{"id":11440,"date":"2023-07-19T15:14:53","date_gmt":"2023-07-19T15:14:53","guid":{"rendered":"https:\/\/aerospacerepository.org\/?page_id=11440"},"modified":"2026-09-10T12:12:42","modified_gmt":"2026-09-10T12:12:42","slug":"repository-aeronautics-fluid-dynamics","status":"publish","type":"page","link":"https:\/\/aerospacerepository.org\/index.php\/repository-aeronautics-fluid-dynamics\/","title":{"rendered":"Repository Aeronautics Fluid Dynamics"},"content":{"rendered":"\t\t<div data-elementor-type=\"wp-page\" data-elementor-id=\"11440\" class=\"elementor elementor-11440\" 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 Fluid Dynamics 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;:[3973],&quot;exclude_terms_ids&quot;:[],&quot;exclude_posts_ids&quot;:[],&quot;custom_fields_source&quot;:&quot;&quot;,&quot;limit_query&quot;:5,&quot;limit_query_tablet&quot;:&quot;&quot;,&quot;limit_query_mobile&quot;:&quot;&quot;,&quot;limit_query_in_result_area&quot;:25,&quot;results_order_by&quot;:&quot;relevance&quot;,&quot;results_order&quot;:&quot;asc&quot;,&quot;sentence&quot;:&quot;&quot;,&quot;search_in_taxonomy&quot;:&quot;&quot;,&quot;search_in_taxonomy_source&quot;:&quot;&quot;,&quot;results_area_width_by&quot;:&quot;form&quot;,&quot;results_area_custom_width&quot;:&quot;&quot;,&quot;results_area_custom_position&quot;:&quot;&quot;,&quot;results_area_columns&quot;:1,&quot;results_area_columns_tablet&quot;:&quot;&quot;,&quot;results_area_columns_mobile&quot;:&quot;&quot;,&quot;results_area_columns_mobile_portrait&quot;:&quot;&quot;,&quot;thumbnail_visible&quot;:&quot;yes&quot;,&quot;thumbnail_size&quot;:&quot;thumbnail&quot;,&quot;thumbnail_placeholder&quot;:{&quot;url&quot;:&quot;https:\\\/\\\/aerospacerepository.org\\\/wp-content\\\/plugins\\\/elementor\\\/assets\\\/images\\\/placeholder.png&quot;,&quot;id&quot;:&quot;&quot;,&quot;size&quot;:&quot;&quot;},&quot;post_content_source&quot;:&quot;content&quot;,&quot;post_content_custom_field_key&quot;:&quot;&quot;,&quot;post_content_length&quot;:30,&quot;show_product_price&quot;:&quot;&quot;,&quot;show_product_rating&quot;:&quot;&quot;,&quot;show_add_to_cart&quot;:&quot;&quot;,&quot;show_result_new_tab&quot;:&quot;&quot;,&quot;highlight_searched_text&quot;:&quot;&quot;,&quot;listing_id&quot;:&quot;&quot;,&quot;bullet_pagination&quot;:&quot;&quot;,&quot;number_pagination&quot;:&quot;&quot;,&quot;navigation_arrows&quot;:&quot;in_header&quot;,&quot;navigation_arrows_type&quot;:&quot;angle&quot;,&quot;show_title_related_meta&quot;:&quot;&quot;,&quot;meta_title_related_position&quot;:&quot;&quot;,&quot;title_related_meta&quot;:&quot;&quot;,&quot;show_content_related_meta&quot;:&quot;&quot;,&quot;meta_content_related_position&quot;:&quot;&quot;,&quot;content_related_meta&quot;:&quot;&quot;,&quot;negative_search&quot;:&quot;Sorry, but nothing matched your search terms.&quot;,&quot;server_error&quot;:&quot;Sorry, but we cannot handle your search query now. Please, try again later!&quot;,&quot;show_search_suggestions&quot;:&quot;&quot;,&quot;search_suggestions_position&quot;:&quot;&quot;,&quot;search_suggestions_source&quot;:&quot;&quot;,&quot;search_suggestions_limits&quot;:&quot;&quot;,&quot;search_suggestions_item_title_length&quot;:&quot;&quot;,&quot;search_source_terms&quot;:&quot;&quot;,&quot;search_source_terms_title&quot;:&quot;&quot;,&quot;search_source_terms_icon&quot;:&quot;&quot;,&quot;search_source_terms_limit&quot;:&quot;&quot;,&quot;search_source_terms_listing_id&quot;:&quot;&quot;,&quot;search_source_terms_taxonomy&quot;:&quot;&quot;,&quot;search_source_users&quot;:&quot;&quot;,&quot;search_source_users_title&quot;:&quot;&quot;,&quot;search_source_users_icon&quot;:&quot;&quot;,&quot;search_source_users_limit&quot;:&quot;&quot;,&quot;search_source_users_listing_id&quot;:&quot;&quot;}\"><form class=\"jet-ajax-search__form\" method=\"get\" action=\"https:\/\/aerospacerepository.org\/\" role=\"search\" target=\"\">\n\t<div class=\"jet-ajax-search__fields-holder\">\n\t\t<div class=\"jet-ajax-search__field-wrapper\">\n\t\t\t<label for=\"search-input-28eb3a3\" class=\"screen-reader-text\">Search ...<\/label>\n\t\t\t\t\t\t<input id=\"search-input-28eb3a3\" class=\"jet-ajax-search__field\" type=\"search\" placeholder=\"Search all fluid dynamics papers..\" value=\"\" name=\"s\" autocomplete=\"off\" \/>\n\t\t\t\t\t\t\t<input type=\"hidden\" value=\"{&quot;include_terms_ids&quot;:[3973]}\" 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-b272f62 elementor-widget elementor-widget-spacer\" data-id=\"b272f62\" 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-4460fa1 elementor-widget elementor-widget-spacer\" data-id=\"4460fa1\" 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-54e57bd elementor-widget elementor-widget-spacer\" data-id=\"54e57bd\" 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-c5f6038 elementor-widget elementor-widget-spacer\" data-id=\"c5f6038\" 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-45918a4 elementor-widget elementor-widget-spacer\" data-id=\"45918a4\" 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-de8eee3 elementor-widget elementor-widget-spacer\" data-id=\"de8eee3\" 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-bfd8a83 elementor-widget elementor-widget-spacer\" data-id=\"bfd8a83\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t<div class=\"elementor-column elementor-col-50 elementor-top-column elementor-element elementor-element-3a3cb99\" data-id=\"3a3cb99\" data-element_type=\"column\" data-e-type=\"column\" data-settings=\"{&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-c7b2ceb elementor-widget elementor-widget-spacer\" data-id=\"c7b2ceb\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-fb80527 elementor-widget elementor-widget-heading\" data-id=\"fb80527\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"heading.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<h2 class=\"elementor-heading-title elementor-size-default\">Results<\/h2>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-424a040 elementor-widget elementor-widget-jet-smart-filters-active hide-widget\" data-id=\"424a040\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"jet-smart-filters-active.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<div class=\"jet-smart-filters-active jet-active-filters jet-filter\" data-label=\"Active filters:\" data-content-provider=\"jet-engine\" data-additional-providers=\"\" data-apply-type=\"ajax\" data-query-id=\"default\"><\/div>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-03c22e8 elementor-widget elementor-widget-jet-smart-filters-sorting\" data-id=\"03c22e8\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"jet-smart-filters-sorting.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<div class=\"jet-smart-filters-sorting jet-filter\"><div\n\tclass=\"jet-sorting jet-sorting--flex-column\"\n\t data-smart-filter=\"sorting\" data-query-type=\"sort\" data-query-var=\"standard\" data-content-provider=\"\" data-query-id=\"default\" data-apply-type=\"ajax\" data-apply-on=\"value\" data-additional-providers=\"\">\n\t\t<select\n\t\tclass=\"jet-sorting-select\"\n\t\tname=\"select-name\"\n\t\t\t\taria-label=\"Sort filter\"\n\t>\n\t\t\t\t\t<option value=\"\">\n\t\t\t\tSort...\t\t\t<\/option>\n\t\t\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;title&quot;,&quot;order&quot;:&quot;ASC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy title from lowest to highest\t\t\t<\/option>\n\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;title&quot;,&quot;order&quot;:&quot;DESC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy title from highest to lowest\t\t\t<\/option>\n\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;date&quot;,&quot;order&quot;:&quot;ASC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy date from lowest to highest\t\t\t<\/option>\n\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;date&quot;,&quot;order&quot;:&quot;DESC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy date from highest to lowest\t\t\t<\/option>\n\t\t\t<\/select>\n<\/div>\n<\/div>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-5b3ecaf elementor-grid-1 elementor-grid-tablet-2 elementor-grid-mobile-1 elementor-posts--thumbnail-top elementor-card-shadow-yes elementor-posts__hover-gradient elementor-widget elementor-widget-posts\" data-id=\"5b3ecaf\" data-element_type=\"widget\" data-e-type=\"widget\" data-settings=\"{&quot;cards_columns&quot;:&quot;1&quot;,&quot;pagination_type&quot;:&quot;load_more_infinite_scroll&quot;,&quot;cards_row_gap&quot;:{&quot;unit&quot;:&quot;px&quot;,&quot;size&quot;:13,&quot;sizes&quot;:[]},&quot;cards_columns_tablet&quot;:&quot;2&quot;,&quot;cards_columns_mobile&quot;:&quot;1&quot;,&quot;cards_row_gap_tablet&quot;:{&quot;unit&quot;:&quot;px&quot;,&quot;size&quot;:&quot;&quot;,&quot;sizes&quot;:[]},&quot;cards_row_gap_mobile&quot;:{&quot;unit&quot;:&quot;px&quot;,&quot;size&quot;:&quot;&quot;,&quot;sizes&quot;:[]},&quot;load_more_spinner&quot;:{&quot;value&quot;:&quot;fas fa-spinner&quot;,&quot;library&quot;:&quot;fa-solid&quot;}}\" data-widget_type=\"posts.cards\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-posts-container elementor-posts elementor-posts--skin-cards elementor-grid\">\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-25464 post type-post status-publish format-standard hentry category-1-aerospace-europe-conference-2023 category-events category-3-cfd-multi-physics-simulation-in-aerospace tag-cfd tag-multi-body-separation tag-overset-methods homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-3766 category-993 category-3769 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2026\/04\/03\/a-local-unstructured-re-meshing-technique-for-handling-multi-body-separation-in-2d-flows\/\" target=&quot;_blank&quot;>\n\t\t\t\tA local unstructured re-meshing technique for handling multi-body separation in 2D flows.\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p>CARLO ALBERTO RASONI; ALESSIA ASSONITIS; RENATO PACIORRI; ALDO <b>BONFIGLIOLI; ENRICO CAVALLINI; SIMONE ILLIANO; SIMONE PIZZURRO; SIMONE CIABUSCHI<\/b><\/p>\n<p>DOI Number: 10.13009\/EUCASS2023-037<\/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-25448 post type-post status-publish format-standard hentry category-1-aerospace-europe-conference-2023 category-events category-3-cfd-multi-physics-simulation-in-aerospace tag-discontinuous-galerkin-method tag-embedded-boundaries tag-high-order-accuracy tag-thermal-fluid-structure-interaction homepage_sections-aerodynamics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-3766 category-993 category-3769 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2026\/04\/03\/a-high-order-accurate-framework-for-thermal-fluid-structure-interaction\/\" target=&quot;_blank&quot;>\n\t\t\t\tA high-order accurate framework for thermal fluid-structure interaction\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>VINCENZO GULIZZI<\/b><\/p>\n<p>DOI Number: 10.13009\/EUCASS2023-029<\/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-19709 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-cfd tag-closed-loop-gust-encounter tag-gust-loads tag-military-fighter-aircraft homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/gust-encounter-of-a-supersonic-fighter-aircraft-using-cfd-methods\/\" target=&quot;_blank&quot;>\n\t\t\t\tGust Encounter of a Supersonic Fighter Aircraft using CFD Methods\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Arne Voss<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-001<\/p>\n<p>Conference number: IFASD-2024-001<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19703 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-altitude-variation tag-continuous-turbulence tag-flight-loads tag-load-collectives homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/influence-of-cruise-altitude-variation-on-the-turbulence-loads-of-a-medium-range-transport-configuration\/\" target=&quot;_blank&quot;>\n\t\t\t\tInfluence of Cruise Altitude Variation on the Turbulence Loads of a Medium-Range Transport Configuration\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vega Handojo, Sunpeth Cumnuantip<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-004<\/p>\n<p>Conference number: IFASD-2024-004<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19697 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aerodynamic-gap tag-box-pressure-modifications tag-doublet-lattice-method-dlm tag-flutter tag-gust tag-static-lift-and-moment tag-zaero homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/flutter-and-gust-response-of-a-wing-with-aerodynamic-gaps\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlutter and Gust Response of a Wing with Aerodynamic Gaps\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Dale Pitt<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-006<\/p>\n<p>Conference number: IFASD-2024-006<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19688 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-conceptual-aircraft-design tag-gradient-based-optimization tag-multi-disciplinary-design-optimization tag-time-domain homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/aeroelastic-mission-optimization-of-very-flexible-vehicles-including-take-off-and-climb-constraints\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic Mission Optimization of Very Flexible Vehicles including Take-Off and Climb Constraints\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christopher Lupp<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-009<\/p>\n<p>Conference number: IFASD-2024-009<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19682 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-aeroelasticity tag-distributed-propeller tag-gust-response tag-wind-tunnel-test tag-wing-deformation homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/wind-tunnel-test-of-gust-response-for-distributed-propeller-wing-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tWind tunnel test of gust response for distributed propeller-wing 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>Kunhui Huang, Zhitao Zhang, Dawei Liu, Changchuan Xie<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-011<\/p>\n<p>Conference number: IFASD-2024-011<\/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-19676 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-aeroelastic-wind-tunnel tag-vehicle-design-process homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/aeroelastic-wind-tunnel-testing-of-3d-printed-semispan-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic Wind Tunnel Testing of 3D-Printed Semispan 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>Alexander Pankonien, Nicholas Jones, Asa Palmer, Joshua Deslich, Kevin McHugh, Robert Taylor<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-013<\/p>\n<p>Conference number: IFASD-2024-013<\/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-19667 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-fluid-structural-interaction-fsi tag-limit-cycle-oscillation-lco tag-shock-impingement homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/exploring-the-effect-of-different-shock-impingement-angles-on-aeroelastic-response-for-a-thin-panel\/\" target=&quot;_blank&quot;>\n\t\t\t\tExploring the Effect of Different Shock Impingement Angles on Aeroelastic Response for a Thin Panel\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Luisa Piccolo Serafim, Earl Dowell<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-016<br \/>\nConference number: IFASD-2024-016<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19664 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-constrained-optimisation tag-efficient-global-optimisation tag-lamination-parameters tag-reliability-based-design-optimisation homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/aeroelastic-reliability-based-optimisation-of-composite-plates-via-surrogate-modeling\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic reliability based optimisation of composite plates via surrogate modeling\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Roger Ballester Claret, Nicolo Fabbiane, Christian Fagiano, Cedric Julien, Didier Lucor<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-017<\/p>\n<p>Conference number: IFASD-2024-017<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19652 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-cfd tag-control-surfaces tag-dlm tag-unsteady-aerodynamics tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/experimental-and-numerical-assessment-on-the-aeroelastic-behavior-of-a-nlf-airfoil-with-oscillating-control-surfaces\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental