{"id":18254,"date":"2024-10-09T23:00:32","date_gmt":"2024-10-09T23:00:32","guid":{"rendered":"https:\/\/aerospacerepository.org\/?page_id=18254"},"modified":"2025-02-25T19:30:34","modified_gmt":"2025-02-25T19:30:34","slug":"repository-ifasd-2019","status":"publish","type":"page","link":"https:\/\/aerospacerepository.org\/index.php\/repository-ifasd-2019\/","title":{"rendered":"Repository IFASD 2019"},"content":{"rendered":"\t\t<div data-elementor-type=\"wp-page\" data-elementor-id=\"18254\" class=\"elementor elementor-18254\" 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 IFASD 2019 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;:[2433],&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;yes&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 IFASD 2019 Papers...\" value=\"\" name=\"s\" autocomplete=\"off\" \/>\n\t\t\t\t\t\t\t<input type=\"hidden\" value=\"{&quot;include_terms_ids&quot;:[2433],&quot;sentence&quot;:true}\" 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-962fb9c elementor-widget elementor-widget-heading\" data-id=\"962fb9c\" 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<h4 class=\"elementor-heading-title elementor-size-default\">Search by Event Topic<\/h4>\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-e6e888c elementor-widget elementor-widget-jet-smart-filters-checkboxes\" data-id=\"e6e888c\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"jet-smart-filters-checkboxes.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<div class=\"jet-smart-filters-checkboxes jet-filter \" data-indexer-rule=\"show\" data-show-counter=\"\" data-change-counter=\"always\"><div class=\"jet-checkboxes-list\" data-query-type=\"tax_query\" data-query-var=\"category\" data-smart-filter=\"checkboxes\" data-filter-id=\"18274\" data-apply-type=\"ajax\" data-content-provider=\"epro-posts\" data-additional-providers=\"\" data-query-id=\"default\" data-active-label=\"\" data-layout-options=\"{&quot;show_label&quot;:&quot;&quot;,&quot;display_options&quot;:{&quot;show_items_label&quot;:false,&quot;show_decorator&quot;:&quot;yes&quot;,&quot;filter_image_size&quot;:&quot;full&quot;,&quot;show_counter&quot;:false}}\" data-query-var-suffix=\"\" data-apply-on=\"value\">\n\t<fieldset class=\"jet-checkboxes-list-wrapper\"><legend style=\"display:none;\">IFASD2019<\/legend><div class=\"jet-list-tree\"><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2434\"\n\t\t\tdata-label=\"Aeroelastic Analysis Frameworks\"\n\t\t\t\t\t\taria-label=\"Aeroelastic Analysis Frameworks\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroelastic Analysis Frameworks\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2435\"\n\t\t\tdata-label=\"Aeroelastic Design Applications\"\n\t\t\t\t\t\taria-label=\"Aeroelastic Design Applications\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroelastic Design Applications\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2437\"\n\t\t\tdata-label=\"Aeroelastic Optimization\"\n\t\t\t\t\t\taria-label=\"Aeroelastic Optimization\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroelastic Optimization\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2436\"\n\t\t\tdata-label=\"Aeroelastic Optimization Frameworkes\"\n\t\t\t\t\t\taria-label=\"Aeroelastic Optimization Frameworkes\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroelastic Optimization Frameworkes\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2438\"\n\t\t\tdata-label=\"Aeroservoelasticity\"\n\t\t\t\t\t\taria-label=\"Aeroservoelasticity\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroservoelasticity\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2439\"\n\t\t\tdata-label=\"Computational Aeroelasticity\"\n\t\t\t\t\t\taria-label=\"Computational Aeroelasticity\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tComputational Aeroelasticity\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2440\"\n\t\t\tdata-label=\"Computational Flutter\"\n\t\t\t\t\t\taria-label=\"Computational Flutter\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tComputational Flutter\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2441\"\n\t\t\tdata-label=\"Control of Very Flexible Aircraft\"\n\t\t\t\t\t\taria-label=\"Control of Very Flexible Aircraft\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tControl of Very Flexible Aircraft\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2442\"\n\t\t\tdata-label=\"Dynamic Loads\"\n\t\t\t\t\t\taria-label=\"Dynamic Loads\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tDynamic Loads\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2443\"\n\t\t\tdata-label=\"Experimental Active Control\"\n\t\t\t\t\t\taria-label=\"Experimental Active Control\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tExperimental Active Control\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2444\"\n\t\t\tdata-label=\"Experimental Methods in Aeroelasticity\"\n\t\t\t\t\t\taria-label=\"Experimental Methods in Aeroelasticity\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tExperimental Methods in Aeroelasticity\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2445\"\n\t\t\tdata-label=\"Experimental Methods in Structural Dynamics\"\n\t\t\t\t\t\taria-label=\"Experimental Methods in Structural Dynamics\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tExperimental Methods in Structural Dynamics\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2446\"\n\t\t\tdata-label=\"Flight Testing\"\n\t\t\t\t\t\taria-label=\"Flight Testing\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tFlight Testing\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2447\"\n\t\t\tdata-label=\"Ground Vibration Testing\"\n\t\t\t\t\t\taria-label=\"Ground Vibration Testing\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tGround Vibration Testing\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2448\"\n\t\t\tdata-label=\"Limit Cycle Oscillation\"\n\t\t\t\t\t\taria-label=\"Limit Cycle Oscillation\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tLimit Cycle Oscillation\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2449\"\n\t\t\tdata-label=\"Maneuver and Gust Loads\"\n\t\t\t\t\t\taria-label=\"Maneuver and Gust Loads\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tManeuver and Gust Loads\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2450\"\n\t\t\tdata-label=\"Modeling for Design of Highly Flexible Aircraft\"\n\t\t\t\t\t\taria-label=\"Modeling for Design of Highly Flexible Aircraft\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tModeling for Design of Highly Flexible Aircraft\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2451\"\n\t\t\tdata-label=\"Panel Flutter\"\n\t\t\t\t\t\taria-label=\"Panel Flutter\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tPanel Flutter\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2452\"\n\t\t\tdata-label=\"Reduced Order Models\"\n\t\t\t\t\t\taria-label=\"Reduced Order Models\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tReduced Order Models\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><\/div><\/fieldset><\/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-217e6ca elementor-widget elementor-widget-spacer\" data-id=\"217e6ca\" 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-d8b18a0 elementor-widget elementor-widget-spacer\" data-id=\"d8b18a0\" 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-1fac479 elementor-widget elementor-widget-spacer\" data-id=\"1fac479\" 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-fa9661a elementor-widget elementor-widget-spacer\" data-id=\"fa9661a\" 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-5432385 elementor-widget elementor-widget-spacer\" data-id=\"5432385\" 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-667366d elementor-widget elementor-widget-spacer\" data-id=\"667366d\" 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-7047487 elementor-widget elementor-widget-spacer\" data-id=\"7047487\" 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-ee10ab8 elementor-widget elementor-widget-spacer\" data-id=\"ee10ab8\" 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-5ffe419 elementor-widget elementor-widget-spacer\" data-id=\"5ffe419\" 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-ab572bb elementor-widget elementor-widget-spacer\" data-id=\"ab572bb\" 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-e20ec19 elementor-widget elementor-widget-spacer\" data-id=\"e20ec19\" 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=\"epro-posts\" 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=\"epro-posts\" 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-18724 post type-post status-publish format-standard hentry category-computational-flutter category-1-ifasd-2019 tag-cfd-csd-simulation tag-dynamic-eigen-decomposition tag-dynamic-eigenmodes tag-flutter-prediction tag-frequency-domain-stability tag-gust-response category-2440 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/flutter-prediction-based-on-dynamic-eigen-decomposition-of-coupled-cfd-csd-flight-simulation\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER PREDICTION BASED ON DYNAMIC EIGEN DECOMPOSITION OF COUPLED CFD-CSD FLIGHT SIMULATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kim, T.<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-001<\/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-18727 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-cfd tag-angle-of-attack-effect tag-transonic-flutter-boundary tag-turbulence-modelling tag-unsteady-cfd category-2433 category-2454 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/turbulence-modelling-and-angle-of-attack-effects-on-transonic-flutter-boundary-using-unsteady-navierstokes-solvers\/\" target=&quot;_blank&quot;>\n\t\t\t\tTURBULENCE MODELLING AND ANGLE OF ATTACK EFFECTS ON TRANSONIC FLUTTER BOUNDARY USING UNSTEADY NAVIERSTOKES SOLVERS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>L. Daumas, N. Forestier, M. Perrocheau, G. Broux, F. Chalot, Z. Johan, M. Mallet<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-002<\/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-18730 post type-post status-publish format-standard hentry category-control-of-very-flexible-aircraft category-1-ifasd-2019 tag-aeroservoelasticity tag-control-of-exible-aircraft tag-loop-separation tag-model-predictive-control tag-reference-governor category-2441 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/very-flexible-aircraft-control-based-on-loop-separation-and-reference-governor\/\" target=&quot;_blank&quot;>\n\t\t\t\tVERY FLEXIBLE AIRCRAFT CONTROL BASED ON LOOP-SEPARATION AND REFERENCE GOVERNOR\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Pedro J. Gonzalez, Mateus de Freitas Virgilio Pereira, Flavio J. Silvestre, Ilya Kolmanovsky, Carlos E. S. Cesnik<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-005<\/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-18733 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-cfd tag-aerodynamic-resonance tag-ow-separation tag-uid-mode-utter tag-p-k-method tag-transonic-buffet tag-unsteady-aerodynamics category-2433 category-2454 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/fluid-mode-flutter-in-plane-transonic-flows\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUID-MODE FLUTTER IN PLANE TRANSONIC FLOWS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jens Nitzsche, Lisa M. Ringel, Christoph Kaiser, Holger Hennings<\/b><\/p>\n<p>DOI number: N\/A<\/p>\n<p>Conference number: IFASD-2019-006<\/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-18736 post type-post status-publish format-standard hentry category-1-ifasd-2019 tag-aeroelastic-validation tag-computational-aeroelasticity tag-flutter tag-flutter-bucket tag-fun3d tag-transonic-dip tag-unsteady-aerodynamics category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/predicting-transonic-flutter-using-nonlinear-computational-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tPREDICTING TRANSONIC FLUTTER USING NONLINEAR COMPUTATIONAL 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>Jennifer Heeg, Pawel Chwalowski<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-007<\/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-18739 post type-post status-publish format-standard hentry category-experimental-active-control category-1-ifasd-2019 tag-aeroelasticity tag-optimal-control tag-structural-dynamics tag-wind-tunnel-experiments category-2443 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/low-cost-wind-tunnel-studies-of-gust-alleviation-control-techniques\/\" target=&quot;_blank&quot;>\n\t\t\t\tLOW-COST WIND TUNNEL STUDIES OF GUST ALLEVIATION CONTROL 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>B. Barzgaran, J. Quenzer, A. Zongolowicz, K. Hinson, M. Mesbahi, K. Morgansen, E. Livne<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-008<\/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-18742 