{"id":18252,"date":"2024-10-09T23:00:16","date_gmt":"2024-10-09T23:00:16","guid":{"rendered":"https:\/\/aerospacerepository.org\/?page_id=18252"},"modified":"2025-02-25T19:29:12","modified_gmt":"2025-02-25T19:29:12","slug":"repository-ifasd-2015","status":"publish","type":"page","link":"https:\/\/aerospacerepository.org\/index.php\/repository-ifasd-2015\/","title":{"rendered":"Repository IFASD 2015"},"content":{"rendered":"\t\t<div data-elementor-type=\"wp-page\" data-elementor-id=\"18252\" class=\"elementor elementor-18252\" data-elementor-post-type=\"page\">\n\t\t\t\t\t\t<section class=\"elementor-section elementor-top-section elementor-element elementor-element-2c9bccf elementor-section-stretched elementor-section-boxed elementor-section-height-default elementor-section-height-default\" data-id=\"2c9bccf\" data-element_type=\"section\" data-e-type=\"section\" data-settings=\"{&quot;stretch_section&quot;:&quot;section-stretched&quot;,&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t\t\t\t<div class=\"elementor-container elementor-column-gap-default\">\n\t\t\t\t\t<div class=\"elementor-column elementor-col-100 elementor-top-column elementor-element elementor-element-b8dafde\" data-id=\"b8dafde\" data-element_type=\"column\" data-e-type=\"column\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-4b8cde6 elementor-widget elementor-widget-spacer\" data-id=\"4b8cde6\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-37c8102 elementor-widget elementor-widget-heading\" data-id=\"37c8102\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"heading.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<h1 class=\"elementor-heading-title elementor-size-default\"><b> Search all IFASD 2015 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;:[2413],&quot;exclude_terms_ids&quot;:[],&quot;exclude_posts_ids&quot;:[],&quot;custom_fields_source&quot;:&quot;&quot;,&quot;limit_query&quot;:5,&quot;limit_query_tablet&quot;:&quot;&quot;,&quot;limit_query_mobile&quot;:&quot;&quot;,&quot;limit_query_in_result_area&quot;:25,&quot;results_order_by&quot;:&quot;relevance&quot;,&quot;results_order&quot;:&quot;asc&quot;,&quot;sentence&quot;:&quot;yes&quot;,&quot;search_in_taxonomy&quot;:&quot;&quot;,&quot;search_in_taxonomy_source&quot;:&quot;&quot;,&quot;results_area_width_by&quot;:&quot;form&quot;,&quot;results_area_custom_width&quot;:&quot;&quot;,&quot;results_area_custom_position&quot;:&quot;&quot;,&quot;results_area_columns&quot;:1,&quot;results_area_columns_tablet&quot;:&quot;&quot;,&quot;results_area_columns_mobile&quot;:&quot;&quot;,&quot;results_area_columns_mobile_portrait&quot;:&quot;&quot;,&quot;thumbnail_visible&quot;:&quot;yes&quot;,&quot;thumbnail_size&quot;:&quot;thumbnail&quot;,&quot;thumbnail_placeholder&quot;:{&quot;url&quot;:&quot;https:\\\/\\\/aerospacerepository.org\\\/wp-content\\\/plugins\\\/elementor\\\/assets\\\/images\\\/placeholder.png&quot;,&quot;id&quot;:&quot;&quot;,&quot;size&quot;:&quot;&quot;},&quot;post_content_source&quot;:&quot;content&quot;,&quot;post_content_custom_field_key&quot;:&quot;&quot;,&quot;post_content_length&quot;:30,&quot;show_product_price&quot;:&quot;&quot;,&quot;show_product_rating&quot;:&quot;&quot;,&quot;show_add_to_cart&quot;:&quot;&quot;,&quot;show_result_new_tab&quot;:&quot;&quot;,&quot;highlight_searched_text&quot;:&quot;&quot;,&quot;listing_id&quot;:&quot;&quot;,&quot;bullet_pagination&quot;:&quot;&quot;,&quot;number_pagination&quot;:&quot;&quot;,&quot;navigation_arrows&quot;:&quot;in_header&quot;,&quot;navigation_arrows_type&quot;:&quot;angle&quot;,&quot;show_title_related_meta&quot;:&quot;&quot;,&quot;meta_title_related_position&quot;:&quot;&quot;,&quot;title_related_meta&quot;:&quot;&quot;,&quot;show_content_related_meta&quot;:&quot;&quot;,&quot;meta_content_related_position&quot;:&quot;&quot;,&quot;content_related_meta&quot;:&quot;&quot;,&quot;negative_search&quot;:&quot;Sorry, but nothing matched your search terms.&quot;,&quot;server_error&quot;:&quot;Sorry, but we cannot handle your search query now. Please, try again later!&quot;,&quot;show_search_suggestions&quot;:&quot;&quot;,&quot;search_suggestions_position&quot;:&quot;&quot;,&quot;search_suggestions_source&quot;:&quot;&quot;,&quot;search_suggestions_limits&quot;:&quot;&quot;,&quot;search_suggestions_item_title_length&quot;:&quot;&quot;,&quot;search_source_terms&quot;:&quot;&quot;,&quot;search_source_terms_title&quot;:&quot;&quot;,&quot;search_source_terms_icon&quot;:&quot;&quot;,&quot;search_source_terms_limit&quot;:&quot;&quot;,&quot;search_source_terms_listing_id&quot;:&quot;&quot;,&quot;search_source_terms_taxonomy&quot;:&quot;&quot;,&quot;search_source_users&quot;:&quot;&quot;,&quot;search_source_users_title&quot;:&quot;&quot;,&quot;search_source_users_icon&quot;:&quot;&quot;,&quot;search_source_users_limit&quot;:&quot;&quot;,&quot;search_source_users_listing_id&quot;:&quot;&quot;}\"><form class=\"jet-ajax-search__form\" method=\"get\" action=\"https:\/\/aerospacerepository.org\/\" role=\"search\" target=\"\">\n\t<div class=\"jet-ajax-search__fields-holder\">\n\t\t<div class=\"jet-ajax-search__field-wrapper\">\n\t\t\t<label for=\"search-input-28eb3a3\" class=\"screen-reader-text\">Search ...<\/label>\n\t\t\t\t\t\t<input id=\"search-input-28eb3a3\" class=\"jet-ajax-search__field\" type=\"search\" placeholder=\"Search all IFASD 2015 Papers...\" value=\"\" name=\"s\" autocomplete=\"off\" \/>\n\t\t\t\t\t\t\t<input type=\"hidden\" value=\"{&quot;include_terms_ids&quot;:[2413],&quot;sentence&quot;:true}\" name=\"jet_ajax_search_settings\" \/>\n\t\t\t\t\t\t\n\t\t\t\t\t<\/div>\n\t\t\t<\/div>\n\t\n<button class=\"jet-ajax-search__submit\" type=\"submit\" aria-label=\"Search submit\"><span class=\"jet-ajax-search__submit-icon jet-ajax-search-icon\"><i aria-hidden=\"true\" class=\"fas fa-search\"><\/i><\/span><\/button>\n<\/form>\n\n<div class=\"jet-ajax-search__results-area\" >\n\t<div class=\"jet-ajax-search__results-holder\">\n\t\t\t\t\t<div class=\"jet-ajax-search__results-header\">\n\t\t\t\t\n<button class=\"jet-ajax-search__results-count\" aria-label=\"View all results\"><span><\/span> Results<\/button>\n\t\t\t\t<div class=\"jet-ajax-search__navigation-holder\"><\/div>\n\t\t\t<\/div>\n\t\t\t\t\t\t<div class=\"jet-ajax-search__results-list results-area-col-desk-1 results-area-col-tablet-0 results-area-col-mobile-0 results-area-col-mobile-portrait-1\" >\n\t\t\t            <div class=\"jet-ajax-search__results-list-inner \"><\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t\t<div class=\"jet-ajax-search__results-footer\">\n\t\t\t\t\t\t\t\t\t<button class=\"jet-ajax-search__full-results\">See all results<\/button>\t\t\t\t\t\t\t\t<div class=\"jet-ajax-search__navigation-holder\"><\/div>\n\t\t\t<\/div>\n\t\t\t<\/div>\n\t<div class=\"jet-ajax-search__message\"><\/div>\n\t\n<div class=\"jet-ajax-search__spinner-holder\">\n\t<div class=\"jet-ajax-search__spinner\">\n\t\t<div class=\"rect rect-1\"><\/div>\n\t\t<div class=\"rect rect-2\"><\/div>\n\t\t<div class=\"rect rect-3\"><\/div>\n\t\t<div class=\"rect rect-4\"><\/div>\n\t\t<div class=\"rect rect-5\"><\/div>\n\t<\/div>\n<\/div>\n<\/div>\n<\/div>\n<\/div>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-e6a0308 elementor-widget elementor-widget-spacer\" data-id=\"e6a0308\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t<section class=\"elementor-section elementor-top-section elementor-element elementor-element-5406a7d elementor-section-stretched elementor-section-boxed elementor-section-height-default elementor-section-height-default\" data-id=\"5406a7d\" data-element_type=\"section\" data-e-type=\"section\" data-settings=\"{&quot;stretch_section&quot;:&quot;section-stretched&quot;,&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t\t\t\t<div class=\"elementor-container elementor-column-gap-default\">\n\t\t\t\t\t<div class=\"elementor-column elementor-col-25 elementor-top-column elementor-element elementor-element-f9cb2de\" data-id=\"f9cb2de\" data-element_type=\"column\" data-e-type=\"column\" data-settings=\"{&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-1c7c89c elementor-widget elementor-widget-spacer\" data-id=\"1c7c89c\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-962fb9c elementor-widget elementor-widget-heading\" data-id=\"962fb9c\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"heading.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<h4 class=\"elementor-heading-title elementor-size-default\">Search by Event Topic<\/h4>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-d23dc2a elementor-widget elementor-widget-spacer\" data-id=\"d23dc2a\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-e6e888c elementor-widget elementor-widget-jet-smart-filters-checkboxes\" data-id=\"e6e888c\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"jet-smart-filters-checkboxes.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<div class=\"jet-smart-filters-checkboxes jet-filter \" data-indexer-rule=\"show\" data-show-counter=\"\" data-change-counter=\"always\"><div class=\"jet-checkboxes-list\" data-query-type=\"tax_query\" data-query-var=\"category\" data-smart-filter=\"checkboxes\" data-filter-id=\"18275\" data-apply-type=\"ajax\" data-content-provider=\"epro-posts\" data-additional-providers=\"\" data-query-id=\"default\" data-active-label=\"\" data-layout-options=\"{&quot;show_label&quot;:&quot;&quot;,&quot;display_options&quot;:{&quot;show_items_label&quot;:false,&quot;show_decorator&quot;:&quot;yes&quot;,&quot;filter_image_size&quot;:&quot;full&quot;,&quot;show_counter&quot;:false}}\" data-query-var-suffix=\"\" data-apply-on=\"value\">\n\t<fieldset class=\"jet-checkboxes-list-wrapper\"><legend style=\"display:none;\">IFASD2015<\/legend><div class=\"jet-list-tree\"><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2416\"\n\t\t\tdata-label=\"Aerodynamics\/CFD\"\n\t\t\t\t\t\taria-label=\"Aerodynamics\/CFD\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAerodynamics\/CFD\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2415\"\n\t\t\tdata-label=\"Aeroelastic Optimisation\"\n\t\t\t\t\t\taria-label=\"Aeroelastic Optimisation\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroelastic Optimisation\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2422\"\n\t\t\tdata-label=\"Aeroelastic Response &amp; Stability\"\n\t\t\t\t\t\taria-label=\"Aeroelastic Response &amp; Stability\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroelastic Response &amp; Stability\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2423\"\n\t\t\tdata-label=\"Aeroelasticity in Aircraft Design\"\n\t\t\t\t\t\taria-label=\"Aeroelasticity in Aircraft Design\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroelasticity in Aircraft Design\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2424\"\n\t\t\tdata-label=\"Aeroelasticity of Morphing Aircraft\"\n\t\t\t\t\t\taria-label=\"Aeroelasticity of Morphing Aircraft\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroelasticity of Morphing Aircraft\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2414\"\n\t\t\tdata-label=\"Aeroservoelasticity\"\n\t\t\t\t\t\taria-label=\"Aeroservoelasticity\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroservoelasticity\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2425\"\n\t\t\tdata-label=\"Aeroservoelasticity &amp; Active Control\"\n\t\t\t\t\t\taria-label=\"Aeroservoelasticity &amp; Active Control\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tAeroservoelasticity &amp; Active Control\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2419\"\n\t\t\tdata-label=\"Computational Aeroelasticity\"\n\t\t\t\t\t\taria-label=\"Computational Aeroelasticity\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tComputational Aeroelasticity\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2426\"\n\t\t\tdata-label=\"Crashworthiness\"\n\t\t\t\t\t\taria-label=\"Crashworthiness\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tCrashworthiness\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2421\"\n\t\t\tdata-label=\"Experimental Methods\"\n\t\t\t\t\t\taria-label=\"Experimental Methods\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tExperimental Methods\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2427\"\n\t\t\tdata-label=\"Experimental Methods &amp; Bridges\"\n\t\t\t\t\t\taria-label=\"Experimental Methods &amp; Bridges\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tExperimental Methods &amp; Bridges\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2428\"\n\t\t\tdata-label=\"GVT &amp; Flight Test\"\n\t\t\t\t\t\taria-label=\"GVT &amp; Flight Test\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tGVT &amp; Flight Test\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2420\"\n\t\t\tdata-label=\"Loads\"\n\t\t\t\t\t\taria-label=\"Loads\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tLoads\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2429\"\n\t\t\tdata-label=\"Loads Alleviation\"\n\t\t\t\t\t\taria-label=\"Loads Alleviation\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tLoads Alleviation\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2417\"\n\t\t\tdata-label=\"Nonlinearities &amp; Uncertainties\"\n\t\t\t\t\t\taria-label=\"Nonlinearities &amp; Uncertainties\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tNonlinearities &amp; Uncertainties\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2430\"\n\t\t\tdata-label=\"Poster presentations\"\n\t\t\t\t\t\taria-label=\"Poster presentations\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tPoster presentations\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2418\"\n\t\t\tdata-label=\"Reduced Order Modelling\"\n\t\t\t\t\t\taria-label=\"Reduced Order Modelling\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tReduced Order Modelling\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2431\"\n\t\t\tdata-label=\"Rotation System\"\n\t\t\t\t\t\taria-label=\"Rotation System\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tRotation System\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><div class=\"jet-checkboxes-list__row jet-filter-row\">\n\t\t<label\n\t\tclass=\"jet-checkboxes-list__item\"\n\t\t\t>\n\t\t<input\n\t\t\ttype=\"checkbox\"\n\t\t\tclass=\"jet-checkboxes-list__input\"\n\t\t\tname=\"category\"\n\t\t\tvalue=\"2432\"\n\t\t\tdata-label=\"Structural Dynamics &amp; Shimmy\"\n\t\t\t\t\t\taria-label=\"Structural Dynamics &amp; Shimmy\"\n\t\t\t\t\t>\n\t\t<div class=\"jet-checkboxes-list__button\">\n\t\t\t\t\t\t\t<span class=\"jet-checkboxes-list__decorator\">\n\t\t\t\t\t<i class=\"jet-checkboxes-list__checked-icon\">\n\t\t\t\t\t\t<svg width=\"28\" height=\"28\" viewBox=\"0 0 28 28\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\">\n\t<path d=\"M26.109 8.844c0 0.391-0.156 0.781-0.438 1.062l-13.438 13.438c-0.281 0.281-0.672 0.438-1.062 0.438s-0.781-0.156-1.062-0.438l-7.781-7.781c-0.281-0.281-0.438-0.672-0.438-1.062s0.156-0.781 0.438-1.062l2.125-2.125c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l4.594 4.609 10.25-10.266c0.281-0.281 0.672-0.438 1.062-0.438s0.781 0.156 1.062 0.438l2.125 2.125c0.281 0.281 0.438 0.672 0.438 1.062z\"><\/path>\n<\/svg>\n\t\t\t\t\t<\/i>\n\t\t\t\t<\/span>\n\t\t\t\t\t\t<span class=\"jet-checkboxes-list__label\">\n\t\t\t\tStructural Dynamics &amp; Shimmy\t\t\t<\/span>\n\t\t\t\t\t<\/div>\n\t<\/label>\n<\/div><\/div><\/fieldset><\/div>\n<\/div>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-217e6ca elementor-widget elementor-widget-spacer\" data-id=\"217e6ca\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-d8b18a0 elementor-widget elementor-widget-spacer\" data-id=\"d8b18a0\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-1fac479 elementor-widget elementor-widget-spacer\" data-id=\"1fac479\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-fa9661a elementor-widget elementor-widget-spacer\" data-id=\"fa9661a\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-5432385 elementor-widget elementor-widget-spacer\" data-id=\"5432385\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-667366d elementor-widget elementor-widget-spacer\" data-id=\"667366d\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-7047487 elementor-widget elementor-widget-spacer\" data-id=\"7047487\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-ee10ab8 elementor-widget elementor-widget-spacer\" data-id=\"ee10ab8\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-5ffe419 elementor-widget elementor-widget-spacer\" data-id=\"5ffe419\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-ab572bb elementor-widget elementor-widget-spacer\" data-id=\"ab572bb\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-e20ec19 elementor-widget elementor-widget-spacer\" data-id=\"e20ec19\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t<div class=\"elementor-column elementor-col-50 elementor-top-column elementor-element elementor-element-3a3cb99\" data-id=\"3a3cb99\" data-element_type=\"column\" data-e-type=\"column\" data-settings=\"{&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-c7b2ceb elementor-widget elementor-widget-spacer\" data-id=\"c7b2ceb\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-fb80527 elementor-widget elementor-widget-heading\" data-id=\"fb80527\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"heading.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<h2 class=\"elementor-heading-title elementor-size-default\">Results<\/h2>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-424a040 elementor-widget elementor-widget-jet-smart-filters-active hide-widget\" data-id=\"424a040\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"jet-smart-filters-active.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<div class=\"jet-smart-filters-active jet-active-filters jet-filter\" data-label=\"Active filters:\" data-content-provider=\"epro-posts\" data-additional-providers=\"\" data-apply-type=\"ajax\" data-query-id=\"default\"><\/div>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-03c22e8 elementor-widget elementor-widget-jet-smart-filters-sorting\" data-id=\"03c22e8\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"jet-smart-filters-sorting.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t<div class=\"jet-smart-filters-sorting jet-filter\"><div\n\tclass=\"jet-sorting jet-sorting--flex-column\"\n\t data-smart-filter=\"sorting\" data-query-type=\"sort\" data-query-var=\"standard\" data-content-provider=\"epro-posts\" data-query-id=\"default\" data-apply-type=\"ajax\" data-apply-on=\"value\" data-additional-providers=\"\">\n\t\t<select\n\t\tclass=\"jet-sorting-select\"\n\t\tname=\"select-name\"\n\t\t\t\taria-label=\"Sort filter\"\n\t>\n\t\t\t\t\t<option value=\"\">\n\t\t\t\tSort...\t\t\t<\/option>\n\t\t\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;title&quot;,&quot;order&quot;:&quot;ASC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy title from lowest to highest\t\t\t<\/option>\n\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;title&quot;,&quot;order&quot;:&quot;DESC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy title from highest to lowest\t\t\t<\/option>\n\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;date&quot;,&quot;order&quot;:&quot;ASC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy date from lowest to highest\t\t\t<\/option>\n\t\t\t\t\t<option\n\t\t\t\tvalue=\"{&quot;orderby&quot;:&quot;date&quot;,&quot;order&quot;:&quot;DESC&quot;}\"\n\t\t\t\t\t\t\t>\n\t\t\t\tBy date from highest to lowest\t\t\t<\/option>\n\t\t\t<\/select>\n<\/div>\n<\/div>\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-5b3ecaf elementor-grid-1 elementor-grid-tablet-2 elementor-grid-mobile-1 elementor-posts--thumbnail-top elementor-card-shadow-yes elementor-posts__hover-gradient elementor-widget elementor-widget-posts\" data-id=\"5b3ecaf\" data-element_type=\"widget\" data-e-type=\"widget\" data-settings=\"{&quot;cards_columns&quot;:&quot;1&quot;,&quot;pagination_type&quot;:&quot;load_more_infinite_scroll&quot;,&quot;cards_row_gap&quot;:{&quot;unit&quot;:&quot;px&quot;,&quot;size&quot;:13,&quot;sizes&quot;:[]},&quot;cards_columns_tablet&quot;:&quot;2&quot;,&quot;cards_columns_mobile&quot;:&quot;1&quot;,&quot;cards_row_gap_tablet&quot;:{&quot;unit&quot;:&quot;px&quot;,&quot;size&quot;:&quot;&quot;,&quot;sizes&quot;:[]},&quot;cards_row_gap_mobile&quot;:{&quot;unit&quot;:&quot;px&quot;,&quot;size&quot;:&quot;&quot;,&quot;sizes&quot;:[]},&quot;load_more_spinner&quot;:{&quot;value&quot;:&quot;fas fa-spinner&quot;,&quot;library&quot;:&quot;fa-solid&quot;}}\" data-widget_type=\"posts.cards\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-posts-container elementor-posts elementor-posts--skin-cards elementor-grid\">\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18289 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 tag-model-updation tag-multi-objective-optimization tag-servoelastic-response category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/multiobjective-optimization-for-servoelastic-response-predictions-of-a-fly-by-wire-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tMULTIOBJECTIVE OPTIMIZATION FOR SERVOELASTIC RESPONSE PREDICTIONS OF A FLY-BY-WIRE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Prabha Srinivasan, Ashok Joshi, Hemalatha E<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-001<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18292 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-aeroelastic-optimization tag-composite-wing tag-high-efficiency tag-kriging-model category-2413 category-2415 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/a-high-efficiency-aeroelastic-optimization-method-based-on-kriging-model-and-genetic-algorithm\/\" target=&quot;_blank&quot;>\n\t\t\t\tA HIGH-EFFICIENCY AEROELASTIC OPTIMIZATION METHOD BASED ON KRIGING MODEL AND GENETIC ALGORITHM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Wang Xiaozhe, Wan Zhiqiang, Yang Chao<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-002<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18298 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-high-aspect-ratio-wings-2 tag-nonlinear-aeroelasticity tag-simulation category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/aeroelastic-modeling-and-simulation-of-flexible-jet-transport-aircraft-with-high-aspect-ratio-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC MODELING AND SIMULATION OF FLEXIBLE JET TRANSPORT AIRCRAFT WITH HIGH-ASPECT-RATIO WINGS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ryan C. Kitson, Carlos E. S. Cesnik<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-005<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18301 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-reduced-order-modelling