang, Xiaozhe Wang, Zhiqiang Wan, Liang Ma, Chang Li<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-064<\/p>\n<p>Conference number: IFASD-2024-064<\/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-19547 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-operational-modal-analysis tag-structural-dynamics tag-wind-tunnel-testing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/experimental-investigation-of-a-highly-flexible-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental investigation of a highly flexible 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>Giuliano Coppotelli, Roberto Sbarra, Ludovic Onofri, Marcello Righi<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-065<\/p>\n<p>Conference number: IFASD-2024-065<\/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-19538 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-load-analysis tag-nonlinear tag-vortex-lattice-method homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/efficient-and-high-precision-nonlinear-static-aeroelastic-load-analysis-method-based-on-vortex-lattice-method-acceleration\/\" target=&quot;_blank&quot;>\n\t\t\t\tEfficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Zou Zhicheng, Xie Changchuan, An Chao, Yang Lan, Zhu Lipeng, Ni Zao<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-068<\/p>\n<p>Conference number: IFASD-2024-068<\/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-19535 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-doublet-lattice-method tag-flutter tag-gust tag-linearized-frequency-domain tag-optimization homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/gradient-based-optimization-of-the-common-research-model-wing-subject-to-cfd-based-gust-and-flutter-constraints\/\" target=&quot;_blank&quot;>\n\t\t\t\tGradient-based Optimization of the Common Research Model Wing Subject to CFD-based Gust and Flutter Constraints\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Andrew Thelen, Kevin Jacobson, Bret Stanford<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-069<\/p>\n<p>Conference number: IFASD-2024-069<\/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-19526 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-horizontal-stabilator tag-mil-a-8870 tag-spindle-freeplay homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/testing-and-analysis-of-a-simplified-nonlinear-horizontal-stabilator-of-an-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tTesting and Analysis of a Simplified Nonlinear Horizontal Stabilator of an 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>Nichoas Stathopoulos, Viresh Wickramasinghe, Devon Downes<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-073<\/p>\n<p>Conference number: IFASD-2024-073<\/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-19520 post type-post status-publish format-standard hentry category-events category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-flight-dynamics-and-aeroelastic-coupling tag-large-deformations tag-maneuvering-aircraft tag-nonlinear-dynamics tag-stability-analysis homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3038 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\/flight-dynamics-aeroelastic-coupling-in-flexible-and-very-flexible-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlight-dynamics aeroelastic coupling in flexible and very flexible 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>Dor Naftaly, Daniella E. Raveh<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-078<\/p>\n<p>Conference number: IFASD-2024-078<\/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-19517 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity-of-very-flexible-aircraft tag-finite-element-model-updating tag-ground-vibration-testing tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/finite-element-model-update-of-a-very-flexible-wing-using-ground-vibration-testing-data\/\" target=&quot;_blank&quot;>\n\t\t\t\tFinite element model update of a very flexible wing using ground vibration testing 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>Bilal Sharqi, Carlos E. S. Cesnik<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-079<\/p>\n<p>Conference number: IFASD-2024-079<\/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-19514 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-damping tag-fixed-wing tag-flutter tag-optimisation homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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-optimisation-of-a-cantilevered-plate-with-local-damping-application\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic optimisation of a cantilevered plate with local damping application\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ali Tatar, Stephane Fournier, Jonathan Cooper<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-080<\/p>\n<p>Conference number: IFASD-2024-080<\/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-19508 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-dynamic-loads tag-high-performance tag-jax tag-nonlinear-aeroelasticity homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/differentiable-aeroelastic-framework-suitable-for-industrial-modelling-of-nonlinear-loads-on-accelerators\/\" target=&quot;_blank&quot;>\n\t\t\t\tDifferentiable Aeroelastic Framework Suitable for Industrial Modelling of Nonlinear Loads on Accelerators\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alvaro Cea, Rafael Palacios<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-082<\/p>\n<p>Conference number: IFASD-2024-082<\/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-19502 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aerothermoelasticity tag-hypersonic-vehicles tag-meshfree-method homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/aerothermoelasticity-analysis-of-hypersonic-vehicle-based-on-meshfree-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tAerothermoelasticity analysis of hypersonic vehicle based on meshfree 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>Zhan Sun, Zhiqiang Wan, Xiaozhe Wang, Liang Ma, Chang Li<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-084<\/p>\n<p>Conference number: IFASD-2024-084<\/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-19496 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-aerothermoelasticity tag-functionally-graded-materials tag-hypersonic-vehicles homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/an-integrated-static-dynamic-aerothermoelastic-analysis-framework-for-functionally-graded-structures-in-hypersonic-vehicles\/\" target=&quot;_blank&quot;>\n\t\t\t\tAn integrated static\/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Chang Li, Zhiqiang Wan, Xiaozhe Wang, Chao Yang, Zhiying Chen<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-087<\/p>\n<p>Conference number: IFASD-2024-087<\/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-19484 post type-post status-publish format-standard hentry category-events category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-aspect-ratio-variation tag-bell-shaped-lift-distribution tag-cpacs-mona tag-high-aspect-ratio-wing tag-preliminary-design tag-taper-ratio homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3038 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\/25\/the-effect-of-aspect-ratio-variation-on-the-preliminary-aeroelastic-assessment-of-a-mid-range-transport-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tThe Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport 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>Matthias Schulze, Florian M\u00fcller, Sunpeth Cumnuantip, Vega Handojo, Tobias Hecken, Thomas Klimmek, Markus Ritter, Markus Zimmer<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-090<\/p>\n<p>Conference number: IFASD-2024-090<\/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-19475 post type-post status-publish format-standard hentry category-events category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-deformation-reconstruction tag-highly-flexible-wing tag-inertial-measurement-unit homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3038 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\/25\/imu-based-deformation-reconstruction-for-highly-flexible-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tIMU-based deformation reconstruction for highly flexible 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>Yuhui Zhang, Changchuan Xie, Yang Meng<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-094<\/p>\n<p>Conference number: IFASD-2024-094<\/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-19453 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-active-gust-load-alleviation tag-flexible-wing tag-gust-generator tag-optical-measurement-technology tag-particle-image-velocimetry tag-unsteady-aerodynamics tag-wind-tunnel-testing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/integrated-aerodynamic-and-structural-measurements-of-the-gust-response-of-a-hinged-folding-wingtip\/\" target=&quot;_blank&quot;>\n\t\t\t\tIntegrated Aerodynamic and Structural Measurements of the Gust Response of a Hinged Folding Wingtip\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christoph Mertens, Anna Biancotto, Jurij Sodja, Andrea Sciacchitano<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-101<\/p>\n<p>Conference number: IFASD-2024-101<\/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-19450 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-feedforward-decoupling-controller tag-ground-flutter-simulation-test tag-shaker-structure-coupling-system homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/modeling-of-shaker-structure-coupling-system-and-its-application-in-ground-aeroelastic-stability-test\/\" target=&quot;_blank&quot;>\n\t\t\t\tModeling of shaker-structure coupling system and its application in ground aeroelastic stability 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>Wei Xiao, Changkun Yu, Zhigang Wu, Chao Yang<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-102<\/p>\n<p>Conference number: IFASD-2024-102<\/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-19444 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-enhanced-dlm tag-flutter tag-linearized-rans tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/flutter-prediction-correlations-with-wind-tunnel-measurements-on-a-t-tail-flutter-mock-up\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlutter prediction correlations with wind tunnel measurements on a T-tail flutter mock-up\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Elsa Br\u00e9us, Nicolas Forestier, Zdenek Johan, Eric Garrigues<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-104<\/p>\n<p>Conference number: IFASD-2024-104<\/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-19441 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-neural-network tag-sensor-selection tag-strain tag-temperature homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/investigation-on-sensor-selection-applied-on-a-vehicle-as-a-sensor-concept-in-high-speed-flight\/\" target=&quot;_blank&quot;>\n\t\t\t\tInvestigation on Sensor Selection Applied on a Vehicle-as-a-Sensor Concept in High-Speed Flight\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ana C. Meinicke, Carlos E. S. Cesnik<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-105<\/p>\n<p>Conference number: IFASD-2024-105<\/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-19438 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-experimental-aeroelasticity tag-gust-flow-aerodynamics tag-gust-generator-design tag-structural-modeling homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/design-and-experimental-characterization-of-a-gust-generator-concept-with-rotating-slotted-cylinders-in-the-low-speed-wind-tunnel-dnw-nwb\/\" target=&quot;_blank&quot;>\n\t\t\t\tDesign and Experimental Characterization of a Gust-Generator Concept with Rotating-Slotted Cylinders in the Low-Speed Wind Tunnel DNW-NWB\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Thomas G. Schmidt, Johannes Dillinger, Markus Ritter, Anna Altkuckatz, Charlotte Hanke, Marc Braune, Holger Mai, Wolf