post type-post status-publish format-standard hentry category-experimental-active-control category-1-ifasd-2019 tag-energy-harvesting-2 tag-flag tag-flutter tag-lco tag-non-linearity tag-piezoelectricity category-2443 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/improving-piezoelectric-energy-harvesting-from-an-aeroelastic-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tIMPROVING PIEZOELECTRIC ENERGY HARVESTING FROM AN AEROELASTIC 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>Dani Levin, Earl H. Dowell<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-009<\/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-18745 post type-post status-publish format-standard hentry category-computational-flutter category-1-ifasd-2019 tag-linearized-frequency-domain-solver tag-strip-theory tag-t-tail-flutter tag-unsteady-aerodynamics category-2440 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/assessment-of-t-tail-flutter-using-an-enhanced-potential-flow-theory-approach-and-linearized-frequency-domain-cfd-data\/\" target=&quot;_blank&quot;>\n\t\t\t\tASSESSMENT OF T-TAIL FLUTTER USING AN ENHANCED POTENTIAL FLOW THEORY APPROACH AND LINEARIZED FREQUENCY DOMAIN CFD 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>Dominik Sch\u00e4fer, J\u00fcrgen Arnold<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-010<\/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-18748 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-cfd tag-aeroelastic-simulations tag-cfd category-2433 category-2454 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/aeroelastic-simulations-of-complicated-configuration-using-overset-unstructured-cfd-solver\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC SIMULATIONS OF COMPLICATED CONFIGURATION USING OVERSET UNSTRUCTURED CFD 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>Hitoshi Arizono, Hamid Reza Kheirandish<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-011<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18751 post type-post status-publish format-standard hentry category-control-of-very-flexible-aircraft category-1-ifasd-2019 tag-exible-aircraft tag-projective-control tag-sas tag-x-hale category-2441 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/design-of-stability-augmentation-systems-for-flexible-aircraft-using-projective-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN OF STABILITY AUGMENTATION SYSTEMS FOR FLEXIBLE AIRCRAFT USING PROJECTIVE 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>Rafael M. Bertolin, Antonio B. Guimaraes Neto, Guilherme C. Barbosa, Juliano A. Paulino, Fl\u00b4avio J. Silvestre<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-012<\/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-18754 post type-post status-publish format-standard hentry category-control-of-very-flexible-aircraft category-1-ifasd-2019 tag-control-design tag-exible-aircraft tag-fuzzy-logic tag-gain-scheduling-2 category-2441 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/fuzzy-gain-scheduling-for-mimo-systems-applied-to-flexible-aircraft-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tFUZZY GAIN-SCHEDULING FOR MIMO SYSTEMS APPLIED TO FLEXIBLE AIRCRAFT 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>Guilherme C. Barbosa, Antonio B. Guimaraes Neto, Rafael M. Bertolin, Flavio J. Silvestre<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-013<\/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-18757 post type-post status-publish format-standard hentry category-experimental-active-control category-1-ifasd-2019 tag-aeroelastic-model tag-flutter-suppression tag-wind-tunnel-test category-2443 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/12\/numerical-and-experimental-investigations-on-active-flutter-suppression-technologies\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL AND EXPERIMENTAL INVESTIGATIONS ON ACTIVE FLUTTER SUPPRESSION TECHNOLOGIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Federico Fonte, Alessandro De Gaspari, Luca Riccobene, Francesco Toffol, Sheharyar Malik, Luca Marchetti, Sergio Ricci, Paolo Mantegazza, Eli Livne<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-014<\/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-18761 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-cfd tag-cfd tag-chimera tag-control-surfaces tag-overlap tag-overset tag-unsteady-cfd category-2433 category-2454 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/13\/control-surface-modelling-of-unsteady-large-amplitude-motion-via-chimera-cfd-technique\/\" target=&quot;_blank&quot;>\n\t\t\t\tCONTROL SURFACE MODELLING OF UNSTEADY LARGE AMPLITUDE MOTION VIA CHIMERA CFD TECHNIQUE\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, Reik Thormann, Hans Bleecke<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-015<\/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-18764 post type-post status-publish format-standard hentry category-computational-flutter category-1-ifasd-2019 tag-distributed-aeroelastic-energy tag-fighter-aircraft-utter tag-flutter-analysis tag-flutter-mechanism category-2440 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/13\/flutter-mechanisms-characterization-using-distributed-aeroelastic-energy-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER MECHANISMS CHARACTERIZATION USING DISTRIBUTED AEROELASTIC ENERGY 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>Cap. Yaara Karniel and Cap. Daniel Kariv, Maj. Michael Iovnovich<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-016<\/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-18767 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-cantilever tag-lco tag-nonlinear tag-piston-theory category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/13\/flutter-and-limit-cycle-oscillations-of-a-cantilevered-plate-in-supersonic-hypersonic-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER AND LIMIT CYCLE OSCILLATIONS OF A CANTILEVERED PLATE IN SUPERSONIC\/HYPERSONIC 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>Kevin A. McHugh , Philip Beran, Maxim Freydin, Earl Dowell<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-017<\/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-18770 post type-post status-publish format-standard hentry category-control-of-very-flexible-aircraft category-1-ifasd-2019 tag-exible-aircraft tag-load-alleviation tag-model-predictive-control category-2441 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/13\/model-predictive-control-for-maneuver-load-alleviation-in-flexible-airliners\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODEL PREDICTIVE CONTROL FOR MANEUVER LOAD ALLEVIATION IN FLEXIBLE AIRLINERS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Mateus de F. V. Pereira, Ilya Kolmanovsky, Carlos E. S. Cesnik, Fabio Vetrano<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-018<\/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-18772 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-cfd tag-buffeting tag-double-delta-wing tag-grid-adaptation tag-vortex-lift category-2433 category-2454 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/13\/characterizing-a-multi-delta-wing-for-aeroelastic-wind-tunnel-experiments\/\" target=&quot;_blank&quot;>\n\t\t\t\tCHARACTERIZING A MULTI DELTA WING FOR AEROELASTIC WIND TUNNEL 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>Jonas Zastrow<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-019<\/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-18776 post type-post status-publish format-standard hentry category-aeroelastic-optimization-framewroks category-1-ifasd-2019 tag-aeroelastic-optimization tag-meta-model tag-preliminary-and-conceptual-design category-2436 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/13\/neopt-an-optimization-suite-for-the-aeroelastic-preliminary-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tNEOPT: AN OPTIMIZATION SUITE FOR THE AEROELASTIC 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>F. Toffol, S. Ricci<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-020<\/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-18779 post type-post status-publish format-standard hentry category-aeroelastic-optimization-framewroks category-1-ifasd-2019 tag-aeroelastic-analysis tag-conceptual-design tag-neocass category-2436 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/13\/recent-developments-of-neocass-the-open-source-suite-for-structural-sizing-and-aeroelastic-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tRECENT DEVELOPMENTS OF NEOCASS THE OPEN SOURCE SUITE FOR STRUCTURAL SIZING AND AEROELASTIC 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>Federico Fonte, Sergio Ricci<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-021<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18782 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-cfd tag-buffet tag-cfd tag-lco category-2433 category-2454 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/12\/13\/rans-and-dns-study-of-buffet-in-subsonic-and-transonic-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tRANS AND DNS STUDY OF BUFFET IN SUBSONIC AND TRANSONIC 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>Kai M. Kruger Bastos, Earl H. Dowell<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-022<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18787 post type-post status-publish format-standard hentry category-control-of-very-flexible-aircraft category-1-ifasd-2019 tag-active-control tag-aeroelasticity tag-feedback-linearisation tag-nonlinearity category-2441 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/active-control-for-nonlinear-aeroelastic-systems\/\" target=&quot;_blank&quot;>\n\t\t\t\tACTIVE CONTROL FOR NONLINEAR AEROELASTIC SYSTEMS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Shakir Jiffri, Hamed H. Khodaparast, Marinos Manolesos, Sebastiano Fichera<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-023<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18790 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-computational-aeroelasticity tag-reduced-order-models category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/self-adaptive-pod-based-rom-3d-aeroelastic-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tSELF ADAPTIVE POD BASED ROM 3D AEROELASTIC SIMULATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ruben Moreno-Ramos, Fernando Varas, Jose M. Vega<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-024<\/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-18793 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-flutter tag-gaf-approximation tag-lfd tag-pod category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/error-estimation-and-pod-based-reference-selection-to-approximate-gaf-matrices-for-flutter\/\" target=&quot;_blank&quot;>\n\t\t\t\tERROR ESTIMATION AND POD-BASED REFERENCE SELECTION TO APPROXIMATE GAF MATRICES FOR FLUTTER\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Hendrik Verdonck, Reik Thormann, Hans Bleecke, Bernd Stickan<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-025<\/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-18796 post type-post status-publish format-standard hentry category-control-of-very-flexible-aircraft category-1-ifasd-2019 tag-aeroservoelasticity tag-control-of-exible-aircraft tag-notch-lter category-2441 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/advantages-of-using-aeroelastic-feedback-in-flexible-aircraft-control-instead-of-applying-notch-filtering\/\" target=&quot;_blank&quot;>\n\t\t\t\tADVANTAGES OF USING AEROELASTIC FEEDBACK IN FLEXIBLE AIRCRAFT CONTROL INSTEAD OF APPLYING NOTCH-FILTERING\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 Drewiacki, Flavio J. Silvestre, Antonio Bernardo Guimaraes Neto<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-026<\/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-18799 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-cfd tag-abl tag-cfd tag-fun3d tag-mddes tag-tdt tag-unsteady-aerodynamics category-2433 category-2454 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/modeling-of-an-atmospheric-boundary-layer-profile-in-support-of-experiments-in-the-nasa-langley-transonic-dynamics-tunnel\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODELING OF AN ATMOSPHERIC-BOUNDARY-LAYER PROFILE IN SUPPORT OF EXPERIMENTS IN THE NASA LANGLEY TRANSONIC DYNAMICS TUNNEL\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Pawel Chwalowski, Thomas G. Ivanco<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-027<\/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-18802 post type-post status-publish format-standard hentry category-aeroelastic-optimization-framewroks category-1-ifasd-2019 tag-aeroelastic-design tag-cpacs-mona tag-high-fidelity-based-mdo tag-loads-analysis tag-parametric-modelling category-2436 