tag-geometric-nonlinearities tag-reduced-order-model-2 tag-static-aeroelasticity tag-trim-analysis 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-18307 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-cumulative-fatigue-damage tag-flight-parameters tag-variable-loads category-2413 category-2420 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/flight-loads-and-cumulative-fatique-damages-monitoring-for-each-aircraft-during-service-life\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT LOADS AND CUMULATIVE FATIQUE DAMAGES MONITORING FOR EACH AIRCRAFT DURING SERVICE LIFE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Victor I. Kleptsov , Vladimir I. Tsimbalyuk , Tatiana I. Orlova<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-008<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18310 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-bifurcation tag-freeplay tag-limit-cycle-oscillations tag-nonlinear-aeroelasticity category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/asymmetric-limit-cycle-oscillations-in-systems-with-symmetric-freeplay\/\" target=&quot;_blank&quot;>\n\t\t\t\tAsymmetric limit cycle oscillations in systems with symmetric freeplay\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Grigorios Dimitriadis<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-009<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18313 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 tag-co-design tag-control-vector-parametrisation tag-gebm tag-mdo tag-mdsdo tag-open-loop-control tag-optimisation tag-single-shooting category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/co-design-of-very-flexible-actuated-structures\/\" target=&quot;_blank&quot;>\n\t\t\t\tCO-DESIGN OF VERY FLEXIBLE ACTUATED STRUCTURES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Salvatore Maraniello, Rafael Palacios<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-010<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-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 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-18322 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-aeroelasticity tag-typical-section tag-viscoelastic-damping category-2413 category-2422 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/a-parametric-and-topological-study-on-the-use-of-viscoelastic-material-for-flutter-suppression\/\" target=&quot;_blank&quot;>\n\t\t\t\tA PARAMETRIC AND TOPOLOGICAL STUDY ON THE USE OF VISCOELASTIC MATERIAL FOR FLUTTER SUPPRESSION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Gabriel I. Barbejat, Maur\u00edcio V. Donadon, Roberto G. Silva, Antonio M. G. de Lima, Andr\u00e9 G.C. Filho, Leandro S. Le\u00e3o<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-013<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-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-2 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-18331 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-of-morphing-aircraft tag-compliant-structure tag-morphing-aircraft tag-morphing-winglet category-2413 category-2424 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/investigating-the-benefits-of-morphing-wing-tip-devices-a-case-study\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATING THE BENEFITS OF MORPHING WING TIP DEVICES A CASE STUDY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Chen Wang, Hamed Haddad Khodaparast, Michael I Friswell<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-018<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18335 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-adjoint-technique tag-aeroelastic-gradient tag-optimization category-2413 category-2415 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/recent-achievements-towards-aero-structure-gradient-computation-using-high-fidelity-cfd-csm-in-the-onera-elsa-software\/\" target=&quot;_blank&quot;>\n\t\t\t\tRECENT ACHIEVEMENTS TOWARDS AERO-STRUCTURE GRADIENT COMPUTATION USING HIGH-FIDELITY CFD-CSM IN THE ONERA ELSA SOFTWARE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>C. Blondeau, T. Achard, P. Girodroux-Lavigne, R. Ohayon<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-019<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18338 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-of-morphing-aircraft tag-eigenanalysis tag-generalized-beam-models tag-jordan-form tag-wing-morphing category-2413 category-2424 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/a-generalized-beam-formulation-for-the-dynamic-analysis-of-camber-morphing-helicopter-blades\/\" target=&quot;_blank&quot;>\n\t\t\t\tA GENERALIZED BEAM FORMULATION FOR THE DYNAMIC ANALYSIS OF CAMBER-MORPHING HELICOPTER BLADES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Luca Cirrottola, Marco Morandini, Giuseppe Quaranta<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-020<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18341 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-aeroelastic-deformation tag-cror tag-experimental-measurement tag-spa category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/cror-blade-deformation-part-1-experimental-results-by-strain-pattern-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tCROR BLADE DEFORMATION, PART 1: EXPERIMENTAL RESULTS BY STRAIN PATTERN ANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. GEERAERT, C. STEPHAN<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-023<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18344 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-finite-element-model-updating tag-ground-vibration-testing tag-modal-identification tag-phase-resonance-method tag-phase-separation-method tag-structural-nonlinearities category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/airbus-a320-neo-gvt-and-fem-updating-state-of-the-art-techniques-to-perform-an-industrial-vibration-test-campaign-and-a-rapid-process-to-update-renewed-fem-for-clearance-of-first-flight-test\/\" target=&quot;_blank&quot;>\n\t\t\t\tAIRBUS A320 NEO GVT AND FEM UPDATING STATE-OF-THE-ART TECHNIQUES TO PERFORM AN INDUSTRIAL VIBRATION TEST CAMPAIGN AND A RAPID PROCESS TO UPDATE RENEWED FEM FOR CLEARANCE OF FIRST FLIGHT TEST\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>C. Stephan , T-P Vo-Hoang , S. Giclais , Y. Govers , P. Lubrina , M. Boeswald , A. Laporte<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-024<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18347 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-active-twist-blade tag-individual-blade-control tag-output-feedback tag-periodic-control category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/periodic-output-feedback-control-for-helicopter-vibration-reduction\/\" target=&quot;_blank&quot;>\n\t\t\t\tPERIODIC OUTPUT FEEDBACK CONTROL FOR HELICOPTER VIBRATION REDUCTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Claudio Brillante, Marco Morandini, Paolo Mantegazza<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-025<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18353 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-crashworthiness tag-ditching tag-fluid-structure-interaction tag-structural-dynamics category-2413 category-2426 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/numerical-simulation-of-ditching-dynamic-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL SIMULATION OF DITCHING DYNAMIC LOADS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>J. T. Viana, J. Romera, G. Pastor, L. Ben\u00edtez, H. Climent, M. H. Siemann<\/b><\/p>\n<p>DOI Number; N\/A<\/p>\n<p>Conference number: IFASD-2015-028<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18359 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-aeroelasticity tag-mdo tag-parametric-studies tag-shape-optimization tag-strength category-2413 category-2423 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/aeroelastic-optimization-of-wing-shape-and-structural-parameters-for-different-aircraft-configurations\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC OPTIMIZATION OF WING SHAPE AND STRUCTURAL PARAMETERS FOR DIFFERENT AIRCRAFT CONFIGURATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kirill A. Balunov, Vasily V. Chedrik, Fanil Z. Ishmuratov, Petr G. Karkle<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-034<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18362 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-f-16-aircraft tag-ground-vibration-testing tag-sine-sweep-excitation tag-structural-nonlinearities category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/nonlinear-ground-vibration-identification-of-an-f-16-aircraft-part-ii-understanding-nonlinear-behaviour-in-aerospace-structures-using-sine-sweep-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR GROUND VIBRATION IDENTIFICATION OF AN F-16 AIRCRAFT PART II: UNDERSTANDING NONLINEAR BEHAVIOUR IN AEROSPACE STRUCTURES USING SINE-SWEEP TESTING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Dossogne, J.P. No\u00ebl, C. Grappasonni, G. Kerschen, B. Peeters, J. Debille, M. Vaes, J. Schoukens<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-035<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18365 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-dynamic-loads tag-run tag-structural-damping tag-turbulence category-2413 category-2420 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/influence-of-structural-damping-on-airplane-dynamic-loads-at-flight-in-turbulence-and-at-run\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF STRUCTURAL DAMPING ON AIRPLANE DYNAMIC LOADS AT FLIGHT IN TURBULENCE AND AT RUN\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Oleg A. Kuznetsov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-036<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-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 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-18374 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-active-control tag-aeroservoelasticity tag-dynamic-stiffness tag-flutter tag-horizontal-stabilizer tag-link category-2413 category-2425 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/nonlinear-aeroservoelastic-analysis-for-a-three-dimensional-horizontal-stabilizer-with-an-actuator-composed-of-elastic-links\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR AEROSERVOELASTIC ANALYSIS FOR A THREE DIMENSIONAL HORIZONTAL STABILIZER WITH AN ACTUATOR COMPOSED OF ELASTIC LINKS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yoo Jin Kang, Chan Hoon Chung, Jae Hyeok Jeon, Sang Joon Shin, Young Ho Na<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-039<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18380 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-aeroelasticity tag-experimental tag-polynomial-chaos-expansion-structural-dynamics tag-validation category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/sensor-calibration-for-calculation-of-loads-on-a-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tSENSOR CALIBRATION FOR CALCULATION OF LOADS ON A FLEXIBLE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Marcus Vinicius P. Viana<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-042<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18383 