{"id":17396,"date":"2024-06-13T10:10:25","date_gmt":"2024-06-13T10:10:25","guid":{"rendered":"https:\/\/aerospacerepository.org\/?page_id=17396"},"modified":"2025-02-25T19:29:49","modified_gmt":"2025-02-25T19:29:49","slug":"repository-ifasd-2017","status":"publish","type":"page","link":"https:\/\/aerospacerepository.org\/index.php\/repository-ifasd-2017\/","title":{"rendered":"Repository IFASD 2017"},"content":{"rendered":"\t\t<div data-elementor-type=\"wp-page\" data-elementor-id=\"17396\" class=\"elementor elementor-17396\" 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 2017 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 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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=\"17401\" 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;\">IFASD2017<\/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=\"1954\"\n\t\t\tdata-label=\"Active Control and Adaptive Structures\"\n\t\t\t\t\t\taria-label=\"Active Control and Adaptive Structures\"\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\tActive Control and Adaptive Structures\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=\"1955\"\n\t\t\tdata-label=\"Aeroelasticity in Conceptual Aircraft Design\"\n\t\t\t\t\t\taria-label=\"Aeroelasticity in Conceptual 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 Conceptual 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=\"1956\"\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 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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-17421 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-adjoint-method tag-multidisciplinary-optimization tag-sensitivity-analysis category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/comparison-of-high-fidelity-aero-structure-gradient-computation-techniques-application-on-the-crm-wing-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tComparison of High-Fidelity Aero-Structure Gradient Computation Techniques. Application on the CRM Wing 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>T. Achard, C. Blondeau and R. Ohayon<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-002<\/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-17427 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-nonlinearity tag-numerical-simulation-2 tag-stall-flutter tag-wind-tunnel-test category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/experimental-and-numerical-simulations-of-naca-0018-airfoil-undergoing-stall-flutter-with-structural-nonlinearity\/\" target=&quot;_blank&quot;>\n\t\t\t\tExperimental and Numerical Simulations of NACA 0018 Airfoil undergoing Stall Flutter with Structural Nonlinearity\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.F. Razaami, M.K.H.M. Zorkipli, N.A.Razak<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-003<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17430 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-aeroelasticity tag-buffeting tag-combined-random-loads tag-multidimensional-design-load-envelope category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/validation-and-evaluation-of-a-nonlinear-aeroelastic-framework-using-flight-test-data\/\" target=&quot;_blank&quot;>\n\t\t\t\tValidation and evaluation of a nonlinear aeroelastic framework using flight test data\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>F. Afonso, J. Vale, \u00c9. Oliveira and F. Lau, F. Moreira, J. Marra, A. Meinicke, M. Pedras, O. Mello, J. Richards, W. Brussow, S. Warwick, A. Suleman<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-004<\/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-17433 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-aeroelasticity tag-buffeting tag-combined-random-loads tag-multidimensional-design-load-envelope category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/a-method-for-predicting-multivariate-random-loads-and-a-discrete-appoximation-of-the-mutidimensional-design-load-envelope\/\" target=&quot;_blank&quot;>\n\t\t\t\tA method for predicting multivariate random loads and a discrete appoximation of the mutidimensional design load envelope\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.Aquilini, D.Parisse<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference Number: IFASD-2017-005<\/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-17436 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-awacs tag-dynamic-loads tag-dynamic-model category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/airbus-defence-and-space-awacs-prototypes-awacs-dome-aeroelastic-and-dynamic-loads-challenges\/\" target=&quot;_blank&quot;>\n\t\t\t\tAirbus Defence and Space AWACS PROTOTYPES: AWACS-DOME AEROELASTIC AND DYNAMIC LOADS CHALLENGES\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, M.R.Guiti\u00e1n, P.M.L\u00f3pez, J.L.P.Gal\u00e1n, H.Climent<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-006<\/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-17439 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelastic-system-identification tag-flutter-prediction category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/computational-fluid-dynamics-based-aeroelastic-system-identification-and-flutter-prediction\/\" target=&quot;_blank&quot;>\n\t\t\t\tComputational Fluid Dynamics Based Aeroelastic System Identification and Flutter Prediction\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M.Argaman, D.E.Raveh<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-007<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17442 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aspect-ratio tag-conceptual-design-2 tag-subsonic-aircraft category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/aerodynamic-and-structural-design-studies-for-fuel-consumption-reduction-on-subsonic-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tAerodynamic and Structural Design Studies for Fuel Consumption Reduction on Subsonic 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>H.Arizono, D.Kwak, T.Nomura<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-008<\/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-17445 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity-2 tag-parametric-studies tag-strength tag-structural-optimization category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/structural-design-of-wing-tip-part-from-aeroelasticity-consideration\/\" target=&quot;_blank&quot;>\n\t\t\t\tStructural design of wing tip part from aeroelasticity consideration\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.Balunov, V.Chedrik, F.Ishmuratov<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-011<\/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-17448 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aeroelasticity tag-dynamic-loads tag-flight-control-system tag-structural-coupling category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/flight-control-design-to-improve-aircraft-performance-by-reducing-the-flutter-and-dynamic-loads-margins\/\" target=&quot;_blank&quot;>\n\t\t\t\tFlight control design to improve aircraft performance by reducing the flutter and dynamic loads margins\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>L.Benassi<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-014<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17451 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-multiple-limit-cycles tag-nonlinear-transonic-flutter category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/nested-limit-cycles-in-transonic-flutter\/\" target=&quot;_blank&quot;>\n\t\t\t\tNested Limit Cycles in Transonic Flutter\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Oddvar O. Bendiksen<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-015<\/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-17454 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-adjoint-variables tag-bifurcation tag-flutter tag-sensitivity-analysis category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/fast-prediction-of-flutter-and-flutter-sensitivities\/\" target=&quot;_blank&quot;>\n\t\t\t\tFast Prediction of Flutter and Flutter Sensitivities\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Philip S. Beran, Bret K. Stanford, Kevin G. Wang<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-016<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17457 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-adaptive-control tag-control-of-flexible-aircraft tag-hale-aircraft tag-lyapunov-direct-method tag-model-reference-adaptive-control category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/dynamic-gain-scheduling-of-highly-flexible-aircraft-applying-adaptive-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tDynamic Gain Scheduling of Highly Flexible Aircraft Applying Adaptive Control\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>R.M.Bertolin, F.J.Silvestre, A.B.Guimaraes Neto, P.J.Gonzalez, G.C.Barbosa, C.E.S.Cesnik<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-017<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17460 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-computational-aeroelasticity tag-computational-fluid-dynamics tag-transonic-flutter category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/influence-of-aerodynamic-nonlinearity-onflutter-of-curved-panels-at-transonic-andlow-supersonic-mach-numbers\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF AERODYNAMIC NONLINEARITY ON FLUTTER OF CURVED PANELS AT TRANSONIC AND LOW SUPERSONIC MACH NUMBERS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Manav Bhatia, Philip S. Beran<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-018<\/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-17463 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-continuous-time-model tag-state-space-model tag-unsteady-aerodynamics tag-unsteady-induced-drag tag-unsteady-vortex-lattice-method category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/13\/extension-of-the-continuous-time-unsteady-vortexlattice-method-for-arbitrary-motion-controlsurface-deflection-and-induced-drag-calculation\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXTENSION OF THE CONTINUOUS TIME UNSTEADY VORTEX LATTICE METHOD FOR ARBITRARY MOTION, CONTROL SURFACE DEFLECTION AND INDUCED DRAG CALCULATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Simon Binder, Andreas Wildschek, Roeland De Breuker<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-019<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17729 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aerodynamics tag-aeroelasticity tag-composite tag-optimization tag-surrogate category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/13\/surrogate-based-aerodynamics-for-composite-wing-boxsizing\/\" target=&quot;_blank&quot;>\n\t\t\t\tSURROGATE-BASED AERODYNAMICS FOR COMPOSITE WING BOXSIZING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Marco Tito Bordogna, Dimitri Bettebghor, Christophe Blondeau, Roeland De Breuker<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-021<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17736 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelastic-tailoring tag-blending tag-composite tag-esl tag-gust category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/aeroelastic-tailoring-for-static-and-dynamic-loads-withblending-constraints\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC TAILORING FOR STATIC AND DYNAMIC LOADS WITH BLENDING 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>Marco Tito Bordogna, Paul Lancelot, Dimitri Bettebghor, Roeland De Breuker<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-022<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17739 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-fluid-structure-interaction-2 tag-nonlinear-transient-response tag-validation tag-wind-tunnel-testing category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/wind-tunnel-testing-for-validation-of-a-method-fornonlinear-fluid-structure-interaction-usingsurrogate-models\/\" target=&quot;_blank&quot;>\n\t\t\t\tWIND-TUNNEL TESTING FOR VALIDATION OF A METHOD FOR NONLINEAR FLUID\/STRUCTURE INTERACTION USING SURROGATE 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>Elisa Bosco, Albert Lucchetti, Simon Trapier, F. G. Di Vincenzo, N. Gourdain, J. Morlier<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-023<\/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-17742 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-dynamic-stall tag-leading-edge-vortex tag-wind-tunnel-testing category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/dynamic-stall-onset-variation-with-reducedfrequency-for-three-stall-mechanisms\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC STALL ONSET VARIATION WITH REDUCED FREQUENCY FOR THREE STALL MECHANISMS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Boutet Johan, Dimitriadis Grigorios, Amandolese Xavier<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-024<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17745 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-energy-harvesting tag-hale tag-piezoelectricity tag-slender-wing tag-wind-tunnel-tests category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/practical-considerations-for-the-design-of-anaeroelastic-energy-harvester\/\" target=&quot;_blank&quot;>\n\t\t\t\tPRACTICAL CONSIDERATIONS FOR THE DESIGN OF AN AEROELASTIC ENERGY HARVESTER\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Bruni