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/cpacs-mona-an-independent-and-in-high-fidelity-based-mdo-tasks-integrated-process-for-the-structural-and-aeroelastic-design-of-aircraft-configurations\/\" target=&quot;_blank&quot;>\n\t\t\t\tCPACS-MONA \u2013 AN INDEPENDENT AND IN HIGH-FIDELITY BASED MDO TASKS INTEGRATED PROCESS FOR THE STRUCTURAL AND AEROELASTIC DESIGN OF 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>T. Klimmek, M. Schulze, M. Abu-Zurayk, C. Ilic, A. Merle<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-028<\/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-18805 post type-post status-publish format-standard hentry category-aeroelastic-analysis-frameworks category-1-ifasd-2019 tag-modal-shapes-derivative tag-morinos-method tag-unsteady-aerodynamic-differentiation category-2434 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/flutter-sensitivity-analysis-for-wing-planform-optimization\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER SENSITIVITY ANALYSIS FOR WING PLANFORM OPTIMIZATION\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 Torrigiani, Jan-Niclas Walther, Rocco Bombardieri, Rauno Cavallaro, Pier Davide Ciampa<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-029<\/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-18808 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-adjoint tag-optimization tag-time-spectral-method category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/a-modular-implementation-of-the-time-spectral-method-for-aeroelastic-analysis-and-optimization-on-structured-meshes\/\" target=&quot;_blank&quot;>\n\t\t\t\tA MODULAR IMPLEMENTATION OF THE TIME SPECTRAL METHOD FOR AEROELASTIC ANALYSIS AND OPTIMIZATION ON STRUCTURED MESHES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christophe Blondeau, C\u00e9dric Liauzun<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-032<\/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-18811 post type-post status-publish format-standard hentry category-ground-vibration-testing category-1-ifasd-2019 tag-aircraft-certification tag-experimental-modal-analysis tag-ground-vibration-testing tag-operational-modal-analysis tag-taxi-vibration-testing category-2447 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/taxi-vibration-testing-a-new-and-time-efficient-procedure-for-the-identification-of-modal-parameters-on-aircrafts\/\" target=&quot;_blank&quot;>\n\t\t\t\tTAXI VIBRATION TESTING: A NEW AND TIME EFFICIENT PROCEDURE FOR THE IDENTIFICATION OF MODAL PARAMETERS ON AIRCRAFTS\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. Soal, Y. Govers, M. B\u00f6swald, A.<\/b>Vollmer<\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-033<\/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-18814 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-aerodynamics-1-ifasd-2019 tag-aeroelasticity tag-dlm-correction-2 tag-small-disturbance-cfd tag-structural-dynamics category-2433 category-2453 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/improvement-of-unsteady-aerodynamic-loads-prediction-of-the-doublet-lattice-method-using-small-disturbance-cfd\/\" target=&quot;_blank&quot;>\n\t\t\t\tIMPROVEMENT OF UNSTEADY AERODYNAMIC LOADS PREDICTION OF THE DOUBLET-LATTICE METHOD USING SMALL DISTURBANCE 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>Cyrille Vidy, Lukas Katzenmeier<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-034<\/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-18817 post type-post status-publish format-standard hentry category-aeroelastic-design-applications category-1-ifasd-2019 tag-aeroelasticity tag-fatigue-loads tag-gust-loads tag-structural-optimization tag-strut-braced-wing-2 category-2435 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/dynamic-aeroelastic-tailoring-of-a-strut-braced-wing-including-fatigue-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC AEROELASTIC TAILORING OF A STRUT BRACED WING INCLUDING FATIGUE 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-2019-035<\/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-18820 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-dynamic-mode-decomposition tag-dynamic-stall category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/analysis-of-light-dynamic-stall-using-dynamic-mode-decomposition\/\" target=&quot;_blank&quot;>\n\t\t\t\tANALYSIS OF LIGHT DYNAMIC STALL USING DYNAMIC MODE DECOMPOSITION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Wrik Mallik, Daniella E. Raveh<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-036<\/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-18823 post type-post status-publish format-standard hentry category-ground-vibration-testing category-1-ifasd-2019 tag-electric-aircraft tag-flutter tag-ground-vibration-testing tag-virtual-driving-point category-2447 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/07\/structural-dynamics-assessment-on-a-full-electric-aircraft-ground-vibration-testing-and-in-flight-measurements\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTRUCTURAL DYNAMICS ASSESSMENT ON A FULL-ELECTRIC AIRCRAFT: GROUND VIBRATION TESTING AND IN-FLIGHT MEASUREMENTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>E. Di Lorenzo, U. Musella, S. Vettori, R. Hallez, J. Debille, B. Peeters, W. Flynn, P.Z. Csurcsia<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-037<\/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-18827 post type-post status-publish format-standard hentry category-aeroelastic-design-applications category-1-ifasd-2019 tag-flutter tag-parametric tag-regional-aviation tag-strut-braced category-2435 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/parametric-flutter-analysis-of-strut-braced-wing-aircraft-for-regional-aviation\/\" target=&quot;_blank&quot;>\n\t\t\t\tPARAMETRIC FLUTTER ANALYSIS OF STRUT BRACED WING AIRCRAFT FOR REGIONAL AVIATION\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, Roberto G. A. da Silva, Patrice L. Guedes<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-038<\/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-18830 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-aerodynamics-1-ifasd-2019 tag-dynamic-stall tag-nite-wing tag-panel-method tag-semi-empirical-model tag-unsteady-aerodynamics category-2433 category-2453 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/onera-type-corrections-into-the-unsteady-vortex-lattice-method-for-dynamic-stall-representation\/\" target=&quot;_blank&quot;>\n\t\t\t\tONERA-TYPE CORRECTIONS INTO THE UNSTEADY VORTEX LATTICE METHOD FOR DYNAMIC STALL REPRESENTATION\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 R. dos Santos, Fl\u00b4avio D. Marques, Haithem E. Taha<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-039<\/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-18833 post type-post status-publish format-standard hentry category-ground-vibration-testing category-1-ifasd-2019 tag-finite-element-method tag-ground-vibration-test tag-model-update tag-optimization category-2447 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/fe-model-update-after-gvt-of-a-gripen-e-test-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tFE-MODEL UPDATE AFTER GVT OF A GRIPEN E TEST 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>Erik Holmberg<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-040<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18836 post type-post status-publish format-standard hentry category-ground-vibration-testing category-1-ifasd-2019 tag-ground-vibration-testing tag-modal-identification tag-phase-separation-method tag-structural-nonlinearities category-2447 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/airbus-beluga-xl-state-of-the-art-techniques-to-perform-a-ground-vibration-test-campaign-of-a-large-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tAIRBUS BELUGA XL STATE-OF-THE-ART TECHNIQUES TO PERFORM A GROUND VIBRATION TEST CAMPAIGN OF A LARGE 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. Stephan, P. Lubrina, J. Sinske, Y. Govers, N. Last\u00e8re<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-041<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18839 post type-post status-publish format-standard hentry category-aeroelastic-design-applications category-1-ifasd-2019 tag-aerodynamic-geometrical-nonlinearities tag-aeroelasticity tag-exible-aircraft tag-ight-dynamics tag-small-deformations category-2435 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/approximation-of-aerodynamic-geometrical-nonlinearities-in-aircraft-with-high-aspect-ratio-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPROXIMATION OF AERODYNAMIC GEOMETRICAL NONLINEARITIES IN AIRCRAFT WITH HIGH-ASPECT-RATIO WINGS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Antonio B. Guimaraes Neto<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-043<\/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-18842 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-computational-aeroelasticity tag-flutter-analysis tag-reduced-order-modeling tag-unsteady-aerodynamics category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/effect-of-external-stores-aerodynamics-on-analytic-fighter-aircraft-flutter-predictions-evaluation-of-a-superposition-modeling-approach\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFECT OF EXTERNAL STORES AERODYNAMICS ON ANALYTIC FIGHTER AIRCRAFT FLUTTER PREDICTIONS: EVALUATION OF A SUPERPOSITION MODELING 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>Maj. Michael Iovnovich<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-045<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18847 post type-post status-publish format-standard hentry category-aeroelastic-design-applications category-1-ifasd-2019 tag-aeroelastic-stability tag-curved-wing tag-fully-intrinsic-equations tag-unsteady-aerodynamics tag-veering category-2435 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/flutter-analysis-of-curved-wings-using-fully-intrinsic-equations\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER ANALYSIS OF CURVED WINGS USING FULLY INTRINSIC EQUATIONS\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.R. Amoozgar, S.A. Fazelzadeh, H. Haddad Khodaparast, M.I. Friswell, J.E. Cooper<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-046<\/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-18850 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-aerodynamics-1-ifasd-2019 tag-aerodynamic-forces tag-modal-coordinates tag-unsteady category-2433 category-2453 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/efficient-method-of-aerodynamic-force-calculation\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT METHOD OF AERODYNAMIC FORCE CALCULATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Masato Tamayama, Shusuke Yoshida, Tomohiro Yokozeki<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-047<\/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-18853 post type-post status-publish format-standard hentry category-aeroservoelasticity-1-ifasd-2019 category-1-ifasd-2019 tag-a330-mrtt tag-aeroservoelasticity tag-arbs tag-boom tag-in-flight-refuelling category-2438 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/aeroelastic-role-in-the-road-to-a-fully-automated-refuelling-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC ROLE IN THE ROAD TO A FULLY AUTOMATED REFUELLING 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 Lozano, J. Barrera Rodr\u00edguez, H\u00e9ctor Climent<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-048<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18856 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-whirl-flutte tag-aeroelasticity tag-full-span-model tag-ifasd tag-stick-model category-2433 category-2456 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/whirl-flutter-related-certification-according-to-far-cs-23-and-25-regulation-standards\/\" target=&quot;_blank&quot;>\n\t\t\t\tWHIRL FLUTTER-RELATED CERTIFICATION ACCORDING TO FAR\/CS 23 AND 25 REGULATION STANDARDS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ji\u0159\u00ed \u010ce\u010drdle<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-049<\/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-18859 post type-post status-publish format-standard hentry category-aeroservoelasticity-1-ifasd-2019 category-1-ifasd-2019 tag-aeroservoelasticity tag-broken-loop-analysis tag-closed-loop-flutter category-2438 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/two-views-of-the-same-problem-aeroservoelasticity-from-a-controls-and-flutter-perspective\/\" target=&quot;_blank&quot;>\n\t\t\t\tTWO VIEWS OF THE SAME PROBLEM: AEROSERVOELASTICITY FROM A CONTROLS AND FLUTTER PERSPECTIVE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Raj K. Narisetti, Paul F. Taylor, Jerry Newsom<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p> Conference number: IFASD-2019-050<\/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-18862 