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-aeroelasticity tag-experimental tag-structural-dynamics tag-validation category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/cror-blade-deformation-part-2-aeroelastic-computations-and-comparison-with-experiments\/\" target=&quot;_blank&quot;>\n\t\t\t\tCROR BLADE DEFORMATION, PART 2: AEROELASTIC COMPUTATIONS AND COMPARISON WITH EXPERIMENTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Y. Mauffrey, A. Geeraert, S. Verley<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-043<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18386 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-non-linear-modelling tag-vortex-induced-vibration 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-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-2 tag-limit-cycle-oscillation-2 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-18394 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-dynamic-behavior tag-lattice-composite-structures tag-unidirectional-composite category-2413 category-2423 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/modeling-of-dynamic-behavior-of-lattice-composite-aircraft-structures\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODELING OF DYNAMIC BEHAVIOR OF LATTICE COMPOSITE AIRCRAFT STRUCTURES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. Bezuevsky, I. Kondakov, A. Shanygin, M. Zichenkov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-049<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18402 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-cfd-csm tag-folding-wing-tip-2 tag-load-alleviation tag-simulation category-2413 category-2423 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/high-fidelity-simulation-of-the-folding-wing-tip-for-loads-alleviaton\/\" target=&quot;_blank&quot;>\n\t\t\t\tHIGH FIDELITY SIMULATION OF THE FOLDING WING TIP FOR LOADS ALLEVIATON\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>John Pattinson, Thomas Wilson, Martin Herring<\/b><\/p>\n<p>DOI number: N\/A<\/p>\n<p>Conference number: IFASD-2015-052<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18404 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-elastically-scaled-models tag-fem tag-influence-coefficient-matrix tag-optimization tag-static-aeroelasticity category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/designing-of-elastically-scaled-model-of-a-high-acpect-ratio-wing-using-digital-technologies\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGNING OF ELASTICALLY SCALED MODEL OF A HIGH ACPECT RATIO WING USING DIGITAL TECHNOLOGIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>O. Orlova<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-053<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18408 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/nonlinear-actuator-modeling-for-aeroservoelastic-dynamic-loads-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tNonlinear Actuator Modeling for Aeroservoelastic Dynamic Loads Simulations\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Rami Veiberman, Martin Weiss, Moti Karpel<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-054<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18411 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-aeroelasticity tag-buckling tag-finite-element-model-layout tag-structural-optimization tag-structural-strength tag-topology-optimization category-2413 category-2415 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/evolutionary-approach-to-structural-design-of-wing-under-stress-buckling-and-aeroelasticity-requirements\/\" target=&quot;_blank&quot;>\n\t\t\t\tEVOLUTIONARY APPROACH TO STRUCTURAL DESIGN OF WING UNDER STRESS, BUCKLING AND AEROELASTICITY REQUIREMENTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vasily V. Chedrik, Sergey A. Tuktarov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-055<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18414 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads-alleviation tag-aeroelastic-testing tag-gust-load-alleviation tag-wind-tunnel-testing category-2413 category-2429 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/wind-tunnel-experimental-validation-of-future-green-regional-a-c-gust-load-alleviation-control-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tWIND TUNNEL EXPERIMENTAL VALIDATION OF FUTURE GREEN REGIONAL A\/C GUST LOAD ALLEVIATION CONTROL SYSTEM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>S. Ricci, S.Adden, C.Servadio, M.Karpel, J.Cooper<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-057<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18417 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-aeroelasticity tag-control-surface tag-frequency-response tag-geared-tab tag-structural-dynamics category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/influence-of-the-structural-elasticity-on-the-static-and-dynamic-effectiveness-of-control-surfaces-with-the-geared-tab\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF THE STRUCTURAL ELASTICITY ON THE STATIC AND DYNAMIC EFFECTIVENESS OF CONTROL SURFACES WITH THE GEARED TAB\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Olga V. Zubakova , Mikhail C. Zichenkov, Anatoly V. Zubakov, Fanil Z. Ishmuratov, Yuri A. Nayko, Alexander V. Khalo<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-059<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18420 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-loads tag-state-space tag-unsteady-aerodynamics 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-18423 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-dynamically-scaled-model tag-flutter tag-ground-vibration-tests-gvt tag-influence-coefficient-matrix tag-suchoi-ssj-100 category-2413 category-2423 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/experience-of-flutter-clearance-of-the-suchoi-ssj-100-regional-jet\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIENCE OF FLUTTER CLEARANCE OF THE SUCHOI SSJ 100 REGIONAL JET\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alexey E. Orlov, Sergey E. Paryshev, Sergey V. Shalaev, Sergey I. Kalabuchov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-061<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18426 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads-alleviation tag-aeroelastic-constraint-optimization tag-dynamic-aircraft-model tag-gust-analysis tag-manoeuver-loads category-2413 category-2429 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/aeroelastic-analysis-modelling-process-to-predict-the-critical-loads-in-an-mdo-environment\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC ANALYSIS MODELLING PROCESS TO PREDICT THE CRITICAL LOADS IN AN MDO ENVIRONMENT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ren\u00e9 Liepelt, Vega Handojo, Thomas Klimmek<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-062<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18429 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-aeroelastic tag-geometric-nonlinearity tag-static-stability tag-trim category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/the-aeroelastic-trim-and-static-stability-analysis-of-highly-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHE AEROELASTIC TRIM AND STATIC STABILITY ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Hu Rui, Xie Changchuan, Liu Yi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p> Conference Number: IFASD-2015-064<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18434 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-aeroelastic tag-high-aspect-ratio-wing tag-sensitivity-analysis tag-stiffness-design tag-structural-optimization category-2413 category-2423 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/stiffness-distribution-and-aeroelastic-performance-optimization-of-high-aspect-ratio-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTIFFNESS DISTRIBUTION AND AEROELASTIC PERFORMANCE OPTIMIZATION OF HIGH-ASPECT-RATIO WINGS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Du Ziliang, Wan Zhiqiang, Yang Chao<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-067<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18438 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-fixed-axis tag-flexible-aircraft-dynamics tag-flight-simulation tag-gaf tag-mean-axis tag-uvlm category-2413 category-2422 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/a-comparison-of-modeling-methods-for-the-simulation-of-free-flying-elastic-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tA COMPARISON OF MODELING METHODS FOR THE SIMULATION OF FREE FLYING ELASTIC AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>K. Seywald, A. Wildschek, F. Holzapfel<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-068<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18441 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-crashworthiness tag-a400m tag-dynamic-loads tag-landing-gear tag-uerf category-2413 category-2426 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/18\/certification-of-landing-gear-structure-under-uerf-event\/\" target=&quot;_blank&quot;>\n\t\t\t\tCERTIFICATION OF LANDING GEAR STRUCTURE UNDER UERF EVENT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Gomez Vinas, Esteban, Chorro Matinez. J.Manuel, Martinez Perez Angel, Perez Hernandez, J.M, Perez San Jose, Jorge<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-069<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18448 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 tag-dielectric-elastomers tag-feedback-control tag-fluid-structure-interaction tag-hyperelastic tag-low-reynolds tag-reduced-order-modelling tag-system-identication category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/reduced-order-modelling-and-feedback-control-of-integrally-actuated-membrane-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tREDUCED-ORDER MODELLING AND FEEDBACK CONTROL OF INTEGRALLY ACTUATED MEMBRANE WINGS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Stefano Buoso, Rafael Palacios<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-072<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18451 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-landing-gear tag-local-non-linearity tag-shimmy category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/shimmy-of-wheels-of-landing-gear-of-aircraft-with-local-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tSHIMMY OF WHEELS OF LANDING GEAR OF AIRCRAFT WITH LOCAL 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>A.V. Krapivko<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-073<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18454 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 tag-damping-coefficients tag-natural-frequencies tag-refueling-system category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/dynamic-stability-of-a-hose-drogue-wing-system-for-aerial-refueling\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC STABILITY OF A HOSE-DROGUE-WING SYSTEM FOR AERIAL REFUELING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>P. Garc\u00eda-Fogeda, F. Ar\u00e9valo<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-074<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18457 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-mdo tag-moga-ii