C., Cestino E., Frulla G., Marzocca P., Gibert J., D&#8217;Onghia N<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-026<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17748 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-aircraft-loads tag-flexible-aircraft tag-multibody-dynamics tag-nonlinear-aeroelasticity category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/flight-loads-prediction-of-high-aspect-ratio-wingaircraft-using-multibody-dynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT LOADS PREDICTION OF HIGH ASPECT RATIO WING AIRCRAFT USING MULTIBODY DYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Michele Castellani, Jonathan E. Cooper, Yves Lemmens<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-030<\/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-17751 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-damping tag-gvt tag-modal-analysis tag-structural-dynamics category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/cross-modal-damping-model-an-experimentalextraction-approach-and-aircraft-dynamic-loadsapplication\/\" target=&quot;_blank&quot;>\n\t\t\t\tCROSS-MODAL DAMPING MODEL: AN EXPERIMENTAL EXTRACTION APPROACH AND AIRCRAFT DYNAMIC LOADS APPLICATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Oscar Castro Alvarez, John A. Coote<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-032<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17754 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-full-span-model tag-ifasd tag-stick-model category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/some-special-modelling-techniques-for-preparationof-aeroelastic-stick-models\/\" target=&quot;_blank&quot;>\n\t\t\t\tSOME SPECIAL MODELLING TECHNIQUES FOR PREPARATION OF AEROELASTIC STICK 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>Jiri Cecrdle<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-034<\/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-17757 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-nonlinear-modal-analysis tag-reduced-order-modeling tag-very-exible-aircraft category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/modal-formulation-for-geometrically-nonlinearstructural-dynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODAL FORMULATION FOR GEOMETRICALLY NONLINEAR STRUCTURAL DYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Renato R. Medeiros, Carlos E. S. Cesnik, Etienne B. Coetzee<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-035<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17760 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-geometric-nonlinearities tag-reduced-order-model-2 tag-response-analysis category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/efficient-aeroelastic-response-analysis-includinggeometric-nonlinearities-based-on-structural-rom\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT AEROELASTIC RESPONSE ANALYSIS INCLUDING GEOMETRIC NONLINEARITIES BASED ON STRUCTURAL ROM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>An Chao, Xie Changchuan, Meng Yang, Yang Chao<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-037<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17763 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-generalized-aerodynamic-forces tag-linearized-unsteady-solver tag-transpiration-boundary-condition category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/flutter-boundary-prediction-for-a-twin-enginetransport-flutter-model-using-a-linearized-unsteadysolver\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER BOUNDARY PREDICTION FOR A TWIN-ENGINE TRANSPORT FLUTTER MODEL USING A LINEARIZED UNSTEADY SOLVER\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Shuchi Yang, Zhicun Wang, Zhichao Zhang, P.C. Chen<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-039<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17766 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-flutter-boundary tag-proper-orthogonal-decomposition tag-reduced-order-model-2 tag-structural-dynamic-reanalysis tag-transonic-aeroelasticity category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/consideration-of-pod-interpolation-for-aeroelasticdesign-with-large-global-structural-variations-usestructural-dynamic-reanalysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tCONSIDERATION OF POD INTERPOLATION FOR AEROELASTIC DESIGN WITH LARGE GLOBAL STRUCTURAL VARIATIONS USE STRUCTURAL DYNAMIC REANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Dongfeng Li, Gang Chen, A.Da Ronch, Qiang Zhou, Yueming Li<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-040<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17769 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aeroelasticity tag-control-system tag-flutter tag-frequency-response category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/investigation-of-flutter-characteristics-of-aircraftwith-control-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATION OF FLUTTER CHARACTERISTICS OF AIRCRAFT WITH CONTROL SYSTEM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M. Zichenkov, A. Chizhov, S. Kuzmina, F. Ishmuratov, A. Zubakov<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-043<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17772 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-computational-aeroelasticity tag-dynamic-aeroelastic tag-flutter tag-fun3d category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/cfd-model-of-the-transonic-dynamics-tunnel-withapplications\/\" target=&quot;_blank&quot;>\n\t\t\t\tCFD MODEL OF THE TRANSONIC DYNAMICS TUNNEL WITH APPLICATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Pawel Chwalowski, Walter A. Silva, Carol D. Wieseman and Jennifer Heeg<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-044<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17775 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-ditching-loads tag-dynamic-loads tag-structural-dynamics category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/experimental-ditching-loads-on-aeronauticalflexible-structures\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL DITCHING LOADS ON AERONAUTICAL FLEXIBLE STRUCTURES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>H. Climent, G. Pastor, J.T. Viana<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-045<\/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-17778 post type-post status-publish format-standard hentry category-events category-environmental-dynamics-and-aeroelasticity category-ifasd-2017 tag-aerolasticity tag-hht tag-hilbert-transform tag-hilbert-huang-transform tag-ht tag-oma tag-operational-modal-analysis tag-panel-flutter tag-time-varying-system category-993 category-1959 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/modal-parameter-estimate-of-time-varying-systemusing-operational-modal-analysis-based-on-hilberttransform\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODAL PARAMETER ESTIMATE OF TIME-VARYING SYSTEM USING OPERATIONAL MODAL ANALYSIS BASED ON HILBERT TRANSFORM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Elisabetta Conti, Francesco Saltari, Marco Eugeni, Valerio Camerini, Giuliano Coppotelli<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-046<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17781 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-geometric-structural-nonlinearity tag-nonlinear-aeroelasticity tag-polynomial-chaos-expansion-structural-dynamics tag-uncertainty-quantication category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/uncertainty-quantification-in-gust-loads-analysis-ofa-highly-flexible-aircraft-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tUNCERTAINTY QUANTIFICATION IN GUST LOADS ANALYSIS OF A HIGHLY FLEXIBLE 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>Robert G. Cook, Chris J. A. Wales, Ann L. Gaitonde, Dorian P. Jones, Jonathan E. Cooper<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-047<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17784 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-aeroelastic-optimisation tag-aeroelastic-tailoring tag-tow-steering category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/experimental-validation-of-tow-steered-compositewings-for-aeroelastic-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL VALIDATION OF TOW-STEERED COMPOSITE WINGS FOR AEROELASTIC DESIGN\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>O. Stodieck, G. Francois, D. Heathcote, E. Zympeloudis, B.C. Kim, A.T. Rhead, D. Cleaver, J.E. Cooper<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-048<\/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-17787 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-folding-wing-tip tag-gust-loads-alleviation tag-wind-tunnel-testing category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/wind-tunnel-testing-of-folding-wing-tipdevices-for-gust-loads-alleviation\/\" target=&quot;_blank&quot;>\n\t\t\t\tWIND TUNNEL TESTING OF FOLDING WING-TIP DEVICES FOR GUST LOADS ALLEVIATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>R.C.M. Cheung, A. Castrichini, D. Rezgui, J.E. Cooper, T. Wilson<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-049<\/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-17790 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-hpc-scalability tag-large-scale-computations tag-linearized-cfd tag-turbulence-gradient category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/industrial-frequency-domain-linearizednavier-stokes-calculations-for-aeroelastic-problemsin-the-transonic-flow-regime\/\" target=&quot;_blank&quot;>\n\t\t\t\tINDUSTRIAL FREQUENCY-DOMAIN LINEARIZED NAVIER-STOKES CALCULATIONS FOR AEROELASTIC PROBLEMS IN THE TRANSONIC FLOW REGIME\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Laurent Daumas, Nicolas Forestier, Alo\u00efs Bissuel, Gabriel Broux, Fr\u00e9d\u00e9ric Chalot, Zdenek Johan, Michel Mallet<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-050<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17793 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-computational-uid-dynamics tag-polynomial-nonlinear-state-space-modelling tag-vortex-induced-vibrations category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/polynomial-nonlinear-state-space-modelling-ofvortex-induced-vibrations-black-box-vs-grey-boxapproach\/\" target=&quot;_blank&quot;>\n\t\t\t\tPOLYNOMIAL NONLINEAR STATE-SPACE MODELLING OF VORTEX-INDUCED VIBRATIONS: BLACK-BOX VS GREY-BOX APPROACH\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>J. Decuyper, J. P. No\u00ebl, T. De Troyer, M. C. Runacres, J. Schoukens<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-053<\/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-17796 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-dynamic-coupled-simulations tag-lco tag-reduced-model category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/aeroelastic-limit-cycle-oscillations-on-a-3d-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC LIMIT CYCLE OSCILLATIONS ON A 3D WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sylvie Dequand, Guy-Daniel Mortch\u00e9l\u00e9wicz, Anne-Sophie Sens<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference numer: IFASD-2017-054<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17799 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-aerodynamic-correction tag-aeroelasticity tag-ifasd tag-wind-tunnel-test category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/improving-aeroelastic-model-accuracy-andaffordability-by-exploiting-wind-tunnel-test-results\/\" target=&quot;_blank&quot;>\n\t\t\t\tIMPROVING AEROELASTIC MODEL ACCURACY AND AFFORDABILITY BY EXPLOITING WIND TUNNEL TEST RESULTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Marco Di Gifico, Vincenzo Vaccaro<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-055<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17802 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-cfd tag-fluid-structure-interaction tag-highly-flexible-rotating-blades tag-mav tag-nonlinear-steady-state category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/nonlinear-aeroelastic-steady-simulation-applied-tohighly-flexible-blades-for-mav\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR AEROELASTIC STEADY SIMULATION APPLIED TO HIGHLY FLEXIBLE BLADES FOR MAV\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 Gill Di Vincenzo, Mauro Linari, Dr F. Mohdzawawi, Dr J. Morlier<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-056<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17805 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-aeroelasticity tag-flutter tag-hysteresis tag-iom-method tag-structural-dynamics category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/nonlinear-flutter-analysis-of-a-missile-withnonlinearity-and-hysteresis\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR FLUTTER ANALYSIS OF A MISSILE WITH NONLINEARITY AND HYSTERESIS\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<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-057<\/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-17808 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-coupling tag-multi-stage tag-navier-stokes tag-turbomachine category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/overview-of-some-onera-recent-advances-in-rotatingmachines-numerical-aeroelasticity\/\" target=&quot;_blank&quot;>\n\t\t\t\tOVERVIEW OF SOME ONERA RECENT ADVANCES IN ROTATING MACHINES NUMERICAL 