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-maneuver-and-gust-loads tag-cfd tag-flying-wing tag-maneuver-loads tag-structural-optimization tag-vlm category-2433 category-2449 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/comparing-vlm-and-cfd-maneuver-loads-calculations-for-a-flying-wing-configuration\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPARING VLM AND CFD MANEUVER LOADS CALCULATIONS FOR A FLYING WING 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>Arne Vo\u00df<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-051<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18865 post type-post status-publish format-standard hentry category-modeling-for-design-of-highly-flexible-aircraft tag-dynamic-loads tag-highly-flexible-aircraft-structures category-2450 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/the-structural-dynamics-of-flying-non-stop-for-100-days\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHE STRUCTURAL DYNAMICS OF FLYING NON STOP FOR 100 DAYS\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 Benassi, Carlo Aquilini<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-052<\/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-18868 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-maneuver-and-gust-loads tag-counter tag-gust-en tag-load-prediction tag-nasa-common-research-model-aeroelasticity tag-nonlinear-cfd tag-time-linearized-cfd tag-transonic-ow category-2433 category-2449 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/quantification-of-nonlinear-effects-in-gust-load-prediction\/\" target=&quot;_blank&quot;>\n\t\t\t\tQUANTIFICATION OF NONLINEAR EFFECTS IN GUST LOAD 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>Christoph Kaiser, David Quero, Jens Nitzsche<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-054<\/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-18871 post type-post status-publish format-standard hentry category-aeroelastic-optimization category-1-ifasd-2019 tag-aeroelastic-tailoring tag-composite-aircraft tag-load-alleviation tag-optimization category-2437 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/aeroelastic-tailoring-of-flexible-composite-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC TAILORING OF FLEXIBLE COMPOSITE 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>Mario Natella, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-055<\/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-18874 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-whirl-flutte tag-camrad tag-dymore tag-whirl-flutter tag-x-57-maxwell category-2433 category-2456 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/whirl-flutter-and-the-development-of-the-nasa-x-57-maxwell\/\" target=&quot;_blank&quot;>\n\t\t\t\tWHIRL FLUTTER AND THE DEVELOPMENT OF THE NASA X-57 MAXWELL\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jennifer Heeg, Bret K. Stanford, Andrew Kreshock, Jinwei Shen, Christian B. Hoover, Roger Truax<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-056<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18877 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-whirl-flutte tag-floquet-theory tag-multiblade-coordinate-transformation tag-multibody-and-multidisciplinary-simulation tag-rotor-tower-coupling-instability tag-whirl-flutter-2 tag-wind-turbine-aeroelasticity category-2433 category-2456 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/aeroelastic-stability-analysis-of-wind-turbines-considering-the-instabilities-known-from-rotary-wing-dynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC STABILITY ANALYSIS OF WIND TURBINES CONSIDERING THE INSTABILITIES KNOWN FROM ROTARY WING DYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alireza Rezaeian<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference numer: IFASD-2019-057<\/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-18880 post type-post status-publish format-standard hentry category-aeroelastic-optimization category-1-ifasd-2019 tag-aeroelasticity tag-topology-optimization tag-uncertainty tag-wingbox category-2437 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/sizing-and-topology-design-of-an-aeroelastic-wingbox-under-uncertainty\/\" target=&quot;_blank&quot;>\n\t\t\t\tSIZING AND TOPOLOGY DESIGN OF AN AEROELASTIC WINGBOX UNDER 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>Bret K. Stanford, Satadru Roy<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-058<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18883 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-maneuver-and-gust-loads tag-fluid-structure-interaction tag-nonlinear-structure tag-pitching-moment-coefficient tag-static-aeroelasticity tag-static-loads category-2433 category-2449 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/nonlinear-high-fidelity-static-aeroelastic-effect-on-the-flexible-pitching-moment-aerodynamic-coefficient-for-a-transport-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR HIGH FIDELITY STATIC AEROELASTIC EFFECT ON THE FLEXIBLE PITCHING MOMENT AERODYNAMIC COEFFICIENT FOR A 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>Angelo A. Verri ,, Kelvin C. de Morais , Fl\u00e1vio Luiz S. Bussamra, Carlos E. S. Cesnik<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-059<\/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-18886 post type-post status-publish format-standard hentry category-aeroservoelasticity-1-ifasd-2019 category-1-ifasd-2019 tag-aeroservoelasticity tag-biodynamic-feedthrough tag-pilot-augmented-oscillations category-2438 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/coupling-of-aeroelastic-and-pilot-dynamics-via-biodynamic-feedthrough-in-pilot-augmented-oscillations\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOUPLING OF AEROELASTIC AND PILOT DYNAMICS VIA BIODYNAMIC-FEEDTHROUGH IN PILOT-AUGMENTED OSCILLATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Daniel Drewiacki, Flavio J. Silvestre, Antonio Bernardo Guimaraes Neto<\/b><\/p>\n<p>DOI number: N\/A<\/p>\n<p>Conference number: IFASD-2019-061<\/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-18889 post type-post status-publish format-standard hentry category-aeroelastic-optimization category-1-ifasd-2019 tag-computational-uid-dynamics tag-doublet-lattice-method tag-flutter tag-manifold-mapping tag-metamodeling tag-multidelity-methods category-2437 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/multifidelity-flutter-prediction-using-local-corrections-to-the-generalized-aic\/\" target=&quot;_blank&quot;>\n\t\t\t\tMULTIFIDELITY FLUTTER PREDICTION USING LOCAL CORRECTIONS TO THE GENERALIZED AIC\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, Leifur Leifsson, Philip Beran<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-062<\/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-18892 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-whirl-flutte tag-aeroservoelasticity tag-gust-load-alleviation tag-h-controller-synthesis tag-loewner-framework tag-reduced-order-model-2 tag-tangential-interpolation category-2433 category-2456 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/parametric-study-and-mitigation-methods-for-whirl-flutter-after-occurrence-on-an-electric-propeller-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tPARAMETRIC STUDY AND MITIGATION METHODS FOR WHIRL FLUTTER AFTER OCCURRENCE ON AN ELECTRIC PROPELLER 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>Kyle J. Nelson, Christian B. Hoover, Jinwei Shen<\/b><\/p>\n<p>DOI NUmber: N\/A<\/p>\n<p>Conference number: IFASD-2019-063<\/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-18895 post type-post status-publish format-standard hentry category-aeroelastic-optimization category-1-ifasd-2019 tag-aeroservoelasticity tag-gust-load-alleviation tag-h-controller-synthesis tag-loewner-framework tag-reduced-order-model-2 tag-tangential-interpolation category-2437 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/a-state-space-model-for-loads-analysis-based-on-tangential-interpolation\/\" target=&quot;_blank&quot;>\n\t\t\t\tA STATE-SPACE MODEL FOR LOADS ANALYSIS BASED ON TANGENTIAL INTERPOLATION\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, Pierre Vuillemin, Charles Poussot-Vassal<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-066<\/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-18898 post type-post status-publish format-standard hentry category-dynamic-loads-1-ifasd-2019 category-1-ifasd-2019 tag-cfd tag-gust-load-alleviation tag-large-aircraft tag-lfd category-2442 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/investigation-into-gust-load-alleviation-using-computational-fluid-dynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATION INTO GUST LOAD ALLEVIATION USING COMPUTATIONAL FLUID DYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Philipp Bekemeyer, Reik Thormann, Sebastian Timme<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-068<\/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-18901 post type-post status-publish format-standard hentry category-aeroelastic-optimization category-1-ifasd-2019 tag-algorithmic-differentiation tag-blended-wing-body tag-finite-element-method tag-multidisciplinary-design-optimization category-2437 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/including-geometrically-nonlinear-flutter-constraints-in-high-fidelity-aircraft-optimization\/\" target=&quot;_blank&quot;>\n\t\t\t\tINCLUDING GEOMETRICALLY NONLINEAR FLUTTER CONSTRAINTS IN HIGH FIDELITY AIRCRAFT OPTIMIZATION\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 A. Lupp, Carlos E.S. Cesnik, Philip Beran, Joshua Deaton, David Easterling<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-069<\/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-18904 post type-post status-publish format-standard hentry category-flight-testing category-1-ifasd-2019 category-wind-tunnel-testing tag-flutter-stability tag-output-only-modal-analysis tag-real-time-aeroelastic-identification tag-wind-tunnel-testing category-2446 category-2433 category-2457 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/13\/online-monitoring-of-flutter-stability-during-wind-tunnel-testing-of-an-elastic-wing-with-pylon-and-engine-nacelle-within-the-hmae1-project\/\" target=&quot;_blank&quot;>\n\t\t\t\tONLINE MONITORING OF FLUTTER STABILITY DURING WIND TUNNEL TESTING OF AN ELASTIC WING WITH PYLON AND ENGINE NACELLE WITHIN THE HMAE1 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>M. B\u00f6swald, Y. Govers, G. Jelicic, R. Buchbach<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-070<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18908 post type-post status-publish format-standard hentry category-experimental-active-control category-1-ifasd-2019 tag-active-aeroelastic-control tag-utter-suppression tag-morphing tag-piezoceramic-patches tag-receptance-method category-2443 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/high-bandwidth-morphing-actuator-for-experimental-aeroelastic-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tHIGH BANDWIDTH MORPHING ACTUATOR FOR EXPERIMENTAL 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>Irma Isnardi, Sebastiano Fichera<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-071<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18911 post type-post status-publish format-standard hentry category-computational-flutter category-1-ifasd-2019 tag-block-newton tag-flutter tag-invariant-pairs-theory tag-nlevp category-2440 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/a-new-flutter-prediction-algorithm-to-avoid-p-k-method-shortcomings\/\" target=&quot;_blank&quot;>\n\t\t\t\tA NEW FLUTTER PREDICTION ALGORITHM TO AVOID P-K METHOD SHORTCOMINGS\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 Colo, Gabriel Broux, Eric Garrigues<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-072<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18914 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-modeling-for-design-of-highly-flexible-aircraft tag-high-altitude-pseudo-satellite-haps tag-highly-exible-aircraft tag-multibody-dynamics category-2433 category-2450 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/flight-mechanical-design-flight-dynamics-and-flight-control-for-multibody-aircraft-a-summary\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT MECHANICAL DESIGN, FLIGHT DYNAMICS, AND FLIGHT CONTROL FOR MULTIBODY AIRCRAFT: A SUMMARY\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 Kothe<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-074<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18917 post type-post status-publish format-standard hentry category-computational-flutter category-1-ifasd-2019 tag-aerodynamic-engine-effects tag-common-research-model tag-linearized-boundary-conditions tag-linearized-cfd tag-small-disturbance-cfd-2 