tag-moo tag-pareto-frontier tag-sqp tag-wgc category-2413 category-2415 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/genetic-and-gradient-based-algorithms-for-the-multi-objective-optimization-of-aircraft-design-with-aeroelastic-constraints\/\" target=&quot;_blank&quot;>\n\t\t\t\tGENETIC AND GRADIENT-BASED ALGORITHMS FOR THE MULTI-OBJECTIVE OPTIMIZATION OF AIRCRAFT DESIGN WITH AEROELASTIC CONSTRAINTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Stefania Gemma, Franco Mastroddi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-075<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18460 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-aeroelastic tag-flutter tag-geometric-nonlinearity tag-high-aspect-ratio category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/geometrical-nonlinear-aeroelastic-analysis-of-large-aircraft-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tGEOMETRICAL NONLINEAR AEROELASTIC ANALYSIS OF LARGE AIRCRAFT WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Zhang Chao, He Jingwu , Xie Changchuan, Liu Yi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-076<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18463 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads-alleviation tag-aeroelasticity tag-gust-load-alleviation tag-probability tag-robust category-2413 category-2429 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/probabilistic-robust-control-strategy-for-gust-load-alleviation\/\" target=&quot;_blank&quot;>\n\t\t\t\tProbabilistic Robust Control Strategy for Gust Load Alleviation\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yuting Dai, Chao Yang, Chaolei Wang<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-077<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18469 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-curved-timoshenko-beams tag-isogeometric-analysis tag-low-fidelity-aeroelasticity tag-morphing-airfoil tag-potential-flow category-2413 category-2415 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/low-fidelity-2d-isogeometric-aeroelastic-optimization-with-application-to-a-morphing-airfoil\/\" target=&quot;_blank&quot;>\n\t\t\t\tLOW-FIDELITY 2D ISOGEOMETRIC AEROELASTIC OPTIMIZATION WITH APPLICATION TO A MORPHING AIRFOIL\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Erik Gillebaart, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-079<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18472 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-evolutionary tag-flutter tag-optimisation tag-topology category-2413 category-2415 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/a-novel-method-for-the-vibration-optimisation-of-structures-subjected-to-dynamic-loading\/\" target=&quot;_blank&quot;>\n\t\t\t\tA Novel Method for the Vibration Optimisation of Structures Subjected to Dynamic Loading\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>David J. Munk, Gareth A. Vio, Grant P. Steven<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-081<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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-2 tag-unsteady-aerodynamics 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-18478 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-structural-dynamics-shimmy tag-coupling tag-landing-gear tag-modal-analysis-2 tag-shimmy tag-structural-dynamics category-2413 category-2432 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/study-of-shimmy-in-industrial-context\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTUDY OF SHIMMY IN INDUSTRIAL CONTEXT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ludovic MARTIN, Vincent JACQUES, Yves MARTIN-SIEGFRIED<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-083<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18481 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-couple tag-dynamic-response tag-gust tag-hale tag-nonlinear category-2413 category-2420 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/gust-response-analysis-of-high-altitude-long-endurance-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tGUST RESPONSE ANALYSIS OF HIGH ALTITUDE, LONG ENDURANCE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Chen Zhanjun, Fu Zhichao, Lv Jinan, Liu Ziqiang<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-086<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18484 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-component-wise tag-composites tag-free-vibrations tag-higher-order-beam-models tag-wing-box category-2413 category-2423 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/enhanced-free-vibration-analysis-of-composite-wingbox-structures-by-one-dimensional-component-wise-and-dynamic-stiffness-formulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tENHANCED FREE VIBRATION ANALYSIS OF COMPOSITE WINGBOX STRUCTURES BY ONE-DIMENSIONAL COMPONENT-WISE AND DYNAMIC STIFFNESS FORMULATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>E. Carrera, A. Pagani, P.H. Cabral, G. Silva, A. Prado<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-087<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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-2 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-18490 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-aircraft tag-hard-landing tag-msc-adams tag-numerical-simulation category-2413 category-2420 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/application-of-numerical-simulation-for-the-detection-and-analyzing-rough-landings-of-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF NUMERICAL SIMULATION FOR THE DETECTION AND ANALYZING ROUGH LANDINGS OF AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Andrey Rybin<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-089<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18493 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-aeroelasticity tag-luid-structure-interaction category-2413 category-2422 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/computational-benchmark-of-commercial-fluid-structure-interaction-software-for-aeroelastic-applications\/\" target=&quot;_blank&quot;>\n\t\t\t\tComputational Benchmark of Commercial Fluid-Structure Interaction Software for Aeroelastic Applications\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nicholas F. Giannelis, Gareth A. Vio<\/b><\/p>\n<p>DOI Number:  N\/A<\/p>\n<p>Conference number: IFASD-2015-091<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18499 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-flutter-testing tag-free-decays tag-modal-analysis-2 tag-system-identification category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/an-efficient-approach-for-in-operation-modal-analysis-of-flutter-flight-tests\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN EFFICIENT APPROACH FOR IN-OPERATION MODAL ANALYSIS OF FLUTTER FLIGHT TESTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>B. Jacquier, P. Vacher, S. Leroy, D. Walker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-095<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-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 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-18508 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-active-control tag-lateral-response tag-multi-parameter-updation tag-sensitivity-study tag-structural-coupling category-2413 category-2425 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/sensitivity-based-approach-for-improved-predictions-of-servo-elastic-response-of-a-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tSENSITIVITY BASED APPROACH FOR IMPROVED PREDICTIONS OF SERVO-ELASTIC RESPONSE OF A FLEXIBLE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Prabha Srinivasan, Ashok Joshi, Indira Narayanaswamy, Hemalatha E<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-098<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18511 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-structural-dynamics-shimmy tag-dampers tag-development-testing tag-ground-testing tag-ground-vibration-testing tag-landing-gear tag-resonant-characteristics tag-shimmy category-2413 category-2432 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/experimental-methods-of-studying-of-dynamic-characteristics-of-airplane-landing-gear\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL METHODS OF STUDYING OF DYNAMIC CHARACTERISTICS OF AIRPLANE LANDING GEAR\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A.V. Krapivko, V.N. Zadonskay, E.S. Kolyshev, S.E. Paryshev, E.A. Dubovsky<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-099<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18514 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-best-linear-approximation tag-nonlinear-distortions tag-system-identification category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/nonlinear-ground-vibration-identification-of-an-f-16-aircraft-part-i-fast-nonparametric-analysis-of-distortions-in-frf-measurements\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR GROUND VIBRATION IDENTIFICATION OF AN F-16 AIRCRAFT PART I: FAST NONPARAMETRIC ANALYSIS OF DISTORTIONS IN FRF MEASUREMENTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M. Vaes, J. Schoukens, Y. Rolain, B. Peeters, J. Debille, T. Dossogne3, J.P. No\u00ebl, C. Grappasonni, G. Kerschen<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-101<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18517 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads-alleviation tag-automatic-control-systems tag-cumulative-fatigue-damage tag-variable-loading category-2413 category-2429 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/influence-of-regular-control-system-on-aircraft-loads-repeatability\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF REGULAR CONTROL SYSTEM ON AIRCRAFT LOADS REPEATABILITY\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 S. Ustinov, Vladimir I. Tsimbalyuk, Tatiana I. Orlova<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-102<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18520 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads-alleviation tag-active-alleviation tag-aeroelasticity tag-closed-loop tag-gust-load tag-wind-tunnel category-2413 category-2429 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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-complete-experimental-investigation-of-gust-load-from-generation-to-active-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tA COMPLETE EXPERIMENTAL INVESTIGATION OF GUST LOAD: FROM GENERATION TO ACTIVE 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>Arnaud Lepage, Yannick Amosse, Dominique Le Bihan, Charles Poussot-Vassal2, Vincent Brion, Eric Rantet<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-103<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18523 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-aerodynamic-analysis tag-aerodynamic-singularities tag-blade tag-campbells-diagramm tag-design-process-flutter tag-elastic-modes tag-helicopter-aeroelasticity tag-rotor category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/alternative-problem-formulations-for-identification-of-mathematical-model-of-helicopter-rotor-blade-and-some-problems-of-aeroelasticity-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tALTERNATIVE