and numerical assessment on the aeroelastic behavior of a NLF airfoil with oscillating control surfaces\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Carlos Sebastia Saez, Mirko Hornung<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-024<\/p>\n<p>Conference number: IFASD-2024-024<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19649 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity-in-conceptual-aircraft-design tag-computational-aeroelasticity tag-flutter tag-highly-flexible-aircraft-structures tag-loads-alleviation tag-mdo homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/13\/control-surface-sizing-and-design-through-integrated-mdo-approach-enhancing-load-alleviation-while-preserving-handling-quality-criteria\/\" target=&quot;_blank&quot;>\n\t\t\t\tControl surface sizing and design through integrated MDO approach: Enhancing load alleviation while preserving handling quality criteria\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Daniel Muradas Odriozola, Sylvie Marquier, Joseph Morlier, Christian Gogu<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-025<\/p>\n<p>Conference number: IFASD-2024-025<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19639 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-dynamic-gust-response tag-gust-vane-modelling tag-very-flexible-wing homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/effect-of-gust-models-on-the-response-prediction-of-a-very-flexible-wind-tunnel-wing-model\/\" target=&quot;_blank&quot;>\n\t\t\t\tEffect of gust models on the response prediction of a very flexible wind tunnel 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>Stefanie D\u00fcssler, Christoph Mertens, Rafael Palacios<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-028<br \/>\nConference number: IFASD-2024-028<\/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-19633 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-flutter tag-high-aspect-ratio-wing tag-machine-learning tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/machine-learning-to-forecast-unsteady-motion-induced-unsteady-forces\/\" target=&quot;_blank&quot;>\n\t\t\t\tMachine learning to forecast unsteady, motion-induced unsteady forces\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Reik Thormann, Hans Martin Bleecke<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-030<\/p>\n<p>Conference number: IFASD-2024-030<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19624 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-hybrid-testing tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/aeroelastic-hybrid-testing-for-industrial-applications\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic hybrid testing for industrial applications\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Davide Balatti, Hamed Haddad Khodaparast, Shakir Jiffri, Michael Friswell, Sebastiano Fichera, Alessandra Vizzaccaro, Andrea Castrichini<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-033<\/p>\n<p>Conference number: IFASD-2024-033<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19621 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-adjoint-tsm tag-gust-response tag-harmonic-balance tag-time-spectral-method tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/a-modular-tsm-solver-for-aeroelastic-analysis-and-optimizations\/\" target=&quot;_blank&quot;>\n\t\t\t\tA modular TSM solver for aeroelastic analysis and optimizations\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Cedric Liauzun, Christophe Blondeau<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-034 <\/p>\n<p>Conference number: IFASD-2024-034<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19615 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/advances-in-aeroelastic-prediction-and-design-optimization-for-next-generation-aerospace-vehicles\/\" target=&quot;_blank&quot;>\n\t\t\t\tAdvances in Aeroelastic Prediction and Design Optimization for Next-Generation Aerospace Vehicles\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sai Vishal Gali, Cristina Riso<\/b><\/p>\n<p>DOI Number: 10.82439\/ceas-ifasd-2024-036<\/p>\n<p>Conference number: IFASD-2024-036<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19592 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-buffet tag-design tag-pod tag-random-loads tag-turbulence homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/robust-design-through-identification-of-main-components-from-multivariate-random-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tRobust design through identification of main components from multivariate random loads\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Cyrille Vidy, Carlo Aquilini<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-044<\/p>\n<p>Conference number: IFASD-2024-044<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19586 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-doublet-lattice-method tag-uav tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/doublet-lattice-modelling-and-analysis-of-unsteady-aerodynamic-effects-for-a-flexible-unmanned-aircraft-during-maneuvers-and-gust-encounters\/\" target=&quot;_blank&quot;>\n\t\t\t\tDoublet lattice modelling and analysis of unsteady aerodynamic effects for a flexible unmanned aircraft during maneuvers and gust encounters\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Leif Rieck, Benjamin Herrmann, Frank Thielecke<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-046<br \/>\nConference number: IFASD-2024-046<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19583 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-buffet tag-design tag-nodal-loads tag-random-loads tag-stress tag-turbulence homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/from-multivariate-random-loads-to-deterministic-load-distributions-an-exact-method-for-aeroelastic-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tFrom Multivariate Random Loads To Deterministic Load Distributions: An Exact Method For Aeroelastic Design\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Carlo Aquilini, Gabriele Grasso, Cyrille Vidy<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-047<\/p>\n<p>Conference number: IFASD-2024-047<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19574 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-correlation-based-transition-modeling tag-transition-model-validation tag-turbulent-wedges tag-unsteady-transonic-flow homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/effect-of-turbulent-wedges-on-the-steady-and-unsteady-aerodynamics-of-a-forward-swept-laminar-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tEffect of Turbulent Wedges on the Steady and Unsteady Aerodynamics of a Forward Swept Laminar Wing\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Michael Fehrs, Christoph Kaiser<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-054<\/p>\n<p>Conference number: IFASD-2024-054<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19565 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-gvt tag-high-aspect-ratio tag-model-validation tag-wind-tunnel-test homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/wind-tunnel-testing-and-modal-validation-of-tu-flexs-high-aspect-ratio-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tWind tunnel testing and modal validation of TU-Flex&#8217;s 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>Pedro J. Gonz\u00e1lez, Guilherme C. Barbosa, \u00c1lvaro A. G. Quesada, Gerrit Stavorinus, Fl\u00e1vio J. Silvestre, Jonathan Hilger, Charlotte Hanke, Arne Voss, Wolf R. Kr\u00fcger<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-058<\/p>\n<p>Conference number: IFASD-2024-058<\/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-19553 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aero-thermo-elasticity tag-cfd-method tag-fem-method tag-hypersonic tag-partitioned-loose-coupling-strategy homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/a-cfd-ctd-csd-based-aero-thermo-elastic-framework-for-full-vehicle-scale-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tA CFD\/CTD\/CSD based aero-thermo-elastic framework for full-vehicle scale analysis\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Liang Ma, Zhiqiang Wan, Xiaozhe Wang, Keyu Li, Chang Li, Longfei He<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-063<\/p>\n<p>Conference number: IFASD-2024-063<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19550 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelastic-tailoring tag-commercial-aircraft tag-kriging-surrogate-model homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/aeroelastic-optimization-of-commercial-aircraft-considering-high-precision-aerodynamic-performance\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Keyu Li, Chao Yang, Xiaozhe Wang, Zhiqiang Wan, Liang Ma, Chang Li<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-064<\/p>\n<p>Conference number: IFASD-2024-064<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19538 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-load-analysis tag-nonlinear tag-vortex-lattice-method homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/efficient-and-high-precision-nonlinear-static-aeroelastic-load-analysis-method-based-on-vortex-lattice-method-acceleration\/\" target=&quot;_blank&quot;>\n\t\t\t\tEfficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Zou Zhicheng, Xie Changchuan, An Chao, Yang Lan, Zhu Lipeng, Ni Zao<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-068<\/p>\n<p>Conference number: IFASD-2024-068<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19535 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-doublet-lattice-method tag-flutter tag-gust tag-linearized-frequency-domain tag-optimization homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/gradient-based-optimization-of-the-common-research-model-wing-subject-to-cfd-based-gust-and-flutter-constraints\/\" target=&quot;_blank&quot;>\n\t\t\t\tGradient-based Optimization of the Common Research Model Wing Subject to CFD-based Gust and Flutter Constraints\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Andrew Thelen, Kevin Jacobson, Bret Stanford<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-069<\/p>\n<p>Conference number: IFASD-2024-069<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19514 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-damping tag-fixed-wing tag-flutter tag-optimisation homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/aeroelastic-optimisation-of-a-cantilevered-plate-with-local-damping-application\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic optimisation of a cantilevered plate with local damping application\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ali Tatar, Stephane Fournier, Jonathan Cooper<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-080<\/p>\n<p>Conference number: IFASD-2024-080<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19508 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-dynamic-loads tag-high-performance tag-jax tag-nonlinear-aeroelasticity homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/differentiable-aeroelastic-framework-suitable-for-industrial-modelling-of-nonlinear-loads-on-accelerators\/\" target=&quot;_blank&quot;>\n\t\t\t\tDifferentiable Aeroelastic Framework Suitable for Industrial Modelling of Nonlinear Loads on Accelerators\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alvaro Cea, Rafael Palacios<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-082<\/p>\n<p>Conference number: IFASD-2024-082<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19505 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-reduced-order-models-1-ifasd-2024 tag-co-rotational tag-harmonic-balance-method tag-reduced-order-model tag-static-aeroelastic-analysis homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-3022 category-3041 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/reduced-order-modeling-analysis-for-flexible-wing-using-a-co-rotational-beam-element\/\" target=&quot;_blank&quot;>\n\t\t\t\tReduced order modeling analysis for flexible wing using a co-rotational beam element\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yali Shao, Changchuan Xie, Chao An, Duoyao Zhang, Yuhui Zhang<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-083<\/p>\n<p>Conference number: IFASD-2024-083<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19502 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aerothermoelasticity tag-hypersonic-vehicles tag-meshfree-method homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/aerothermoelasticity-analysis-of-hypersonic-vehicle-based-on-meshfree-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tAerothermoelasticity analysis of hypersonic vehicle based on meshfree method\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Zhan Sun, Zhiqiang Wan, Xiaozhe Wang, Liang Ma, Chang Li<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-084<\/p>\n<p>Conference number: IFASD-2024-084<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19499 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-topology-optimization tag-wind-tunnel-model homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/elastic-wind-tunnel-model-design-via-eigenvector-based-level-set-topology-optimization\/\" target=&quot;_blank&quot;>\n\t\t\t\tElastic wind tunnel model design via eigenvector-based level-set topology 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>Eisuke Nakagawa, Tomohiro Yokozeki, Natsuki Tsushima<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-085<\/p>\n<p>Conference number: IFASD-2024-085<\/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-19496 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-aerothermoelasticity tag-functionally-graded-materials tag-hypersonic-vehicles homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/05\/12\/an-integrated-static-dynamic-aerothermoelastic-analysis-framework-for-functionally-graded-structures-in-hypersonic-vehicles\/\" target=&quot;_blank&quot;>\n\t\t\t\tAn integrated static\/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Chang Li, Zhiqiang Wan, Xiaozhe Wang, Chao Yang, Zhiying Chen<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-087<\/p>\n<p>Conference number: IFASD-2024-087<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19459 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-reduced-order-models-1-ifasd-2024 tag-active-control tag-conceptual-aircraft-design tag-reduced-order-modelling homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-3022 category-3041 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/flexible-aircraft-conceptual-co-design-based-on-the-rce-framework\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlexible aircraft conceptual co-design based on the RCE framework\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>B\u00e9la Takarics, B\u00e1lint Patarics, B\u00e1lint Vanek, Fanglin Yu, Yasser M. Meddaikar, Matthias Wuestenhagen, Thiemo Kier<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-099<\/p>\n<p>Conference number: IFASD-2024-099<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19444 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-enhanced-dlm tag-flutter tag-linearized-rans tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/flutter-prediction-correlations-with-wind-tunnel-measurements-on-a-t-tail-flutter-mock-up\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlutter prediction correlations with wind tunnel measurements on a T-tail flutter mock-up\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Elsa Br\u00e9us, Nicolas Forestier, Zdenek Johan, Eric Garrigues<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-104<\/p>\n<p>Conference number: IFASD-2024-104<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19441 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-neural-network tag-sensor-selection tag-strain tag-temperature homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/investigation-on-sensor-selection-applied-on-a-vehicle-as-a-sensor-concept-in-high-speed-flight\/\" target=&quot;_blank&quot;>\n\t\t\t\tInvestigation on Sensor Selection Applied on a Vehicle-as-a-Sensor Concept in High-Speed Flight\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ana C. Meinicke, Carlos E. S. Cesnik<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-105<\/p>\n<p>Conference number: IFASD-2024-105<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19435 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-aeroservoelasticity tag-gust-load-alleviation