R. Krueger<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-106<\/p>\n<p>Conference number: IFASD-2024-106<\/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-19422 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelastic-derivatives tag-buffet tag-flutter tag-loewner-framework tag-mode-tracking tag-transonic-flow homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/a-general-solver-for-the-prediction-of-flutter-and-buffet-onset\/\" target=&quot;_blank&quot;>\n\t\t\t\tA general solver for the prediction of flutter and buffet onset\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, Christoph Kaiser, Jens Nitzsche<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-112<\/p>\n<p>Conference number: IFASD-2024-112<\/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-19419 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-automated-modal-analysis tag-experimental-flutter-analysis tag-flight-vibration-testing tag-modal-parameter-tracking homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/reliable-monitoring-of-modal-parameters-during-a-flight-vibration-test-using-autonomous-modal-analysis-and-a-kalman-filter\/\" target=&quot;_blank&quot;>\n\t\t\t\tReliable monitoring of modal parameters during a flight vibration test using autonomous modal analysis and a Kalman filter\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Robin Volkmar, Julian Sinske, Keith Soal, Yves Govers, Marc B\u00f6swald<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-113<\/p>\n<p>Conference number: IFASD-2024-113<\/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-19416 post type-post status-publish format-standard hentry category-events category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-geometric-nonlinearity tag-large-deformation tag-modal-approach tag-mode-shapes tag-shape-sensing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3038 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\/an-incremental-modal-shape-sensing-method-for-geometrically-non-linear-deformed-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tAn Incremental Modal Shape Sensing Method for Geometrically Non-Linear Deformed 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>Janto Gundlach, Marc B\u00f6swald, Jurij Sodja<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-114<\/p>\n<p>Conference number: IFASD-2024-114<\/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-19410 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-force-summation-method tag-horizontal-tail tag-inertially-coupled-equations tag-internal-loads tag-quasi-steady tag-vlm tag-wing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/comparative-analysis-of-flight-maneuver-loads-between-flexible-and-rigid-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tComparative analysis of flight maneuver loads between flexible and rigid 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>Eduardo de Melo Pinto, Fl\u00e1vio Cardoso-Ribeiro, Fernando de Oliveira Moreira<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-117<\/p>\n<p>Conference number: IFASD-2024-117<\/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-19407 post type-post status-publish format-standard hentry category-events category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-high-flexible tag-multibody tag-rayleigh-ritz-method tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3038 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\/rayleigh-ritz-method-with-multibody-dynamics-for-highly-flexible-structures\/\" target=&quot;_blank&quot;>\n\t\t\t\tRayleigh-Ritz method with multibody dynamics for highly flexible 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>Leonardo Barros da Luz, Fl\u00e1vio Cardoso-Ribeiro, Pedro Paglione<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-118<\/p>\n<p>Conference number: IFASD-2024-118<\/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-19397 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-aircraft-loads tag-conceptual-aircraft-design tag-liquid-hydrogen tag-wingbox-sizing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/design-manufacturing-and-identification-of-an-active-controlled-flexible-wing-for-subsonic-wind-tunnel-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tDesign, manufacturing and identification of an active controlled flexible wing for subsonic wind tunnel 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>Johannes Dillinger, Holger Mai, Wolf R. Krueger, Thomas Schmidt, Felix Stalla<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-121<\/p>\n<p> Conference number: IFASD-2024-121<\/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-19394 post type-post status-publish format-standard hentry category-events category-aeroelastic-design-applications-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-aircraft-loads tag-conceptual-aircraft-design tag-liquid-hydrogen tag-wingbox-sizing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3024 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\/wing-mounted-hydrogen-fuel-tanks-mitigating-the-aeroelastic-penalties-of-dry-wing-configurations\/\" target=&quot;_blank&quot;>\n\t\t\t\tWing mounted hydrogen fuel tanks: mitigating the aeroelastic penalties of dry wing 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>Fintan Healy, Huaiyuan Gu, Djamel Rezgui, Jonathan Cooper<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-122<\/p>\n<p>Conference number: IFASD-2024-122<\/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-19390 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-flutter tag-gust tag-lfd-solver tag-linearized-cfd tag-pulse tag-system-identification homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/analysis-of-linearized-motion-and-gust-induced-airloads-with-a-next-generation-computational-fluid-dynamics-solver\/\" target=&quot;_blank&quot;>\n\t\t\t\tAnalysis of Linearized Motion- and Gust-Induced Airloads with a Next-Generation Computational Fluid Dynamics Solver\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christoph Kaiser, David Quero, Jens Nitzsche, Bernd Stickan<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-123<\/p>\n<p>Conference number: IFASD-2024-123<\/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-19381 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-distributed-electric-propulsion tag-whirl-flutter tag-wing-flutter homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/aeroelastic-analysis-of-distributed-electric-propulsion-flexible-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic analysis of distributed electric propulsion flexible 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>Samet Dede, Ali Tatar, Djamel Rezgui, Jonathan Cooper<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-129<\/p>\n<p>Conference number: IFASD-2024-129<\/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-19378 post type-post status-publish format-standard hentry category-events category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-flexible-structures tag-hamiltonian-mechanics tag-neural-networks tag-surrogate-models homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3038 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\/surrogate-modeling-of-highly-flexible-structures-and-aerodynamics-using-neural-networks\/\" target=&quot;_blank&quot;>\n\t\t\t\tSurrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vitor Borges Santos, Breno Soares da Costa Vieira, Fl\u00e1vio Luiz Cardoso-Ribeiro, Ant\u00f4nio Bernardo Guimar\u00e3es Neto<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-132<\/p>\n<p>Conference number: IFASD-2024-132<\/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-19365 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-flared-hinged-wings tag-flight-dynamics tag-folding-wing-tips tag-gust-load-alleviation tag-hale-aircraft homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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-gust-effects-on-flexible-aircraft-with-flared-hinged-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear Gust Effects On Flexible Aircraft With Flared Hinged 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>Kelvin Chi-Wing Cheng, Alvaro Cea, Rafael Palacios, Andrea Castrichini, Thomas Wilson<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-137<\/p>\n<p>Conference number: IFASD-2024-137<\/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-19362 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-adjoint-sensitivity tag-aeroelasticity tag-computational tag-feature-mapping tag-topology homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/a-panel-free-aeroelastic-solver-with-adjoint-sensitivities\/\" target=&quot;_blank&quot;>\n\t\t\t\tA Panel-Free Aeroelastic Solver with Adjoint Sensitivities\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Hollis Smith, Joshua Deaton<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-138<\/p>\n<p>Conference number: IFASD-2024-138<\/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-19359 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-smart-wing tag-supersonic-flow homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/aeroelasticity-of-smart-wing-in-supersonic-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelasticity of smart wing in supersonic 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>Reza Moosavi<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-139<\/p>\n<p>Conference number: IFASD-2024-139<\/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-19355 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-high-aspect-ratio-wing-aircraft tag-load-control tag-wind-tunnel-experiment homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/assessment-of-active-load-control-approaches-for-transport-aircraft-ae-simulation-and-wind-tunnel-test\/\" target=&quot;_blank&quot;>\n\t\t\t\tAssessment of Active Load Control Approaches for Transport Aircraft &#8211; Simulation and Wind Tunnel 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>Wolf Krueger, Holger Mai, Thiemo Kier, Lars Reimer<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-141<\/p>\n<p>Conference number: IFASD-2024-141<\/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-19349 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-distributed-electric-propulsor tag-electric-aircraft tag-gust-loads tag-load-alleviation tag-thrust-vectoring homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/gust-load-alleviation-of-electric-aircraft-with-distributed-propulsors-using-thrust-vectoring\/\" target=&quot;_blank&quot;>\n\t\t\t\tGust load alleviation of electric aircraft with distributed propulsors using thrust vectoring\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Mohammadreza Amoozgar, Grigorios Dimitriadis, Jonathan Cooper, Rafic Ajaj<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-145<\/p>\n<p>Conference numer: IFASD-2024-145<\/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-19345 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/constrained-flexible-wing-with-folding-wingtip-dynamics-model-based-on-lagranges-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tConstrained flexible wing with folding wingtip dynamics model based on Lagrange&#8217;s 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>Lina Dehmlow, Pedro Gonz\u00e1lez, Gerrit Stavorinus, Fl\u00e1vio Silvestre<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-149<\/p>\n<p>Conference number: IFASD-2024-149<\/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-19336 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-data-acquisition tag-measurement-and-control-system tag-propeller-wing-system tag-wind-tunnel-experiment homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/measurement-and-control-system-design-for-propeller-wing-system-experiments\/\" target=&quot;_blank&quot;>\n\t\t\t\tMeasurement and Control System Design for Propeller-Wing System 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>Wei Wang, Zhitao Zhang, Changchuan Xie, Chao Yang, Kunhui Huang<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-156<\/p>\n<p>Conference number: IFASD-2024-156<\/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-19333 