PROBLEM FORMULATIONS FOR IDENTIFICATION OF MATHEMATICAL MODEL OF HELICOPTER ROTOR BLADE AND SOME PROBLEMS OF AEROELASTICITY ANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vadim Yu.Eremin, Sergei E.Paryshev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-105<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18526 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-a330-mrtt tag-boom tag-buffet tag-dynamic-loads category-2413 category-2420 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/non-linear-structural-dynamics-aspects-of-the-aerial-refuelling-boom-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tNON-LINEAR STRUCTURAL DYNAMICS ASPECTS OF THE AERIAL REFUELLING BOOM SYSTEM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>F. Ar\u00e9valo, S. Claver\u00edas, H. Climent<\/b><\/p>\n<p>DOI Number:  N\/A<\/p>\n<p>Conference number: IFASD-2015-107<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18529 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-backlash tag-dead-zone tag-flutter tag-partial-frequencies category-2413 category-2422 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/investigation-of-uav-control-surfaces-characteristics\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATION OF UAV CONTROL SURFACES\u2019 CHARACTERISTICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sergey N. Gartsev, Anton V. Dolgopolov, Vsevolod I. Smyslov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-113<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18532 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-structural-dynamics-shimmy tag-aeroelasticity tag-structural-dynamics tag-unsteady-aerodynamics tag-vibrations category-2413 category-2432 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/main-landing-gear-door-dynamic-loads-due-to-unsteady-aerodynamics-a-predictive-and-validated-methodology\/\" target=&quot;_blank&quot;>\n\t\t\t\tMAIN LANDING GEAR DOOR DYNAMIC LOADS DUE TO UNSTEADY AERODYNAMICS: A PREDICTIVE AND VALIDATED METHODOLOGY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>R. Abarca, D. Arenillas, O. Castro, B. Masi\u00e1, E. Menga, M. Barth<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-114<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18540 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-aeroelastic-constraints tag-cfd-correction tag-composite tag-doublet-lattice-method tag-stacking-sequence-optimization tag-stiness-optimization category-2413 category-2415 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/static-aeroelastic-stiffness-optimization-of-a-forward-swept-composite-wing-with-cfd-corrected-aero-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTATIC AEROELASTIC STIFFNESS OPTIMIZATION OF A FORWARD SWEPT COMPOSITE WING WITH CFD CORRECTED AERO LOADS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Johannes K.S. Dillinger, Mostafa M. Abdalla, Yasser M. Meddaikar, Thomas Klimmek<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-116<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18546 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-aeroelasticity tag-flutter tag-load tag-optimization tag-structural-optimization category-2413 category-2415 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/accelerated-convergence-of-high-fidelity-aeroelasticity-using-low-fidelity-aerodynamics-2\/\" target=&quot;_blank&quot;>\n\t\t\t\tACCELERATED CONVERGENCE OF HIGH-FIDELITY AEROELASTICITY USING LOW-FIDELITY AERODYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sean Meldrum, Pierre Hardy, Gabriel Broux, Eric Garrigues<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-121<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18549 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-ground-vibration-testing tag-strain-modal-analysis tag-strain-sensors category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/the-use-of-dynamic-strain-sensors-and-measurements-on-the-ground-vibration-testing-of-an-f-16-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHE USE OF DYNAMIC STRAIN SENSORS AND MEASUREMENTS ON THE GROUND VIBRATION TESTING OF AN F-16 AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Fabio L. M. dos Santos, Bart Peeters, Jan Debille, Carmine Salzano, Luiz Carlos, S. Goes, Wim Desmet<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-122<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18552 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-aeroelastic-tailoring tag-aeroelasticity tag-design tag-experiment tag-load-alleviation category-2413 category-2423 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/design-and-testing-of-an-aeroelastically-tailored-wing-under-manoeuvre-loading\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN AND TESTING OF AN AEROELASTICALLY TAILORED WING UNDER MANOEUVRE LOADING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Noud P.M Werter, Jurij Sodja, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-123<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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-2 tag-gust-generator 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-18558 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-geometric-nonlinearity tag-gust-response tag-high-aspect-ratio-wing-2 tag-uvlm-unsteady-vortex-lattice-method category-2413 category-2422 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/gust-response-analysis-for-high-aspect-ratio-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tGUST RESPONSE ANALYSIS FOR HIGH-ASPECT RATIO WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Liu Yi, Xie Changchuan, Yang Chao<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-126<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18561 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-aerodynamic-thermal-structure-coupling tag-aerothermoelastic tag-hypersonic tag-interval-method tag-the-uncertainty-of-aerodynamic-heat-flux category-2413 category-2422 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/a-static-aerothermoelastic-response-analysis-method-considering-heat-flux-uncertainty\/\" target=&quot;_blank&quot;>\n\t\t\t\tA STATIC AEROTHERMOELASTIC RESPONSE ANALYSIS METHOD CONSIDERING HEAT FLUX UNCERTAINTY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nan Yi, Zhiqiang Wan , GuoShu Li, Chao Yang<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-128<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18564 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-aeroelastic-tailoring tag-aeroelasticity tag-structural-dynamics category-2413 category-2423 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/aeroelastic-tailoring-using-crenelated-skins-modelling-and-experiment\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC TAILORING USING CRENELATED SKINS \u2013 MODELLING AND EXPERIMENT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Guillaume Francois, Jonathan E. Cooper, Paul M. Weaver<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-129<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18567 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-aeroelasticity tag-health-monitoring tag-loads tag-observer tag-state-estimation category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/embedding-a-multi-body-model-of-a-fixed-wing-aircraft-in-a-nonlinear-state-observer\/\" target=&quot;_blank&quot;>\n\t\t\t\tEMBEDDING A MULTI-BODY MODEL OF A FIXED-WING AIRCRAFT IN A NONLINEAR STATE OBSERVER\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Tuur L. Benoit, Yves C. Lemmens, Wim A. Desmet<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-130<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18570 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads-alleviation tag-aeroelastic-control tag-exible-aircraft-dynamics tag-load-alleviation tag-wake-encounter category-2413 category-2429 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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-load-alleviation-of-flexible-aircraft-in-wake-vortex-encounters\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC LOAD ALLEVIATION OF FLEXIBLE AIRCRAFT IN WAKE VORTEX 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>Henrik Hesse, Rafael Palacios<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-133<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18576 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-automatic-control-systems tag-cumulative-fatigue-damage tag-optimization tag-variable-loading tag-vibration-suppression category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/peculiarities-of-aircraft-variable-loading-and-vibration-suppression-abilities\/\" target=&quot;_blank&quot;>\n\t\t\t\tPECULIARITIES OF AIRCRAFT VARIABLE LOADING AND VIBRATION SUPPRESSION ABILITIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vladimir I. Tsimbalyuk, Tatiana I. Orlova, Kirill A. Mitenkov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-135<\/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-18579 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-active-control tag-aeroelastic-instability tag-autonomous-free-floating-flap tag-limit-cycle-oscillation-2 category-2413 category-2425 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/experimental-and-numerical-study-of-an-autonomous-flap\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL AND NUMERICAL STUDY OF AN AUTONOMOUS FLAP\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Lars O. Bernhammer, Sachin T. Navalkar, Jurij Sodja, Roeland De Breuker , Moti Karpel<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-136<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18582 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-optimisation tag-aeroelastic-tailoring tag-aeroelasticity tag-wing-design category-2413 category-2415 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/aeroelastic-tailoring-and-structural-optimisation-using-an-advanced-dynamic-aeroelastic-framework\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC TAILORING AND STRUCTURAL OPTIMISATION USING AN ADVANCED DYNAMIC AEROELASTIC FRAMEWORK\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Noud P.M. Werter, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-137<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18585 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-aeroelasticity tag-flutter tag-frequency-response-functions tag-wind-tunnel category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/application-of-imposed-motion-method-for-model-flutter-tests-in-high-speed-wind-tunnels\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF IMPOSED MOTION METHOD FOR MODEL FLUTTER TESTS IN HIGH-SPEED WIND TUNNELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Boris D. Bryantsev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-138<\/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-18588 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-crashworthiness tag-ditching tag-fluid-structure-interaction tag-structural-dynamics category-2413 category-2426 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/experimental-ditching-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL DITCHING