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>A.Dugeai, A.Placzek, Y. Mauffrey, S. Verley<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-060<\/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-17811 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aerodynamic-propeller-effects tag-particle-vortex-aerodynamics tag-very-exible-wing category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/inclusion-of-propeller-effects-on-aeroelasticbehavior-of-very-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tINCLUSION OF PROPELLER EFFECTS ON AEROELASTIC BEHAVIOR OF VERY FLEXIBLE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Patricia C. Teixeira, Carlos E. S. Cesnik<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-061<\/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-17814 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-high-angle-of-attack tag-nonlinear tag-stall tag-wind-tunnel category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/study-of-the-nonlinearity-in-the-aeroelasticresponse-at-high-angle-of-attack-by-wind-tunneltests-on-the-active-aeroelastic-test-bench\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTUDY OF THE NONLINEARITY IN THE AEROELASTIC RESPONSE AT HIGH ANGLE OF ATTACK BY WIND TUNNEL TESTS ON THE ACTIVE AEROELASTIC TEST BENCH\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Julien Ertveldt, Alfredo Lamberti, Ben De Pauw, Ali Rezayat, Rik Pintelon, Steve Vanlanduit<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-063<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17817 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-geometrically-non-linear-structures tag-quadratic-mode-shape-components tag-reducedorder-models category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/towards-a-non-linear-full-aircraft-model-forpassenger-aircraft-loads-calculations\/\" target=&quot;_blank&quot;>\n\t\t\t\tTOWARDS A NON-LINEAR FULL AIRCRAFT MODEL FOR PASSENGER AIRCRAFT LOADS CALCULATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Javon C. Farao, Arnaud G. Malan, Francesco Gambioli<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-064<\/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-17820 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-airfoil-utter tag-boundary-layer-transition tag-local-correlation-based-transition-model category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/cfd-based-flutter-prediction-for-high-reynoldsnumber-flows-with-free-boundary-layer-transition\/\" target=&quot;_blank&quot;>\n\t\t\t\tCFD-BASED FLUTTER PREDICTION FOR HIGH REYNOLDS NUMBER FLOWS WITH FREE BOUNDARY LAYER TRANSITION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Michael Fehrs, Jens Nitzsche, Anne Hebler<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-066<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17823 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-gust-load-alleviation tag-static-output-feedback tag-wind-tunnel-test category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/wind-tunnel-evaluation-of-a-static-output-feedbackcontroller-for-gust-load-alleviation-on-a-regionalaircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tWIND TUNNEL EVALUATION OF A STATIC OUTPUT FEEDBACK CONTROLLER FOR GUST LOAD ALLEVIATION ON A REGIONAL 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>Federico Fonte, Sergio Ricci, Paolo Mantegazza<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-068<\/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-17826 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-hypersonic-aerothermoelasticity tag-linearized-stability-analysis tag-reduced-order-modeling tag-scaling-laws category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/efficient-reduced-order-modeling-for-skin-panels-inhypersonic-flow-and-its-application-to-generatingaerothermoelastic-scaling-laws\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT REDUCED-ORDER MODELING FOR SKIN PANELS IN HYPERSONIC FLOW AND ITS APPLICATION TO GENERATING AEROTHERMOELASTIC SCALING LAWS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Daning Huang, Tomer Rokita, Peretz P. Friedmann<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-069<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17829 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-morphing tag-robust-optimization tag-rotorcraft tag-uncertainty-quantication category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/robust-aerodynamic-optimization-for-helicopterblade-morphing-airfoils\/\" target=&quot;_blank&quot;>\n\t\t\t\tROBUST AERODYNAMIC OPTIMIZATION FOR HELICOPTER BLADE MORPHING AIRFOILS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Francesca Fusi, Giuseppe Quaranta, Pietro M. Congedo<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-070<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17832 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-flutter tag-green-aviation tag-u-tail tag-wind-tunnel-tests category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/wind-tunnel-flutter-tests-of-a-u-tail-configuration-part-1model-design-and-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tWIND TUNNEL FLUTTER TESTS OF A U-TAIL CONFIGURATION PART 1:MODEL DESIGN AND TESTING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. Geeraert, A. Lepage, P. Stephani, D. Feldmann, W. H\u00e4berli<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-072<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17835 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-frequency-lock-in tag-transonic-shock-buffet tag-unsteady-aerodynamics category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/investigation-of-frequency-lock-in-phenomena-on-asupercritical-aerofoil-in-the-presence-of-transonicshock-oscillations\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATION OF FREQUENCY LOCK-IN PHENOMENA ON A SUPERCRITICAL AEROFOIL IN THE PRESENCE OF TRANSONIC SHOCK 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>Nicholas F. Giannelis, Gareth A. Vio<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-074<\/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-17838 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-flutter tag-limit-cycle-oscillations tag-von-karman-thin-plate-theory tag-vortex-lattice-method category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/limit-cycle-oscillations-of-cantilever-rectangularflat-plates-in-a-wind-tunnel\/\" target=&quot;_blank&quot;>\n\t\t\t\tLIMIT CYCLE OSCILLATIONS OF CANTILEVER RECTANGULAR FLAT PLATES IN A WIND TUNNEL\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>N. Giannelis, G. A. Vio, G. Dimitriadis<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-075<\/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-17841 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aeroservoelasticity tag-control-of-exible-aircraft tag-gain-scheduling category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/x-hale-autopilot-with-stability-augmentation-andshape-control-based-on-loop-separation\/\" target=&quot;_blank&quot;>\n\t\t\t\tX-HALE AUTOPILOT WITH STABILITY AUGMENTATION AND SHAPE CONTROL BASED ON LOOP SEPARATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Pedro J. Gonz\u00e1lez, Ant\u00f4nio B. Guimar\u00e3es Neto, Guilherme Chaves Barbosa, Rafael M. Bertolin, Fl\u00b4avio J. Silvestre, Carlos E. S. Cesnik<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-077<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17844 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-computational-uid-dynamics tag-crm tag-hirenasd tag-optimization tag-transonic category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/transonic-aeroelasticity-using-the-2-5d-non-linearvortex-lattice-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tTRANSONIC AEROELASTICITY USING THE 2.5D NON-LINEAR VORTEX-LATTICE 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>A.Grozdanov, E.Laurendeau<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-079<\/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-17847 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-exible-aircraft tag-ight-dynamics tag-large-deformations tag-small-deformations category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/validity-of-the-assumption-of-small-deformations-inaircraft-with-different-levels-of-structuralflexibility\/\" target=&quot;_blank&quot;>\n\t\t\t\tVALIDITY OF THE ASSUMPTION OF SMALL DEFORMATIONS IN AIRCRAFT WITH DIFFERENT LEVELS OF STRUCTURAL FLEXIBILITY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ant\u00f4nio B. Guimar\u00e3es Neto, Fl\u00e1vio J. Silvestre, Fl\u00e1vio L. C. Ribeiro, Fl\u00e1vio L. S. Bussamra, Roberto G. A. da Silva, Carlos E. S. Cesnik<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-080<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17851 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-exible-aircraft tag-ight-dynamics tag-wind-tunnel category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/response-and-stability-of-the-remotely-piloted-constrained-x-hale-aircraft-in-wind-tunnel\/\" target=&quot;_blank&quot;>\n\t\t\t\tRESPONSE AND STABILITY OF THE REMOTELY-PILOTED, CONSTRAINED X-HALE AIRCRAFT IN WIND TUNNEL\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ant\u00f4nio B. Guimar\u00e3es Neto, Fl\u00e1vio J. Silvestre, Fl\u00e1vio L. S. Bussamra, Roberto G. A. da Silva, Carlos E. S. Cesnik<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-081<\/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-17854 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-aeroelasticity tag-computational-uid-dynamics tag-dynamic-mode-decomposition tag-harmonic-balance-method tag-transonic-ow tag-unsteady-aerodynamics-modeling category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/research-on-fast-aeroelastic-modeling-methods-forthe-transonic-regime\/\" target=&quot;_blank&quot;>\n\t\t\t\tRESEARCH ON FAST AEROELASTIC MODELING METHODS FOR THE TRANSONIC REGIME\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>H\u00fcseyin G\u00fcner, Grigorios Dimitriadis, Vincent E. Terrapon<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-083<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17857 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-degenerate-transformation tag-dynamic-eigenmodes tag-modally-equivalent-perturbed-system tag-modes tag-nonlinear-system tag-reduced-order-model-2 category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/parametrically-rich-nonlinear-reduced-order-modeling-anapplication-in-viscous-incompressible-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tPARAMETRICALLY RICH NONLINEAR REDUCED-ORDER MODELING: AN APPLICATION IN VISCOUS INCOMPRESSIBLE FLOW\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>T. Kim, E.H. Dowell<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-085<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17860 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-aeroelasticity tag-flight-loads tag-turbulence category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/flight-loads-analysis-and-measurements-of-externalstores-on-an-atmospheric-research-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT LOADS ANALYSIS AND MEASUREMENTS OF EXTERNAL STORES ON AN ATMOSPHERIC RESEARCH AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vega Handojo, Thomas Klimmek, Wolf Kr\u00fcger<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-086<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17864 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-aeroelastic-stability tag-experiment tag-flutter-boundary tag-laminar-airfoil tag-transonic-flow-2 category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/experimental-assessment-of-the-flutter-stability-of-a-laminar-airfoil-in-transonic-flow\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL ASSESSMENT OF THE FLUTTER STABILITY OF A LAMINAR AIRFOIL IN TRANSONIC FLOW\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Anne Hebler<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-089<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17867 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-disturbance-velocity-approach tag-gust-encounter tag-resolved-atmosphere-approach tag-unsteady-simulation tag-wake-vortex-encounter category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/comparison-of-different-approaches-for-modeling-of-atmospheric-effects-like-gusts-and-wake-vortices-in-the-cfd-code-tau\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPARISON OF DIFFERENT APPROACHES FOR MODELING OF ATMOSPHERIC EFFECTS LIKE GUSTS AND WAKE-VORTICES IN THE CFD CODE TAU\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>R. Heinrich, L. Reimer<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-091<\/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-17870 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-computational-fluid-structure-interaction tag-high-aspect-ratio-wings tag-structural-wing-design category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/high-fidelity-trim-calculation-under-consideration-of-aeroelastic-effects-of-a-high-aspect-ratio-swept-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tHIGH FIDELITY TRIM CALCULATION UNDER CONSIDERATION OF AEROELASTIC EFFECTS OF A HIGH ASPECT RATIO SWEPT WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Andreas Hermanutz, Mirko Hornung<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-92<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17873 