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelastic-tailoring tag-flutter tag-flying-demonstrator homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/aeroelastic-design-of-a-drone-for-research-on-active-flutter-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic design of a drone for research on active flutter 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>Nicol\u00f2 Fabbiane, Vincent Bouillaut, Arnaud Lepage<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-157<\/p>\n<p>Conference number: IFASD-2024-157<\/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-19327 post type-post status-publish format-standard hentry category-events category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-flutter tag-structural-dynamics tag-wing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3038 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\/design-and-experimental-tests-of-a-flexible-wing-of-high-aspect-ratio-for-investigating-flutter-mechanisms\/\" target=&quot;_blank&quot;>\n\t\t\t\tDesign and experimental tests of a flexible wing of high-aspect ratio for investigating flutter mechanisms\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 Stephan, Xavier Amandolese<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-160<\/p>\n<p>Conference number: IFASD-2024-160<\/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-19324 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-neural-network tag-nonlinear-aeroelasticity tag-reduced-order-models homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/nonlinear-aeroelastic-analysis-of-a-regional-airliner-wing-via-a-neural-network-based-reduced-order-model-for-aerodynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear aeroelastic analysis of a regional airliner wing via a neural-network based reduced order model for 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>Nicol\u00f2 Laureti, Luca Pustina, Marco Pizzoli, Francesco Saltari, Franco Mastroddi<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-161<\/p>\n<p>Conference number: IFASD-2024-161<\/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-19315 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-beats tag-coupled-oscillators tag-shock-dynamics tag-transonic-buffet homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/mechanism-of-transonic-aeroelastic-instabilities-via-synchronization-of-coupled-oscillators\/\" target=&quot;_blank&quot;>\n\t\t\t\tMechanism of transonic aeroelastic instabilities via synchronization of coupled oscillators\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Srikanth Vasudevan, Xuerui Wang, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-164<\/p>\n<p>Conference number: IFASD-2024-164<\/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-19312 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-flutter tag-t-tail tag-transonic tag-wind-tunnel-test homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/t-tail-transonic-flutter-wind-tunnel-test-part-1-sealing-system-design-and-model-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tT-tail transonic flutter wind tunnel test part 1: Sealing system design and model 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>Valentin Lanari, Arnaud Lepage, Elsa Br\u00e9us<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-165<\/p>\n<p>Conference number: IFASD-2024-165<\/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-19309 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-anti-resonance tag-gust-loads tag-inertial-load-relief homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/analysis-of-inertial-gust-load-relief-characteristics-of-high-aspect-ratio-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tAnalysis of inertial gust load relief characteristics of 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>Sanuja Jayatilake, Mark Lowenberg, Benjamin King Sutton Woods, Branislav Titurus<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-166<\/p>\n<p>Conference number: IFASD-2024-166<\/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-19295 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-clean-aviation tag-distributed-propulsion tag-hybrid-electric-regional-architecture homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/25\/aeroelastic-challenges-in-the-clean-aviation-hybrid-electric-regional-aircraft-project\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic challenges in the clean aviation hybrid-electric regional aircraft 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>Emilio Santos, Alan Serena, Mordechay Karpel, Felix Arevalo, Hector Climent<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-170<\/p>\n<p>Conference number: IFASD-2024-170<\/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-19292 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-data-analytics tag-dynamic-loads tag-neural-networks homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/25\/feedforward-backpropagation-artificial-neural-networks-applied-to-dynamic-loads-of-a-military-transport-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tFeedforward backpropagation artificial neural networks applied to dynamic loads of a military transport 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>Gabriel Buendia, Beatriz Pulido, MIguel Torralba, Manuel Reyes, Felix Arevalo, Hector Climent<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-171<\/p>\n<p>Conference number: IFASD-2024-171<\/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-19283 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-global-stability-analysis tag-shock-buffet tag-transonic-flow homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/25\/prediction-of-transonic-buffet-in-an-axial-flow-fan-using-global-stability-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tPrediction of transonic buffet in an axial flow fan using global stability 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>Jyoti Majhi, Kartik Venkatraman<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-175<\/p>\n<p>Conference number: IFASD-2024-175<\/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-19276 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-buffeting tag-elastic-model tag-fairing tag-launch-vehicle tag-transonic tag-wind-tunnel-test homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/experimental-study-on-transonic-buffeting-of-launch-vehicles-with-large-diameter-fairing-using-elastic-models\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental study on transonic buffeting of launch vehicles with large-diameter fairing using elastic 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>Chen Ji, Jue Wang<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-179<\/p>\n<p>Conference number: IFASD-2024-179<\/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-20701 post type-post status-publish format-standard hentry category-events category-aeroelastic-design-applications-1-ifasd-2024 category-flight-testing-1-ifasd-2024 category-maneuver-and-gust-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-distributed-electric-propulsion tag-flight-dynamic-aeroelastic-coupling tag-geometric-nonlinearities tag-highly-flexible-wings tag-whirl-flutter homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3024 category-3035 category-3038 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\/flight-dynamic-aeroelastic-response-of-a-highly-flexible-aircraft-with-distributed-propellers\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlight Dynamic-Aeroelastic Response of a Highly Flexible Aircraft with Distributed Propellers\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Albert Gallego Pozo, Rauno Cavallaro<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-182<\/p>\n<p>Conference number: IFASD-2024-182<\/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-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-19267 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-hypersonic tag-inverse-model tag-loads tag-neural-network homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 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\/experimental-validation-of-strain-load-neural-network-model-on-a-slender-hypersonic-vehicle\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental Validation of Strain-Load Neural Network Model on a Slender 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>Ana Cristine Meinicke, Carlos Cesnik, Brianna Blocher, Aditya Panigrahi, Jayant Sirohi, Noel Clemens<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-185<\/p>\n<p>Conference number: IFASD-2024-185<\/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-19264 post type-post status-publish format-standard hentry category-events category-aeroelastic-design-applications-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-describing-function tag-flexible-model tag-freeplay tag-lco tag-limit-cycle-oscillation tag-preloading tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3024 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-a-flexible-half-wing-model-tested-in-a-subsonic-wind-tunnel-with-control-surface-freeplay-and-preloading\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear analysis of a flexible half-wing model tested in a subsonic wind tunnel with control-surface freeplay and preloading\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Breno Moura Castro, Wellington Luziano Paulo Junior, Douglas Domingues Bueno, Cleber Spode<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-186<\/p>\n<p>Conference number: IFASD-2024-186<\/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-19249 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-experimental tag-gust-alleviation tag-high-aspect-ratio tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/gust-load-alleviation-wind-tunnel-tests-of-a-folding-wing-tip-configuration\/\" target=&quot;_blank&quot;>\n\t\t\t\tGust load alleviation wind tunnel tests of a folding wing tip 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>Luca Marchetti, Sergio Ricci, Luca Riccobene, Donato Grassi, Paolo Mantegazza, Stephan Adden, Huaiyuan Gu, Jonathan Cooper<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-192<\/p>\n<p>Conference number: IFASD-2024-192<\/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-19243 post type-post status-publish format-standard hentry category-events category-aeroelastic-design-applications-1-ifasd-2024 category-ifasd-2024 tag-folding-wingtip tag-multi-disciplinary-design-optimisation tag-semi-aeroelastic-hinge tag-static-aeroelasticity homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3024 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\/multidisciplinary-design-optimisation-of-an-aircraft-with-the-semi-aeroelastic-hinge-device\/\" target=&quot;_blank&quot;>\n\t\t\t\tMultidisciplinary design optimisation of an aircraft with the semi-aeroelastic hinge device\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Marta Colella, Mario Peinado Garcia, Francesco Saltari, Franco Mastroddi, Fabio Vetrano, Paolo Mastracci, Andrea Castrichini<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-194<\/p>\n<p>Conference number: IFASD-2024-194<\/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-19236 post type-post status-publish format-standard hentry category-events category-aeroelastic-design-applications-1-ifasd-2024 category-ifasd-2024 tag-co-design tag-flutter-control homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3024 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\/co-design-of-the-aeroelastic-wing-parameters-and-the-flutter-control-law\/\" target=&quot;_blank&quot;>\n\t\t\t\tCo-Design of the Aeroelastic Wing Parameters and the Flutter Control Law\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Zsombor Wermeser, B\u00e9la Takarics, B\u00e1lint Vanek<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-196<\/p>\n<p>Conference number: IFASD-2024-196<\/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-19233 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-electric-aircraft tag-flutter tag-ground-vibration-testing tag-virtual-driving-point homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/explainable-nonlinear-state-space-modelling-analysing-the-gvt-of-a-battery-operated-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tExplainable nonlinear state-space modelling: analysing the GVT of a battery-operated 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>P\u00e9ter Zolt\u00e1n Csurcsia, Tim De Troyer<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-197<\/p>\n<p>Conference number: IFASD-2024-197<\/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-19227 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-flutter tag-source-and-doublet-panel-method homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/application-of-the-unsteady-compressible-source-and-doublet-panel-method-to-flutter-calculations\/\" target=&quot;_blank&quot;>\n\t\t\t\tApplication of the unsteady compressible source and doublet panel method to flutter calculations\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, Spyridon Kilimtzidis, Vassilis Kostopoulos, Vito Laraspata, Leonardo Soria<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-199<\/p>\n<p>Conference numer: IFASD-2024-199<\/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-19216 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-maneuver-simulation tag-simulation-based-certification tag-simulation-validation tag-virtual-flight-testing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/11\/high-fidelity-multidisciplinary-maneuver-simulations-of-the-falcon-2000lx-istar\/\" target=&quot;_blank&quot;>\n\t\t\t\tHigh-Fidelity Multidisciplinary Maneuver Simulations of the Falcon 2000LX ISTAR\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Martin Bauer, Johan Feldwisch<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-205<\/p>\n<p>Conference number: IFASD-2024-205<\/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-19210 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-evtol-electric-vertical-take-off-and-landing tag-experimental-modal-analysis-ema tag-finite-element-analysis-fea tag-rotorstructure-interaction tag-sequential-quadratic-programming-sqp homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 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\/11\/experimental-investigation-into-the-dynamic-characteristics-of-a-tilting-multirotor-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental investigation into the dynamic characteristics of a tilting multirotor 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>Tanuj Sharma, Djamel Rezgui, Branislav Titurus<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-208<\/p>\n<p>Conference number: IFASD-2024-208<\/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-19204 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-detached-eddy-simulation tag-limit-cycle-oscillations tag-lock-in tag-vortex-induced-vibrations homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/11\/investigation-of-vortex-induced-vibrations-to-compare-reynolds-averaged-navier-stokes-and-detached-eddy-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tInvestigation of vortex-induced vibrations to compare Reynolds-averaged Navier-Stokes and detached-eddy 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>Kilian Streitenberger, Jens Nitzsche<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-214<\/p>\n<p>Conference number: IFASD-2024-214<\/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-19198 post type-post status-publish format-standard hentry category-events category-unsteady-aerodynamics-1-ifasd-2024 tag-adaptive tag-aeroelasticity tag-euler tag-fem tag-fenics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3042 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\/11\/adaptive-euler-efficient-and-predictive-aerodynamics-validation-and-prototype-development-toward-aeroelasticity\/\" target=&quot;_blank&quot;>\n\t\t\t\tAdaptive Euler &#8211; efficient and predictive aerodynamics: validation and prototype development toward 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>Johan Jansson, Kristoffer Wingstedt, Rebecca Durst<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-218<\/p>\n<p>Conference number: IFASD-2024-218<\/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-19190 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-cfd tag-digital-image-correlation tag-fsi tag-kalman-filter homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/07\/experimental-and-numerical-activities-for-aeroelastic-analysis-of-an-aluminum-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum 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>Davide Mastrodicasa, Silvia Vettori, Massimiliano Chillemi, Alessandro Laurini, Aleli Sosa Chavez, Emilio Di Lorenzo, Karl Janssens<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-225<\/p>\n<p>Conference number: IFASD-2024-225<\/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-19187 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-cfd tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/07\/comparison-between-computational-and-experimental-non-stationary-pressure-distribution-on-a-pitch-oscilating-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tComparison between computational and experimental non-stationary pressure distribution on a pitch-oscilating 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>Bruno Regina, Eduardo Molina, Roberto Silva<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-226<\/p>\n<p>Conference number: IFASD-2024-226<\/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-19173 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-gust-load tag-test-rig tag-transonic-flows tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-3033 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\/02\/28\/wind-tunnel-tests-for-gust-load-investigation-in-transonic-flows-ae-part-1-development-of-an-innovative-test-rig\/\" target=&quot;_blank&quot;>\n\t\t\t\tWind tunnel tests for gust load investigation in transonic flows &#8211; Part 1 : Development of an innovative test rig\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, Nicola Paletta, Serena Russo, Sergio Ricci, Eric Rantet, Arnaud Barnique<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-231<\/p>\n<p>Conference number: IFASD-2024-231<\/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-19168 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/optimization-of-nonlinear-periodic-aeroelastic-systems-using-boundary-value-problem-formulation\/\" target=&quot;_blank&quot;>\n\t\t\t\tOptimization of Nonlinear Periodic Aeroelastic Systems using Boundary Value Problem Formulation\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Anshuman Mehta, Pankil N. Mishra, Abhijit Gogulapati<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2024-233<\/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-19159 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-large-angle-of-attack tag-plane-symmetry-vehicle tag-stability-of-trailing-edge-rudder-surface homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 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\/aeroelastic-characteristics-of-plane-symmetry-vehicle-main-wing-trailing-edge-rudder-at-high-angle-of-attack\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Guo Li, Gongde Li, Yingyou Hou<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-240<\/p>\n<p>Conference number: IFASD-2024-240<\/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-18699 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-aeroservoelasticity-characteristics-aeroelasticity tag-flutter tag-gyroscopic-forces tag-polynomial-ritz-method homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2422 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\/gyroscopic-forces-influence-on-aeroelasticity-characteristics-of-an-airplane-with-engines-on-pylons-under-the-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tGYROSCOPIC FORCES INFLUENCE ON AEROELASTICITY CHARACTERISTICS OF AN AIRPLANE WITH ENGINES ON PYLONS 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>A. Kuznetsov, S. Kuzmina, F. Ishmuratov, V. Mosunov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-193<\/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-18696 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-aerodynamic-damping tag-asymmetric-eigenmode tag-critical-speed tag-engine-aeroelasticity tag-engine-thrust tag-flutter tag-utter-frequency tag-follower-force tag-gyroscopics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2422 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\/the-aeroelastic-impact-of-engine-thrust-and-gyroscopics-on-aircraft-flutter-instabilities\/\" target=&quot;_blank&quot;>\n\t\t\t\tThe Aeroelastic Impact of Engine Thrust and Gyroscopics on Aircraft Flutter Instabilities\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Stefan Waitz, Holger Hennings<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-192<\/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-18678 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-increased-order-modeling tag-increased-order-modeling-iom tag-morphing tag-structural-dynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-2413 category-2420 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\/aircraft-dynamic-loads-with-varying-geometry-and-flight-mechanics-effects\/\" target=&quot;_blank&quot;>\n\t\t\t\tAircraft Dynamic Loads with Varying Geometry and Flight Mechanics Effects\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Moti Karpe, Aviv Romm, Manuel Reyes, Hector Climent<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-183<\/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-18652 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-flight-loads tag-static-aeroelasticity tag-three-dimensional-aerodynamics tag-trim-analysis homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-2413 category-2420 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\/analysis-of-flight-loads-and-static-aeroelasticity-characteristics-of-the-airplane-with-the-use-of-three-dimensional-aerodynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tANALYSIS OF FLIGHT LOADS AND STATIC AEROELASTICITY CHARACTERISTICS OF THE AIRPLANE WITH THE USE OF THREE-DIMENSIONAL 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>Fausto G. Di Vinvenzo , Marina V. Kwiatkowska , Regina V. Leonteva , Denis V. Nekhaev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-173<\/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-18649 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-active-control tag-auto-oscillations tag-elastic-ufv-cs-loop tag-electromechanical-actuator tag-flutter homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2425 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\/research-experience-of-aeroelastic-vibrations-of-the-ufv-with-electromechanical-actuator-of-control-fin\/\" target=&quot;_blank&quot;>\n\t\t\t\tRESEARCH EXPERIENCE OF AEROELASTIC VIBRATIONS OF THE UFV WITH ELECTROMECHANICAL ACTUATOR OF CONTROL FIN\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 I. Smyslov, Artyom V. Bykov, Stanislav I. Sychev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-172<\/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-18634 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-aeroelasticity tag-aviation-regulations tag-certification tag-deformations tag-dynamic-loading tag-finite-element-method tag-ifasd tag-loads tag-mathematical-models tag-multidisciplinary-design tag-service-life tag-static-strength tag-stresses tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2423 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\/multidisciplinary-computational-system-parus-int-for-design-and-certification-of-airplanes-in-static-and-dynamic-strength-and-service-life\/\" target=&quot;_blank&quot;>\n\t\t\t\tMULTIDISCIPLINARY COMPUTATIONAL SYSTEM \u00abPARUS-INT\u00bb FOR DESIGN AND CERTIFICATION OF AIRPLANES IN STATIC AND DYNAMIC STRENGTH AND SERVICE LIFE\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. I. Turchannikov, M. M. Levchenko, V. V. Chedrik, D. V. Chemisov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-162<\/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-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-18612 