tag-robust-control tag-wind-tunnel-testing homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/wind-tunnel-testing-active-gust-load-alleviation-of-a-flexible-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tWind Tunnel Testing Active Gust Load Alleviation of a 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>Felix Stalla, Thiemo M. Kier, Gertjan Looye, Kolja Michel, Thomas G. Schmidt, Charlotte Hanke, Johannes Dillinger, Markus Ritter, Martin Tang<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-107<\/p>\n<p>Conference number: IFASD-2024-107<\/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-19432 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-aeroelasticity tag-body-freedom-flutter tag-stability tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/wind-tunnel-experiment-for-body-freedom-flutter-of-flying-wing-unmanned-aerial-vehicle\/\" target=&quot;_blank&quot;>\n\t\t\t\tWind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Elijah Ang, Jieli, Daryl Leo, Jun Kang Tan, Jonathan Tay, Yongdong Cui, Bing Feng Ng<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-108<\/p>\n<p>Conference number: IFASD-2024-108<\/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-19422 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelastic-derivatives tag-buffet tag-flutter tag-loewner-framework tag-mode-tracking tag-transonic-flow homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/a-general-solver-for-the-prediction-of-flutter-and-buffet-onset\/\" target=&quot;_blank&quot;>\n\t\t\t\tA general solver for the prediction of flutter and buffet onset\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>David Quero, Christoph Kaiser, Jens Nitzsche<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-112<\/p>\n<p>Conference number: IFASD-2024-112<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19410 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-force-summation-method tag-horizontal-tail tag-inertially-coupled-equations tag-internal-loads tag-quasi-steady tag-vlm tag-wing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/comparative-analysis-of-flight-maneuver-loads-between-flexible-and-rigid-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tComparative analysis of flight maneuver loads between flexible and rigid aircraft\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Eduardo de Melo Pinto, Fl\u00e1vio Cardoso-Ribeiro, Fernando de Oliveira Moreira<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-117<\/p>\n<p>Conference number: IFASD-2024-117<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19403 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-aeroelasticity tag-flipased tag-flutter-flight-testing tag-structural-dynamics tag-uav homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/flutter-flight-testing-using-operational-modal-analysis-to-identify-track-and-predict-flutter-for-safe-and-efficient-flight-test-campaigns\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Keith Soal, Jan Schwochow, Robin Volkmar, Martin Tang, Carsten Thiem, Yves Govers, Marc B\u00f6swald, Thiemo Kier, \u00d6zge S\u00fcel\u00f6zgen, Nicolas Guerin, Daniel Teubl, Julius Bartasevicius, Balint Vanek, Szabolcs Toth, Misi Nagy<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-119<\/p>\n<p>Conference number: IFASD-2024-119<\/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-19397 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-aircraft-loads tag-conceptual-aircraft-design tag-liquid-hydrogen tag-wingbox-sizing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/23\/design-manufacturing-and-identification-of-an-active-controlled-flexible-wing-for-subsonic-wind-tunnel-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tDesign, manufacturing and identification of an active controlled flexible wing for subsonic wind tunnel testing\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Johannes Dillinger, Holger Mai, Wolf R. Krueger, Thomas Schmidt, Felix Stalla<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-121<\/p>\n<p> Conference number: IFASD-2024-121<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19390 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-flutter tag-gust tag-lfd-solver tag-linearized-cfd tag-pulse tag-system-identification homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/analysis-of-linearized-motion-and-gust-induced-airloads-with-a-next-generation-computational-fluid-dynamics-solver\/\" target=&quot;_blank&quot;>\n\t\t\t\tAnalysis of Linearized Motion- and Gust-Induced Airloads with a Next-Generation Computational Fluid Dynamics Solver\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christoph Kaiser, David Quero, Jens Nitzsche, Bernd Stickan<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-123<\/p>\n<p>Conference number: IFASD-2024-123<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19381 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-distributed-electric-propulsion tag-whirl-flutter tag-wing-flutter homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/aeroelastic-analysis-of-distributed-electric-propulsion-flexible-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic analysis of distributed electric propulsion flexible wings\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Samet Dede, Ali Tatar, Djamel Rezgui, Jonathan Cooper<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-129<\/p>\n<p>Conference number: IFASD-2024-129<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19372 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-reduced-order-models-1-ifasd-2024 tag-gust-load-analysis tag-machine-learning tag-nonlinear-parametric-model-order-reduction homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-3022 category-3041 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/machine-learning-based-parametric-model-order-reduction-for-the-gust-load-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tMachine learning-based parametric model order reduction for the gust load analysis\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sangmin Lee, SiHun Lee, Younggeun Park, Seung-Hoon Kang, Kijoo Jang, Haeseong Cho, SangJoon Shin<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-135<\/p>\n<p>Conference number: IFASD-2024-135<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19365 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-flared-hinged-wings tag-flight-dynamics tag-folding-wing-tips tag-gust-load-alleviation tag-hale-aircraft homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/nonlinear-gust-effects-on-flexible-aircraft-with-flared-hinged-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear Gust Effects On Flexible Aircraft With Flared Hinged Wings\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kelvin Chi-Wing Cheng, Alvaro Cea, Rafael Palacios, Andrea Castrichini, Thomas Wilson<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-137<\/p>\n<p>Conference number: IFASD-2024-137<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19362 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-adjoint-sensitivity tag-aeroelasticity tag-computational tag-feature-mapping tag-topology homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/a-panel-free-aeroelastic-solver-with-adjoint-sensitivities\/\" target=&quot;_blank&quot;>\n\t\t\t\tA Panel-Free Aeroelastic Solver with Adjoint Sensitivities\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Hollis Smith, Joshua Deaton<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-138<\/p>\n<p>Conference number: IFASD-2024-138<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19359 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelasticity tag-smart-wing tag-supersonic-flow homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/aeroelasticity-of-smart-wing-in-supersonic-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelasticity of smart wing in supersonic flow\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Reza Moosavi<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-139<\/p>\n<p>Conference number: IFASD-2024-139<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19355 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-high-aspect-ratio-wing-aircraft tag-load-control tag-wind-tunnel-experiment homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/assessment-of-active-load-control-approaches-for-transport-aircraft-ae-simulation-and-wind-tunnel-test\/\" target=&quot;_blank&quot;>\n\t\t\t\tAssessment of Active Load Control Approaches for Transport Aircraft &#8211; Simulation and Wind Tunnel Test\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Wolf Krueger, Holger Mai, Thiemo Kier, Lars Reimer<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-141<\/p>\n<p>Conference number: IFASD-2024-141<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19352 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-reduced-order-models-1-ifasd-2024 tag-flexible-wing tag-large-amplitude-motion tag-model-order-reduction tag-nonlinear homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-3022 category-3041 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/nonlinear-dynamic-response-of-a-pazy-wing-variant-using-koiter-newton-model-reduction\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear dynamic response of a pazy wing variant using Koiter-Newton model reduction\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kautuk Sinha, Farbod Alijani, Wolf Krueger, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-142<\/p>\n<p>Conference number: IFASD-2024-142<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19349 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-distributed-electric-propulsor tag-electric-aircraft tag-gust-loads tag-load-alleviation tag-thrust-vectoring homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/11\/gust-load-alleviation-of-electric-aircraft-with-distributed-propulsors-using-thrust-vectoring\/\" target=&quot;_blank&quot;>\n\t\t\t\tGust load alleviation of electric aircraft with distributed propulsors using thrust vectoring\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Mohammadreza Amoozgar, Grigorios Dimitriadis, Jonathan Cooper, Rafic Ajaj<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-145<\/p>\n<p>Conference numer: IFASD-2024-145<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19345 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/09\/constrained-flexible-wing-with-folding-wingtip-dynamics-model-based-on-lagranges-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tConstrained flexible wing with folding wingtip dynamics model based on Lagrange&#8217;s method\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Lina Dehmlow, Pedro Gonz\u00e1lez, Gerrit Stavorinus, Fl\u00e1vio Silvestre<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-149<\/p>\n<p>Conference number: IFASD-2024-149<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19333 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-aeroelastic-tailoring tag-flutter tag-flying-demonstrator homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/09\/aeroelastic-design-of-a-drone-for-research-on-active-flutter-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic design of a drone for research on active flutter control\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nicol\u00f2 Fabbiane, Vincent Bouillaut, Arnaud Lepage<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-157<\/p>\n<p>Conference number: IFASD-2024-157<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19324 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-neural-network tag-nonlinear-aeroelasticity tag-reduced-order-models homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/09\/nonlinear-aeroelastic-analysis-of-a-regional-airliner-wing-via-a-neural-network-based-reduced-order-model-for-aerodynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear aeroelastic analysis of a regional airliner wing via a neural-network based reduced order model for aerodynamics\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nicol\u00f2 Laureti, Luca Pustina, Marco Pizzoli, Francesco Saltari, Franco Mastroddi<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-161<\/p>\n<p>Conference number: IFASD-2024-161<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19315 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-beats tag-coupled-oscillators tag-shock-dynamics tag-transonic-buffet homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/09\/mechanism-of-transonic-aeroelastic-instabilities-via-synchronization-of-coupled-oscillators\/\" target=&quot;_blank&quot;>\n\t\t\t\tMechanism of transonic aeroelastic instabilities via synchronization of coupled oscillators\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Srikanth Vasudevan, Xuerui Wang, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-164<\/p>\n<p>Conference number: IFASD-2024-164<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19309 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-anti-resonance tag-gust-loads tag-inertial-load-relief homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/04\/09\/analysis-of-inertial-gust-load-relief-characteristics-of-high-aspect-ratio-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tAnalysis of inertial gust load relief characteristics of high aspect ratio wings\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sanuja Jayatilake, Mark Lowenberg, Benjamin King Sutton Woods, Branislav Titurus<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-166<\/p>\n<p>Conference number: IFASD-2024-166<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19295 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-clean-aviation tag-distributed-propulsion tag-hybrid-electric-regional-architecture homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/25\/aeroelastic-challenges-in-the-clean-aviation-hybrid-electric-regional-aircraft-project\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic challenges in the clean aviation hybrid-electric regional aircraft project\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Emilio Santos, Alan Serena, Mordechay Karpel, Felix Arevalo, Hector Climent<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-170<\/p>\n<p>Conference number: IFASD-2024-170<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19292 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-data-analytics tag-dynamic-loads tag-neural-networks homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/25\/feedforward-backpropagation-artificial-neural-networks-applied-to-dynamic-loads-of-a-military-transport-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tFeedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Gabriel Buendia, Beatriz Pulido, MIguel Torralba, Manuel Reyes, Felix Arevalo, Hector Climent<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-171<\/p>\n<p>Conference number: IFASD-2024-171<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19289 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-aeroelasticity tag-aerothermoelasticity tag-hypersonic tag-wind-tunnel-testing homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/25\/measurement-of-natural-frequency-and-damping-of-a-slender-model-in-mach-5-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tMeasurement of Natural Frequency and Damping of a Slender Model in Mach 5 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 Diaz Villa, Marc Eitner, Jayant Sirohi, Noel Clemens<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-172<\/p>\n<p>Conference number: IFASD-2024-172<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19283 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-global-stability-analysis tag-shock-buffet tag-transonic-flow homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/25\/prediction-of-transonic-buffet-in-an-axial-flow-fan-using-global-stability-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tPrediction of transonic buffet in an axial flow fan using global stability analysis\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jyoti Majhi, Kartik Venkatraman<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-175<\/p>\n<p>Conference number: IFASD-2024-175<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19267 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity-1-ifasd-2024 category-ifasd-2024 tag-hypersonic tag-inverse-model tag-loads tag-neural-network homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3028 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/24\/experimental-validation-of-strain-load-neural-network-model-on-a-slender-hypersonic-vehicle\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ana