category-2440 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/small-disturbance-cfd-based-aircraft-flutter-investigation-including-powered-engine-model\/\" target=&quot;_blank&quot;>\n\t\t\t\tSMALL-DISTURBANCE-CFD-BASED AIRCRAFT FLUTTER INVESTIGATION INCLUDING POWERED ENGINE 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>Vladyslav Rozov, Marco Stuhlpfarrer, Mario Fernandez Osma, Christian Breitsamter<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-075<\/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-18920 post type-post status-publish format-standard hentry category-flight-testing category-1-ifasd-2019 tag-aeroelastic tag-albatrossone tag-flight-testing tag-flutter tag-flying-demonstrator tag-gusts tag-hinged-folding-wing-tips tag-load-alleviation tag-manoeuvres tag-semi-aeroelastic-hinge category-2446 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/small-scale-flying-demonstration-of-semi-aeroelastic-hinged-wing-tips\/\" target=&quot;_blank&quot;>\n\t\t\t\tSMALL SCALE FLYING DEMONSTRATION OF SEMI AEROELASTIC 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>Thomas Wilson, James Kirk, John Hobday, Andrea Castrichini<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-076<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18923 post type-post status-publish format-standard hentry category-experimental-active-control category-1-ifasd-2019 tag-aeroservoelasticity tag-composite-optimization tag-wind-tunnel-testing category-2443 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/design-and-optimization-of-an-aeroservoelastic-wind-tunnel-model\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN AND OPTIMIZATION OF AN AEROSERVOELASTIC 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>Johannes K.S. Dillinger, Yasser M. Meddaikar, Jannis L\u00fcbker , Manuel Pusch, Thiemo Kier<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-078<\/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-18926 post type-post status-publish format-standard hentry category-experimental-active-control category-1-ifasd-2019 tag-aeroelastic tag-attenuation tag-experimental-validation tag-robust-control tag-slender-wing category-2443 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/experimental-and-numerical-implementation-of-robust-control-for-attenuation-of-buffet-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL AND NUMERICAL IMPLEMENTATION OF ROBUST CONTROL FOR ATTENUATION OF BUFFET 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>Sheharyar Malik, Sergio Ricci, Luca Riccobene, Daniele Monti<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-079<\/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-18929 post type-post status-publish format-standard hentry category-aeroelastic-optimization category-1-ifasd-2019 tag-aerodynamic-characterisation tag-aeroelasticity tag-control-surfaces tag-gust-loads tag-structural-sizing category-2437 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/transonic-flight-and-movable-load-modelling-for-wing-box-preliminary-sizing\/\" target=&quot;_blank&quot;>\n\t\t\t\tTRANSONIC FLIGHT AND MOVABLE LOAD MODELLING FOR WING-BOX PRELIMINARY SIZING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Paul Lancelot, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number:  IFASD-2019-080<\/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-18932 post type-post status-publish format-standard hentry category-flight-testing category-1-ifasd-2019 tag-aeroelasticity tag-ight-test tag-utter tag-operational-modal-analysis tag-robust-utter-analysis tag-structural-dynamics category-2446 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/operational-modal-analysis-for-simulated-flight-flutter-test-of-an-unconventional-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tOPERATIONAL MODAL ANALYSIS FOR SIMULATED FLIGHT FLUTTER TEST OF AN UNCONVENTIONAL 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>Ozge Suelozgen, Matthias Wustenhagen<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-081<\/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-18935 post type-post status-publish format-standard hentry category-computational-flutter category-1-ifasd-2019 tag-computational-aeroelasticity tag-utter-prediction tag-high-aspect-ratio-exible-wing category-2440 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/influence-on-the-flutter-behavior-of-pre-stressed-wing-structures-under-aerodynamic-loading\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE ON THE FLUTTER BEHAVIOR OF PRE-STRESSED WING STRUCTURES UNDER AERODYNAMIC 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>Andreas Hermanutz, Mirko Hornung<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-082<\/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-18938 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-modeling-for-design-of-highly-flexible-aircraft tag-flight-test tag-multi-body-aircraft tag-stability tag-trim category-2433 category-2450 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/flight-mechanical-analysis-and-test-of-unmanned-multi-body-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT MECHANICAL ANALYSIS AND TEST OF UNMANNED MULTI-BODY 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>An Chao, Xie Changchuan, Meng Yang, Yang Chao<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-083<\/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-18940 post type-post status-publish format-standard hentry category-computational-flutter category-1-ifasd-2019 tag-damping-modeling tag-passive-utter-suppression tag-viscoelastic-materials category-2440 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/structural-damping-models-for-passive-aeroelastic-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTRUCTURAL DAMPING MODELS FOR PASSIVE 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>Marco Eugeni, Francesco Saltari, Franco Mastroddi, Cristina Riso<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-085<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18944 post type-post status-publish format-standard hentry category-flight-testing category-1-ifasd-2019 tag-control-surface tag-flap tag-flutter tag-gust-load-alleviation tag-nlr7301 tag-shock-dynamics tag-supercritical-airfoil tag-wind-tunnel category-2446 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/control-surface-dynamics-at-transonic-airspeeds\/\" target=&quot;_blank&quot;>\n\t\t\t\tCONTROL SURFACE DYNAMICS AT TRANSONIC AIRSPEEDS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Holger Mai, Jens Nitzsche, Kenichi Saitoh, Norio Yoshimoto<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-086<\/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-18947 post type-post status-publish format-standard hentry category-aeroelastic-optimization category-1-ifasd-2019 tag-aerodynamics tag-aeroelasticity tag-aircraft-design tag-full-potential tag-transonic-ow category-2437 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/a-full-potential-static-aeroelastic-solver-for-preliminary-aircraft-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tA FULL POTENTIAL STATIC AEROELASTIC SOLVER FOR PRELIMINARY AIRCRAFT 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>Adrien Crovato, Romain Boman, Huseyin Guner, Vincent E. Terrapon, Grigorios Dimitriadis, Hugo S. Almeida, Alex P. Prado, Carlos Breviglieri, Pedro H. Cabral, Gustavo H. Silva<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-087<\/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-18950 post type-post status-publish format-standard hentry category-experimental-active-control category-1-ifasd-2019 tag-aeroelastic-model tag-load-control tag-wind-tunnel-testing category-2443 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/design-and-wind-tunnel-test-of-an-actively-controlled-flexible-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN AND WIND TUNNEL TEST OF AN ACTIVELY CONTROLLED 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>Wolf R. Kr\u00fcger, Johannes K.S. Dillinger, Yasser M. Meddaikar, Jannis L\u00fcbker, Martin Tang, Tobias Meier, Marc B\u00f6swald, Keith Soal, Manuel Pusch, Thiemo Kier<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-088<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18953 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-modeling-for-design-of-highly-flexible-aircraft tag-computational-aeroelasticity tag-flight-dynamics tag-gust-re-sponse tag-lateral-gust tag-nonlinear-aeroelasticity tag-very-flexible-aircraft category-2433 category-2450 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/nonlinear-response-of-a-very-flexible-aircraft-under-lateral-gust\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR RESPONSE OF A VERY FLEXIBLE AIRCRAFT UNDER LATERAL GUST\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alfonso del Carre, Patricia Teixeira, Rafael Palacios, Carlos E.S. Cesnik<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-090<\/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-18956 post type-post status-publish format-standard hentry category-computational-aeroelasticity-1-ifasd-2019 category-1-ifasd-2019 tag-aeroelasticity tag-aircraft tag-multi-fidelity-analysis tag-structural-analysis category-2439 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/geometrically-nonlinear-aeroelastic-analysis-with-unsteady-vortex-lattice-method-and-cfd\/\" target=&quot;_blank&quot;>\n\t\t\t\tGEOMETRICALLY NONLINEAR AEROELASTIC ANALYSIS WITH UNSTEADY VORTEX-LATTICE METHOD AND 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>Natsuki Tsushima, Hitoshi Arizono, Masato Tamayama, Tomohiro Yokozeki, Weihua Su<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-091<\/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-18959 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-aeroelasticity tag-reduced-order-modeling-2 tag-sloshing category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/aircraft-fuel-sloshing-roms-for-aeroelastic-analyses\/\" target=&quot;_blank&quot;>\n\t\t\t\tAIRCRAFT-FUEL SLOSHING ROMS FOR AEROELASTIC ANALYSES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Franco Mastroddi, Francesco Saltari, Michael Wright, Arnaud G. Malan, Simone Simeone, Francesco Gambioli<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-092<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18962 post type-post status-publish format-standard hentry category-experimental-methods-in-aeroelasticity category-1-ifasd-2019 category-maneuver-and-gust-loads tag-dynamic-gust-loads tag-forward-swept-wing tag-gust-generator category-2444 category-2433 category-2449 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/investigation-of-gust-loads-on-a-flexible-forward-swept-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATION OF GUST LOADS ON A FLEXIBLE FORWARD 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>Vega Handojo, Yasser M. Meddaikar, Johannes K.S. Dillinger, Jurij Sodja, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-093<\/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-18965 post type-post status-publish format-standard hentry category-experimental-methods-in-aeroelasticity category-1-ifasd-2019 tag-high-aspect-ratio-wings tag-nonlinear-aeroelasticity tag-wind-tunnel-testing category-2444 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/wind-tunnel-testing-of-a-high-aspect-ratio-wing-model\/\" target=&quot;_blank&quot;>\n\t\t\t\tWind Tunnel Testing of a High Aspect Ratio Wing 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>J.E. Cooper R.G. Cook G. Francois, O. de la Torre, S.A. Neild, M.H. Lowenberg S.S. Alexander, E.B. Coetzee, M. Evans<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-094<\/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-18968 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-balanced-truncation tag-local-bases tag-model-order-reduction tag-piecewise-linear-model tag-very-exible-aircraft category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/model-order-reduction-for-coupled-nonlinear-aeroelastic-flight-mechanics-of-very-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODEL ORDER REDUCTION FOR COUPLED NONLINEAR AEROELASTIC-FLIGHT MECHANICS OF VERY 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>Manuel Lanchares, Ilya Kolmanovsky, Carlos E.S. Cesnik, Fabio Vetrano<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-095<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18971 post type-post status-publish format-standard hentry category-aeroelastic-design-applications category-1-ifasd-2019 tag-active-winglet tag-cfd-csm-2 tag-multidisciplinary-optimization-2 tag-static-aeroelasticity tag-surrogate-models category-2435 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/surrogate-based-optimization-of-a-morphing-winglet-for-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tSURROGATE BASED OPTIMIZATION OF A MORPHING WINGLET FOR 