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-active-control tag-active-control tag-flutter tag-limit-cycle-oscillation tag-piezoelectric homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2425 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\/suppression-of-simulated-self-excited-oscillation-using-smart-materials-on-flexible-wing-strcuture\/\" target=&quot;_blank&quot;>\n\t\t\t\tSUPPRESSION OF SIMULATED SELF-EXCITED OSCILLATION USING SMART MATERIALS ON FLEXIBLE WING STRCUTURE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Norizham A. Razak<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-150<\/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-18609 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-of-morphing-aircraft tag-aeroelasticity tag-cae tag-compliant-mechanisms tag-genetic-algorithm tag-morphing tag-multi-objective-optimization homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2424 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\/aeroelastic-analysis-of-a-regional-aircraft-with-active-camber-morphing-device\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC ANALYSIS OF A REGIONAL AIRCRAFT WITH ACTIVE CAMBER MORPHING DEVICE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alessandro De Gaspari, Sergio Ricci, Lorenzo Travaglini<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-149<\/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-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-18582 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-aeroelastic-tailoring tag-aeroelasticity tag-wing-design homepage_sections-aerodynamics homepage_sections-aircraft-design category-2413 category-2415 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\/aeroelastic-tailoring-and-structural-optimisation-using-an-advanced-dynamic-aeroelastic-framework\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC TAILORING AND STRUCTURAL OPTIMISATION USING AN ADVANCED DYNAMIC AEROELASTIC 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>Noud P.M. Werter, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-137<\/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-18579 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-active-control tag-aeroelastic-instability tag-autonomous-free-floating-flap tag-limit-cycle-oscillation homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2425 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-and-numerical-study-of-an-autonomous-flap\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL AND NUMERICAL STUDY OF AN AUTONOMOUS FLAP\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Lars O. Bernhammer, Sachin T. Navalkar, Jurij Sodja, Roeland De Breuker , Moti Karpel<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-136<\/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-18564 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-aeroelastic-tailoring tag-aeroelasticity tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2423 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\/aeroelastic-tailoring-using-crenelated-skins-modelling-and-experiment\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC TAILORING USING CRENELATED SKINS \u2013 MODELLING AND EXPERIMENT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Guillaume Francois, Jonathan E. Cooper, Paul M. Weaver<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-129<\/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-18561 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-aerodynamic-thermal-structure-coupling tag-aerothermoelastic tag-hypersonic tag-interval-method tag-the-uncertainty-of-aerodynamic-heat-flux homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2422 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-static-aerothermoelastic-response-analysis-method-considering-heat-flux-uncertainty\/\" target=&quot;_blank&quot;>\n\t\t\t\tA STATIC AEROTHERMOELASTIC RESPONSE ANALYSIS METHOD CONSIDERING HEAT FLUX UNCERTAINTY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nan Yi, Zhiqiang Wan , GuoShu Li, Chao Yang<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-128<\/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-18558 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-geometric-nonlinearity tag-gust-response tag-high-aspect-ratio-wing tag-uvlm-unsteady-vortex-lattice-method homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2422 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\/gust-response-analysis-for-high-aspect-ratio-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tGUST RESPONSE ANALYSIS FOR HIGH-ASPECT RATIO 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>Liu Yi, Xie Changchuan, Yang Chao<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-126<\/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-18552 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-aeroelastic-tailoring tag-aeroelasticity tag-design tag-experiment tag-load-alleviation homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2423 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-an-aeroelastically-tailored-wing-under-manoeuvre-loading\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN AND TESTING OF AN AEROELASTICALLY TAILORED WING UNDER MANOEUVRE LOADING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Noud P.M Werter, Jurij Sodja, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-123<\/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-18546 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-aeroelasticity tag-flutter tag-load tag-optimization tag-structural-optimization homepage_sections-aerodynamics homepage_sections-aircraft-design category-2413 category-2415 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-2\/\" 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>Sean Meldrum, Pierre Hardy, Gabriel Broux, Eric Garrigues<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-121<\/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-18540 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-aeroelastic-constraints tag-cfd-correction tag-composite tag-doublet-lattice-method tag-stacking-sequence-optimization tag-stiness-optimization homepage_sections-aerodynamics homepage_sections-aircraft-design category-2413 category-2415 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\/static-aeroelastic-stiffness-optimization-of-a-forward-swept-composite-wing-with-cfd-corrected-aero-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTATIC AEROELASTIC STIFFNESS OPTIMIZATION OF A FORWARD SWEPT COMPOSITE WING WITH CFD CORRECTED AERO 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>Johannes K.S. Dillinger, Mostafa M. Abdalla, Yasser M. Meddaikar, Thomas Klimmek<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-116<\/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-18529 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-backlash tag-dead-zone tag-flutter tag-partial-frequencies homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2422 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\/investigation-of-uav-control-surfaces-characteristics\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATION OF UAV CONTROL SURFACES\u2019 CHARACTERISTICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sergey N. Gartsev, Anton V. Dolgopolov, Vsevolod I. Smyslov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-113<\/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-18526 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-a330-mrtt tag-boom tag-buffet tag-dynamic-loads homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-2413 category-2420 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\/non-linear-structural-dynamics-aspects-of-the-aerial-refuelling-boom-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tNON-LINEAR STRUCTURAL DYNAMICS ASPECTS OF THE AERIAL REFUELLING BOOM 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>F. Ar\u00e9valo, S. Claver\u00edas, H. Climent<\/b><\/p>\n<p>DOI Number:  N\/A<\/p>\n<p>Conference number: IFASD-2015-107<\/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-18508 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-active-control tag-lateral-response tag-multi-parameter-updation tag-sensitivity-study tag-structural-coupling homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2425 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\/sensitivity-based-approach-for-improved-predictions-of-servo-elastic-response-of-a-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tSENSITIVITY BASED APPROACH FOR IMPROVED PREDICTIONS OF SERVO-ELASTIC RESPONSE OF 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>Prabha Srinivasan, Ashok Joshi, Indira Narayanaswamy, Hemalatha E<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-098<\/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-18493 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-aeroelasticity tag-luid-structure-interaction homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2422 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\/computational-benchmark-of-commercial-fluid-structure-interaction-software-for-aeroelastic-applications\/\" target=&quot;_blank&quot;>\n\t\t\t\tComputational Benchmark of Commercial Fluid-Structure Interaction Software for Aeroelastic Applications\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-2015-091<\/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-18490 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-aircraft tag-hard-landing tag-msc-adams tag-numerical-simulation homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-2413 category-2420 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\/application-of-numerical-simulation-for-the-detection-and-analyzing-rough-landings-of-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF NUMERICAL SIMULATION FOR THE DETECTION AND ANALYZING ROUGH LANDINGS OF 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>Andrey Rybin<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-089<\/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-18484 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-component-wise tag-composites tag-free-vibrations tag-higher-order-beam-models tag-wing-box homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2423 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\/enhanced-free-vibration-analysis-of-composite-wingbox-structures-by-one-dimensional-component-wise-and-dynamic-stiffness-formulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tENHANCED FREE VIBRATION ANALYSIS OF COMPOSITE WINGBOX STRUCTURES BY ONE-DIMENSIONAL COMPONENT-WISE AND DYNAMIC STIFFNESS FORMULATIONS\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. Carrera, A. Pagani, P.H. Cabral, G. Silva, A. Prado<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-087<\/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-18481 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-couple tag-dynamic-response tag-gust tag-hale tag-nonlinear homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-2413 category-2420 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\/gust-response-analysis-of-high-altitude-long-endurance-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tGUST RESPONSE ANALYSIS OF HIGH ALTITUDE, LONG ENDURANCE 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>Chen Zhanjun, Fu Zhichao, Lv Jinan, Liu Ziqiang<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-086<\/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-18472 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-evolutionary tag-flutter tag-optimisation tag-topology homepage_sections-aerodynamics homepage_sections-aircraft-design category-2413 category-2415 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-novel-method-for-the-vibration-optimisation-of-structures-subjected-to-dynamic-loading\/\" target=&quot;_blank&quot;>\n\t\t\t\tA Novel Method for the Vibration Optimisation of Structures Subjected to Dynamic Loading\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 J. Munk, Gareth A. Vio, Grant