LOADS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>H. Climent, G. Pastor, J.T. Viana, L. Ben\u00edtez, A. Iafrati<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-139<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18591 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-aeroelasticity tag-gvt-ground-vibration-tests tag-ifasd tag-structural-dynamics category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/state-of-the-art-of-gvt-technology-in-russia-and-possible-directions-to-increase-accuracy-and-reliability\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTATE OF THE ART OF GVT TECHNOLOGY IN RUSSIA AND POSSIBLE DIRECTIONS TO INCREASE ACCURACY AND RELIABILITY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Petr G. Karkle, Michail A. Pronin, Michail M. Bogatyrev, Gleb V. Liseykin, Klaas Dijkstra<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-140<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18594 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-reduced-order-modelling tag-aic-correction-2 tag-dynamic-loads tag-gust-encounter tag-rom 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-18597 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-aeroelastic-galloping tag-narmax tag-system-identification category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/bifurcation-analysis-of-the-aeroelastic-galloping-problem-via-input-output-parametric-modelling\/\" target=&quot;_blank&quot;>\n\t\t\t\tBifurcation Analysis of the Aeroelastic Galloping Problem via Input-Output Parametric Modelling\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nicholas F. Giannelis, Gareth A. Vio<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-144<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18600 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-aeroelastic tag-cfd-csd tag-coupling-simulation category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/cfd-csd-approach-to-evaluate-the-aeroelastic-response-of-hypersonic-vehicle-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tCFD\/CSD APPROACH TO EVALUATE THE AEROELASTIC RESPONSE OF HYPERSONIC VEHICLE 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>Jinan Lv, Li Guo, Fangjian Wang, Ziqiang Liu<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-146<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-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 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-18609 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-of-morphing-aircraft tag-aeroelasticity tag-cae tag-compliant-mechanisms tag-genetic-algorithm tag-morphing tag-multi-objective-optimization category-2413 category-2424 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/aeroelastic-analysis-of-a-regional-aircraft-with-active-camber-morphing-device\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC ANALYSIS OF A REGIONAL AIRCRAFT WITH ACTIVE CAMBER MORPHING DEVICE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alessandro De Gaspari, Sergio Ricci, Lorenzo Travaglini<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-149<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18612 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-active-control tag-active-control tag-flutter tag-limit-cycle-oscillation-2 tag-piezoelectric category-2413 category-2425 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/19\/suppression-of-simulated-self-excited-oscillation-using-smart-materials-on-flexible-wing-strcuture\/\" target=&quot;_blank&quot;>\n\t\t\t\tSUPPRESSION OF SIMULATED SELF-EXCITED OSCILLATION USING SMART MATERIALS ON FLEXIBLE WING STRCUTURE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Norizham A. Razak<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-150<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18615 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd tag-computational-uid-dynamics tag-limit-cycle-oscillation-2 tag-transonic-aerodynamics 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-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 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-18622 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-structural-dynamics-shimmy tag-frequency-response tag-nonlinear-dynamics tag-rubber tag-softening-effect tag-structural-dynamic-modification category-2413 category-2432 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/nonlinear-dynamic-analysis-of-assembled-aircraft-structures-with-concentrated-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR DYNAMIC ANALYSIS OF ASSEMBLED AIRCRAFT STRUCTURES WITH CONCENTRATED NONLINEARITIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>E. Menga, S. Hernandez, S. Moledo, C. Lopez<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-155<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-18628 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-gvt-flight-test tag-engine-imbalance tag-ground-vibration-tests tag-rotating-inertial-force tag-simulation category-2413 category-2428 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/airplane-ground-tests-with-rotating-force-simulation\/\" target=&quot;_blank&quot;>\n\t\t\t\tAIRPLANE GROUND TESTS WITH ROTATING FORCE SIMULATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Regina V. Leonteva<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-158<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18631 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-structural-dynamics-shimmy tag-aerial-delivery tag-loads tag-structural-dynamics category-2413 category-2432 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/aerial-delivery-dynamic-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tAERIAL DELIVERY DYNAMIC LOADS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. P\u00e9rez de la Serna, A. J. Rodr\u00edguez Jim\u00e9nez, M. Oliver, H. Climent<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-160<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18634 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelasticity-in-aircraft-design tag-aeroelasticity tag-aviation-regulations tag-certification tag-deformations tag-dynamic-loading tag-finite-element-method tag-ifasd tag-loads tag-mathematical-models tag-multidisciplinary-design tag-service-life tag-static-strength tag-stresses tag-unsteady-aerodynamics category-2413 category-2423 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/multidisciplinary-computational-system-parus-int-for-design-and-certification-of-airplanes-in-static-and-dynamic-strength-and-service-life\/\" target=&quot;_blank&quot;>\n\t\t\t\tMULTIDISCIPLINARY COMPUTATIONAL SYSTEM \u00abPARUS-INT\u00bb FOR DESIGN AND CERTIFICATION OF AIRPLANES IN STATIC AND DYNAMIC STRENGTH AND SERVICE LIFE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>G. I. Turchannikov, M. M. Levchenko, V. V. Chedrik, D. V. Chemisov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-162<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18637 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-compact-gas-turbine tag-foil-gasdynamic-bearings tag-nonlinear-vibrations tag-rotor-dynamics tag-test-rig category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/rotor-dynamics-of-compact-gas-turbine-unit-with-gas-bearings-investigation\/\" target=&quot;_blank&quot;>\n\t\t\t\tROTOR DYNAMICS OF COMPACT GAS TURBINE UNIT WITH GAS BEARINGS INVESTIGATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>D. Sc., Prof. Temis J.M., PhD Temis M.J., Egorov A.M.<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-164<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-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 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-18646 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-aeroelasticity tag-morphing tag-morphing-wing tag-uav tag-variable-span tag-vsmw category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/development-of-an-uav-with-a-variable-span-morphing-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tDEVELOPMENT OF AN UAV WITH A VARIABLE-SPAN MORPHING 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>Jae-Sung Bae, Jong-Hwan Kim, Soo-Yong Lee, Jung-Sun Park, Jin-Sung Kim, In Lee<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-170<\/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-18649 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-active-control tag-auto-oscillations tag-elastic-ufv-cs-loop tag-electromechanical-actuator tag-flutter category-2413 category-2425 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/research-experience-of-aeroelastic-vibrations-of-the-ufv-with-electromechanical-actuator-of-control-fin\/\" target=&quot;_blank&quot;>\n\t\t\t\tRESEARCH EXPERIENCE OF AEROELASTIC VIBRATIONS OF THE UFV WITH ELECTROMECHANICAL ACTUATOR OF CONTROL FIN\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vsevolod I. Smyslov, Artyom V. Bykov, Stanislav I. Sychev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-172<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18652 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-flight-loads tag-static-aeroelasticity tag-three-dimensional-aerodynamics tag-trim-analysis category-2413 category-2420 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/analysis-of-flight-loads-and-static-aeroelasticity-characteristics-of-the-airplane-with-the-use-of-three-dimensional-aerodynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tANALYSIS OF FLIGHT LOADS AND STATIC AEROELASTICITY CHARACTERISTICS OF THE AIRPLANE WITH THE USE OF THREE-DIMENSIONAL AERODYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Fausto G. Di Vinvenzo , Marina V. Kwiatkowska , Regina V. Leonteva , Denis V. Nekhaev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-173<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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-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 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-18663 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-aeroelasticity tag-cfd-csm-2 tag-coupling tag-fluid-structure tag-gust tag-openfsi 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-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 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-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 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-18672 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aerodynamics-cfd 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-18675 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties tag-aeroelasticity tag-arbitrary-polynomial-chaos tag-composite-materials tag-polar-method category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/uncertainty-quantification-in-aeroelastic-response-of-an-idealized-composite-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tUNCERTAINTY QUANTIFICATION IN AEROELASTIC RESPONSE OF AN IDEALIZED COMPOSITE WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christian T. Nitschke, Jonas Maruani, Angela Vincenti, Didier Lucor, Jean-Camille Chassaing<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-182<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18678 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads tag-increased-order-modeling tag-increased-order-modeling-iom tag-morphing tag-structural-dynamics category-2413 category-2420 