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-computer-programming tag-frequency-domain tag-matlab tag-nonlinear-connections tag-structural-dynamics category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/an-improved-software-for-frequency-domain-analysis-of-assembled-aircraft-structures-with-local-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN IMPROVED SOFTWARE FOR FREQUENCY DOMAIN ANALYSIS OF ASSEMBLED AIRCRAFT STRUCTURES 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>S. Hern\u00e1ndez, E. Menga, C. L\u00f3pez, A. Baldomir, M. Cid Montoya, D. Freire, S. Moledo, P. Naveira<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-093<\/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-17876 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-cfd tag-control-law tag-dynamic-coupling tag-gust-response category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/numerical-validation-of-gust-response-and-numerical-assessment-of-gust-load-alleviation-for-2d-aeroelastic-airfoil-in-transonic-conditions\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL VALIDATION OF GUST RESPONSE AND NUMERICAL ASSESSMENT OF GUST LOAD ALLEVIATION FOR 2D AEROELASTIC AIRFOIL IN TRANSONIC 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>Fabien HUVELIN, Arnaud LEPAGE, Charles POUSSOT-VASSAL<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-096<\/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-17879 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-arma tag-experimental-methods tag-flutter-ight-testing tag-operational-modal-analysis category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/assessment-of-advanced-flutter-flight-test-techniques-and-flutter-boundary-prediction-methods\/\" target=&quot;_blank&quot;>\n\t\t\t\tASSESSMENT OF ADVANCED FLUTTER FLIGHT TEST TECHNIQUES AND FLUTTER BOUNDARY PREDICTION METHODS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Maj. Michael Iovnovich, Lt. Tzlil Nahom, Lt. Michael Presman, Lt. Dorin Avsaid, Maj. Tomer Braier, Daniella E. Raveh<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-097<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17882 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-cfd tag-flutter tag-navier-stokes-code tag-t-tail tag-transonic category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/numerical-simulation-of-transonic-flutter-of-a-t-tail\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL SIMULATION OF TRANSONIC FLUTTER OF A T-TAIL\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. ISOGAI<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-098<\/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-17885 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-3-d-print tag-aeroelastic tag-cfd-csd tag-topology-optimization category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/topology-optimization-and-3-d-print-according-to-aeroelastic-behavior-of-high-aspect-ratio-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tTOPOLOGY OPTIMIZATION AND 3-D PRINT ACCORDING TO AEROELASTIC BEHAVIOR OF 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>Li Guo, Kaihua Yuan, Jinan Lv, Ziqiang Liu<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-099<\/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-17888 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-dlm-correction tag-gust-encounter tag-nasa-common-research-model tag-reduced-order-model-2 tag-time-linearized-cfd category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/comparison-of-nonlinear-cfd-with-time-linearized-cfd-and-cfd-corrected-dlm-for-gust-encounter-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPARISON OF NONLINEAR CFD WITH TIME-LINEARIZED CFD AND CFD-CORRECTED DLM FOR GUST ENCOUNTER SIMULATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christoph Kaiser, Diliana Friedewald, Jens Nitzsche<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-101<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17932 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-aeroelasticity tag-co-rotational tag-earities tag-ctitious-mass tag-geometric-structural-nonlin tag-large-deformations tag-modal-superposition tag-model-reduction-ifasd category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/nonlinear-structural-nonlinear-aerodynamic-model-for-static-aeroelastic-problems\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR-STRUCTURAL-NONLINEAR-AERODYNAMIC MODEL FOR STATIC AEROELASTIC PROBLEMS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Etay Kantor, Daniella E. Raveh<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-103<\/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-17935 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-flutter tag-limit-cycle-oscillation tag-wind-tunnel-testing category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/experimental-and-analytical-investigations-of-a-fighter-like-wind-tunnel-model-with-external-stores\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL AND ANALYTICAL INVESTIGATIONS OF A FIGHTER-LIKE WIND TUNNEL MODEL WITH EXTERNAL STORES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Anders Karlsson, Ulf Ringertz<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-105<\/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-17938 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-cfd tag-flutter tag-fsi category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/parametric-flutter-margins-of-a-twin-tail-configuration-in-wing-generated-buffet\/\" target=&quot;_blank&quot;>\n\t\t\t\tPARAMETRIC FLUTTER MARGINS OF A TWIN TAIL CONFIGURATION IN WING-GENERATED BUFFET\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Moti Karpel ,Federico Roizner, Robert Carrese, Pier Marzocca<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-106<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17941 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-3d-panel-methods tag-aerodynamic-inuence-coefcients tag-dutch-roll tag-integrated-exible-ight-dynamics-model tag-lateral-gust tag-loads-analysis category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/an-integrated-model-for-lateral-gust-loads-analysis-and-dutch-roll-flight-dynamics-using-a-3d-panel-method\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN INTEGRATED MODEL FOR LATERAL GUST LOADS ANALYSIS AND DUTCH ROLL FLIGHT DYNAMICS USING 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<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-107<\/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-17944 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-3d-printing tag-additive-manufacturing tag-aeroelasticity tag-evolutionary-design tag-experimental-testing tag-size-optimization tag-topology-optimization category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/validation-of-topology-optimized-lifting-surfaces-using-3-d-printing\/\" target=&quot;_blank&quot;>\n\t\t\t\tVALIDATION OF TOPOLOGY OPTIMIZED LIFTING SURFACES USING 3-D PRINTING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Joshua D. Deaton, Raymond M. Kolonay, Robert Reuter, Marcelo H. Kobayashi<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-108<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17947 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-active-control-and-adaptive-structures tag-highly-flexible-aircraft-structures tag-wind-tunnel-and-flight-testing category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/closed-loop-flight-tests-with-an-unmanned-experimental-multi-body-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tCLOSED-LOOP FLIGHT TESTS WITH AN UNMANNED EXPERIMENTAL MULTI-BODY AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alexander K\u00f6the, Alexander Behrens, Alexander Hamann, Phillip Nagel, Danny Nowka, Robert Luckner<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-111<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17950 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-d-partition-method tag-dynamic-stiffness tag-ground-vibration-testing tag-identification tag-laboratory-testing tag-landing-gear tag-mathematical-models-mm tag-oscillation-modes tag-shimmy tag-spectral-analysis category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/experimental-determination-of-dynamic-characteristics-of-aircraft-landing-gear-and-methods-of-identification-of-their-modal-characteristics\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL DETERMINATION OF DYNAMIC CHARACTERISTICS OF AIRCRAFT LANDING GEAR AND METHODS OF IDENTIFICATION OF THEIR MODAL 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>A.V. Krapivko, O.A. Orlova, V.N. Zadonskaya<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-112<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17953 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-blade-off tag-engine-imbalance tag-forced-vibrations tag-ground-vibration-tests tag-simulation tag-wind-milling category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/modeling-of-forced-vibrations-of-the-airplane-with-the-engine-imbalance-%d0%b0t-ground-resonance-tests\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODELING OF FORCED VIBRATIONS OF THE AIRPLANE WITH THE ENGINE IMBALANCE \u0410T GROUND RESONANCE 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>Regina V. Leonteva, Mikhail A. Pronin, Vsevolod I. Smyslov<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-114<\/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-17956 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-fluid-structure-interaction-fsi tag-full-aircraft-model-fam tag-nasa-common-research-problem-crm tag-split-velocity-method-svm category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/a-cfd-based-aeroelastic-gust-model-for-full-aircraft-simulation\/\" target=&quot;_blank&quot;>\n\t\t\t\tA CFD BASED AEROELASTIC GUST MODEL FOR FULL AIRCRAFT SIMULATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>William D. C. Liw Tat Man, Andrew G. B. Mowat, Arnaud G. Malan, Javon C. Farao<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-117<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17959 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-co-simulation tag-mesh-deformation tag-multibody tag-radial-basis-functions category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/16\/static-fully-coupled-simulation-of-a-transport-aircraft-high-lift-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTATIC FULLY COUPLED SIMULATION OF A TRANSPORT AIRCRAFT HIGH-LIFT 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>Alessandro Lurgo, Robert Jung<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-119<\/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-17984 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-rotorcraft-aeroelasticity tag-double-sweep tag-rotary-wing-aeroelasticity tag-structural-dynamics category-993 category-1953 category-1963 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/19\/aeroelastic-analysis-of-double-swept-rotor-blade-in-hovering-conditions\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC ANALYSIS OF DOUBLE-SWEPT ROTOR BLADE IN HOVERING 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. Rohin Kumar, Lokeswara Rao. V<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-121<\/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-17987 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-aeroelasticity tag-airbrake tag-buffet tag-hankel tag-mitigation tag-uncertainty category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/19\/development-of-a-buffet-load-mitigation-system-based-on-multi-surface-control\/\" target=&quot;_blank&quot;>\n\t\t\t\tDEVELOPMENT OF A BUFFET LOAD MITIGATION SYSTEM BASED ON MULTI-SURFACE CONTROL\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Sheharyar Malik, Luca Riccobene, Sergio Ricci, Daniele Monti<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-122<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17990 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-experimental-database tag-flutter tag-intersecting-surfaces tag-numerical-correlation tag-u-tail tag-wind-tunnel-tests category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/19\/wind-tunnel-flutter-tests-of-a-u-tail-configuration-part-2-experimental-and-numerical-results\/\" target=&quot;_blank&quot;>\n\t\t\t\tWIND TUNNEL FLUTTER TESTS OF A U-TAIL CONFIGURATION PART 2: EXPERIMENTAL AND NUMERICAL RESULTS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Hadrien J. Mamelle, Gabriel Broux, Eric C. Garrigues<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-124<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17993 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aircraft tag-fem tag-lco tag-pylon category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/19\/an-investigation-in-hi-fi-finite-element-modelling-aimed-to-improve-lco-prediction\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN INVESTIGATION IN HI-FI FINITE ELEMENT MODELLING AIMED TO IMPROVE LCO PREDICTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. Manes, A. Gilioli, M. Giglio<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-125<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17996 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-aerostructural-optimization tag-aircraft-design tag-multidisciplinary-design-optimization category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/19\/enabling-practical-wing-design-via-high-fidelity-multidisciplinary-optimization\/\" target=&quot;_blank&quot;>\n\t\t\t\tENABLING PRACTICAL WING