Cristine Meinicke, Carlos Cesnik, Brianna Blocher, Aditya Panigrahi, Jayant Sirohi, Noel Clemens<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-185<\/p>\n<p>Conference number: IFASD-2024-185<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19227 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-flutter tag-source-and-doublet-panel-method homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/20\/application-of-the-unsteady-compressible-source-and-doublet-panel-method-to-flutter-calculations\/\" target=&quot;_blank&quot;>\n\t\t\t\tApplication of the unsteady compressible source and doublet panel method to flutter calculations\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Grigorios Dimitriadis, Spyridon Kilimtzidis, Vassilis Kostopoulos, Vito Laraspata, Leonardo Soria<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-199<\/p>\n<p>Conference numer: IFASD-2024-199<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19222 post type-post status-publish format-standard hentry category-events category-flight-testing-1-ifasd-2024 category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-additive-manufacturing tag-strain-sensors tag-structural-monitoring tag-transonic-wing-model homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3035 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/11\/shape-identification-of-a-wing-model-by-additive-manufacturing-for-transonic-tunnel-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tShape Identification of a wing model by additive manufacturing for transonic tunnel testing\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Natsuki Tsushima, Holger Mai, Marc Braune, Thomas Buete<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-200<\/p>\n<p>Conference number: IFASD-2024-200<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19219 post type-post status-publish format-standard hentry category-events category-flight-testing-1-ifasd-2024 category-ifasd-2024 category-wind-tunnel-testing-1-ifasd-2024 tag-flatter tag-lco tag-shock-control-bumps-scbs tag-transonic-dip homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-3035 category-3022 category-3046 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/11\/experimental-investigation-of-shock-control-bumbs-on-the-transonic-dip-of-the-oat15a-airfoil\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental investigation of shock control bumbs on the transonic dip of the OAT15A 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>Anna Altkuckatz, Marc Braune, Johannes Dillinger, Martin M\u00fcller, Thomas B\u00fcte, Charlotte Hanke, Holger Ernst, Heiko B\u00f6hlken, Patrick Hartl, Thomas Schmidt, Holger Mai<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-202<\/p>\n<p>Conference number: IFASD-2024-202<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19216 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-maneuver-simulation tag-simulation-based-certification tag-simulation-validation tag-virtual-flight-testing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/11\/high-fidelity-multidisciplinary-maneuver-simulations-of-the-falcon-2000lx-istar\/\" target=&quot;_blank&quot;>\n\t\t\t\tHigh-Fidelity Multidisciplinary Maneuver Simulations of the Falcon 2000LX ISTAR\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Martin Bauer, Johan Feldwisch<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-205<\/p>\n<p>Conference number: IFASD-2024-205<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19210 post type-post status-publish format-standard hentry category-events category-dynamic-loads-1-ifasd-2024 category-ifasd-2024 tag-evtol-electric-vertical-take-off-and-landing tag-experimental-modal-analysis-ema tag-finite-element-analysis-fea tag-rotorstructure-interaction tag-sequential-quadratic-programming-sqp homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-3031 category-3022 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/11\/experimental-investigation-into-the-dynamic-characteristics-of-a-tilting-multirotor-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental investigation into the dynamic characteristics of a tilting multirotor system\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Tanuj Sharma, Djamel Rezgui, Branislav Titurus<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-208<\/p>\n<p>Conference number: IFASD-2024-208<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19204 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-detached-eddy-simulation tag-limit-cycle-oscillations tag-lock-in tag-vortex-induced-vibrations homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/11\/investigation-of-vortex-induced-vibrations-to-compare-reynolds-averaged-navier-stokes-and-detached-eddy-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tInvestigation of vortex-induced vibrations to compare Reynolds-averaged Navier-Stokes and detached-eddy simulations\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kilian Streitenberger, Jens Nitzsche<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-214<\/p>\n<p>Conference number: IFASD-2024-214<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19198 post type-post status-publish format-standard hentry category-events category-unsteady-aerodynamics-1-ifasd-2024 tag-adaptive tag-aeroelasticity tag-euler tag-fem tag-fenics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/11\/adaptive-euler-efficient-and-predictive-aerodynamics-validation-and-prototype-development-toward-aeroelasticity\/\" target=&quot;_blank&quot;>\n\t\t\t\tAdaptive Euler &#8211; efficient and predictive aerodynamics: validation and prototype development toward aeroelasticity\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Johan Jansson, Kristoffer Wingstedt, Rebecca Durst<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-218<\/p>\n<p>Conference number: IFASD-2024-218<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19187 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-cfd tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/03\/07\/comparison-between-computational-and-experimental-non-stationary-pressure-distribution-on-a-pitch-oscilating-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tComparison between computational and experimental non-stationary pressure distribution on a pitch-oscilating wing\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Bruno Regina, Eduardo Molina, Roberto Silva<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-226<\/p>\n<p>Conference number: IFASD-2024-226<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19168 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/28\/optimization-of-nonlinear-periodic-aeroelastic-systems-using-boundary-value-problem-formulation\/\" target=&quot;_blank&quot;>\n\t\t\t\tOptimization of Nonlinear Periodic Aeroelastic Systems using Boundary Value Problem Formulation\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Anshuman Mehta, Pankil N. Mishra, Abhijit Gogulapati<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2024-233<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19165 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-reduced-order-models-1-ifasd-2024 tag-aeroelastic-tailoring tag-aeroelasticity tag-concurrent-design tag-mdo tag-rom tag-symbolic-model tag-tensor-product-model homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-3022 category-3041 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/28\/mathematical-method-for-prediction-aeroelastic-phenomena-and-multidisciplinary-optimization-lifting-surfaces-of-flight-vehicle-at-preliminary-stage-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tMathematical method for prediction aeroelastic phenomena and multidisciplinary optimization lifting surfaces of flight vehicle at preliminary stage design\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Oleh Havaza, Vitalii Sukhov, Ruslan Nikitin<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-235<\/p>\n<p>Conference number: IFASD-2024-235<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-19159 post type-post status-publish format-standard hentry category-events category-ifasd-2024 category-unsteady-aerodynamics-1-ifasd-2024 tag-aeroelasticity tag-large-angle-of-attack tag-plane-symmetry-vehicle tag-stability-of-trailing-edge-rudder-surface homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-astronautics-flight-mechanics homepage_sections-flight-mechanics homepage_sections-fluid-dynamics category-993 category-3022 category-3042 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2025\/02\/28\/aeroelastic-characteristics-of-plane-symmetry-vehicle-main-wing-trailing-edge-rudder-at-high-angle-of-attack\/\" target=&quot;_blank&quot;>\n\t\t\t\tAeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Guo Li, Gongde Li, Yingyou Hou<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82439\/ceas-ifasd-2024-240<\/p>\n<p>Conference number: IFASD-2024-240<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18720 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-reduced-order-modelling tag-aircraft-loads tag-flexible-aircraft tag-load-alleviation tag-nonlinear-aeroelasticity tag-parametric-rom homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2418 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/parametric-reduced-order-model-for-rapid-prediction-of-dynamic-loads-and-aeroelastic-response-with-structural-nonlinearitie\/\" target=&quot;_blank&quot;>\n\t\t\t\tPARAMETRIC REDUCED ORDER MODEL FOR RAPID PREDICTION OF DYNAMIC LOADS AND AEROELASTIC RESPONSE WITH STRUCTURAL NONLINEARITIE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Michele Castellani, Yves Lemmens, Jonathan E. Cooper<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-208<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18714 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/reynolds-averaged-navier-stokes-study-of-thetransonic-limit-cycle-oscillation-phenomenon-onthe-f-16-fighter-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tReynolds-averaged Navier-Stokes Study of theTransonic Limit Cycle Oscillation Phenomenon onthe F-16 Fighter Aircraft\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Michael Iovnovich, Daniella E. Raveh, Dan Michaels, Motti Adar<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-206<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18711 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-approximation-of-unsteady-aerodynamic-coefficients tag-flutter-calculation-method tag-non-linear-transonic-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/non-linear-unsteady-aerodynamics-application-for-airliner-flutter-research\/\" target=&quot;_blank&quot;>\n\t\t\t\tNON-LINEAR UNSTEADY AERODYNAMICS APPLICATION FOR AIRLINER FLUTTER RESEARCH\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Chuban A.V., Chuban V.D.<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-204<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18681 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-dlr-tau-code tag-flutter tag-gcro-dr tag-gmres tag-gust-response tag-krylov-subspace-recycling tag-linearised-computational-fluid-dynamics tag-shock-buet homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/krylov-subspace-recycling-for-linearised-aerodynamics-analysis-using-dlr-tau\/\" target=&quot;_blank&quot;>\n\t\t\t\tKRYLOV SUBSPACE RECYCLING FOR LINEARISED AERODYNAMICS ANALYSIS USING DLR\u2013TAU\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>S. Xu, S. Timme, K. J. Badcock<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-186<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18672 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/an-advanced-panel-method-for-compressible-subsonic-unsteady-flow-past-complex-geometries\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN ADVANCED PANEL METHOD FOR COMPRESSIBLE SUBSONIC UNSTEADY FLOW PAST COMPLEX GEOMETRIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Steven P. Fiddes, Chris W. Burkett, Thiemo Kier<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-181<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18669 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-abaqus tag-aeroelasticy tag-aircraft tag-exible tag-simulation homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/aeroelastic-simulations-of-flexible-aircraft-with-the-commercial-structural-solver-abaqus\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC SIMULATIONS OF FLEXIBLE AIRCRAFT WITH THE COMMERCIAL STRUCTURAL SOLVER ABAQUS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Marcos C. Ruggeri, Roberto G. A. da Silva, Carlos E. de Souza<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-180<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18666 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-3d tag-aerodynamic-inuence-coecients-integrated-exible-ight-dynamics-model tag-manoeuvre-loads-analysis tag-panel-method homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/integrated-flexible-dynamic-loads-models-based-on-aerodynamic-influence-coefficients-of-a-3d-panel-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tINTEGRATED FLEXIBLE DYNAMIC LOADS MODELS BASED ON AERODYNAMIC INFLUENCE COEFFICIENTS OF A 3D PANEL 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>Thiemo M. Kier, Mark J. Verveld, Chris W. Burkett<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-179<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18663 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-cfd-csm tag-coupling tag-fluid-structure tag-gust tag-openfsi homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/openfsi-interface-for-strongly-coupled-steady-and-unsteady-aeroelasticity\/\" target=&quot;_blank&quot;>\n\t\t\t\tOPENFSI INTERFACE FOR STRONGLY COUPLED STEADY AND UNSTEADY AEROELASTICITY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>C. Valente, D. Jones, A. Gaitonde, J. E. Cooper, Y. Lemmens<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-178<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18657 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-computational-aeroelastic-analysis tag-euler-analysis-of-unsteady-flows tag-flutter-flight-test tag-real-time-damping-estimation homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/a-correlation-study-of-modal-parameters-between-flutter-testing-and-cfd-simulation\/\" target=&quot;_blank&quot;>\n\t\t\t\tA CORRELATION STUDY OF MODAL PARAMETERS BETWEEN FLUTTER TESTING AND CFD SIMULATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>S. Orlando, M. Brughmans, T. Karaa\u011fa\u00e7l\u0131, \u00dc. Ceyhan, \u00d6. S\u00fcmer, M.E. Cerit, B. Durak<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-175<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18655 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-aerodynamics tag-aeroelasticity tag-flapping-wing tag-mav tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/analysis-and-computational-study-of-the-aerodynamics-and-aeroelasticity-of-generic-flapping-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tANALYSIS AND COMPUTATIONAL STUDY OF THE AERODYNAMICS AND AEROELASTICITY OF GENERIC FLAPPING 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>Harijono Djojodihardjo, Alif Syazwan Syamim Ramli<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-174<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18643 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-boundary-layer tag-panel-utter homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/influence-of-the-boundary-layer-on-flutter-of-elastic-plate-in-supersonic-gas-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF THE BOUNDARY LAYER ON FLUTTER OF ELASTIC PLATE IN SUPERSONIC GAS FLOW\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vsevolod O. Bondarev, Vasily V. Vedeneev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-168<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18640 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-action tag-aerodynamic-non-linearities tag-uid-structure-inter tag-p-k-method-limit-cycle-oscillations homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/prediction-of-aeroelastic-limit-cycle-oscillations-based-on-harmonic-forced-motion-oscillations\/\" target=&quot;_blank&quot;>\n\t\t\t\tPREDICTION OF AEROELASTIC LIMIT-CYCLE OSCILLATIONS BASED ON HARMONIC FORCED MOTION OSCILLATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A.C.L.M van Rooij, J. Nitzsche, R.P. Dwight<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-166<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18625 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-frequency-domain