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/aircraft-dynamic-loads-with-varying-geometry-and-flight-mechanics-effects\/\" target=&quot;_blank&quot;>\n\t\t\t\tAircraft Dynamic Loads with Varying Geometry and Flight Mechanics Effects\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Moti Karpe, Aviv Romm, Manuel Reyes, Hector Climent<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-183<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18681 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 tag-dlr-tau-code-2 tag-flutter tag-gcro-dr tag-gmres tag-gust-response tag-krylov-subspace-recycling tag-linearised-computational-fluid-dynamics tag-shock-buet 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-18684 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-degradation-of-characteristics tag-fan-blades tag-foreign-object-damage tag-pieces-of-ice category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/on-the-influence-of-aircraft-engine-components-damage-caused-by-foreign-objects-ingestion-on-the-aeroelastic-characteristics-of-compressors\/\" target=&quot;_blank&quot;>\n\t\t\t\tON THE INFLUENCE OF AIRCRAFT ENGINE COMPONENTS DAMAGE CAUSED BY FOREIGN OBJECTS INGESTION ON THE AEROELASTIC CHARACTERISTICS OF COMPRESSORS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Victor Matsarenko, Galina Melnikova, Boris Shorr<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-187<\/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-18687 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-rotation-system tag-blade-shape-optimization tag-disk-weight-minimization tag-structural-optimization category-2413 category-2431 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/compressor-blade-and-disc-optimal-structural-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPRESSOR BLADE AND DISC OPTIMAL STRUCTURAL DESIGN\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Joury M. Temis, , Denis A. Yakushev<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-188<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18690 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroservoelasticity-1-ifasd-2015 tag-aerodynamics tag-morphing tag-shear-layer tag-time-resolved-piv tag-turbulence category-2413 category-2414 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/time-resolved-piv-measurements-of-a-hybrid-morphing-naca4412-airfoil\/\" target=&quot;_blank&quot;>\n\t\t\t\tTime resolved PIV measurements of a hybrid morphing NACA4412 airfoil\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Johannes Scheller, Karl-Joseph Rizzo, Gurvan Jodin, Eric Duhayon, Jean-Francois Rouchon, Giles Harran, Marianna Braza<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-190<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18693 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-bi-wing-ornithopter tag-flapping-wing-aerodynamics tag-flapping-wing-flight-dynamics tag-micro-air-vehicle tag-unsteady-aerodynamics category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/flight-dynamic-modelling-and-numerical-simulation-of-a-flapping-wing-ornithopter-with-pitching-and-flapping-phase-lag\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT DYNAMIC MODELLING AND NUMERICAL SIMULATION OF A FLAPPING WING ORNITHOPTER WITH PITCHING AND FLAPPING PHASE LAG\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 Syamim Syazwan Ramli<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-191<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18696 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-aerodynamic-damping tag-asymmetric-eigenmode tag-critical-speed tag-engine-aeroelasticity tag-engine-thrust tag-flutter tag-utter-frequency tag-follower-force tag-gyroscopics category-2413 category-2422 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/the-aeroelastic-impact-of-engine-thrust-and-gyroscopics-on-aircraft-flutter-instabilities\/\" target=&quot;_blank&quot;>\n\t\t\t\tThe Aeroelastic Impact of Engine Thrust and Gyroscopics on Aircraft Flutter Instabilities\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Stefan Waitz, Holger Hennings<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-192<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18699 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-aeroelastic-response-stability tag-aeroservoelasticity-characteristics-aeroelasticity tag-flutter tag-gyroscopic-forces tag-polynomial-ritz-method category-2413 category-2422 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/gyroscopic-forces-influence-on-aeroelasticity-characteristics-of-an-airplane-with-engines-on-pylons-under-the-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tGYROSCOPIC FORCES INFLUENCE ON AEROELASTICITY CHARACTERISTICS OF AN AIRPLANE WITH ENGINES ON PYLONS UNDER THE WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. Kuznetsov, S. Kuzmina, F. Ishmuratov, V. Mosunov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-193<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18702 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-loads-alleviation tag-aileron-design tag-flexible-aircraft tag-gust-load-alleviation tag-multidisciplinary-design-optimization category-2413 category-2429 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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-optimization-of-ailerons-for-active-gust-load-alleviation\/\" target=&quot;_blank&quot;>\n\t\t\t\tINTEGRATED OPTIMIZATION OF AILERONS FOR ACTIVE GUST LOAD ALLEVIATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Manuel Pusch, Andreas Knoblach, Thiemo Kier<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-199<\/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-18705 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-aviation-regulations tag-composite-control-system tag-flight-loads tag-flight-simulator tag-ground-loads tag-software category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/development-of-flight-paramenters-simulation-technology-for-an-aircraft-with-complex-control-system-on-flight-simulators-for-more-precise-definition-of-in-service-loads-to-solve-the-strength-structura\/\" target=&quot;_blank&quot;>\n\t\t\t\tDEVELOPMENT OF FLIGHT PARAMENTERS SIMULATION TECHNOLOGY FOR AN AIRCRAFT WITH COMPLEX CONTROL SYSTEM ON FLIGHT SIMULATORS FOR MORE PRECISE DEFINITION OF IN-SERVICE LOADS TO SOLVE THE STRENGTH STRUCTURAL AND LIFE PROBLEMS EFFECTIVELY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>G. I. Turchannikov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-200<\/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-18708 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-poster-presentations tag-critical-speed tag-highway-bridge tag-strouhal-number tag-vortex-excitation category-2413 category-2430 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-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\/method-of-preliminary-estimation-of-highway-solidweb-bridges-under-the-wind-forcing\/\" target=&quot;_blank&quot;>\n\t\t\t\tMETHOD OF PRELIMINARY ESTIMATION OF HIGHWAY SOLIDWEB BRIDGES UNDER THE WIND FORCING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Konstantin S. Strelkov, Michael S. Komarov, Andrey V. Kozichev, Olga A. Markina, Anatoliy V. Bykovsky, Boris A. Logunov, Leonid L. Teperin<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-201<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\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 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-18714 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-computational-aeroelasticity-1-ifasd-2015 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-18717 post type-post status-publish format-standard hentry category-1-ifasd-2015 category-nonlinearities-uncertainties category-2413 category-2417 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/11\/20\/limit-cycle-oscillations-of-a-pretensed-membrane-strip\/\" target=&quot;_blank&quot;>\n\t\t\t\tLimit-cycle Oscillations of a pretensed Membrane Strip\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ariel Drachinsky, Daniella E. Raveh<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2015-207<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-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 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<\/div>\n\t\t\t\t\t<span class=\"e-load-more-spinner\">\n\t\t\t\t<i aria-hidden=\"true\" class=\"fas fa-spinner\"><\/i>\t\t\t<\/span>\n\t\t\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-607c26a elementor-widget elementor-widget-spacer\" data-id=\"607c26a\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t<div class=\"elementor-column elementor-col-25 elementor-top-column elementor-element elementor-element-4b92472\" data-id=\"4b92472\" data-element_type=\"column\" data-e-type=\"column\" data-settings=\"{&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t<div class=\"elementor-widget-wrap\">\n\t\t\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t<section class=\"elementor-section elementor-top-section elementor-element elementor-element-5f254a1 elementor-section-stretched elementor-section-boxed elementor-section-height-default elementor-section-height-default\" data-id=\"5f254a1\" data-element_type=\"section\" data-e-type=\"section\" data-settings=\"{&quot;stretch_section&quot;:&quot;section-stretched&quot;,&quot;background_background&quot;:&quot;classic&quot;}\">\n\t\t\t\t\t\t<div class=\"elementor-container elementor-column-gap-default\">\n\t\t\t\t\t<div class=\"elementor-column elementor-col-100 elementor-top-column elementor-element elementor-element-ff101ec\" data-id=\"ff101ec\" data-element_type=\"column\" data-e-type=\"column\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-bbafcf0 elementor-widget elementor-widget-spacer\" data-id=\"bbafcf0\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-9389dce elementor-widget elementor-widget-spacer\" data-id=\"9389dce\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"spacer.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t<div class=\"elementor-spacer\">\n\t\t\t<div class=\"elementor-spacer-inner\"><\/div>\n\t\t<\/div>\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t<\/div>\n\t\t","protected":false},"excerpt":{"rendered":"<p>Search all IFASD 2015 papers Search &#8230; Results See all results Search by Event Topic IFASD2015 Aerodynamics\/CFD Aeroelastic Optimisation Aeroelastic Response &amp; Stability Aeroelasticity in Aircraft Design Aeroelasticity of Morphing Aircraft Aeroservoelasticity Aeroservoelasticity &amp; Active Control Computational Aeroelasticity Crashworthiness Experimental Methods Experimental Methods &amp; Bridges GVT &amp; Flight Test Loads Loads Alleviation Nonlinearities &amp; Uncertainties&hellip;<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"footnotes":""},"class_list":["post-18252","page","type-page","status-publish","hentry","category-2413","category-2418","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/18252","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=18252"}],"version-history":[{"count":13,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/18252\/revisions"}],"predecessor-version":[{"id":19149,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/18252\/revisions\/19149"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18252"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}