DESIGN VIA HIGH-FIDELITY MULTIDISCIPLINARY OPTIMIZATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Joaquim R. R. A. Martins, Timothy R. Brooks<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-127<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-17999 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-aeroelastic-tailoring tag-composite-optimization tag-forward-swept-wing category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/19\/optimization-testing-of-aeroelastically-tailored-forward-swept-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tOPTIMIZATION &amp; TESTING OF AEROELASTICALLY-TAILORED FORWARD SWEPT 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>Yasser M. Meddaikar, Johannes K.S. Dillinger, Yves Govers<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-129<\/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-18002 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-composite tag-flutter tag-optimization tag-stacking-table tag-structural-sizing category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/19\/a-new-dassault-industrial-approach-for-aero-structural-optimization-of-composite-structures-with-stacking-table-constraints\/\" target=&quot;_blank&quot;>\n\t\t\t\tA NEW DASSAULT INDUSTRIAL APPROACH FOR AERO-STRUCTURAL OPTIMIZATION OF COMPOSITE STRUCTURES WITH STACKING TABLE 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>Sean M. Meldrum , Ludovic Colo, Gabriel Broux, Eric Garrigues<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-130<\/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-18006 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-junctions tag-metamodel tag-structural-dynamics tag-uncertainty-quantication category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/uncertainty-quantification-in-the-dynamic-response-of-assembled-structures\/\" target=&quot;_blank&quot;>\n\t\t\t\tUNCERTAINTY QUANTIFICATION IN THE DYNAMIC RESPONSE OF ASSEMBLED 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>E. Menga, C. L\u00f3pez, S. Hern\u00e1ndez, A. Baldomir, I. Romero, M. J. S\u00e1nchez<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-132<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18009 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-business-jet tag-comfort tag-model-reduction tag-vibration-control category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/demonstration-of-innovative-vibration-control-on-a-falcon-business-jet\/\" target=&quot;_blank&quot;>\n\t\t\t\tDEMONSTRATION OF INNOVATIVE VIBRATION CONTROL ON A FALCON BUSINESS JET\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Claire MEYER, Gabriel BROUX, Julien PRODIGUE, Olivier CANTINAUD, Charles POUSSOT-VASSAL<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-133<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18012 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-bscw tag-ddes tag-shock-buffet category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/delayed-des-in-su2-test-case-3-from-the-second-aiaa-aeroelastic-prediction-workshop\/\" target=&quot;_blank&quot;>\n\t\t\t\tDELAYED DES IN SU2: TEST CASE 3 FROM THE SECOND AIAA AEROELASTIC PREDICTION WORKSHOP\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Eduardo S. Molina, Cleber Spode, Roberto Gil A. da Silva, Marcello Righi, Thomas D. Economon, Juan J. Alonso<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-134<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18015 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-arma tag-dmd tag-flutter-testing category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/flight-flutter-testing-using-higher-order-dynamic-mode-decomposition\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT FLUTTER TESTING USING HIGHER ORDER DYNAMIC MODE DECOMPOSITION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Rub\u00e9n Moreno-Ramos, Soledad Le Clainche, Jos\u00e9 M. Vega, Paul F. Taylor<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-135<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18018 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-computational-aeroelasticity tag-reduced-order-models category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/self-adaptive-pod-based-rom-aeroelastic-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tSELF ADAPTIVE POD BASED ROM AEROELASTIC SIMULATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Rub\u00e9n Moreno-Ramos, Fernando Varas, Jos\u00e9 M. Vega<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-136<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18021 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-active-utter-control tag-linear-compressor-cascade tag-plasma-actuators tag-virtual-surfaces category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/numerical-investigation-of-virtual-control-surfaces-for-aeroelastic-control-on-compressor-blades\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL INVESTIGATION OF VIRTUAL CONTROL SURFACES FOR AEROELASTIC CONTROL ON COMPRESSOR BLADES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Valentina Motta, Leonie Malzacher, Dieter Peitsch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-137<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18024 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-eigen-behavior tag-gyroscopic-moment tag-multibody tag-uhbr category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/structural-dynamic-influence-of-an-uhbr-engine-on-a-coanda-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTRUCTURAL DYNAMIC INFLUENCE OF AN UHBR ENGINE ON A COANDA-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>T. S. M\u00fcller, H. Hennings<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-138<\/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-18027 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-optimisation tag-resonance tag-topology tag-vibrations category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/topology-optimisation-of-representative-aircraft-wing-geometries-with-an-experimental-validation\/\" target=&quot;_blank&quot;>\n\t\t\t\tTOPOLOGY OPTIMISATION OF REPRESENTATIVE AIRCRAFT WING GEOMETRIES WITH AN EXPERIMENTAL VALIDATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>David J. Munk, Gareth A. Vio, Nicholas F. Giannelis, Jonathan E. Cooper<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-139<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18030 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-apping-wing-propulsion tag-ow-structure-interactions tag-swimming-ying tag-vortex-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/the-leading-edge-vortex-in-flexible-wing-propulsion\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHE LEADING EDGE VORTEX IN FLEXIBLE WING PROPULSION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ravi C. Mysa, Kartik Venkatraman<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-140<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18033 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-aerothermoelastic tag-hypersonic tag-perturbation-method category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/a-static-aerothermoelastic-response-analysis-method-with-considering-stiffness-uncertainty\/\" target=&quot;_blank&quot;>\n\t\t\t\tA STATIC AEROTHERMOELASTIC RESPONSE ANALYSIS METHOD WITH CONSIDERING STIFFNESS UNCERTAINTY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Nan Yi, Zhiqiang Wan, Chao Yang, Siyan Zhu<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-141<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18036 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aepw tag-aeroelasticity tag-bscw tag-computational tag-dynamics tag-uid tag-utter tag-transonic category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/effect-of-angle-of-attack-gas-composition-and-reynolds-number-on-flutter-boundary-of-benchmark-super-critical-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFECT OF ANGLE OF ATTACK, GAS COMPOSITION AND REYNOLDS NUMBER ON FLUTTER BOUNDARY OF BENCHMARK SUPER-CRITICAL WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jan Navr\u00e1til, Adam Jir\u00e1sek, Peter Hamlington, Lt. Col. Andrew Lofthouse<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-142<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18039 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-composite-materials tag-machine-learning tag-polynomial-chaos tag-uncertainty-quantication category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/uncertainty-quantification-in-the-vicinity-of-mode-switches-in-the-flutter-response-of-a-composite-cantilevered-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tUNCERTAINTY QUANTIFICATION IN THE VICINITY OF MODE SWITCHES IN THE FLUTTER RESPONSE OF A COMPOSITE CANTILEVERED 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, Angela Vincenti, Jean-Camille Chassaing<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-144<\/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-18042 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-asymmetry tag-electromechanical-modeling tag-flutter tag-numerical-simulation category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/numerical-simulation-and-experimental-flutter-research-of-an-aircraft-with-asymmetric-control-surfaces\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL SIMULATION AND EXPERIMENTAL FLUTTER RESEARCH OF AN AIRCRAFT WITH ASYMMETRIC CONTROL SURFACES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>O. A. Orlova, M. A. Pronin, V. I. Smyslov<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-146<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18045 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-computational-uid-dynamics tag-ight-dynamics tag-model-reduction category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/model-reduction-for-gust-load-analysis-of-free-flying-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tMODEL REDUCTION FOR GUST LOAD ANALYSIS OF FREE-FLYING AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>G. Pagliuca, P. Bekemeyer, R. Thormann, S. Timme<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-148<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18048 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-adjoint-sensititivities tag-algorithmic-differentiation tag-uid-structure-interaction tag-geometrically-nonlinear-structures tag-multidisciplinary-optimization tag-viscous-ows category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/computing-derivatives-in-nonlinear-aeroelasticity-using-algorithm-differentiation\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPUTING DERIVATIVES IN NONLINEAR AEROELASTICITY USING ALGORITHM DIFFERENTIATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ruben Sanchez, Rafael Palacios<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-149<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18051 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-aeroelasticity tag-state-space-models tag-unsteady-aerodynamics tag-unsteady-vortexlattice-method category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/state-space-realizations-and-model-reduction-of-potential-flow-unsteady-aerodynamics-with-arbitrary-kinematics\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTATE-SPACE REALIZATIONS AND MODEL REDUCTION OF POTENTIAL-FLOW UNSTEADY AERODYNAMICS WITH ARBITRARY KINEMATICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Rafael Palacios, Robert J. S. Simpson, Salvatore Maraniello<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-150<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18054 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-additive tag-fabrication tag-morphing tag-sensing tag-stretchable tag-topology category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/from-model-to-manufacture-additive-aeroelastic-morphing-testbeds\/\" target=&quot;_blank&quot;>\n\t\t\t\tFROM MODEL TO MANUFACTURE: ADDITIVE AEROELASTIC MORPHING TESTBEDS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Alexander M. Pankonien, James O. Hardin, Nitin Bhagat, Gregory W. Reich, John D. Berrigan<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-151<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18057 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-aeroelasticity-real-time-simulation tag-exible-aircraft tag-ight-dynamics tag-reduced-order-modeling-2 category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/application-of-nonlinear-model-order-reduction-technique-to-a-flexible-aircraft-for-real-time-simulations\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF NONLINEAR MODEL ORDER REDUCTION TECHNIQUE TO A FLEXIBLE AIRCRAFT FOR REAL-TIME SIMULATIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Juliano A. Paulino, Fl\u00e1vio J. Silvestre, Ant\u00f4nio B. Guimar\u00e3es Neto, Tiago P. Monteiro, Roberto Gil A. da Silva, Andrea Da Ronch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-152<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18060 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-landing tag-loads tag-structural-dynamics category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/hard-landing-and-rebound-landing-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tHARD LANDING AND REBOUND LANDING LOADS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. P\u00e9rez de la Serna, S. Parra Ad\u00e1n, E. G\u00f3mez Vi\u00f1as, H. Climent M\u00e1\u00f1ez<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-153<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18063 