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>Martin Delavenne, Bernard Barriety, Fabio Vetrano, Valerie Ferrand, Michel Salaun<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-098<\/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-18974 post type-post status-publish format-standard hentry category-aeroelastic-design-applications category-1-ifasd-2019 tag-embedded-strain-gage tag-exible-aircraft tag-thermal-correction category-2435 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/thermal-correction-of-strain-gage-measurements-on-flexible-x-hale-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHERMAL CORRECTION OF STRAIN GAGE MEASUREMENTS ON FLEXIBLE X-HALE 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>Jessica S. Martins, Flavio L. S. Bussamra, Juliano A. Paulino, Antonio B. Guimaraes Neto<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-099<\/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-18977 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-modeling-for-design-of-highly-flexible-aircraft tag-aeroelasticity tag-flutter tag-reduced-order-model-3 category-2433 category-2450 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/a-high-efficiency-nonlinear-flutter-analysis-method-in-timedomain-for-large-aspect-ratio-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tA high efficiency nonlinear flutter analysis method in timedomain for large 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<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-100<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18980 post type-post status-publish format-standard hentry category-computational-aeroelasticity-1-ifasd-2019 category-1-ifasd-2019 tag-aeroelasticity tag-flutter tag-reduced-order-model-3 category-2439 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/flutter-analysis-at-variable-mach-and-angle-of-attack-utilizing-reduced-order-models\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER ANALYSIS AT VARIABLE MACH AND ANGLE OF ATTACK UTILIZING REDUCED-ORDER-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>Christopher S. Talley, Timothy J. Wray, Yi Wang, Sami D. Habchi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-101<\/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-18983 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-aeroelasticity tag-aeroservoelastic tag-cfd tag-state-space-2 tag-subspace-realization tag-system-identification category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/discrete-time-state-space-aeroservoelastic-modeling-using-fun3d\/\" target=&quot;_blank&quot;>\n\t\t\t\tDISCRETE TIME STATE-SPACE AEROSERVOELASTIC MODELING USING FUN3D\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Z. Wang , D. Sarhaddi , P.C. Chen<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-102<\/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-18986 post type-post status-publish format-standard hentry category-dynamic-loads-1-ifasd-2019 category-1-ifasd-2019 tag-ditching-loads tag-dynamic-loads tag-structural-dynamics category-2442 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/ditching-loads-numerical-and-experimental-alternatives\/\" target=&quot;_blank&quot;>\n\t\t\t\tDITCHING LOADS NUMERICAL AND EXPERIMENTAL ALTERNATIVES\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, F. Ar\u00e9valo, J.T. Viana, E. P\u00e9rez Heredia<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-103<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18990 post type-post status-publish format-standard hentry category-experimental-methods-in-aeroelasticity category-1-ifasd-2019 tag-aeroelasticity tag-structural-dynamics tag-wind-tunnel-testing category-2444 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/development-building-and-testing-of-a-low-cost-aeroelastic-wind-tunnel-model-for-educational-purposes\/\" target=&quot;_blank&quot;>\n\t\t\t\tDEVELOPMENT, BUILDING AND TESTING OF A LOW-COST AEROELASTIC WIND TUNNEL MODEL FOR EDUCATIONAL PURPOSES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Marcello Righi, Flavio Campanile<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-104<\/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-18992 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-aeroelastic-model-reduction tag-computational-fluid-dynamics tag-large-transport-aircraft tag-synthetic-modes category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/aeroelastic-loads-predictions-using-cfd-based-reduced-order-models\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC LOADS PREDICTIONS USING CFD-BASED REDUCED ORDER 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>Philipp Bekemeyer, Tobias Wunderlich, Stefan Gortz, Sascha Dahne<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-105<\/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-18996 post type-post status-publish format-standard hentry category-computational-aeroelasticity-1-ifasd-2019 category-1-ifasd-2019 tag-2952 tag-741-theodore-theodorsen-i-e-garrick tag-flutter-naca-reports-496 category-2439 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/theodorsens-and-garricks-computational-aeroelasticity-revisited\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHEODORSEN\u2019S AND GARRICK\u2019S COMPUTATIONAL AEROELASTICITY, REVISITED\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Boyd Perry, III<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-106<\/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-18999 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-modeling-for-design-of-highly-flexible-aircraft tag-aeroelasticity tag-exible-aircraft tag-ight-dynamics tag-ground-effect tag-takeoff category-2433 category-2450 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/takeoff-dynamics-of-flexible-aircraft-with-multiple-underwing-pod-mounted-landing-gears\/\" target=&quot;_blank&quot;>\n\t\t\t\tTAKEOFF DYNAMICS OF FLEXIBLE AIRCRAFT WITH MULTIPLE UNDERWING POD-MOUNTED LANDING GEARS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Antonio B. Guimaraes Neto<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-107<\/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-19002 post type-post status-publish format-standard hentry category-ground-vibration-testing category-1-ifasd-2019 tag-fixed-base-correction tag-flexible-wing tag-frequency-response-function tag-ground-vibration-test tag-modal-test tag-structural-dynamics category-2447 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/modal-testing-of-a-flexible-wing-on-a-dynamically-active-test-fixture-using-the-fixed-base-correction-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODAL TESTING OF A FLEXIBLE WING ON A DYNAMICALLY ACTIVE TEST FIXTURE USING THE FIXED BASE CORRECTION 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>Natalie Spivey, Kia Miller, Rachel Saltzman, Kevin Napolitano<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-108<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19005 post type-post status-publish format-standard hentry category-control-of-very-flexible-aircraft category-1-ifasd-2019 tag-control-allocation tag-exible-aircraft tag-maneuver-load-alleviation category-2441 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/maneuver-load-alleviation-of-flexible-aircraft-through-control-allocation-a-case-study-using-x-hale\/\" target=&quot;_blank&quot;>\n\t\t\t\tMANEUVER LOAD ALLEVIATION OF FLEXIBLE AIRCRAFT THROUGH CONTROL ALLOCATION: A CASE STUDY USING X-HALE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Molong Duan, John H. Hansen, Ilya V. Kolmanovsky, Carlos E. S. Cesnik<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-109<\/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-19008 post type-post status-publish format-standard hentry category-aeroelastic-analysis-frameworks category-1-ifasd-2019 tag-cfd tag-fem tag-fluid-structure-interaction tag-highly-flexible-aircraft tag-morphing tag-nonlinear-panel-flutter category-2434 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/14\/a-new-open-fluid-structure-interface-for-steady-and-unsteady-nonlinear-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tA NEW OPEN FLUID-STRUCTURE INTERFACE FOR STEADY AND UNSTEADY NONLINEAR 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>F. G. Di Vincenzo<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-110<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19012 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-laminar-flow tag-cryogenic-wind-tunnel tag-flutter tag-laminar-airfoil tag-laminar-turbulent-transition tag-nlf-0415 tag-unsteady-aerodynamics category-2433 category-2455 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/high-reynolds-number-testing-of-a-laminar-airfoil-under-forced-harmonic-pitching-oscillations-at-cryogenic-conditions\/\" target=&quot;_blank&quot;>\n\t\t\t\tHIGH REYNOLDS NUMBER TESTING OF A LAMINAR AIRFOIL UNDER FORCED HARMONIC PITCHING OSCILLATIONS AT CRYOGENIC 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>Holger Mai, Anne Hebler, Stefan Koch<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-112<\/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-19015 post type-post status-publish format-standard hentry category-aeroelastic-analysis-frameworks category-ground-vibration-testing category-1-ifasd-2019 tag-ground-vibration-testing tag-structural-dynamics category-2434 category-2447 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/dgt-a-new-methodology-for-highspeed-aircraft-ground-vibration-tests\/\" target=&quot;_blank&quot;>\n\t\t\t\tDGT: A NEW METHODOLOGY FOR HIGHSPEED AIRCRAFT GROUND VIBRATION TESTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Guillaume Osmond, Fabien Ayme, Nicolas Lastere<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-114<\/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-19018 post type-post status-publish format-standard hentry category-aeroelastic-analysis-frameworks category-1-ifasd-2019 tag-non-linear-aerodynamics tag-rapid-method tag-static-aeroelasticity tag-transonic category-2434 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/fast-fluid-structure-computational-method-taking-into-account-non-linear-aerodynamic\/\" target=&quot;_blank&quot;>\n\t\t\t\tFAST FLUID-STRUCTURE COMPUTATIONAL METHOD TAKING INTO ACCOUNT NON-LINEAR AERODYNAMIC\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>B.Barriety, J-P. Boin , O. Chandre-Vila, T.Mauermann<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-115<\/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-19021 post type-post status-publish format-standard hentry category-dynamic-loads-1-ifasd-2019 category-1-ifasd-2019 tag-direct-transient-response tag-dynamic-landing-loads tag-finite-element-analysis tag-multibody-simulation category-2442 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/a-hybrid-approach-for-the-analysis-of-aircraft-ground-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tA HYBRID APPROACH FOR THE ANALYSIS OF AIRCRAFT GROUND 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>Wolf R. Kr\u00fcger, Sunpeth Cumnuantip<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-117<\/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-19024 post type-post status-publish format-standard hentry category-aeroelastic-analysis-frameworks category-1-ifasd-2019 tag-aeroelasticity tag-aeroservoelasticity tag-loads category-2434 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/unified-framework-for-aeroservoelastic-response-and-stability-analysis-design-and-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tUNIFIED FRAMEWORK FOR AEROSERVOELASTIC RESPONSE AND STABILITY ANALYSIS, DESIGN AND 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>Moti Karpel<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-118<\/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-19027 post type-post status-publish format-standard hentry category-ground-vibration-testing category-1-ifasd-2019 tag-controller-area-network-can-bus tag-ground-vibration-test-gvt tag-microelectromechanical-systems-mems-sensors category-2447 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/an-abstract-ground-vibration-test-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN ABSTRACT GROUND VIBRATION TEST 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>Louw H. van Zyl, Becker van Niekerk<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-119<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19030 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-laminar-flow tag-crossflow-instability tag-laminar-turbulent-aeroelasticity-transition tag-wind-tunnel-tests category-2433 category-2455 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/experimental-investigation-of-the-laminar-turbulent-transition-and-crossflow-instability-of-an-oscillating-airfoil-in-low-speed-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL INVESTIGATION OF THE LAMINAR \u2013 TURBULENT TRANSITION