tag-ifasd tag-reduced-order-models tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/frequency-domain-approach-for-transonic-unsteady-aerodynamics-modelling\/\" target=&quot;_blank&quot;>\n\t\t\t\tFREQUENCY-DOMAIN APPROACH FOR TRANSONIC UNSTEADY AERODYNAMICS MODELLING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Adrien Poncet-Montanges, D. Jones, A.L. Gaitonde, J. E. Cooper, Y. Lemmens<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-157<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18619 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-cfd-csm-interaction tag-nonlinear-structure tag-oscillations tag-tau tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/limit-cylcle-oscillation-simulations-of-aerostabil-windtunnel-experiments\/\" target=&quot;_blank&quot;>\n\t\t\t\tLIMIT-CYLCLE-OSCILLATION SIMULATIONS OF AEROSTABIL WINDTUNNEL EXPERIMENTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Bernd Stickan, Johannes Dillinger, Jens Nitzsche<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-154<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18615 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-computational-uid-dynamics tag-limit-cycle-oscillation tag-transonic-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/transonic-limit-cycle-oscillation-analysis-of-aerostabil-wind-tunnel-model\/\" target=&quot;_blank&quot;>\n\t\t\t\tTRANSONIC LIMIT CYCLE OSCILLATION ANALYSIS OF AEROSTABIL 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>Hitoshi Arizono, Kenichi Saitoh, Masato Tamayama<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-151<\/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-18606 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods-bridges tag-adaptive-wing tag-aeroelastic-analysis tag-videogrammetry homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2427 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/structural-dynamic-investigation-of-adaptive-wing-demonstrator-within-sade-project\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTRUCTURAL DYNAMIC INVESTIGATION OF ADAPTIVE WING DEMONSTRATOR WITHIN SADE PROJECT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Gennady A. Amiryants, Vladimir P. Kulesh, Victor A. Malyutin, Andrey V. Smotrov, Alexander V. Chedrik<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-148<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18603 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-hale tag-large-deformation tag-static tag-uvlm homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/efficient-analysis-of-hale-aircraft-structure-for-static-and-dynamic-aeroelastic-behavior\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT ANALYSIS OF HALE AIRCRAFT STRUCTURE FOR STATIC AND DYNAMIC AEROELASTIC BEHAVIOR\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Lu LIU, Taehyoun KIM, Kwok Leung LAI<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-147<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18594 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-reduced-order-modelling tag-aic-correction tag-dynamic-loads tag-gust-encounter tag-rom homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2418 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/a-reduced-order-model-for-dynamic-loads-prediction-including-aerodynamic-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tA REDUCED ORDER MODEL FOR DYNAMIC LOADS PREDICTION INCLUDING AERODYNAMIC NONLINEARITIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>David Quero, Wolf Kr\u00fcger and Guillermo Jenaro<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-141<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18573 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-circulation-control tag-utter tag-modal-reduction tag-reduced-order-model homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/dynamic-instabilities-of-circulation-controlled-aerofoils\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC INSTABILITIES OF CIRCULATION CONTROLLED AEROFOILS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ian Krukow, Nora Neuert, Dieter Dinkler<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-134<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18555 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods tag-computational-fluid-dynamics tag-experimental-aerodynamics tag-experimental-aeroelasticity tag-fluid-structure-interaction tag-gust-generator homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2421 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/design-and-testing-of-a-low-subsonic-wind-tunnel-gust-generator\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN AND TESTING OF A LOW SUBSONIC WIND TUNNEL GUST GENERATOR\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>P.M.G.J. Lancelot, J. Sodja, N.P.M. Werter, R. De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-124<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18543 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-cfd tag-multi-fidelity-aeroelasticity tag-panel-aerodynamics tag-static-aeroelasticity homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/accelerated-convergence-of-high-fidelity-aeroelasticity-using-low-fidelity-aerodynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tACCELERATED CONVERGENCE OF HIGH-FIDELITY AEROELASTICITY USING LOW-FIDELITY AERODYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>K. Jovanov, R. De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-119<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18535 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods tag-data-acquisition tag-experimental-modal-analysis tag-noise tag-piezoelectric-materials homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2421 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/on-the-data-acquisiton-for-aeroelastic-analysis-using-pzt-lead-zirconate-titanate-excitation-and-test-parameters-definition\/\" target=&quot;_blank&quot;>\n\t\t\t\tON THE DATA ACQUISITON FOR AEROELASTIC ANALYSIS USING PZT (LEAD ZIRCONATE TITANATE) EXCITATION AND TEST PARAMETERS DEFINITION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>\u00c9der L. Oliveira, Roberto G. A. da Silva, Nuno M. M Maia, Adolfo G. Marto, Frederico J. Afonso, Afzal Suleman<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-115<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18505 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-aeroservoelasticity tag-generalized-aerodynamic-forces tag-linearized-euler-solver homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/linearized-fun3d-for-rapid-aeroelastic-design-and-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tLINEARIZED FUN3D FOR RAPID AEROELASTIC DESIGN AND ANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Shuchi Yang, P.C. Chen, Zhicun Wang<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-097<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18502 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-2d-unsteady-aerodynamics tag-body-vortex-interaction tag-conformal-mappings tag-free-wake-analysis homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/nonlinear-aeroelastic-modeling-via-conformal-mappings-for-a-typical-section-in-arbitrary-motion\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR AEROELASTIC MODELING VIA CONFORMAL MAPPINGS FOR A TYPICAL SECTION IN ARBITRARY MOTION\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 , Giorgio Riccardi , Franco Mastroddi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-096<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18496 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods tag-aeroelasticity tag-ecm tag-stiffness-test tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2421 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/experimental-identification-of-the-flexibility-influence-matrix-of-the-aircraft-engine-mounted-on-pylon-under-the-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL IDENTIFICATION OF THE FLEXIBILITY INFLUENCE MATRIX OF THE AIRCRAFT ENGINE MOUNTED ON PYLON UNDER THE WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alexei Grigoriev, Victor Malyutin, Alexei Chizhov, Andrei Gubernatenko<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-093<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18487 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-computational-fluid-dynamics tag-dlr-tau-code tag-half-wing-body-conguration tag-mechanical-vortex-generators tag-shock-buet-onset tag-transonic-flow homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/passive-control-of-transonic-buffet-onset-on-a-half-wing-body-configuration\/\" target=&quot;_blank&quot;>\n\t\t\t\tPASSIVE CONTROL OF TRANSONIC BUFFET ONSET ON A HALF WING\u2013BODY 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>S. Timme, F. Sartor<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-088<\/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-18475 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-reduced-order-modelling tag-aeroelasticity tag-neural-networks tag-reduced-order-modeling tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2418 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/nonlinear-reduced-order-modeling-of-unsteady-aerodynamic-loads-based-on-dynamic-local-linear-neuro-fuzzy-models\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR REDUCED-ORDER MODELING OF UNSTEADY AERODYNAMIC LOADS BASED ON DYNAMIC LOCAL LINEAR NEURO-FUZZY MODELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Maximilian Winter, Christian Breitsamter<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-082<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18466 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-control-volume-approach tag-at-plate tag-ow tag-indirect-load-calculation tag-piv tag-unsteady homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/using-2d-piv-measurements-to-compute-unsteady-aerodynamic-loads-on-a-flat-plate-at-high-angle-of-attack\/\" target=&quot;_blank&quot;>\n\t\t\t\tUSING 2D-PIV MEASUREMENTS TO COMPUTE UNSTEADY AERODYNAMIC LOADS ON A FLAT PLATE AT HIGH ANGLE OF ATTACK\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Amandine Guissart, Luis P. Bernal, Grigorios Dimitriadis, Vincent E. Terrapon<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-078<\/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-18444 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-ight-dynamics tag-potential-ow tag-stall tag-unsteady-aerodynamics tag-vortex-lattice-method homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/unsteady-and-post-stall-aerodynamic-modeling-for-aircraft-dynamics-simulation\/\" target=&quot;_blank&quot;>\n\t\t\t\tUNSTEADY AND POST-STALL AERODYNAMIC MODELING FOR AIRCRAFT DYNAMICS 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>Ryan C. Paul, Joseba Murua, Ashok Gopalarathnam<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-070<\/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-18432 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-continuous-turbulence tag-flutter tag-gust tag-small-disturbance-cfd tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/verification-of-the-use-of-small-disturbance-cfd-aerodynamics-in-flutter-and-gust-analyses-for-simple-to-highly-complex-configurations\/\" target=&quot;_blank&quot;>\n\t\t\t\tVerification of the use of small-disturbance CFD aerodynamics in flutter and gust analyses for simple to highly complex configurations\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Cyrille Vidy, Lukas Katzenmeier, Maximilian Winter, Christian Breitsamter<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-066<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18420 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-loads tag-state-space tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/continuous-time-state-space-unsteady-aerodynamic-modelling-for-efficient-aeroelastic-load-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tCONTINUOUS-TIME STATE-SPACE UNSTEADY AERODYNAMIC MODELLING FOR EFFICIENT AEROELASTIC LOAD ANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Noud P.M. Werter, Roeland De Breuker, Mostafa M. Abdalla<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-060<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18397 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods-bridges tag-aatb tag-nonlinear tag-transfer-function tag-unsteady-aerodynamics tag-wind-tunnel-testing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2427 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/experiments-on-the-active-aeroelastic-test-bench-aatb-for-the-identification-of-unsteady-aerodynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTS ON THE ACTIVE AEROELASTIC TEST BENCH (AATB) FOR THE IDENTIFICATION OF UNSTEADY AERODYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>J. Ertveldt , J. Schoukens , R. Pintelon, S. Vanlanduit<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-050<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18391 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aileron-buzz tag-computational-aeroelasticity tag-describing-function tag-uid-structure-interaction tag-limit-cycle-oscillation homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/multiple-input-dscribing-function-analysis-of-non-classical-aileron-buzz\/\" target=&quot;_blank&quot;>\n\t\t\t\tMULTIPLE INPUT DSCRIBING FUNCTION ANALYSIS OF NON-CLASSICAL AILERON BUZZ\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M. Irfan Zafar, Francesca Fusi, Giuseppe Quaranta<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-048<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18386 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-non-linear-modelling tag-vortex-induced-vibration homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/a-transfer-function-approach-to-model-unsteady-aerodynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tA TRANSFER FUNCTION APPROACH TO MODEL UNSTEADY AERODYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Tim De Troyer, Jan Decuyper, Mark C. Runacres<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-045<\/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-18377 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-apu tag-flap-door tag-flight-test tag-strength-and-fatigue-justification tag-structural-dynamics tag-unsteady-aerodynamic tag-vibrations tag-wind-tunnel-test homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/combined-unsteady-aerodynamics-and-structural-response-on-auxiliary-power-unit-flap-door-strength-and-fatigue-justification-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMBINED UNSTEADY AERODYNAMICS AND STRUCTURAL RESPONSE ON AUXILIARY POWER UNIT FLAP DOOR: STRENGTH AND FATIGUE JUSTIFICATION METHOD\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>PALOMARES A., ABARCA R., BARTH M<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-041<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18371 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods-bridges tag-amplitude-frequency-spectrum tag-pressure-oscillation tag-wake tag-wing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2427 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/loading-parameters-of-a-long-range-aircraft-wing-in-wind-tunnel-close-to-buffet-boundary\/\" target=&quot;_blank&quot;>\n\t\t\t\tLOADING PARAMETERS OF A LONG-RANGE AIRCRAFT WING IN WIND TUNNEL CLOSE TO BUFFET BOUNDARY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nikolay Bragin, Mansur Garifulin, Sergey Skomorokhov, Vitaliy Yanin<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-038<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18368 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-data-bridging tag-experimental-data tag-jet-structure-interaction tag-numerical-simulation homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/sonic-fatigue-on-aft-pylon-fairings\/\" target=&quot;_blank&quot;>\n\t\t\t\tSONIC FATIGUE ON AFT-PYLON FAIRINGS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Dr. Marcus BARTH, Dr. Simon TRAPIER, Mathieu BERTHOMET, Saravanan RAJAN<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-037<\/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-18356 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-composite tag-isogeometric tag-multi-fidelity tag-optimization tag-wind-turbine homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2419 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/isogeometric-framework-for-aeroelastic-wind-turbine-rotor-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tIsogeometric