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-adaptive-structures tag-gust tag-morphing tag-passive-and-semi-active-control category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/camber-morphing-airfoils-to-reduce-gust-susceptibility\/\" target=&quot;_blank&quot;>\n\t\t\t\tCAMBER-MORPHING AIRFOILS TO REDUCE GUST SUSCEPTIBILITY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Giuliano Tuzzi, Giuseppe Quaranta<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-158<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18066 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-continuous-turbulence tag-gust-encounter tag-nonlinear tag-rom tag-volterra-series category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/a-nonlinear-frequency-domain-aerodynamic-model-for-continuous-turbulence-encounter-based-on-functional-series-expansion\/\" target=&quot;_blank&quot;>\n\t\t\t\tA NONLINEAR FREQUENCY DOMAIN AERODYNAMIC MODEL FOR CONTINUOUS TURBULENCE ENCOUNTER BASED ON FUNCTIONAL SERIES EXPANSION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>David Quero, Wolf Kr\u00fcger<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-159<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18069 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-gust-loads tag-optimization tag-reduced-oder-model tag-structural-dynamics category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/preliminary-aeroelastic-design-framework-for-composite-wings-subjected-to-gust-loads\/\" target=&quot;_blank&quot;>\n\t\t\t\tPRELIMINARY AEROELASTIC DESIGN FRAMEWORK FOR COMPOSITE WINGS SUBJECTED TO GUST LOADS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Darwin Rajpal, Roeland De Breuker<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-160<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18073 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-cantilevered-plate tag-exible-wings tag-uid-structure-interaction-2 tag-hale tag-leading-edge-vortices category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/experimental-and-numerical-investigation-of-post-flutter-limit-cycle-oscillations-on-a-cantilevered-flat-plate\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL AND NUMERICAL INVESTIGATION OF POST-FLUTTER LIMIT CYCLE OSCILLATIONS ON A CANTILEVERED FLAT PLATE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kiran Ramesh, Tiago Priolli Monteiro, Fl\u00e1vio Jos\u00e9 Silvestre, Ant\u00f4nio Bernardo Guimar\u00e3es Neto, Thiago de Souza Siqueira Versiani, Roberto Gil Annes da Silva<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-161<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18076 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-cfd tag-apping-wings tag-uid-structure tag-interaction-energy-harvesting tag-leading-edge-vortices category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/numerical-investigation-of-self-sustained-limit-cycle-oscillations-in-a-flapping-foil-energy-harvester\/\" target=&quot;_blank&quot;>\n\t\t\t\tNUMERICAL INVESTIGATION OF SELF-SUSTAINED LIMIT-CYCLE OSCILLATIONS IN A FLAPPING-FOIL ENERGY HARVESTER\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Enhao Wang, Kiran Ramesh, Ignazio Maria Viola, Shaun Killen<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-162<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18079 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelastic-prediction-workshop tag-flutter-analysis category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/flutter-analysis-for-the-second-aeroelastic-prediction-workshop\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLUTTER ANALYSIS FOR THE SECOND AEROELASTIC PREDICTION WORKSHOP\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Daniella E. Raveh<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-163<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18082 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-acoustic-blocage tag-aeroelasticity tag-utter tag-linear-method tag-lrans tag-shock-wave-boundary-layer-interaction-4 tag-turbomachinery category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/influence-of-reduced-frequency-on-choke-flutter-instability-in-transonic-uhbr-fan\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF REDUCED FREQUENCY ON CHOKE FLUTTER INSTABILITY IN TRANSONIC UHBR FAN\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Q. Rendu, S. Aubert, P. Ferrand<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-164<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18085 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-increased-order-modeling tag-structural-dynamics category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/increased-order-aeroservoelastic-modeling-in-practice\/\" target=&quot;_blank&quot;>\n\t\t\t\tINCREASED-ORDER AEROSERVOELASTIC MODELING IN PRACTICE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Manuel Reyes, Hector Climent, Moti Karpel, Felix Ar\u00e9valo, Carlos Maderuelo<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-165<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18088 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-discrete-vortex-method tag-flexible-airfoils tag-free-wake tag-unsteady-aerodynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/semi-analytical-unsteady-aerodynamic-modeling-for-a-flexible-thin-airfoil-in-arbitrary-motion\/\" target=&quot;_blank&quot;>\n\t\t\t\tSEMI-ANALYTICAL UNSTEADY AERODYNAMIC MODELING FOR A FLEXIBLE THIN AIRFOIL IN ARBITRARY MOTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Cristina Riso, Giorgio Riccardi, Franco Mastroddi<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-167<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18091 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-aeroelasticity-turbulence-modelling tag-hybrid-rans-les-2 tag-les tag-rans tag-structural-dynamics tag-unsteady-aerodynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/on-the-adoption-of-hybrid-rans-les-turbulence-modelling-technique-for-aeroelastic-problems\/\" target=&quot;_blank&quot;>\n\t\t\t\tON THE ADOPTION OF HYBRID RANS-LES TURBULENCE MODELLING TECHNIQUE FOR AEROELASTIC PROBLEMS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Marcello Righi<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-168<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18094 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-aeroelasticity tag-utter tag-transonic tag-wind-tunnel category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/design-and-testing-of-a-full-span-aeroelastic-wind-tunnel-model\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN AND TESTING OF A FULL SPAN AEROELASTIC WIND TUNNEL MODEL\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ulf Ringertz, David Eller, Donald F. Keller, Walter A. Silva<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-169<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18097 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-finite-element-method tag-fluid-structure-interaction tag-highly-flexible-aircraft tag-inertia-relief tag-nonlinear-aeroelastic-trim category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/a-fem-based-approach-for-nonlinear-aeroelastic-trim-of-highly-flexible-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tA FEM-BASED APPROACH FOR NONLINEAR AEROELASTIC TRIM OF HIGHLY FLEXIBLE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Cristina Riso, Fausto G. Di Vincenzo, Markus Ritter, Carlos E. S. Cesnik, Franco Mastroddi<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-170<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18100 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-extended-modal-approach tag-geometrically-large-deformations tag-nonlinear-flight-dynamics tag-unsteady-vortex-lattice tag-very-exible-aircraft tag-x-hale category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/free-flight-nonlinear-aeroelastic-simulations-of-the-x-hale-uav-by-an-extended-modal-approach\/\" target=&quot;_blank&quot;>\n\t\t\t\tFREE-FLIGHT NONLINEAR AEROELASTIC SIMULATIONS OF THE X-HALE UAV BY AN EXTENDED MODAL APPROACH\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Markus Ritter, Jessica Jones, Carlos E. S. Cesnik<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-171<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18103 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aeroservoelasticity tag-flutter tag-lco category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/aeroservoelastic-stability-analysis-using-response-based-parametric-flutter-margins\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROSERVOELASTIC STABILITY ANALYSIS USING RESPONSE-BASED PARAMETRIC FLUTTER MARGINS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Federico Roizner, Moti Karpel<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-172<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18106 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-exible-wing tag-utter tag-small-disturbance-cfd tag-structural-dynamics category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/aeroelastic-analysis-of-a-flutter-demonstrator-with-a-very-flexible-high-aspect-ratio-swept-wing\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC ANALYSIS OF A FLUTTER DEMONSTRATOR WITH A VERY FLEXIBLE HIGH-ASPECT-RATIO SWEPT WING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Vladyslav Rozov, Andreas Hermanutz, Christian Breitsamter, Mirko Hornung<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-173<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18109 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-lco tag-supersonic-transport tag-transonic-flow-2 tag-wind-tunnel-test category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/limit-cycle-oscillation-of-a-supersonic-transport-model-in-a-transonic-wind-tunnel-test\/\" target=&quot;_blank&quot;>\n\t\t\t\tLIMIT CYCLE OSCILLATION OF A SUPERSONIC TRANSPORT MODEL IN A TRANSONIC WIND TUNNEL TEST\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kenichi SAITOH, Norio YOSHIMOTO, Hamidreza KHEIRANDISH<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-174<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18112 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-aeroservoelasticity tag-double-lattice-method tag-finite-element-method tag-flexible-aircraft tag-flutter-suppression tag-gust-alleviation category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/on-the-control-of-aeroelastic-flight-dynamic-integrated-stability-of-maneuvering-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tON THE CONTROL OF AEROELASTIC\/FLIGHT DYNAMIC INTEGRATED STABILITY OF MANEUVERING AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Francesco Saltari, Franco Mastroddi, Cristina Riso, Guido De Matteis, Sara Colaianni<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-175<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18115 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-buffet-forcing-functions tag-experimental-unsteady-aerodynamics tag-launch-vehicle-buffet category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/effect-of-circumferential-surface-pressure-integration-on-launch-vehicle-buffet-forcing-functions\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFECT OF CIRCUMFERENTIAL SURFACE PRESSURE INTEGRATION ON LAUNCH VEHICLE BUFFET FORCING FUNCTIONS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Martin K. Sekula, David J. Piatak, Russ D. Rausch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-176<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18118 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-aeroelasticity tag-control tag-repetitive tag-structural-dynamics category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/individual-blade-repetitive-control-for-horizontal-axis-wind-turbines\/\" target=&quot;_blank&quot;>\n\t\t\t\tINDIVIDUAL BLADE REPETITIVE CONTROL FOR HORIZONTAL-AXIS WIND TURBINES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Riccardo Fratini, Jacopo Serafini, Massimo Gennaretti, Riccardo Santini, Stefano Panzieri<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-177<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18121 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-dynamic-wake-inow tag-helicopter-ight-dynamics tag-reduced-order-modeling-2 category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/application-of-low-order-wake-inflow-models-to-rotorcraft-aeromechanics\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF LOW-ORDER WAKE INFLOW MODELS TO ROTORCRAFT AEROMECHANICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>J. Serafini, F. Cardito, G. Bernardini, M. Gennaretti<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-179<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18124 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-wind-tunnel-2 category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/computational-and-experimental-results-for-the-kth-nasa-wind-tunnel-model-used-for-acquisition-of-transonic-nonlinear-aeroelastic-data\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPUTATIONAL AND EXPERIMENTAL RESULTS FOR THE KTH-NASA WIND-TUNNEL MODEL USED FOR ACQUISITION OF TRANSONIC NONLINEAR AEROELASTIC DATA\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Walter A. Silva, Pawel Chwalowski, Carol D. Wieseman, Donald F. Keller, David Eller, Ulf Ringertz<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-180<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18127 