P. Steven<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-081<\/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-18469 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-curved-timoshenko-beams tag-isogeometric-analysis tag-low-fidelity-aeroelasticity tag-morphing-airfoil tag-potential-flow homepage_sections-aerodynamics homepage_sections-aircraft-design category-2413 category-2415 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\/low-fidelity-2d-isogeometric-aeroelastic-optimization-with-application-to-a-morphing-airfoil\/\" target=&quot;_blank&quot;>\n\t\t\t\tLOW-FIDELITY 2D ISOGEOMETRIC AEROELASTIC OPTIMIZATION WITH APPLICATION TO A MORPHING 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>Erik Gillebaart, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-079<\/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-18457 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-mdo tag-moga-ii tag-moo tag-pareto-frontier tag-sqp tag-wgc homepage_sections-aerodynamics homepage_sections-aircraft-design category-2413 category-2415 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\/genetic-and-gradient-based-algorithms-for-the-multi-objective-optimization-of-aircraft-design-with-aeroelastic-constraints\/\" target=&quot;_blank&quot;>\n\t\t\t\tGENETIC AND GRADIENT-BASED ALGORITHMS FOR THE MULTI-OBJECTIVE OPTIMIZATION OF AIRCRAFT DESIGN WITH AEROELASTIC CONSTRAINTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Stefania Gemma, Franco Mastroddi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-075<\/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-18438 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-fixed-axis tag-flexible-aircraft-dynamics tag-flight-simulation tag-gaf tag-mean-axis tag-uvlm homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2422 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\/a-comparison-of-modeling-methods-for-the-simulation-of-free-flying-elastic-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tA COMPARISON OF MODELING METHODS FOR THE SIMULATION OF FREE FLYING ELASTIC 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>K. Seywald, A. Wildschek, F. Holzapfel<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-068<\/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-18434 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-aeroelastic tag-high-aspect-ratio-wing tag-sensitivity-analysis tag-stiffness-design tag-structural-optimization homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2423 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\/stiffness-distribution-and-aeroelastic-performance-optimization-of-high-aspect-ratio-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTIFFNESS DISTRIBUTION AND AEROELASTIC PERFORMANCE OPTIMIZATION OF 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>Du Ziliang, Wan Zhiqiang, Yang Chao<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-067<\/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-18423 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-dynamically-scaled-model tag-flutter tag-ground-vibration-tests-gvt tag-influence-coefficient-matrix tag-suchoi-ssj-100 homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2423 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\/experience-of-flutter-clearance-of-the-suchoi-ssj-100-regional-jet\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIENCE OF FLUTTER CLEARANCE OF THE SUCHOI SSJ 100 REGIONAL 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>Alexey E. Orlov, Sergey E. Paryshev, Sergey V. Shalaev, Sergey I. Kalabuchov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-061<\/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-18411 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-aeroelasticity tag-buckling tag-finite-element-model-layout tag-structural-optimization tag-structural-strength tag-topology-optimization homepage_sections-aerodynamics homepage_sections-aircraft-design category-2413 category-2415 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\/evolutionary-approach-to-structural-design-of-wing-under-stress-buckling-and-aeroelasticity-requirements\/\" target=&quot;_blank&quot;>\n\t\t\t\tEVOLUTIONARY APPROACH TO STRUCTURAL DESIGN OF WING UNDER STRESS, BUCKLING AND AEROELASTICITY REQUIREMENTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vasily V. Chedrik, Sergey A. Tuktarov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-055<\/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-18402 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-cfd-csm tag-folding-wing-tip tag-load-alleviation tag-simulation homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2423 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\/high-fidelity-simulation-of-the-folding-wing-tip-for-loads-alleviaton\/\" target=&quot;_blank&quot;>\n\t\t\t\tHIGH FIDELITY SIMULATION OF THE FOLDING WING TIP FOR LOADS ALLEVIATON\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>John Pattinson, Thomas Wilson, Martin Herring<\/b><\/p>\n<p>DOI number: N\/A<\/p>\n<p>Conference number: IFASD-2015-052<\/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-18394 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-dynamic-behavior tag-lattice-composite-structures tag-unidirectional-composite homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2423 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\/modeling-of-dynamic-behavior-of-lattice-composite-aircraft-structures\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODELING OF DYNAMIC BEHAVIOR OF LATTICE COMPOSITE AIRCRAFT 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>A. Bezuevsky, I. Kondakov, A. Shanygin, M. Zichenkov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-049<\/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-18374 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-active-control tag-aeroservoelasticity tag-dynamic-stiffness tag-flutter tag-horizontal-stabilizer tag-link homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2425 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-aeroservoelastic-analysis-for-a-three-dimensional-horizontal-stabilizer-with-an-actuator-composed-of-elastic-links\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR AEROSERVOELASTIC ANALYSIS FOR A THREE DIMENSIONAL HORIZONTAL STABILIZER WITH AN ACTUATOR COMPOSED OF ELASTIC LINKS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yoo Jin Kang, Chan Hoon Chung, Jae Hyeok Jeon, Sang Joon Shin, Young Ho Na<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-039<\/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-18365 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-dynamic-loads tag-run tag-structural-damping tag-turbulence homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-2413 category-2420 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\/influence-of-structural-damping-on-airplane-dynamic-loads-at-flight-in-turbulence-and-at-run\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF STRUCTURAL DAMPING ON AIRPLANE DYNAMIC LOADS AT FLIGHT IN TURBULENCE AND AT RUN\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Oleg A. Kuznetsov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-036<\/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-18359 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-aeroelasticity tag-mdo tag-parametric-studies tag-shape-optimization tag-strength homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2423 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-optimization-of-wing-shape-and-structural-parameters-for-different-aircraft-configurations\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC OPTIMIZATION OF WING SHAPE AND STRUCTURAL PARAMETERS FOR DIFFERENT AIRCRAFT 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>Kirill A. Balunov, Vasily V. Chedrik, Fanil Z. Ishmuratov, Petr G. Karkle<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-034<\/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-18338 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-of-morphing-aircraft tag-eigenanalysis tag-generalized-beam-models tag-jordan-form tag-wing-morphing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2424 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\/a-generalized-beam-formulation-for-the-dynamic-analysis-of-camber-morphing-helicopter-blades\/\" target=&quot;_blank&quot;>\n\t\t\t\tA GENERALIZED BEAM FORMULATION FOR THE DYNAMIC ANALYSIS OF CAMBER-MORPHING HELICOPTER 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>Luca Cirrottola, Marco Morandini, Giuseppe Quaranta<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-020<\/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-18335 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-adjoint-technique tag-aeroelastic-gradient tag-optimization homepage_sections-aerodynamics homepage_sections-aircraft-design category-2413 category-2415 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\/recent-achievements-towards-aero-structure-gradient-computation-using-high-fidelity-cfd-csm-in-the-onera-elsa-software\/\" target=&quot;_blank&quot;>\n\t\t\t\tRECENT ACHIEVEMENTS TOWARDS AERO-STRUCTURE GRADIENT COMPUTATION USING HIGH-FIDELITY CFD-CSM IN THE ONERA ELSA 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>C. Blondeau, T. Achard, P. Girodroux-Lavigne, R. Ohayon<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-019<\/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-18331 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-of-morphing-aircraft tag-compliant-structure tag-morphing-aircraft tag-morphing-winglet homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2424 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\/investigating-the-benefits-of-morphing-wing-tip-devices-a-case-study\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATING THE BENEFITS OF MORPHING WING TIP DEVICES A CASE 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>Chen Wang, Hamed Haddad Khodaparast, Michael I Friswell<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-018<\/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-18322 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-aeroelasticity tag-typical-section tag-viscoelastic-damping homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-2413 category-2422 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\/a-parametric-and-topological-study-on-the-use-of-viscoelastic-material-for-flutter-suppression\/\" target=&quot;_blank&quot;>\n\t\t\t\tA PARAMETRIC AND TOPOLOGICAL STUDY ON THE USE OF VISCOELASTIC MATERIAL FOR FLUTTER SUPPRESSION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Gabriel I. Barbejat, Maur\u00edcio V. Donadon, Roberto G. Silva, Antonio M. G. de Lima, Andr\u00e9 G.C. Filho, Leandro S. Le\u00e3o<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-013<\/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-18307 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-cumulative-fatigue-damage tag-flight-parameters tag-variable-loads homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-2413 category-2420 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\/flight-loads-and-cumulative-fatique-damages-monitoring-for-each-aircraft-during-service-life\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT LOADS AND CUMULATIVE FATIQUE DAMAGES MONITORING FOR EACH AIRCRAFT DURING SERVICE LIFE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Victor I. Kleptsov , Vladimir I. Tsimbalyuk , Tatiana I. Orlova<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-008<\/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-18292 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-aeroelastic-optimization tag-composite-wing tag-high-efficiency tag-kriging-model homepage_sections-aerodynamics homepage_sections-aircraft-design category-2413 category-2415 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\/a-high-efficiency-aeroelastic-optimization-method-based-on-kriging-model-and-genetic-algorithm\/\" target=&quot;_blank&quot;>\n\t\t\t\tA HIGH-EFFICIENCY AEROELASTIC OPTIMIZATION METHOD BASED ON KRIGING MODEL AND GENETIC ALGORITHM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Wang Xiaozhe, Wan Zhiqiang, Yang