Framework for Aeroelastic Wind Turbine Rotor Analysis\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Etana Ferede, Mostafa M. Abdalla, Johannes K.S. Dillinger<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-030<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18350 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods-bridges tag-artificial-flow tag-dynamic-aeroelasticity tag-electromechanical-modeling tag-flutter homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2427 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/research-on-dynamic-stability-of-an-elastic-model-using-tests-in-artificial-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tRESEARCH ON DYNAMIC STABILITY OF AN ELASTIC MODEL USING TESTS IN ARTIFICIAL FLOW\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Gleb V.Liseykin, Mikhail M.Bogatyrev, Mikhail A.Pronin, Vsevolod I.Smyslov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-027<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18328 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods tag-buffet-control tag-closed-loop tag-fluidic-trailing-edge-device tag-fluidic-vortex-generator tag-open-loop tag-transonic-flow homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2421 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/an-experimental-demonstration-of-active-transonic-buffet-control-using-a-closed-loop-methodology\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN EXPERIMENTAL DEMONSTRATION OF ACTIVE TRANSONIC BUFFET CONTROL USING A CLOSED-LOOP METHODOLOGY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Arnaud Lepage, Julien Dandois, Arnaud Geeraert, Pascal Molton, Frederic Ternoy, Jean Bernard Dor, Eric Coustols<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-015<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18325 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods-bridges tag-aeroelasticity tag-buffeting tag-control tag-flaps tag-flutter tag-long-span-bridge tag-winglets homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2427 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/flutter-and-buffeting-of-long-span-suspension-bridges-in-fully-erected-and-partially-erected-conditions\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER AND BUFFETING OF LONG SPAN SUSPENSION BRIDGES IN FULLY ERECTED AND PARTIALLY ERECTED CONDITIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M. Massaro, K.N. Bakis, D.J.N. Limebeer, M.J.R. Graham<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-014<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18319 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-experimental-methods tag-dynamic-stall tag-leishman-beddoes tag-nonlinear-aeroelasticity tag-stall-utter tag-wind-tunnel-testing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-systems category-2413 category-2421 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/theoretical-and-experimental-investigation-of-a-structurally-and-aerodynamically-nonlinear-pitch-and-%ef%ac%82ap-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tTheoretical and experimental investigation of a structurally and aerodynamically nonlinear pitch and \ufb02ap wing\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Edouard Verstraelen, Johan Boutet, Chiara Grappasonni, Gaetan Kerschen, Grigorios Dimitriadis<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-012<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18316 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-boundary-layer tag-double-wake tag-nite-volume tag-panel-method tag-separated-ow tag-vortex-blob homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/unsteady-viscous-inviscid-coupling-simulations-of-separated-laminar-flows-around-2d-airfoils\/\" target=&quot;_blank&quot;>\n\t\t\t\tUnsteady Viscous-Inviscid Coupling Simulations of Separated Laminar Flows Around 2D Airfoils\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jose I. Rothkegel, Grigorios Dimitriadis<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-011<\/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-18301 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-reduced-order-modelling tag-geometric-nonlinearities tag-reduced-order-model tag-static-aeroelasticity tag-trim-analysis homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-materials-and-structures homepage_sections-systems category-2413 category-2418 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/static-aeroelastic-analysis-including-geometric-nonlinearities-based-on-reduced-ordered-model-rom\/\" target=&quot;_blank&quot;>\n\t\t\t\tStatic aeroelastic analysis including geometric nonlinearities based on Reduced Ordered Model (ROM)\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>An Chao, Xie Changchuan, Liu Yi, Yang Chao<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-006<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18295 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-linearization tag-local-piston-theory tag-perturbation tag-potential-ow tag-quasi-steady homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-2413 category-2416 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/on-the-validity-range-of-piston-theory\/\" target=&quot;_blank&quot;>\n\t\t\t\tON THE VALIDITY RANGE OF PISTON THEORY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Marius-Corne Meijer, Laurent Dala<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-004<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18244 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-fuel tag-loads tag-pressure tag-sloshing homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/fuel-loads-in-large-civil-airplanes\/\" target=&quot;_blank&quot;>\n\t\t\t\tFUEL LOADS IN LARGE CIVIL AIRPLANES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Francesco Gambioli, Arnaud George Malan<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-238<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18241 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-lagrangian-approach tag-pitching-airfoil tag-starting-vortex tag-unsteady-aerodynamics tag-vortex-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/a-variational-approach-for-the-dynamics-of-unsteady-point-vortices\/\" target=&quot;_blank&quot;>\n\t\t\t\tA VARIATIONAL APPROACH FOR THE DYNAMICS OF UNSTEADY POINT VORTICES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ahmed A. Hussein, Haithem E. Taha, Saad Ragab, Muhammad R. Hajj<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-237<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18232 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-cuf tag-free-vibration tag-one-dimensional tag-tapered tag-thin-walled homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/ree-vibration-analysis-of-tapered-wing-structures-using-refined-one-dimensional-models\/\" target=&quot;_blank&quot;>\n\t\t\t\tREE-VIBRATION ANALYSIS OF TAPERED WING STRUCTURES USING REFINED ONE-DIMENSIONAL MODELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. Viglietti, E. Zappino, E. Carrera<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-230<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18229 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aero-elastic tag-cuf tag-thermo-elastic tag-visco-elastic homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/aero-thermo-elastic-stability-analysis-of-multi-layered-visco-elastic-panels\/\" target=&quot;_blank&quot;>\n\t\t\t\tAERO-THERMO-ELASTIC STABILITY ANALYSIS OF MULTI-LAYERED VISCO-ELASTIC PANELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Enrico Zappino, Matteo Filippi, Erasmo Carrera<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-229<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18226 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-aeroelasticity tag-blended-wing-body tag-body-freedom-flutter tag-wind-tunnel-test homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/body-freedom-flutter-of-a-flexible-blended-wing-body-like-plate-an-experimental-study\/\" target=&quot;_blank&quot;>\n\t\t\t\tBODY FREEDOM FLUTTER OF A FLEXIBLE BLENDED WING BODY LIKE PLATE &#8211; AN EXPERIMENTAL STUDY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yingsong Gu, Zhichun Yang, Pier Marzocca, Shun He<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-227<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18223 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-coupling-model tag-flight-dynamics tag-hypersonic tag-local-piston homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/rigidelastic-coupling-stability-analysis-of-hypersonic-vehicles\/\" target=&quot;_blank&quot;>\n\t\t\t\tRIGID&amp;ELASTIC COUPLING STABILITY ANALYSIS OF HYPERSONIC VEHICLES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yan Yihan, Xie Changchuan, He Jingwu, Jiang Chongwen<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-225<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18220 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-folding-wing tag-freeplay-nonlinearity tag-nonlinear-aeroelasticity tag-wind-tunnel-test homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/the-nonlinear-flutter-wind-tunnel-test-of-a-folding-fin-with-freeplay-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHE NONLINEAR FLUTTER WIND TUNNEL TEST OF A FOLDING FIN WITH FREEPLAY NONLINEARITIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p>Yang Ning, Zhang Xin, Wang Nan, Liu Wei<\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-224<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18211 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-limit-cycle-oscillation tag-neural-network tag-openfoam tag-stall-flutter tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/nonlinear-aerodynamic-identification-and-stall-flutter-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR AERODYNAMIC IDENTIFICATION AND STALL FLUTTER ANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>XIANG ZhengPing , DAI YuTing<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-219<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18208 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-complex-conguration tag-crm tag-reduced-order-modeling tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/application-of-unsteady-aerodynamic-reduced-order-modeling-techniques-to-a-complex-configuration\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF UNSTEADY AERODYNAMIC REDUCED-ORDER MODELING TECHNIQUES TO A COMPLEX CONFIGURATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Maximilian Winter, Christian Breitsamter<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-217<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18202 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-adjoint-variables tag-bifurcation tag-utter tag-mesh-adaptation tag-piston-theory homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/adjoint-based-mesh-adaptation-for-direct-flutter-prediction\/\" target=&quot;_blank&quot;>\n\t\t\t\tADJOINT-BASED MESH ADAPTATION FOR DIRECT FLUTTER PREDICTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kevin G. Wang, Philip S. Beran, Shunxiang Cao<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-212<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18183 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-aeroelasticity tag-aic-correction tag-dynamic-coupling tag-small-disturbance-cfd tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/efficient-and-accurate-aeroelastic-analyses-based-on-small-disturbance-cfd-in-early-aircraft-development\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT AND ACCURATE AEROELASTIC ANALYSES BASED ON SMALL-DISTURBANCE CFD IN EARLY AIRCRAFT DEVELOPMENT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Cyrille Vidy, Lukas Katzenmeier, Maximilian Winter, Christian Breitsamter<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-205<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18180 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-freeplay tag-ifasd tag-nltva tag-nonlinear homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/freeplay-induced-limit-cycle-oscillation-mitigation-using-linear-and-nonlinear-tuned-vibration-absorbers\/\" target=&quot;_blank&quot;>\n\t\t\t\tFREEPLAY-INDUCED LIMIT CYCLE OSCILLATION MITIGATION USING LINEAR AND NONLINEAR TUNED VIBRATION ABSORBERS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>E. Verstraelen, G. Kerschen, G. Dimitriadis<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-204<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18177 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-cfd tag-fluid-structure-interaction tag-gust-encounter tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/an-optimized-doublet-lattice-method-correction-approach-for-a-large-civil-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN OPTIMIZED DOUBLET-LATTICE METHOD CORRECTION APPROACH FOR A LARGE CIVIL AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>C. Valente, C. Wales, D. Jones, A. Gaitonde, J. E. Cooper, Y. Lemmens<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-200<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18171 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-geometric-nonlinearity tag-hyper-reduction tag-model-order-reduction tag-simulation-free-trainingj146 tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/simulation-free-hyper-reduced-models-for-geometrically-nonlinear-structural-dynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tSIMULATION-FREE HYPER-REDUCED MODELS FOR GEOMETRICALLY NONLINEAR STRUCTURAL DYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>S. Jain, P. Tiso<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-197<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18146 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-cfd tag-gust homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/linearized-unsteady-cfd-for-gust-loads-with-tau\/\" target=&quot;_blank&quot;>\n\t\t\t\tLinearized Unsteady CFD for Gust Loads with TAU\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Wolfgang Weigold, Bernd Stickan, Inocencio Travieso-Alvarez, Christoph Kaiser, Patrick Teufel<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-187<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18143 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-cfd-mesh-deformation tag-cfd-mesh-repair tag-cfd-csm tag-uid-structure-interaction tag-multi-body-simulation tag-nonlinear-fem homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/high-fidelity-cfd-csm-interaction-in-the-industrial-context\/\" target=&quot;_blank&quot;>\n\t\t\t\tHIGH-FIDELITY CFD-CSM INTERACTION IN THE INDUSTRIAL CONTEXT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Bernd Stickan, Arne Rempke, Sebastian Helm, Hans Bleecke<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-186<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18140 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-gust-generator tag-unsteady-aerodynamics tag-unsteady-loads homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/investigation-of-the-unsteady-flow-over-a-wing-under-gust-excitation\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATION OF THE UNSTEADY FLOW OVER A WING UNDER GUST EXCITATION\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, Jurij Sodja, Roeland De Breuker<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-185<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18133 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-flight-vibration-test tag-online-aeroelastic-identification homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/flight-testing-using-fast-online-aeroelastic-identification-techniques-with-dlr-research-aircraft-halo\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT TESTING USING FAST ONLINE AEROELASTIC IDENTIFICATION TECHNIQUES WITH DLR RESEARCH AIRCRAFT HALO\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. Sinske, Y.Govers, G. Jelicic, R. Buchbach, J. Schwochow, V. Handojo, M. B\u00f6swald, W.R. Kr\u00fcger<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-183<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18127 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-aeroelastic-analysys tag-cfd tag-rom homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/aerom-nasas-unsteady-aerodynamic-and-aeroelastic-reduced-order-modeling-software\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROM: NASA\u2019S UNSTEADY AERODYNAMIC AND AEROELASTIC REDUCED-ORDER MODELING SOFTWARE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Walter