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-aeroelastic-analysys tag-cfd tag-rom category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/aerom-nasas-unsteady-aerodynamic-and-aeroelastic-reduced-order-modeling-software\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROM: NASA\u2019S UNSTEADY AERODYNAMIC AND AEROELASTIC REDUCED-ORDER MODELING SOFTWARE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Walter A. Silva<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-181<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18130 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-cfd tag-gust tag-optimisation tag-parameterisation tag-potential-ow tag-reconstruction tag-rom category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/reconstruction-of-gust-velocity-profiles-via-potential-flow-cfd-and-rom-techniques\/\" target=&quot;_blank&quot;>\n\t\t\t\tRECONSTRUCTION OF GUST VELOCITY PROFILES VIA POTENTIAL FLOW, CFD AND ROM TECHNIQUES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Simone Simeone, Thomas Rendall, Stephen Williams, Christopher Wales, Jonathan E. Cooper, Dorian Jones, Ann L. Gaitonde<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-182<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18133 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-flight-vibration-test tag-online-aeroelastic-identification category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/flight-testing-using-fast-online-aeroelastic-identification-techniques-with-dlr-research-aircraft-halo\/\" target=&quot;_blank&quot;>\n\t\t\t\tFLIGHT TESTING USING FAST ONLINE AEROELASTIC IDENTIFICATION TECHNIQUES WITH DLR RESEARCH AIRCRAFT HALO\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>J. Sinske, Y.Govers, G. Jelicic, R. Buchbach, J. Schwochow, V. Handojo, M. B\u00f6swald, W.R. Kr\u00fcger<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-183<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18136 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-divergence tag-experimental-aeroelasticity tag-flutter tag-parametric-flutter-margin category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/experimental-investigation-of-flutter-boundary-with-controlled-vibration-levels\/\" target=&quot;_blank&quot;>\n\t\t\t\tEXPERIMENTAL INVESTIGATION OF FLUTTER BOUNDARY WITH CONTROLLED VIBRATION LEVELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jurij Sodja , Federico Roizner, Roeland De Breuker, Moti Karpel<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-184<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18140 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-gust-generator tag-unsteady-aerodynamics tag-unsteady-loads category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/investigation-of-the-unsteady-flow-over-a-wing-under-gust-excitation\/\" target=&quot;_blank&quot;>\n\t\t\t\tINVESTIGATION OF THE UNSTEADY FLOW OVER A WING UNDER GUST EXCITATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Paul Lancelot, Jurij Sodja, Roeland De Breuker<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-185<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18143 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-cfd-mesh-deformation tag-cfd-mesh-repair tag-cfd-csm tag-uid-structure-interaction tag-multi-body-simulation-2 tag-nonlinear-fem category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/high-fidelity-cfd-csm-interaction-in-the-industrial-context\/\" target=&quot;_blank&quot;>\n\t\t\t\tHIGH-FIDELITY CFD-CSM INTERACTION IN THE INDUSTRIAL CONTEXT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Bernd Stickan, Arne Rempke, Sebastian Helm, Hans Bleecke<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-186<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18146 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-cfd tag-gust category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/linearized-unsteady-cfd-for-gust-loads-with-tau\/\" target=&quot;_blank&quot;>\n\t\t\t\tLinearized Unsteady CFD for Gust Loads with TAU\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Wolfgang Weigold, Bernd Stickan, Inocencio Travieso-Alvarez, Christoph Kaiser, Patrick Teufel<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-187<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18149 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-distributed-control tag-exible-aircraft tag-optimum-wing-geometry tag-wing-shaping-control category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/22\/optimum-distributed-wing-shaping-and-control-loads-for-highly-flexible-mission-adaptive-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tOPTIMUM DISTRIBUTED WING SHAPING AND CONTROL LOADS FOR HIGHLY FLEXIBLE MISSION-ADAPTIVE AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Jared R. Hammerton, Weihua Su, Guoming Zhu, Sean Shan-Min Swei<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-189<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18153 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-dampers tag-discrete-gust tag-loads-alleviation tag-passive tag-truss-braced-wing category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/passive-gust-loads-alleviation-in-a-truss-braced-wing-using-integrated-dampers\/\" target=&quot;_blank&quot;>\n\t\t\t\tPASSIVE GUST LOADS ALLEVIATION IN A TRUSS-BRACED WING USING INTEGRATED DAMPERS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christopher P. Szczyglowski, Simon A. Neild, Brano Titurus, Jason Z. Jiang, Jonathan E. Cooper, Etienne Coetzee<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-190<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18156 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-adaptive-wing tag-aeroelasticity tag-structural-analysis category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/study-on-adaptive-wing-structure-for-compromising-structural-strength-and-aerodynamic-performance\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTUDY ON ADAPTIVE WING STRUCTURE FOR COMPROMISING STRUCTURAL STRENGTH AND AERODYNAMIC PERFORMANCE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>TAMAYAMA Masato, FUJII Kanata, YOKOZEKI Tomohiro, ARIZONO Hitoshi<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-191<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18159 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-control-system-nonlinearities tag-lyapunov-exponents tag-stability category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/quantitative-aeroelastic-stability-evaluation-of-control-surfaces-with-structural-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tQUANTITATIVE AEROELASTIC STABILITY EVALUATION OF CONTROL SURFACES WITH STRUCTURAL NONLINEARITIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Aykut Tamer, Pierangelo Masarati<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-192<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18162 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-bifucation-analysis tag-landing-gears tag-lco tag-optimization tag-shimmy category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/reliable-robust-optimization-of-a-landing-gear-system\/\" target=&quot;_blank&quot;>\n\t\t\t\tRELIABLE &amp; ROBUST OPTIMIZATION OF A LANDING GEAR SYSTEM\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Irene Tartaruga, Jonathan E. Cooper, Mark H. Lowenberg, Yves Lemmens<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-193<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18165 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-cfd tag-field-velocity-method tag-flight-dynamics tag-resolved-gust category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/influence-of-gust-modelling-on-free-flight-aerofoils\/\" target=&quot;_blank&quot;>\n\t\t\t\tINFLUENCE OF GUST MODELLING ON FREE-FLIGHT 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>Reik Thormann, Giampaolo Pagliuca, Sebastian Timme<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-195<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18168 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-flutter tag-laminar-wing tag-risk-analysis tag-transition tag-transonic-flow-2 tag-unsteady-aerodynamics category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/risk-analysis-for-flutter-of-laminar-wings\/\" target=&quot;_blank&quot;>\n\t\t\t\tRISK ANALYSIS FOR FLUTTER OF LAMINAR WINGS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Lorenz Tichy, Holger Mai, Michael Fehrs, Jens Nitzsche, Anne Hebler<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-196<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18171 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-geometric-nonlinearity tag-hyper-reduction tag-model-order-reduction tag-simulation-free-trainingj146 tag-structural-dynamics category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/simulation-free-hyper-reduced-models-for-geometrically-nonlinear-structural-dynamics\/\" target=&quot;_blank&quot;>\n\t\t\t\tSIMULATION-FREE HYPER-REDUCED MODELS FOR GEOMETRICALLY NONLINEAR STRUCTURAL DYNAMICS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>S. Jain, P. Tiso<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-197<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18174 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-load-control-and-alleviation tag-wingtip-devices category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/design-of-an-innovative-wing-tip-device\/\" target=&quot;_blank&quot;>\n\t\t\t\tDESIGN OF AN INNOVATIVE WING TIP DEVICE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>F. Toffol, F. Fonte, S. Ricci<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-198<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18177 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-cfd tag-fluid-structure-interaction-2 tag-gust-encounter tag-structural-dynamics category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/an-optimized-doublet-lattice-method-correction-approach-for-a-large-civil-aircraft\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN OPTIMIZED DOUBLET-LATTICE METHOD CORRECTION APPROACH FOR A LARGE CIVIL AIRCRAFT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>C. Valente, C. Wales, D. Jones, A. Gaitonde, J. E. Cooper, Y. Lemmens<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-200<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18180 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aeroelasticity tag-freeplay tag-ifasd tag-nltva tag-nonlinear category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/freeplay-induced-limit-cycle-oscillation-mitigation-using-linear-and-nonlinear-tuned-vibration-absorbers\/\" target=&quot;_blank&quot;>\n\t\t\t\tFREEPLAY-INDUCED LIMIT CYCLE OSCILLATION MITIGATION USING LINEAR AND NONLINEAR TUNED VIBRATION ABSORBERS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>E. Verstraelen, G. Kerschen, G. Dimitriadis<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-204<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18183 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-aeroelasticity tag-aic-correction tag-dynamic-coupling tag-small-disturbance-cfd tag-structural-dynamics category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/efficient-and-accurate-aeroelastic-analyses-based-on-small-disturbance-cfd-in-early-aircraft-development\/\" target=&quot;_blank&quot;>\n\t\t\t\tEFFICIENT AND ACCURATE AEROELASTIC ANALYSES BASED ON SMALL-DISTURBANCE CFD IN EARLY AIRCRAFT DEVELOPMENT\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Cyrille Vidy, Lukas Katzenmeier, Maximilian Winter, Christian Breitsamter<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-205<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18186 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-aeroelasticity tag-dynamic-maneuver-loads tag-flight-test tag-preliminary-design tag-sailplane tag-structural-dynamics category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/dynamic-maneuver-loads-calculation-for-a-sailplane-and-comparison-with-flight-test\/\" target=&quot;_blank&quot;>\n\t\t\t\tDYNAMIC MANEUVER LOADS CALCULATION FOR A SAILPLANE AND COMPARISON WITH FLIGHT TEST\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Arne Vo\u00df, Gabriel Pinho Chiozzotto, Per Ohme<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-206<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18189 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-asymmetric-eigenmode tag-critical-speed tag-engine-aeroelasticity tag-engine-thrust tag-utter-frequency tag-follower-force tag-forward-sweep tag-gyroscopics tag-laminar-ow tag-t-tail-utter category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/the-aeroelastic-behaviour-of-a-forward-swept-wing-configuration-with-focus-on-engine-gyroscopics-and-t-tail-flutter\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHE AEROELASTIC BEHAVIOUR OF A FORWARD-SWEPT WING CONFIGURATION WITH FOCUS ON ENGINE GYROSCOPICS AND T-TAIL FLUTTER\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Stefan Waitz<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-207<\/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-18192 post type-post status-publish format-standard hentry category-events category-dynamic-loads category-ifasd-2017 tag-aic-correction-2 tag-dlm tag-gusts tag-uvlm category-993 category-1958 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/comparison-of-aerodynamic-models-for-1-cosine-gust-loads-prediction\/\" target=&quot;_blank&quot;>\n\t\t\t\tCOMPARISON OF