AND CROSSFLOW INSTABILITY OF AN OSCILLATING AIRFOIL IN LOW SPEED 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>A. Lepage, Y. Amosse, J.P. Brazier, M. Forte, O. Vermeersch, C. Liauzun<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-120<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19033 post type-post status-publish format-standard hentry category-dynamic-loads-1-ifasd-2019 category-1-ifasd-2019 tag-aeroelasticity tag-dynamic-loads tag-ifasd tag-store-ejection tag-structural-dynamics category-2442 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/dynamic-response-of-an-elastic-aircraft-to-ripple-store-ejection\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC RESPONSE OF AN ELASTIC AIRCRAFT TO RIPPLE STORE EJECTION\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 Kariv, Daniella E. Raveh<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-121<\/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-19036 post type-post status-publish format-standard hentry category-dynamic-loads-1-ifasd-2019 category-1-ifasd-2019 tag-dynamic-loads tag-statistical-analysis tag-structural-dynamics tag-taxi-loads category-2442 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/statistical-analysis-of-dynamic-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTATISTICAL ANALYSIS OF 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>Jose L. P\u00e9rez, Alvaro Esteban, Guillermo Pastor, Hector Climent<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-123<\/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-19039 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-laminar-flow tag-airfoil-utter tag-transition-modeling tag-unsteady-aerodynamics tag-unsteady-boundary-layer-transition category-2433 category-2455 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/numerical-investigation-of-unsteady-transitional-boundary-layer-flows\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL INVESTIGATION OF UNSTEADY TRANSITIONAL BOUNDARY LAYER FLOWS\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, Sebastian Helm, Christoph Kaiser<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-124<\/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-19042 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-laminar-flow tag-aeroelasticity tag-cfd tag-laminar-wing tag-transition-modelling category-2433 category-2455 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/assessment-of-cfd-methods-taking-into-account-laminar-turbulent-transition-for-aeroelasticity-of-laminar-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tASSESSMENT OF CFD METHODS TAKING INTO ACCOUNT LAMINAR-TURBULENT TRANSITION FOR AEROELASTICITY 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>C\u00e9dric Liauzun, Guy Daniel Mortch\u00e9l\u00e9wicz, Arnaud Lepage<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-125<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19045 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-modeling-for-design-of-highly-flexible-aircraft tag-aeroelasticity tag-modied-strip-theory tag-nonlinear-fem tag-total-lagrangian category-2433 category-2450 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/a-geometrically-nonlinear-finite-element-model-for-aeroelastic-analysis-of-plate-like-wing-aerostructures\/\" target=&quot;_blank&quot;>\n\t\t\t\tA GEOMETRICALLY NONLINEAR FINITE ELEMENT MODEL FOR AEROELASTIC ANALYSIS OF PLATE-LIKE WING AEROSTRUCTURES\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 C. Silva, Mauricio V. Donadon, Flavio J. Silvestre<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-127<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19048 post type-post status-publish format-standard hentry category-dynamic-loads-1-ifasd-2019 category-1-ifasd-2019 tag-folding-wing-tip tag-loads-alleviation tag-sah tag-semi-aeroelastic-hinge category-2442 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/aeroelastics-flight-dynamics-coupling-effects-of-the-semi-aeroelastic-hinge-device\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTICS FLIGHT DYNAMICS COUPLING EFFECTS OF 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>A. Castrichini, F. Saltari, N. Viceconti, T. Wilson, J.E. Cooper, F. Mastroddi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-128<\/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-19051 post type-post status-publish format-standard hentry category-dynamic-loads-1-ifasd-2019 category-1-ifasd-2019 tag-light-loads-analysis tag-load-conditions tag-tail-plane category-2442 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/an-integrated-analysis-model-for-assessment-of-critical-load-conditions-for-the-vertical-tail-plane\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN INTEGRATED ANALYSIS MODEL FOR ASSESSMENT OF CRITICAL LOAD CONDITIONS FOR THE VERTICAL TAIL PLANE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Thiemo M. Kier, Reiko Muller, Gertjan Looye<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-129<\/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-19054 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-aeroelastic-tailoring tag-composite-materials tag-high-aspect-ratio-wing tag-wind-tunnel-test category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/numerical-and-experimental-study-of-aeroelastic-tailoring-effect-using-flexible-composite-laminates-for-haps-application\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL AND EXPERIMENTAL STUDY OF AEROELASTIC TAILORING EFFECT USING FLEXIBLE COMPOSITE LAMINATES FOR HAPS 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>B. Kirsch, O. Montagnier, T.M. Faure, E. Benard<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-131<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19057 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-laminar-flow tag-boundary-layer-transition tag-laminar-airfoil tag-limit-cycle-oscillation-2 tag-shock-motion tag-transonic-dip category-2433 category-2455 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/mechanisms-of-transonic-single-degree-of-freedom-flutter-of-a-laminar-airfoil\/\" target=&quot;_blank&quot;>\n\t\t\t\tMECHANISMS OF TRANSONIC SINGLE DEGREE OF FREEDOM FLUTTER OF A LAMINAR 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>Marc Braune, Anne Hebler<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-132<\/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-19060 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-unsteady-laminar-flow tag-hysteresis tag-laminar-airfoil tag-limit-cycle-oscillation-2 tag-nonlinear-system-response tag-subcritical-bifurcation tag-transonic-flow-2 category-2433 category-2455 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/hysteretic-response-of-a-laminar-airfoil-undergoing-single-degree-of-freedom-limit-cycle-oscillations-in-transonic-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tHYSTERETIC RESPONSE OF A LAMINAR AIRFOIL UNDERGOING SINGLE DEGREE OF FREEDOM LIMIT CYCLE OSCILLATIONS IN TRANSONIC 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>Marc Braune, Anne Hebler<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p> Conference number: IFASD-2019-133<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19063 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-reduced-order-models tag-discrete-empirical-interpolation-method tag-proper-orthogonal-decomposition tag-reduced-order-models tag-time-spectral-method category-2433 category-2452 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/reduced-order-time-spectral-model-for-the-ale-formulation-of-the-compressible-navier-stokes-equations\/\" target=&quot;_blank&quot;>\n\t\t\t\tREDUCED ORDER TIME SPECTRAL MODEL FOR THE ALE FORMULATION OF THE COMPRESSIBLE NAVIER-STOKES EQUATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Fabrizio Di Donfrancesco, Antoine Placzek, Christophe Blondeau, Jean-Camille Chassaing<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-134<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19066 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-modeling-for-design-of-highly-flexible-aircraft tag-geometric-structural-nonlinearities tag-ifasd tag-large-deformations tag-modal-analysis-2 category-2433 category-2450 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/modal-rotations-a-modal-based-method-for-large-structural-deformations\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODAL ROTATIONS: A MODAL-BASED METHOD FOR LARGE STRUCTURAL DEFORMATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ariel Drachinsky, Daniella E. Raveh<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-135<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19068 post type-post status-publish format-standard hentry category-dynamic-loads-1-ifasd-2019 category-1-ifasd-2019 tag-cfd tag-tail-buffeting tag-turbulence-modeling tag-vortical-flows category-2442 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/prediction-of-horizontal-tail-buffeting-loads-based-on-urans-and-des-approaches\/\" target=&quot;_blank&quot;>\n\t\t\t\tPREDICTION OF HORIZONTAL TAIL BUFFETING LOADS BASED ON URANS AND DES APPROACHES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Lukas Katzenmeier, Cyrille Vidy, Luca Benassi, Christian Breitsamter<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-136<\/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-19072 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-limit-cycle-oscillation tag-euler-analysis tag-harmonic-balance-method tag-lco tag-super-sonic-transport tag-transonic-speed category-2433 category-2448 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/numerical-analysis-of-limit-cycle-oscillation-of-a-supersonic-transport-wind-tunnel-test-model\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL ANALYSIS OF LIMIT CYCLE OSCILLATION OF A SUPERSONIC TRANSPORT WIND TUNNEL TEST 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>Kenichi SAITOH, Hamidreza KHEIRANDISH, Norio YOSHIMOTO<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-137<\/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-19075 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-panel-flutter tag-aeroelasticity tag-hypersonic tag-panel-utter tag-piston-theory tag-structural-dynamics category-2433 category-2451 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/computational-study-for-the-design-of-a-hypersonic-panel-flutter-experiment\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPUTATIONAL STUDY FOR THE DESIGN OF A HYPERSONIC PANEL FLUTTER 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>Maxim Freydin, Earl H. Dowell, Gaetano M.D. Currao, Andrew J. Neely<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-138<\/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-19078 post type-post status-publish format-standard hentry category-experimental-methods-in-structural-dynamics category-1-ifasd-2019 tag-damping tag-experiment tag-fluid-structure-interaction tag-identification tag-sloshing category-2445 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/analysis-of-a-sloshing-beam-experiment\/\" target=&quot;_blank&quot;>\n\t\t\t\tANALYSIS OF A SLOSHING BEAM 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>Branislav Titurus, Jonathan E. Cooper, Francesco Saltari, Franco Mastroddi, Francesco Gambioli<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-139<\/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-19081 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-wind-tunnel-testing tag-aeroelasticity tag-utter tag-transonic tag-wind-tunnel category-2433 category-2457 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/wing-design-for-wind-tunnel-flutter-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tWING DESIGN FOR WIND TUNNEL FLUTTER 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>Ulf Ringertz<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-140<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19084 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-wind-tunnel-testing tag-flutter-stability tag-highly-flexible-wing tag-wind-tunnel-testing category-2433 category-2457 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/wind-tunnel-flutter-testing-on-a-highly-flexible-wing-for-aeroelastic-validation-in-the-transonic-regime-within-the-hmae1-project\/\" target=&quot;_blank&quot;>\n\t\t\t\tWIND TUNNEL FLUTTER TESTING ON A HIGHLY FLEXIBLE WING FOR AEROELASTIC VALIDATION IN THE TRANSONIC REGIME WITHIN THE HMAE1 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>Yves Govers, Holger Mai, Juergen Arnold, Johannes K.S. Dillinger, Allan K.A. Pereira, Carlos Breviglieri Jr., Edgard K. Takara, Manoela S. Correa, Olympio A.F. Mello, Rodrigo F.A. Marques, Evert G.M. Geurts, Ralf J.C. Creemers, Huub S. Timmermans, Remco Habing,, Kees Kapteijn<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-141<\/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-19087 post type-post status-publish