Chao<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-002<\/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-18247 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-flight-vibration-testing tag-ground-vibration-testing tag-online-monitoring tag-outputonly-modal-analysis tag-parameter-varying-systems tag-taxi-vibration-testing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1960 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\/recent-developments-in-operational-modal-analysis-for-ground-and-flight-vibration-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tRECENT DEVELOPMENTS IN OPERATIONAL MODAL ANALYSIS FOR GROUND AND FLIGHT VIBRATION 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>M. B\u00f6swald, J. Schwochow, G. Jelicic, Y. Govers<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-239<\/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-18244 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-fuel tag-loads tag-pressure tag-sloshing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/fuel-loads-in-large-civil-airplanes\/\" target=&quot;_blank&quot;>\n\t\t\t\tFUEL LOADS IN LARGE CIVIL AIRPLANES\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 Gambioli, Arnaud George Malan<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-238<\/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-18241 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-lagrangian-approach tag-pitching-airfoil tag-starting-vortex tag-unsteady-aerodynamics tag-vortex-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/a-variational-approach-for-the-dynamics-of-unsteady-point-vortices\/\" target=&quot;_blank&quot;>\n\t\t\t\tA VARIATIONAL APPROACH FOR THE DYNAMICS OF UNSTEADY POINT VORTICES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ahmed A. Hussein, Haithem E. Taha, Saad Ragab, Muhammad R. Hajj<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-237<\/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-18229 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aero-elastic tag-cuf tag-thermo-elastic tag-visco-elastic homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/aero-thermo-elastic-stability-analysis-of-multi-layered-visco-elastic-panels\/\" target=&quot;_blank&quot;>\n\t\t\t\tAERO-THERMO-ELASTIC STABILITY ANALYSIS OF MULTI-LAYERED VISCO-ELASTIC PANELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Enrico Zappino, Matteo Filippi, Erasmo Carrera<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-229<\/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-18217 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-fiber-bragg-grating-fbg-sensors tag-large-deformations tag-shape-prediction tag-strain-displacement-transformation-sdt homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1960 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\/deformed-wing-shape-prediction-using-fiber-optic-strain-data\/\" target=&quot;_blank&quot;>\n\t\t\t\tDEFORMED WING SHAPE PREDICTION USING FIBER OPTIC STRAIN 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>Yang Meng, Changchuan Xie, Zhiqiang Wan<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-222<\/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-18214 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-fsi tag-geometrical-nonlinear-fem tag-static-aeroelastic homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1961 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\/nonlinear-static-aeroelastic-analysis-of-high-aspect-ratio-wing-based-on-cfd-csd-coupling-solution\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR STATIC AEROELASTIC ANALYSIS OF HIGH-ASPECT RATIO WING BASED ON CFD\/CSD COUPLING SOLUTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yang Lan , Xie Changchuan , Yang Chao , Zhang Bing , Andrea Da Rouch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-221<\/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-18202 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-adjoint-variables tag-bifurcation tag-utter tag-mesh-adaptation tag-piston-theory homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/adjoint-based-mesh-adaptation-for-direct-flutter-prediction\/\" target=&quot;_blank&quot;>\n\t\t\t\tADJOINT-BASED MESH ADAPTATION FOR DIRECT FLUTTER PREDICTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kevin G. Wang, Philip S. Beran, Shunxiang Cao<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-212<\/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-18198 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-composite-structure tag-conceptual-design tag-genetic-algorithm tag-multidisciplinary-design-optimization tag-strut-braced-wing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1955 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\/multidisciplinary-design-optimization-of-wing-structure-for-strut-braced-wing-aircraft-considering-aeroelasticity\/\" target=&quot;_blank&quot;>\n\t\t\t\tMULTIDISCIPLINARY DESIGN OPTIMIZATION OF WING STRUCTURE FOR STRUT-BRACED WING AIRCRAFT CONSIDERING 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>Wang Zexi, Wan Zhiqiang, Yang Chao, Zhu Siyan<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-210<\/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-18195 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-conceptual-phase tag-integrated-optimization-design tag-kriging tag-large-aircraft homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1955 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\/an-integrated-optimization-and-surrogate-analysis-of-large-aircraft-in-conceptual-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN INTEGRATED OPTIMIZATION AND SURROGATE ANALYSIS OF LARGE AIRCRAFT IN CONCEPTUAL 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>Xiaozhe Wang, Zhiqiang Wan, Chao Yang<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-209<\/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-18192 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-aic-correction tag-dlm tag-gusts tag-uvlm homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-993 category-1958 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\/comparison-of-aerodynamic-models-for-1-cosine-gust-loads-prediction\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPARISON OF AERODYNAMIC MODELS FOR 1-COSINE GUST LOADS PREDICTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christopher Wales, R. G. Cook, D. P. Jones, A. L. Gaitonde<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-208<\/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-18186 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-aeroelasticity tag-dynamic-maneuver-loads tag-flight-test tag-preliminary-design tag-sailplane tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-993 category-1958 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\/dynamic-maneuver-loads-calculation-for-a-sailplane-and-comparison-with-flight-test\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC MANEUVER LOADS CALCULATION FOR A SAILPLANE AND COMPARISON WITH 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>Arne Vo\u00df, Gabriel Pinho Chiozzotto, Per Ohme<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-206<\/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-18180 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-freeplay tag-ifasd tag-nltva tag-nonlinear homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/freeplay-induced-limit-cycle-oscillation-mitigation-using-linear-and-nonlinear-tuned-vibration-absorbers\/\" target=&quot;_blank&quot;>\n\t\t\t\tFREEPLAY-INDUCED LIMIT CYCLE OSCILLATION MITIGATION USING LINEAR AND NONLINEAR TUNED VIBRATION ABSORBERS\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. Verstraelen, G. Kerschen, G. Dimitriadis<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-204<\/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-18177 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-cfd tag-fluid-structure-interaction tag-gust-encounter tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/an-optimized-doublet-lattice-method-correction-approach-for-a-large-civil-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN OPTIMIZED DOUBLET-LATTICE METHOD CORRECTION APPROACH FOR A LARGE CIVIL 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>C. Valente, C. Wales, D. Jones, A. Gaitonde, J. E. Cooper, Y. Lemmens<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-200<\/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-18174 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-load-control-and-alleviation tag-wingtip-devices homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-993 category-1958 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\/design-of-an-innovative-wing-tip-device\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN OF AN INNOVATIVE WING TIP DEVICE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>F. Toffol, F. Fonte, S. Ricci<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-198<\/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-18168 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-flutter tag-laminar-wing tag-risk-analysis tag-transition tag-transonic-flow tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1955 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\/risk-analysis-for-flutter-of-laminar-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tRISK ANALYSIS FOR FLUTTER OF LAMINAR 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>Lorenz Tichy, Holger Mai, Michael Fehrs, Jens Nitzsche, Anne Hebler<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-196<\/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-18162 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-bifucation-analysis tag-landing-gears tag-lco tag-optimization tag-shimmy homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-993 category-1958 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\/reliable-robust-optimization-of-a-landing-gear-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tRELIABLE &amp; ROBUST OPTIMIZATION OF A LANDING GEAR 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>Irene Tartaruga, Jonathan E. Cooper, Mark H. Lowenberg, Yves Lemmens<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-193<\/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-18153 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-dampers tag-discrete-gust tag-loads-alleviation tag-passive tag-truss-braced-wing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1955 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\/passive-gust-loads-alleviation-in-a-truss-braced-wing-using-integrated-dampers\/\" target=&quot;_blank&quot;>\n\t\t\t\tPASSIVE GUST LOADS ALLEVIATION IN A TRUSS-BRACED WING USING INTEGRATED DAMPERS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christopher P. Szczyglowski, Simon A. Neild, Brano Titurus, Jason Z. Jiang, Jonathan E. Cooper, Etienne Coetzee<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-190<\/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-18149 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-distributed-control tag-exible-aircraft tag-optimum-wing-geometry tag-wing-shaping-control homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1961 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\/optimum-distributed-wing-shaping-and-control-loads-for-highly-flexible-mission-adaptive-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tOPTIMUM DISTRIBUTED WING SHAPING AND CONTROL LOADS FOR HIGHLY FLEXIBLE MISSION-ADAPTIVE 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>Jared R. Hammerton, Weihua Su, Guoming Zhu, Sean Shan-Min Swei<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-189<\/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-18143 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-cfd-mesh-deformation tag-cfd-mesh-repair tag-cfd-csm tag-uid-structure-interaction tag-multi-body-simulation tag-nonlinear-fem homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/high-fidelity-cfd-csm-interaction-in-the-industrial-context\/\" target=&quot;_blank&quot;>\n\t\t\t\tHIGH-FIDELITY CFD-CSM INTERACTION IN THE 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>Bernd