AERODYNAMIC MODELS FOR 1-COSINE GUST LOADS PREDICTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Christopher Wales, R. G. Cook, D. P. Jones, A. L. Gaitonde<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-208<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18195 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-conceptual-phase tag-integrated-optimization-design tag-kriging tag-large-aircraft category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/an-integrated-optimization-and-surrogate-analysis-of-large-aircraft-in-conceptual-design\/\" target=&quot;_blank&quot;>\n\t\t\t\tAN INTEGRATED OPTIMIZATION AND SURROGATE ANALYSIS OF LARGE AIRCRAFT IN CONCEPTUAL DESIGN\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Xiaozhe Wang, Zhiqiang Wan, Chao Yang<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-209<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18198 post type-post status-publish format-standard hentry category-events category-aeroelasticity-in-conceptual-aircraft-design category-ifasd-2017 tag-aeroelasticity tag-composite-structure tag-conceptual-design tag-genetic-algorithm tag-multidisciplinary-design-optimization tag-strut-braced-wing category-993 category-1955 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/27\/multidisciplinary-design-optimization-of-wing-structure-for-strut-braced-wing-aircraft-considering-aeroelasticity\/\" target=&quot;_blank&quot;>\n\t\t\t\tMULTIDISCIPLINARY DESIGN OPTIMIZATION OF WING STRUCTURE FOR STRUT-BRACED WING AIRCRAFT CONSIDERING AEROELASTICITY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Wang Zexi, Wan Zhiqiang, Yang Chao, Zhu Siyan<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-210<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18202 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-adjoint-variables tag-bifurcation tag-utter tag-mesh-adaptation tag-piston-theory category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/adjoint-based-mesh-adaptation-for-direct-flutter-prediction\/\" target=&quot;_blank&quot;>\n\t\t\t\tADJOINT-BASED MESH ADAPTATION FOR DIRECT FLUTTER PREDICTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Kevin G. Wang, Philip S. Beran, Shunxiang Cao<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-212<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18205 post type-post status-publish format-standard hentry category-events category-active-control-and-adaptive-structures category-ifasd-2017 tag-aeroelastic tag-flutter tag-gusts tag-hinged-folding-wing-tips tag-load-alleviation tag-manoeuvres category-993 category-1954 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/aeroelastic-behaviour-of-hinged-wing-tips\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROELASTIC BEHAVIOUR OF HINGED WING TIPS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>T. Wilson, A. Castrichini, A. Azabal, J.E. Cooper, R. Ajaj, M. Herring<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-216<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18208 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-complex-conguration tag-crm tag-reduced-order-modeling-2 tag-unsteady-aerodynamics category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/application-of-unsteady-aerodynamic-reduced-order-modeling-techniques-to-a-complex-configuration\/\" target=&quot;_blank&quot;>\n\t\t\t\tAPPLICATION OF UNSTEADY AERODYNAMIC REDUCED-ORDER MODELING TECHNIQUES TO A COMPLEX CONFIGURATION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Maximilian Winter, Christian Breitsamter<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-217<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18211 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-limit-cycle-oscillation-2 tag-neural-network tag-openfoam tag-stall-flutter tag-unsteady-aerodynamics category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/nonlinear-aerodynamic-identification-and-stall-flutter-analysis\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR AERODYNAMIC IDENTIFICATION AND STALL FLUTTER ANALYSIS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>XIANG ZhengPing , DAI YuTing<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-219<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18214 post type-post status-publish format-standard hentry category-events category-highly-flexible-aircraft-structures category-ifasd-2017 tag-fsi tag-geometrical-nonlinear-fem tag-static-aeroelastic category-993 category-1961 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/nonlinear-static-aeroelastic-analysis-of-high-aspect-ratio-wing-based-on-cfd-csd-coupling-solution\/\" target=&quot;_blank&quot;>\n\t\t\t\tNONLINEAR STATIC AEROELASTIC ANALYSIS OF HIGH-ASPECT RATIO WING BASED ON CFD\/CSD COUPLING SOLUTION\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yang Lan , Xie Changchuan , Yang Chao , Zhang Bing , Andrea Da Rouch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-221<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18217 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-fiber-bragg-grating-fbg-sensors tag-large-deformations tag-shape-prediction tag-strain-displacement-transformation-sdt category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/deformed-wing-shape-prediction-using-fiber-optic-strain-data\/\" target=&quot;_blank&quot;>\n\t\t\t\tDEFORMED WING SHAPE PREDICTION USING FIBER OPTIC STRAIN DATA\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yang Meng, Changchuan Xie, Zhiqiang Wan<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-222<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18220 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-folding-wing tag-freeplay-nonlinearity tag-nonlinear-aeroelasticity tag-wind-tunnel-test category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/the-nonlinear-flutter-wind-tunnel-test-of-a-folding-fin-with-freeplay-nonlinearities\/\" target=&quot;_blank&quot;>\n\t\t\t\tTHE NONLINEAR FLUTTER WIND TUNNEL TEST OF A FOLDING FIN WITH FREEPLAY NONLINEARITIES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p>Yang Ning, Zhang Xin, Wang Nan, Liu Wei<\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-224<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18223 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-steady-unsteady-aerodynamics tag-coupling-model tag-flight-dynamics tag-hypersonic tag-local-piston category-993 category-1953 category-1964 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/rigidelastic-coupling-stability-analysis-of-hypersonic-vehicles\/\" target=&quot;_blank&quot;>\n\t\t\t\tRIGID&amp;ELASTIC COUPLING STABILITY ANALYSIS OF HYPERSONIC VEHICLES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yan Yihan, Xie Changchuan, He Jingwu, Jiang Chongwen<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-225<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18226 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-wind-tunnel-and-flight-testing tag-aeroelasticity tag-blended-wing-body tag-body-freedom-flutter tag-wind-tunnel-test category-993 category-1953 category-1965 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/body-freedom-flutter-of-a-flexible-blended-wing-body-like-plate-an-experimental-study\/\" target=&quot;_blank&quot;>\n\t\t\t\tBODY FREEDOM FLUTTER OF A FLEXIBLE BLENDED WING BODY LIKE PLATE &#8211; AN EXPERIMENTAL STUDY\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Yingsong Gu, Zhichun Yang, Pier Marzocca, Shun He<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-227<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18229 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-aero-elastic tag-cuf tag-thermo-elastic tag-visco-elastic category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/aero-thermo-elastic-stability-analysis-of-multi-layered-visco-elastic-panels\/\" target=&quot;_blank&quot;>\n\t\t\t\tAERO-THERMO-ELASTIC STABILITY ANALYSIS OF MULTI-LAYERED VISCO-ELASTIC PANELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Enrico Zappino, Matteo Filippi, Erasmo Carrera<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-229<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18232 post type-post status-publish format-standard hentry category-events category-ifasd-2017 category-reduced-order-modeling tag-cuf tag-free-vibration tag-one-dimensional-2 tag-tapered tag-thin-walled category-993 category-1953 category-1962 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/ree-vibration-analysis-of-tapered-wing-structures-using-refined-one-dimensional-models\/\" target=&quot;_blank&quot;>\n\t\t\t\tREE-VIBRATION ANALYSIS OF TAPERED WING STRUCTURES USING REFINED ONE-DIMENSIONAL MODELS\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>A. Viglietti, E. Zappino, E. Carrera<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-230<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18235 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aerodynamic-hearting tag-ase-stability tag-unsteady-thrust category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/aeroservoelastic-stability-analysis-of-an-air-breathing-hypersonic-vehicle\/\" target=&quot;_blank&quot;>\n\t\t\t\tAEROSERVOELASTIC STABILITY ANALYSIS OF AN AIR-BREATHING HYPERSONIC VEHICLE\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Huangda Zhao, Chao Yang, Zhigang Wu<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-232<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18238 post type-post status-publish format-standard hentry category-events category-aeroservoelasticity category-ifasd-2017 tag-aeroelasticity tag-flexible-flying-wing tag-flight-dynamics tag-nonlinear-coupled-stability category-993 category-1956 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/stability-analysis-for-a-very-flexible-flying\/\" target=&quot;_blank&quot;>\n\t\t\t\tSTABILITY ANALYSIS FOR A VERY FLEXIBLE FLYING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Liu Yi, Xie Changchuan, Xu Yuntao, Zhou Danjie<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-236<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18241 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-lagrangian-approach tag-pitching-airfoil tag-starting-vortex tag-unsteady-aerodynamics tag-vortex-dynamics category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/a-variational-approach-for-the-dynamics-of-unsteady-point-vortices\/\" target=&quot;_blank&quot;>\n\t\t\t\tA VARIATIONAL APPROACH FOR THE DYNAMICS OF UNSTEADY POINT VORTICES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Ahmed A. Hussein, Haithem E. Taha, Saad Ragab, Muhammad R. Hajj<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-237<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18244 post type-post status-publish format-standard hentry category-events category-computational-aeroelasticity category-ifasd-2017 tag-fuel tag-loads tag-pressure tag-sloshing category-993 category-1957 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/fuel-loads-in-large-civil-airplanes\/\" target=&quot;_blank&quot;>\n\t\t\t\tFUEL LOADS IN LARGE CIVIL AIRPLANES\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>Francesco Gambioli, Arnaud George Malan<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-238<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<article class=\"elementor-post elementor-grid-item post-18247 post type-post status-publish format-standard hentry category-events category-experimental-methods-in-structural-dynamics-and-aeroelasticity category-ifasd-2017 tag-flight-vibration-testing tag-ground-vibration-testing tag-online-monitoring tag-outputonly-modal-analysis tag-parameter-varying-systems tag-taxi-vibration-testing category-993 category-1960 category-1953 description-off\">\n\t\t\t<div class=\"elementor-post__card\">\n\t\t\t\t<div class=\"elementor-post__text\">\n\t\t\t\t<h3 class=\"elementor-post__title\">\n\t\t\t<a href=\"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/29\/recent-developments-in-operational-modal-analysis-for-ground-and-flight-vibration-testing\/\" target=&quot;_blank&quot;>\n\t\t\t\tRECENT DEVELOPMENTS IN OPERATIONAL MODAL ANALYSIS FOR GROUND AND FLIGHT VIBRATION TESTING\t\t\t<\/a>\n\t\t<\/h3>\n\t\t\t\t<div class=\"elementor-post__excerpt\">\n\t\t\t<p><b>M. B\u00f6swald, J. Schwochow, G. Jelicic, Y. Govers<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-239<\/p>\n\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/article>\n\t\t\t\t<\/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 2017 papers Search &#8230; Results See all results Search by Event Topic IFASD2017 Active Control and Adaptive Structures Aeroelasticity in Conceptual Aircraft Design Aeroservoelasticity Computational Aeroelasticity Dynamic loads Environmental dynamics and aeroelasticity Experimental Methods in Structural Dynamics and Aeroelasticity Highly Flexible Aircraft Structures Reduced Order Modeling Rotorcraft Aeroelasticity Steady\/Unsteady Aerodynamics Wind tunnel&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-17396","page","type-page","status-publish","hentry","category-993","category-1960","category-1953","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/17396","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=17396"}],"version-history":[{"count":23,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/17396\/revisions"}],"predecessor-version":[{"id":19152,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/pages\/17396\/revisions\/19152"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=17396"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}