format-standard hentry category-experimental-methods-in-structural-dynamics category-1-ifasd-2019 tag-fluid-structure-interaction-2 tag-sloshing tag-structural-dynamics category-2445 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/experimental-evaluation-of-fuel-sloshing-effects-on-wing-dynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL EVALUATION OF FUEL SLOSHING EFFECTS ON WING DYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>F. Gambioli, R. Alegre Usach, J. Kirby, T. Wilson, P. Behruzi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-142<\/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-19089 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-panel-flutter tag-hypersonic-aerothermoelasticity tag-multi-objective-bayesian-optimization tag-numerical-scaling-laws category-2433 category-2451 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/a-multi-objective-optimization-framework-for-hypersonic-aerothermoelastic-scaling-laws-and-its-application-to-skin-panels\/\" target=&quot;_blank&quot;>\n\t\t\t\tA MULTI-OBJECTIVE OPTIMIZATION FRAMEWORK FOR HYPERSONIC AEROTHERMOELASTIC SCALING LAWS AND ITS APPLICATION TO SKIN 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>Daning Huang, Peretz P. Friedmann<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-143<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19093 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-limit-cycle-oscillation tag-aircraft-with-stores tag-limit-cycle-oscillation-lco tag-nonlinear-aerodynamic-and-nonlinear-structural-interaction tag-nonlinear-structural-damping tag-reduced-order-model-2 tag-truly-lco-predictive-tool-the-objectives-of-this-work-is-to-develop-a-truly-limit-cycle-oscillation-lco category-2433 category-2448 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/limit-cycle-oscillaton-prediction-for-aircraft-with-external-stores\/\" target=&quot;_blank&quot;>\n\t\t\t\tLIMIT CYCLE OSCILLATON PREDICTION FOR AIRCRAFT WITH EXTERNAL STORES\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.C. Chen, Z. Zhang, Z. Zhou, X.Q. Wang, M.P. Mignolet<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-144<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19096 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-limit-cycle-oscillation tag-forecasting tag-limit-cycle-oscillations tag-nonlinear-aeroelasticity category-2433 category-2448 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/model-free-forecasting-of-limit-cycle-oscillations-in-geometrically-nonlinear-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODEL-FREE FORECASTING OF LIMIT CYCLE OSCILLATIONS IN GEOMETRICALLY NONLINEAR 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>Cristina Riso, Amin Ghadami, Carlos E.S. Cesnik, Bogdan I. Epureanu<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-145<\/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-19099 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-whirl-flutte tag-local-piston-theory tag-panel-flutter tag-supersonic tag-surface-spline tag-weight-reduction category-2433 category-2456 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/an-engineering-analysis-for-panel-flutter-of-a-supersonic-inlet\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN ENGINEERING ANALYSIS FOR PANEL FLUTTER OF A SUPERSONIC INLET\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Chenyu Liu, Changchuan Xie, Yihan Yan, Yanjin Man, Mingfeng Zhang, Hui Yang<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-146<\/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-19102 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-wind-tunnel-testing tag-cfd tag-flutter tag-linearized-navier-stokes tag-transonic tag-unsteady tag-wind-tunnel category-2433 category-2457 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/linearized-navier-stokes-cfd-flutter-correlations-with-wind-tunnel-measurements-on-a-transonic-u-tail-flutter-mock-up\/\" target=&quot;_blank&quot;>\n\t\t\t\tLINEARIZED NAVIER-STOKES CFD FLUTTER CORRELATIONS WITH WIND TUNNEL MEASUREMENTS ON A TRANSONIC U-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>Hadrien Mamelle, Gabriel Broux, Nicolas Forestier, Zdenek Johan, Eric Garrigues<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-148<\/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-19105 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-wind-tunnel-testing tag-aeroelasticity tag-empennage tag-flutter tag-high-fidelity-simulations category-2433 category-2457 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/innovative-tail-configuration-numerical-vs-wind-tunnel-test-data\/\" target=&quot;_blank&quot;>\n\t\t\t\tINNOVATIVE TAIL CONFIGURATION: NUMERICAL VS WIND TUNNEL TEST 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>S. Dequand, A. Geeraert, G. Mortchelewicz<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-149<\/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-19107 post type-post status-publish format-standard hentry category-experimental-methods-in-structural-dynamics category-1-ifasd-2019 tag-buffet tag-flight-test tag-ground-vibration-test tag-landing-gear-doors tag-vibration-control category-2445 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/aerolastic-coupling-and-control-means-for-reduction-of-main-landing-gear-doors-responses-under-operational-conditions\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROLASTIC COUPLING AND CONTROL MEANS FOR REDUCTION OF MAIN LANDING GEAR DOORS RESPONSES UNDER OPERATIONAL 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>R. Abarca, C. Aquilini, P. Lubrina, S.\u2013H. Peng, J. Schwochow<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-150<\/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-19111 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-panel-flutter tag-aeroelasticity tag-divergence tag-utter tag-landing-gear tag-vortex-lattice-method category-2433 category-2451 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/influence-of-mixed-boundary-conditions-on-the-instability-of-plates-in-uniform-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF MIXED BOUNDARY CONDITIONS ON THE INSTABILITY OF PLATES IN UNIFORM 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>Benjamin K. Morris, Eetu A. Kohtanen, R. Benjamin Davis<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-151<\/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-19114 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-limit-cycle-oscillation tag-0-1-test tag-chaos tag-flutter tag-nonlinear-aeroelasticity tag-wind-tunnel category-2433 category-2448 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/17\/application-of-0-1-test-for-chaos-in-wind-tunnel-aeroelastic-experiments-of-an-aluminum-flat-plate\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF 0-1 TEST FOR CHAOS IN WIND TUNNEL AEROELASTIC EXPERIMENTS OF AN ALUMINUM 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>Michelle F. Westin, Roberto G. A. da Silva, Jos\u00e9 M. Balthazar<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-152<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19118 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-limit-cycle-oscillation tag-aeroelasticity tag-backlash tag-freeplay tag-ifasd tag-lco tag-nonlinear-models tag-structural-dynamics category-2433 category-2448 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/19\/investigation-on-the-effects-of-control-surface-freeplay-on-the-aeroelastic-characteristics-of-a-trainer-aircraft-and-extension-of-limits-in-support-of-maintenance-tasks\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATION ON THE EFFECTS OF CONTROL SURFACE FREEPLAY ON THE AEROELASTIC CHARACTERISTICS OF A TRAINER AIRCRAFT AND EXTENSION OF LIMITS IN SUPPORT OF MAINTENANCE TASKS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Michele Frumusa, Vincenzo Vaccaro<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-153<\/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-19121 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-panel-flutter tag-aeroelasticity tag-hypersonic-ow tag-panel-utter tag-periodic-structures category-2433 category-2451 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/19\/flutter-of-periodically-stiffened-plates-and-shells-in-hypersonic-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlutter of Periodically Stiffened Plates and Shells in Hypersonic 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>Gautam SenGupta<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-154<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19124 post type-post status-publish format-standard hentry category-experimental-methods-in-structural-dynamics category-1-ifasd-2019 tag-control-based-continuation tag-experimental-bifurcation tag-flutter tag-lco tag-limit-cycle-oscillation-2 category-2445 category-2433 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/19\/experimental-bifurcation-analysis-of-a-wing-profile\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL BIFURCATION ANALYSIS OF A WING PROFILE\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, David Barton, Djamel Rezgui, Simon Neild<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-155<\/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-19127 post type-post status-publish format-standard hentry category-1-ifasd-2019 category-wind-tunnel-testing tag-aeroelasticity tag-finite-element-modeling tag-structural-dynamics tag-windtunnel-testing category-2433 category-2457 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"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\/19\/design-and-validation-of-a-numerical-high-aspect-ratio-aeroelastic-wind-tunnel-model-hmae1\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN AND VALIDATION OF A NUMERICAL HIGH ASPECT RATIO AEROELASTIC WIND TUNNEL MODEL (HMAE1)\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.S. Timmermans, J.H. van Tongeren, E.G.M Geurts, R.F.A. Marques, M.S. Correa, S. Waitz<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-156<\/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<\/div>\n\t\t\t\t\t<span class=\"e-load-more-spinner\">\n\t\t\t\t<i aria-hidden=\"true\" class=\"fas fa-spinner\"><\/i>\t\t\t<\/span>\n\t\t\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-607c26a elementor-widget elementor-widget-spacer\" data-id=\"607c26a\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t<div class=\"elementor-column elementor-col-25 elementor-top-column elementor-element elementor-element-4b92472\" data-id=\"4b92472\" data-element_type=\"column\" data-e-type=\"column\" data-settings=\"{&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t<div class=\"elementor-widget-wrap\">\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t<section class=\"elementor-section elementor-top-section elementor-element elementor-element-5f254a1 elementor-section-stretched elementor-section-boxed elementor-section-height-default elementor-section-height-default\" data-id=\"5f254a1\" data-element_type=\"section\" data-e-type=\"section\" data-settings=\"{&quot;stretch_section&quot;:&quot;section-stretched&quot;,&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t\t\t\t<div class=\"elementor-container elementor-column-gap-default\">\n\t\t\t\t\t<div class=\"elementor-column elementor-col-100 elementor-top-column elementor-element elementor-element-ff101ec\" data-id=\"ff101ec\" data-element_type=\"column\" data-e-type=\"column\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-bbafcf0 elementor-widget elementor-widget-spacer\" data-id=\"bbafcf0\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-9389dce elementor-widget elementor-widget-spacer\" data-id=\"9389dce\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t<\/div>\n\t\t","protected":false},"excerpt":{"rendered":"<p>Search all IFASD 2019 papers Search &#8230; Results See all results Search by Event Topic IFASD2019 Aeroelastic Analysis Frameworks Aeroelastic Design Applications Aeroelastic Optimization Aeroelastic Optimization Frameworkes Aeroservoelasticity Computational Aeroelasticity Computational Flutter Control of Very Flexible Aircraft Dynamic Loads Experimental Active Control Experimental Methods in Aeroelasticity Experimental Methods in Structural Dynamics Flight Testing Ground Vibration&hellip;<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"footnotes":""},"class_list":["post-18254","page","type-page","status-publish","hentry","category-2433","category-2457","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/18254","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=18254"}],"version-history":[{"count":19,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/18254\/revisions"}],"predecessor-version":[{"id":19155,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/18254\/revisions\/19155"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18254"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}