Stickan, Arne Rempke, Sebastian Helm, Hans Bleecke<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-186<\/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-18136 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-divergence tag-experimental-aeroelasticity tag-flutter tag-parametric-flutter-margin homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1960 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\/experimental-investigation-of-flutter-boundary-with-controlled-vibration-levels\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL INVESTIGATION OF FLUTTER BOUNDARY WITH CONTROLLED VIBRATION LEVELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jurij Sodja , Federico Roizner, Roeland De Breuker, Moti Karpel<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-184<\/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-18130 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-cfd tag-gust tag-optimisation tag-parameterisation tag-potential-ow tag-reconstruction tag-rom homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-993 category-1958 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\/reconstruction-of-gust-velocity-profiles-via-potential-flow-cfd-and-rom-techniques\/\" target=&quot;_blank&quot;>\n\t\t\t\tRECONSTRUCTION OF GUST VELOCITY PROFILES VIA POTENTIAL FLOW, CFD AND ROM TECHNIQUES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Simone Simeone, Thomas Rendall, Stephen Williams, Christopher Wales, Jonathan E. Cooper, Dorian Jones, Ann L. Gaitonde<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-182<\/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-18124 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/computational-and-experimental-results-for-the-kth-nasa-wind-tunnel-model-used-for-acquisition-of-transonic-nonlinear-aeroelastic-data\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPUTATIONAL AND EXPERIMENTAL RESULTS FOR THE KTH-NASA WIND-TUNNEL MODEL USED FOR ACQUISITION OF TRANSONIC NONLINEAR AEROELASTIC 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>Walter A. Silva, Pawel Chwalowski, Carol D. Wieseman, Donald F. Keller, David Eller, Ulf Ringertz<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-180<\/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-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-18112 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-aeroservoelasticity tag-double-lattice-method tag-finite-element-method tag-flexible-aircraft tag-flutter-suppression tag-gust-alleviation homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1961 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\/on-the-control-of-aeroelastic-flight-dynamic-integrated-stability-of-maneuvering-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tON THE CONTROL OF AEROELASTIC\/FLIGHT DYNAMIC INTEGRATED STABILITY OF MANEUVERING 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>Francesco Saltari, Franco Mastroddi, Cristina Riso, Guido De Matteis, Sara Colaianni<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-175<\/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-18106 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-exible-wing tag-utter tag-small-disturbance-cfd tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1955 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\/aeroelastic-analysis-of-a-flutter-demonstrator-with-a-very-flexible-high-aspect-ratio-swept-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC ANALYSIS OF A FLUTTER DEMONSTRATOR WITH A VERY FLEXIBLE HIGH-ASPECT-RATIO SWEPT 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>Vladyslav Rozov, Andreas Hermanutz, Christian Breitsamter, Mirko Hornung<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-173<\/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-18100 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-extended-modal-approach tag-geometrically-large-deformations tag-nonlinear-flight-dynamics tag-unsteady-vortex-lattice tag-very-exible-aircraft tag-x-hale homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1961 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\/free-flight-nonlinear-aeroelastic-simulations-of-the-x-hale-uav-by-an-extended-modal-approach\/\" target=&quot;_blank&quot;>\n\t\t\t\tFREE-FLIGHT NONLINEAR AEROELASTIC SIMULATIONS OF THE X-HALE UAV BY AN EXTENDED MODAL 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>Markus Ritter, Jessica Jones, Carlos E. S. Cesnik<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-171<\/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-18097 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-finite-element-method tag-fluid-structure-interaction tag-highly-flexible-aircraft tag-inertia-relief tag-nonlinear-aeroelastic-trim homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1961 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\/a-fem-based-approach-for-nonlinear-aeroelastic-trim-of-highly-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tA FEM-BASED APPROACH FOR NONLINEAR AEROELASTIC TRIM 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>Cristina Riso, Fausto G. Di Vincenzo, Markus Ritter, Carlos E. S. Cesnik, Franco Mastroddi<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-170<\/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-18079 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelastic-prediction-workshop tag-flutter-analysis homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/flutter-analysis-for-the-second-aeroelastic-prediction-workshop\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER ANALYSIS FOR THE SECOND AEROELASTIC PREDICTION WORKSHOP\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Daniella E. Raveh<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-163<\/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-18073 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-cantilevered-plate tag-exible-wings tag-uid-structure-interaction tag-hale tag-leading-edge-vortices homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1961 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\/experimental-and-numerical-investigation-of-post-flutter-limit-cycle-oscillations-on-a-cantilevered-flat-plate\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL AND NUMERICAL INVESTIGATION OF POST-FLUTTER LIMIT CYCLE OSCILLATIONS ON A CANTILEVERED FLAT PLATE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kiran Ramesh, Tiago Priolli Monteiro, Fl\u00e1vio Jos\u00e9 Silvestre, Ant\u00f4nio Bernardo Guimar\u00e3es Neto, Thiago de Souza Siqueira Versiani, Roberto Gil Annes da Silva<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-161<\/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-18069 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-gust-loads tag-optimization tag-reduced-oder-model tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1955 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\/preliminary-aeroelastic-design-framework-for-composite-wings-subjected-to-gust-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tPRELIMINARY AEROELASTIC DESIGN FRAMEWORK FOR COMPOSITE WINGS SUBJECTED TO GUST 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>Darwin Rajpal, Roeland De Breuker<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-160<\/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-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-18060 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-landing tag-loads tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics homepage_sections-materials-and-structures category-993 category-1958 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\/hard-landing-and-rebound-landing-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tHARD LANDING AND REBOUND LANDING 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, S. Parra Ad\u00e1n, E. G\u00f3mez Vi\u00f1as, H. Climent M\u00e1\u00f1ez<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-153<\/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-18054 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-additive tag-fabrication tag-morphing tag-sensing tag-stretchable tag-topology homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1960 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\/from-model-to-manufacture-additive-aeroelastic-morphing-testbeds\/\" target=&quot;_blank&quot;>\n\t\t\t\tFROM MODEL TO MANUFACTURE: ADDITIVE AEROELASTIC MORPHING TESTBEDS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alexander M. Pankonien, James O. Hardin, Nitin Bhagat, Gregory W. Reich, John D. Berrigan<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-151<\/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-18048 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-adjoint-sensititivities tag-algorithmic-differentiation tag-uid-structure-interaction tag-geometrically-nonlinear-structures tag-multidisciplinary-optimization tag-viscous-ows homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/computing-derivatives-in-nonlinear-aeroelasticity-using-algorithm-differentiation\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPUTING DERIVATIVES IN NONLINEAR AEROELASTICITY USING ALGORITHM DIFFERENTIATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ruben Sanchez, Rafael Palacios<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-149<\/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-18042 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-asymmetry tag-electromechanical-modeling tag-flutter tag-numerical-simulation homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1960 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-simulation-and-experimental-flutter-research-of-an-aircraft-with-asymmetric-control-surfaces\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL SIMULATION AND EXPERIMENTAL FLUTTER RESEARCH OF AN AIRCRAFT WITH ASYMMETRIC CONTROL SURFACES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>O. A. Orlova, M. A. Pronin, V. I. Smyslov<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-146<\/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-18036 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aepw tag-aeroelasticity tag-bscw tag-computational tag-dynamics tag-uid tag-utter tag-transonic homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 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\/effect-of-angle-of-attack-gas-composition-and-reynolds-number-on-flutter-boundary-of-benchmark-super-critical-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFECT OF ANGLE OF ATTACK, GAS COMPOSITION AND REYNOLDS NUMBER ON FLUTTER BOUNDARY OF BENCHMARK SUPER-CRITICAL 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>Jan Navr\u00e1til, Adam Jir\u00e1sek, Peter Hamlington, Lt. Col. Andrew Lofthouse<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-142<\/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-18027 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-optimisation tag-resonance tag-topology tag-vibrations homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-flight-mechanics category-993 category-1960 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\/topology-optimisation-of-representative-aircraft-wing-geometries-with-an-experimental-validation\/\" target=&quot;_blank&quot;>\n\t\t\t\tTOPOLOGY OPTIMISATION OF REPRESENTATIVE AIRCRAFT WING GEOMETRIES WITH AN EXPERIMENTAL VALIDATION\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 J. Munk, Gareth A. Vio, Nicholas F. Giannelis, Jonathan E. Cooper<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-139<\/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-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-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<\/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<div class=\"e-load-more-anchor\" data-page=\"1\" data-max-page=\"2\" data-next-page=\"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/11434\/page\/2\/\"><\/div>\n\t\t\t\t<div class=\"e-load-more-message\">No more posts to show<\/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 Aircraft Design 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 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