A. Silva<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-181<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18124 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/computational-and-experimental-results-for-the-kth-nasa-wind-tunnel-model-used-for-acquisition-of-transonic-nonlinear-aeroelastic-data\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPUTATIONAL AND EXPERIMENTAL RESULTS FOR THE KTH-NASA WIND-TUNNEL MODEL USED FOR ACQUISITION OF TRANSONIC NONLINEAR AEROELASTIC DATA\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Walter A. Silva, Pawel Chwalowski, Carol D. Wieseman, Donald F. Keller, David Eller, Ulf Ringertz<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-180<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18121 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-dynamic-wake-inow tag-helicopter-ight-dynamics tag-reduced-order-modeling homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/application-of-low-order-wake-inflow-models-to-rotorcraft-aeromechanics\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF LOW-ORDER WAKE INFLOW MODELS TO ROTORCRAFT AEROMECHANICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>J. Serafini, F. Cardito, G. Bernardini, M. Gennaretti<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-179<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18115 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-buffet-forcing-functions tag-experimental-unsteady-aerodynamics tag-launch-vehicle-buffet homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/effect-of-circumferential-surface-pressure-integration-on-launch-vehicle-buffet-forcing-functions\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFECT OF CIRCUMFERENTIAL SURFACE PRESSURE INTEGRATION ON LAUNCH VEHICLE BUFFET FORCING FUNCTIONS\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 K. Sekula, David J. Piatak, Russ D. Rausch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-176<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18109 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-lco tag-supersonic-transport tag-transonic-flow tag-wind-tunnel-test homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/limit-cycle-oscillation-of-a-supersonic-transport-model-in-a-transonic-wind-tunnel-test\/\" target=&quot;_blank&quot;>\n\t\t\t\tLIMIT CYCLE OSCILLATION OF A SUPERSONIC TRANSPORT MODEL IN A TRANSONIC WIND TUNNEL TEST\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kenichi SAITOH, Norio YOSHIMOTO, Hamidreza KHEIRANDISH<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-174<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18094 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-aeroelasticity tag-utter tag-transonic tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/design-and-testing-of-a-full-span-aeroelastic-wind-tunnel-model\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN AND TESTING OF A FULL SPAN AEROELASTIC 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>Ulf Ringertz, David Eller, Donald F. Keller, Walter A. Silva<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-169<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18091 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-aeroelasticity-turbulence-modelling tag-hybrid-rans-les tag-les tag-rans tag-structural-dynamics tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/on-the-adoption-of-hybrid-rans-les-turbulence-modelling-technique-for-aeroelastic-problems\/\" target=&quot;_blank&quot;>\n\t\t\t\tON THE ADOPTION OF HYBRID RANS-LES TURBULENCE MODELLING TECHNIQUE FOR AEROELASTIC PROBLEMS\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<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-168<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18088 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-discrete-vortex-method tag-flexible-airfoils tag-free-wake tag-unsteady-aerodynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/semi-analytical-unsteady-aerodynamic-modeling-for-a-flexible-thin-airfoil-in-arbitrary-motion\/\" target=&quot;_blank&quot;>\n\t\t\t\tSEMI-ANALYTICAL UNSTEADY AERODYNAMIC MODELING FOR A FLEXIBLE THIN AIRFOIL IN ARBITRARY MOTION\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, Giorgio Riccardi, Franco Mastroddi<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-167<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18085 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-increased-order-modeling tag-structural-dynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/increased-order-aeroservoelastic-modeling-in-practice\/\" target=&quot;_blank&quot;>\n\t\t\t\tINCREASED-ORDER AEROSERVOELASTIC MODELING IN PRACTICE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Manuel Reyes, Hector Climent, Moti Karpel, Felix Ar\u00e9valo, Carlos Maderuelo<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-165<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18082 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-acoustic-blocage tag-aeroelasticity tag-utter tag-linear-method tag-lrans tag-shock-wave-boundary-layer-interaction tag-turbomachinery homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/influence-of-reduced-frequency-on-choke-flutter-instability-in-transonic-uhbr-fan\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF REDUCED FREQUENCY ON CHOKE FLUTTER INSTABILITY IN TRANSONIC UHBR FAN\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Q. Rendu, S. Aubert, P. Ferrand<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-164<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18079 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelastic-prediction-workshop tag-flutter-analysis homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/flutter-analysis-for-the-second-aeroelastic-prediction-workshop\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER ANALYSIS FOR THE SECOND AEROELASTIC PREDICTION WORKSHOP\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Daniella E. Raveh<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-163<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18076 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-cfd tag-apping-wings tag-uid-structure tag-interaction-energy-harvesting tag-leading-edge-vortices homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/numerical-investigation-of-self-sustained-limit-cycle-oscillations-in-a-flapping-foil-energy-harvester\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL INVESTIGATION OF SELF-SUSTAINED LIMIT-CYCLE OSCILLATIONS IN A FLAPPING-FOIL ENERGY HARVESTER\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Enhao Wang, Kiran Ramesh, Ignazio Maria Viola, Shaun Killen<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-162<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18066 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-continuous-turbulence tag-gust-encounter tag-nonlinear tag-rom tag-volterra-series homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/a-nonlinear-frequency-domain-aerodynamic-model-for-continuous-turbulence-encounter-based-on-functional-series-expansion\/\" target=&quot;_blank&quot;>\n\t\t\t\tA NONLINEAR FREQUENCY DOMAIN AERODYNAMIC MODEL FOR CONTINUOUS TURBULENCE ENCOUNTER BASED ON FUNCTIONAL SERIES EXPANSION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>David Quero, Wolf Kr\u00fcger<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-159<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18057 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-aeroelasticity-real-time-simulation tag-exible-aircraft tag-ight-dynamics tag-reduced-order-modeling homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/application-of-nonlinear-model-order-reduction-technique-to-a-flexible-aircraft-for-real-time-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF NONLINEAR MODEL ORDER REDUCTION TECHNIQUE TO A FLEXIBLE AIRCRAFT FOR REAL-TIME SIMULATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Juliano A. Paulino, Fl\u00e1vio J. Silvestre, Ant\u00f4nio B. Guimar\u00e3es Neto, Tiago P. Monteiro, Roberto Gil A. da Silva, Andrea Da Ronch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-152<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18051 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-aeroelasticity tag-state-space-models tag-unsteady-aerodynamics tag-unsteady-vortexlattice-method homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/state-space-realizations-and-model-reduction-of-potential-flow-unsteady-aerodynamics-with-arbitrary-kinematics\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTATE-SPACE REALIZATIONS AND MODEL REDUCTION OF POTENTIAL-FLOW UNSTEADY AERODYNAMICS WITH ARBITRARY KINEMATICS\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 Palacios, Robert J. S. Simpson, Salvatore Maraniello<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-150<\/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-18048 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-adjoint-sensititivities tag-algorithmic-differentiation tag-uid-structure-interaction tag-geometrically-nonlinear-structures tag-multidisciplinary-optimization tag-viscous-ows homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/computing-derivatives-in-nonlinear-aeroelasticity-using-algorithm-differentiation\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPUTING DERIVATIVES IN NONLINEAR AEROELASTICITY USING ALGORITHM DIFFERENTIATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ruben Sanchez, Rafael Palacios<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-149<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18045 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-computational-uid-dynamics tag-ight-dynamics tag-model-reduction homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/model-reduction-for-gust-load-analysis-of-free-flying-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODEL REDUCTION FOR GUST LOAD ANALYSIS OF FREE-FLYING AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>G. Pagliuca, P. Bekemeyer, R. Thormann, S. Timme<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-148<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18036 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aepw tag-aeroelasticity tag-bscw tag-computational tag-dynamics tag-uid tag-utter tag-transonic homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/effect-of-angle-of-attack-gas-composition-and-reynolds-number-on-flutter-boundary-of-benchmark-super-critical-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFECT OF ANGLE OF ATTACK, GAS COMPOSITION AND REYNOLDS NUMBER ON FLUTTER BOUNDARY OF BENCHMARK SUPER-CRITICAL WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jan Navr\u00e1til, Adam Jir\u00e1sek, Peter Hamlington, Lt. Col. Andrew Lofthouse<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-142<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18033 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-aerothermoelastic tag-hypersonic tag-perturbation-method homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/a-static-aerothermoelastic-response-analysis-method-with-considering-stiffness-uncertainty\/\" target=&quot;_blank&quot;>\n\t\t\t\tA STATIC AEROTHERMOELASTIC RESPONSE ANALYSIS METHOD WITH CONSIDERING STIFFNESS UNCERTAINTY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nan Yi, Zhiqiang Wan, Chao Yang, Siyan Zhu<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-141<\/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-18030 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-apping-wing-propulsion tag-ow-structure-interactions tag-swimming-ying tag-vortex-dynamics homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/the-leading-edge-vortex-in-flexible-wing-propulsion\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHE LEADING EDGE VORTEX IN FLEXIBLE WING PROPULSION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ravi C. Mysa, Kartik Venkatraman<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-140<\/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-18018 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-computational-aeroelasticity tag-reduced-order-models homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/self-adaptive-pod-based-rom-aeroelastic-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tSELF ADAPTIVE POD BASED ROM AEROELASTIC SIMULATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Rub\u00e9n Moreno-Ramos, Fernando Varas, Jos\u00e9 M. Vega<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-136<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18015 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-arma tag-dmd tag-flutter-testing homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/flight-flutter-testing-using-higher-order-dynamic-mode-decomposition\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT FLUTTER TESTING USING HIGHER ORDER 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>Rub\u00e9n Moreno-Ramos, Soledad Le Clainche, Jos\u00e9 M. Vega, Paul F. Taylor<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-135<\/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-18012 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-bscw tag-ddes tag-shock-buffet homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/delayed-des-in-su2-test-case-3-from-the-second-aiaa-aeroelastic-prediction-workshop\/\" target=&quot;_blank&quot;>\n\t\t\t\tDELAYED DES IN SU2: TEST CASE 3 FROM THE SECOND AIAA AEROELASTIC PREDICTION WORKSHOP\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Eduardo S. Molina, Cleber Spode, Roberto Gil A. da Silva, Marcello Righi, Thomas D. Economon, Juan J. Alonso<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-134<\/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-17993 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aircraft tag-fem tag-lco tag-pylon homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/19\/an-investigation-in-hi-fi-finite-element-modelling-aimed-to-improve-lco-prediction\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN INVESTIGATION IN HI-FI FINITE ELEMENT MODELLING AIMED TO IMPROVE LCO 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>A. Manes, A. Gilioli, M. Giglio<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-125<\/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-17990 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-experimental-database tag-flutter tag-intersecting-surfaces tag-numerical-correlation tag-u-tail tag-wind-tunnel-tests homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/19\/wind-tunnel-flutter-tests-of-a-u-tail-configuration-part-2-experimental-and-numerical-results\/\" target=&quot;_blank&quot;>\n\t\t\t\tWIND TUNNEL FLUTTER TESTS OF A U-TAIL CONFIGURATION PART 2: EXPERIMENTAL AND NUMERICAL RESULTS\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 J. Mamelle, Gabriel Broux, Eric C. Garrigues<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-124<\/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-17956 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-fluid-structure-interaction-fsi tag-full-aircraft-model-fam tag-nasa-common-research-problem-crm tag-split-velocity-method-svm homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/a-cfd-based-aeroelastic-gust-model-for-full-aircraft-simulation\/\" target=&quot;_blank&quot;>\n\t\t\t\tA CFD BASED AEROELASTIC GUST MODEL FOR FULL AIRCRAFT 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>William D. C. Liw Tat Man, Andrew G. B. Mowat, Arnaud G. Malan, Javon C. Farao<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-117<\/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-17947 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-active-control-and-adaptive-structures tag-highly-flexible-aircraft-structures tag-wind-tunnel-and-flight-testing homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/closed-loop-flight-tests-with-an-unmanned-experimental-multi-body-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tCLOSED-LOOP FLIGHT TESTS WITH AN UNMANNED EXPERIMENTAL 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>Alexander K\u00f6the, Alexander Behrens, Alexander Hamann, Phillip Nagel, Danny Nowka, Robert Luckner<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-111<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17944 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-3d-printing tag-additive-manufacturing tag-aeroelasticity tag-evolutionary-design tag-experimental-testing tag-size-optimization tag-topology-optimization homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/validation-of-topology-optimized-lifting-surfaces-using-3-d-printing\/\" target=&quot;_blank&quot;>\n\t\t\t\tVALIDATION OF TOPOLOGY OPTIMIZED LIFTING SURFACES USING 3-D PRINTING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Joshua D. Deaton, Raymond M. Kolonay, Robert Reuter, Marcelo H. Kobayashi<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-108<\/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-17888 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-dlm-correction tag-gust-encounter tag-nasa-common-research-model tag-reduced-order-model tag-time-linearized-cfd homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/comparison-of-nonlinear-cfd-with-time-linearized-cfd-and-cfd-corrected-dlm-for-gust-encounter-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPARISON OF NONLINEAR CFD WITH TIME-LINEARIZED CFD AND CFD-CORRECTED DLM FOR GUST ENCOUNTER 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>Christoph Kaiser, Diliana Friedewald, Jens Nitzsche<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-101<\/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-17879 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-arma tag-experimental-methods tag-flutter-ight-testing tag-operational-modal-analysis homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/assessment-of-advanced-flutter-flight-test-techniques-and-flutter-boundary-prediction-methods\/\" target=&quot;_blank&quot;>\n\t\t\t\tASSESSMENT OF ADVANCED FLUTTER FLIGHT TEST TECHNIQUES AND FLUTTER BOUNDARY PREDICTION METHODS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Maj. Michael Iovnovich, Lt. Tzlil Nahom, Lt. Michael Presman, Lt. Dorin Avsaid, Maj. Tomer Braier, Daniella E. Raveh<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-097<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17870 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-computational-fluid-structure-interaction tag-high-aspect-ratio-wings tag-structural-wing-design homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/high-fidelity-trim-calculation-under-consideration-of-aeroelastic-effects-of-a-high-aspect-ratio-swept-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tHIGH FIDELITY TRIM CALCULATION UNDER CONSIDERATION OF AEROELASTIC EFFECTS OF A HIGH ASPECT RATIO SWEPT WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Andreas Hermanutz, Mirko Hornung<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-92<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17864 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-aeroelastic-stability tag-experiment tag-flutter-boundary tag-laminar-airfoil tag-transonic-flow homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/experimental-assessment-of-the-flutter-stability-of-a-laminar-airfoil-in-transonic-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL ASSESSMENT OF THE FLUTTER STABILITY OF A LAMINAR AIRFOIL 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>Anne Hebler<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-089<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17860 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-aeroelasticity tag-flight-loads tag-turbulence homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/flight-loads-analysis-and-measurements-of-externalstores-on-an-atmospheric-research-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT LOADS ANALYSIS AND MEASUREMENTS OF EXTERNAL STORES ON AN ATMOSPHERIC RESEARCH 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>Vega Handojo, Thomas Klimmek, Wolf Kr\u00fcger<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-086<\/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-17857 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-degenerate-transformation tag-dynamic-eigenmodes tag-modally-equivalent-perturbed-system tag-modes tag-nonlinear-system tag-reduced-order-model homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/parametrically-rich-nonlinear-reduced-order-modeling-anapplication-in-viscous-incompressible-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tPARAMETRICALLY RICH NONLINEAR REDUCED-ORDER MODELING: AN APPLICATION IN VISCOUS INCOMPRESSIBLE FLOW\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>T. Kim, E.H. Dowell<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-085<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17854 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-aeroelasticity tag-computational-uid-dynamics tag-dynamic-mode-decomposition tag-harmonic-balance-method tag-transonic-ow tag-unsteady-aerodynamics-modeling homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/research-on-fast-aeroelastic-modeling-methods-forthe-transonic-regime\/\" target=&quot;_blank&quot;>\n\t\t\t\tRESEARCH ON FAST AEROELASTIC MODELING METHODS FOR THE TRANSONIC REGIME\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\u00fcseyin G\u00fcner, Grigorios Dimitriadis, Vincent E. Terrapon<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-083<\/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-17832 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-flutter tag-green-aviation tag-u-tail tag-wind-tunnel-tests homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/wind-tunnel-flutter-tests-of-a-u-tail-configuration-part-1model-design-and-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tWIND TUNNEL FLUTTER TESTS OF A U-TAIL CONFIGURATION PART 1:MODEL 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>A. Geeraert, A. Lepage, P. Stephani, D. Feldmann, W. H\u00e4berli<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-072<\/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-17826 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-hypersonic-aerothermoelasticity tag-linearized-stability-analysis tag-reduced-order-modeling tag-scaling-laws homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/efficient-reduced-order-modeling-for-skin-panels-inhypersonic-flow-and-its-application-to-generatingaerothermoelastic-scaling-laws\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT REDUCED-ORDER MODELING FOR SKIN PANELS IN HYPERSONIC FLOW AND ITS APPLICATION TO GENERATING AEROTHERMOELASTIC SCALING LAWS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Daning Huang, Tomer Rokita, Peretz P. Friedmann<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-069<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17820 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-airfoil-utter tag-boundary-layer-transition tag-local-correlation-based-transition-model homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/cfd-based-flutter-prediction-for-high-reynoldsnumber-flows-with-free-boundary-layer-transition\/\" target=&quot;_blank&quot;>\n\t\t\t\tCFD-BASED FLUTTER PREDICTION FOR HIGH REYNOLDS NUMBER FLOWS WITH FREE BOUNDARY LAYER TRANSITION\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, Jens Nitzsche, Anne Hebler<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-066<\/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-17814 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-high-angle-of-attack tag-nonlinear tag-stall tag-wind-tunnel homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/study-of-the-nonlinearity-in-the-aeroelasticresponse-at-high-angle-of-attack-by-wind-tunneltests-on-the-active-aeroelastic-test-bench\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTUDY OF THE NONLINEARITY IN THE AEROELASTIC RESPONSE AT HIGH ANGLE OF ATTACK BY WIND TUNNEL TESTS ON THE ACTIVE AEROELASTIC TEST BENCH\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Julien Ertveldt, Alfredo Lamberti, Ben De Pauw, Ali Rezayat, Rik Pintelon, Steve Vanlanduit<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-063<\/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-17799 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-aerodynamic-correction tag-aeroelasticity tag-ifasd tag-wind-tunnel-test homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/improving-aeroelastic-model-accuracy-andaffordability-by-exploiting-wind-tunnel-test-results\/\" target=&quot;_blank&quot;>\n\t\t\t\tIMPROVING AEROELASTIC MODEL ACCURACY AND AFFORDABILITY BY EXPLOITING WIND TUNNEL TEST RESULTS\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 Di Gifico, Vincenzo Vaccaro<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-055<\/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-17796 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-dynamic-coupled-simulations tag-lco tag-reduced-model homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/aeroelastic-limit-cycle-oscillations-on-a-3d-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC LIMIT CYCLE OSCILLATIONS ON A 3D 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>Sylvie Dequand, Guy-Daniel Mortch\u00e9l\u00e9wicz, Anne-Sophie Sens<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference numer: IFASD-2017-054<\/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-17790 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-hpc-scalability tag-large-scale-computations tag-linearized-cfd tag-turbulence-gradient homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/industrial-frequency-domain-linearizednavier-stokes-calculations-for-aeroelastic-problemsin-the-transonic-flow-regime\/\" target=&quot;_blank&quot;>\n\t\t\t\tINDUSTRIAL FREQUENCY-DOMAIN LINEARIZED NAVIER-STOKES CALCULATIONS FOR AEROELASTIC PROBLEMS IN THE TRANSONIC FLOW REGIME\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Laurent Daumas, Nicolas Forestier, Alo\u00efs Bissuel, Gabriel Broux, Fr\u00e9d\u00e9ric Chalot, Zdenek Johan, Michel Mallet<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-050<\/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-17772 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-computational-aeroelasticity tag-dynamic-aeroelastic tag-flutter tag-fun3d homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/cfd-model-of-the-transonic-dynamics-tunnel-withapplications\/\" target=&quot;_blank&quot;>\n\t\t\t\tCFD MODEL OF THE TRANSONIC DYNAMICS TUNNEL WITH APPLICATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Pawel Chwalowski, Walter A. Silva, Carol D. Wieseman and Jennifer Heeg<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-044<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17766 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-flutter-boundary tag-proper-orthogonal-decomposition tag-reduced-order-model tag-structural-dynamic-reanalysis tag-transonic-aeroelasticity homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/consideration-of-pod-interpolation-for-aeroelasticdesign-with-large-global-structural-variations-usestructural-dynamic-reanalysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tCONSIDERATION OF POD INTERPOLATION FOR AEROELASTIC DESIGN WITH LARGE GLOBAL STRUCTURAL VARIATIONS USE STRUCTURAL DYNAMIC REANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Dongfeng Li, Gang Chen, A.Da Ronch, Qiang Zhou, Yueming Li<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-040<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17763 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-generalized-aerodynamic-forces tag-linearized-unsteady-solver tag-transpiration-boundary-condition homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/flutter-boundary-prediction-for-a-twin-enginetransport-flutter-model-using-a-linearized-unsteadysolver\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER BOUNDARY PREDICTION FOR A TWIN-ENGINE TRANSPORT FLUTTER MODEL USING A LINEARIZED UNSTEADY 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>Shuchi Yang, Zhicun Wang, Zhichao Zhang, P.C. Chen<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-039<\/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-17760 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-geometric-nonlinearities tag-reduced-order-model tag-response-analysis homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/efficient-aeroelastic-response-analysis-includinggeometric-nonlinearities-based-on-structural-rom\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT AEROELASTIC RESPONSE ANALYSIS INCLUDING GEOMETRIC NONLINEARITIES BASED ON STRUCTURAL ROM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>An Chao, Xie Changchuan, Meng Yang, Yang Chao<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-037<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17757 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-nonlinear-modal-analysis tag-reduced-order-modeling tag-very-exible-aircraft homepage_sections-aerodynamics homepage_sections-fluid-dynamics homepage_sections-systems category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/modal-formulation-for-geometrically-nonlinearstructural-dynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODAL FORMULATION FOR GEOMETRICALLY NONLINEAR STRUCTURAL DYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Renato R. Medeiros, Carlos E. S. Cesnik, Etienne B. Coetzee<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-035<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17742 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-dynamic-stall tag-leading-edge-vortex tag-wind-tunnel-testing homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/dynamic-stall-onset-variation-with-reducedfrequency-for-three-stall-mechanisms\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC STALL ONSET VARIATION WITH REDUCED FREQUENCY FOR THREE STALL MECHANISMS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Boutet Johan, Dimitriadis Grigorios, Amandolese Xavier<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-024<\/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-17463 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-continuous-time-model tag-state-space-model tag-unsteady-aerodynamics tag-unsteady-induced-drag tag-unsteady-vortex-lattice-method homepage_sections-aerodynamics homepage_sections-fluid-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/extension-of-the-continuous-time-unsteady-vortexlattice-method-for-arbitrary-motion-controlsurface-deflection-and-induced-drag-calculation\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXTENSION OF THE CONTINUOUS TIME UNSTEADY VORTEX LATTICE METHOD FOR ARBITRARY MOTION, CONTROL SURFACE DEFLECTION AND INDUCED DRAG 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>Simon Binder, Andreas Wildschek, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-019<\/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-17454 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-adjoint-variables tag-bifurcation tag-flutter tag-sensitivity-analysis homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/fast-prediction-of-flutter-and-flutter-sensitivities\/\" target=&quot;_blank&quot;>\n\t\t\t\tFast Prediction of Flutter and Flutter Sensitivities\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Philip S. Beran, Bret K. Stanford, Kevin G. Wang<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-016<\/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-17439 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelastic-system-identification tag-flutter-prediction homepage_sections-aerodynamics homepage_sections-aircraft-design homepage_sections-fluid-dynamics homepage_sections-materials-and-structures category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/computational-fluid-dynamics-based-aeroelastic-system-identification-and-flutter-prediction\/\" target=&quot;_blank&quot;>\n\t\t\t\tComputational Fluid Dynamics Based Aeroelastic System Identification and Flutter Prediction\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M.Argaman, D.E.Raveh<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-007<\/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<\/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\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 Fluid Dynamics Papers Search &#8230; Results See all results Results Sort&#8230; By title from lowest to highest By title from highest to lowest By date from lowest to highest By date from highest to lowest<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"footnotes":""},"class_list":["post-11440","page","type-page","status-publish","hentry","category-993","category-1957","category-1953","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/11440","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=11440"}],"version-history":[{"count":70,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/11440\/revisions"}],"predecessor-version":[{"id":27503,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/11440\/revisions\/27503"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=11440"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}